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OPTICAL SCIENCES The Springer Series in Optical Sciences, under the leadership of Editor-in-Chief William T. Rhodes, Georgia Institute of Technology, USA, provides an expanding selection of research monographs in all major areas of optics: lasers and quantum optics, ultrafast phenomena, optical spectroscopy techniques, optoelectronics, quantum information, information optics, applied laser technology, industrial applications, and other topics of contemporary interest. With this broad coverage of topics, the series is of use to all research scientists and engineers who need up-to-date reference books. The editors encourage prospective authors to correspond with them in advance of submitting a manuscript. Submission of manuscripts should be made to the Editor-in-Chief or one of the Editors. See also www.springer.com/series/624 Editor-in-Chief William T. Rhodes, Ph.D. Professor Emeritus, Georgia Institute of Technology Professor of Electrical Engineering and Associate Director, Imaging Technology Center Florida Atlantic University Boca Raton, FL 33431 USA E-mail: [email protected] Editorial Board Ali Adibi Georgia Institute of Technology School of Electrical and Computer Engineering Atlanta, GA 30332-0250, USA E-mail: [email protected] Toshimitsu Asakura
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Theodor W. Hänsch
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Georg A. Klein
Industrial Color Physics
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Georg A. Klein Herrenberg Germany
ISSN 0342-4111 e-ISSN 1556-1534 ISBN 978-1-4419-1196-4 e-ISBN 978-1-4419-1197-1 DOI 10.1007/978-1-4419-1197-1 Springer New York Dordrecht Heidelberg London Library of Congress Control Number: 2009940329 © Springer Science+Business Media, LLC 2010 All rights reserved. This work may not be translated or copied in whole or in part without the written permission of the publisher (Springer Science+Business Media, LLC, 233 Spring Street, New York, NY 10013, USA), except for brief excerpts in connection with reviews or scholarly analysis. Use in connection with any form of information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed is forbidden. The use in this publication of trade names, trademarks, service marks, and similar terms, even if they are not identified as such, is not to be taken as an expression of opinion as to whether or not they are subject to proprietary rights. Printed on acid-free paper Springer is part of Springer Science+Business Media (www.springer.com)
Translated from German by Todd Meyrath and the author.
In memoriam of Dr. Hartmut K.A. Pauli
Preface to the English Edition
Colors arise only in the brain, normally originating from electromagnetic waves from the outside world.
This book is based on courses given by the author in the Department of Colors, Paints and Plastics at the University of Applied Sciences in Stuttgart and continued at the University of Applied Sciences in Esslingen, Germany. The development of color physics in industry began in the middle of the 19th century with the large-scale manufacturing of natural colors. Since that time, a great variety of new, especially synthetic, colorants have been produced in order to meet increasing demands for non-self-luminous colors with regard to color applications. The rapid progress in color physics and accompanying applications over the last three decades are the reasons for this work. Here, the fundamentals of color physics are outlined and the most important recent developments and applications in the color industry are discussed. In comparison to the first German edition,1 all chapters of the book have been revised and expanded with regard to effect pigments. After the introductory chapter, the optical fundamentals of absorbing and effect colorants are discussed. The exceptional spectral and colorimetric properties of effect pigments are detailed in combination with further characterizing parameters. Color spaces are presented as well as the efficiency of recent color difference formulas. In addition to the normal spectral measuring methods for absorbing colorants, modified procedures for effect colorations are outlined. The typical angle-dependent properties of pearlescent, interference, and diffraction pigments as well as mixtures with metallic pigments are clarified by measurements. In addition, criteria for estimation of measurement errors as well as the statistics of color difference values are detailed.
1 Klein, G.A.: “Farbenphysik für industrielle Anwendungen”, Springer, Berlin, Heidelberg (2004).
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The directional two-flux approximation with directional rays is introduced and allows for the creation of the optical triangle. Some characteristic triangle parameters enable the demonstration of the performance of the two-, three-, and multi-flux approximations up to a maximum of n = 256 fluxes. Based on these different concepts, the fundamentals of the classical color recipe prediction methods are described. These topics are completed with the most important modern methods for recipe prediction for all known sorts of colorations. This edition has only been realized through the kindness of many people, and I am happy to express my thanks to them. First, I owe a special debt of gratitude to Dr. Todd Meyrath (Ventura, CA, USA). Not only did he translate from German, he also offered numerous ideas – most of which have been realized in the text. Possible translation errors in the book should be attributed to the author. A lot of suggestions concerning radiative transfer came from friendly discussions with Dr. Hartmut Pauli (Basel, Switzerland). Many thanks go to Dr. Peter W. Gabel (Darmstadt, Germany), Dr. Alfried Kiehl (Velden, Germany), Dr. Changjun Li (Leeds, UK), Mike Nofi (Santa Rosa, CA, USA), Francis Powers (Shawbury, Shropshire, UK), Ian Wheeler (Leven, UK), Dipl.-Ing. Gerhard Wilker (Frankfurt am Main, Germany), and Dr. Klaus Witt (Berlin, Germany) for their encouragement and, in many cases, the kind permission to reproduce some light and scanning microscope images of colorants. Thanks to Klaus-Juergen Woyczehowski (Frankfurt am Main, Germany) for timely help with these; I very much appreciate his kindness. Last but not least, sincere thanks go to my family. Herrenberg, Germany May 2009
Georg A. Klein
Contents
1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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2 Light Sources, Types of Colorants, Observer . . . . . . . . . . . . . 2.1 Optical Radiation Sources and Interactions of Light . . . . . . . . 2.1.1 Visible Spectrum and Colors . . . . . . . . . . . . . . . . 2.1.2 Types of Light Sources . . . . . . . . . . . . . . . . . . 2.1.3 Technical Light Sources . . . . . . . . . . . . . . . . . . 2.1.4 Illuminants . . . . . . . . . . . . . . . . . . . . . . . . 2.1.5 Geometric Optical Interactions . . . . . . . . . . . . . . 2.1.6 Interference of Light . . . . . . . . . . . . . . . . . . . . 2.1.7 Diffraction from Transmission and Reflection Gratings . . 2.2 Absorbing Colorants . . . . . . . . . . . . . . . . . . . . . . . . 2.2.1 Types and Attributes of Absorbing Colorants . . . . . . . 2.2.2 Pigment Mixtures and Light Transmittance . . . . . . . . 2.2.3 Description of Color Attributes . . . . . . . . . . . . . . 2.2.4 Color-Order Systems . . . . . . . . . . . . . . . . . . . 2.2.5 Surface Phenomenon . . . . . . . . . . . . . . . . . . . 2.3 Effect Pigments . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3.1 Types of Metallic Pigments . . . . . . . . . . . . . . . . 2.3.2 Morphology of Metallic Particles . . . . . . . . . . . . . 2.3.3 Coloristic Properties of Metallic Pigments . . . . . . . . . 2.3.4 Sorts of Pearlescent and Interference Colorants . . . . . . 2.3.5 Interference Pigments Consisting of Multiple Layers . . . 2.3.6 Spectral Behavior of Pearlescent and Interference Colorants 2.3.7 Opaque Films Containing Absorbing and Effect Pigments . 2.3.8 Colors of Diffraction Pigments . . . . . . . . . . . . . . 2.4 Observer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.4.1 Color Perception and Color Theories . . . . . . . . . . . 2.4.2 Color Perception Phenomenon . . . . . . . . . . . . . . . 2.4.3 Subtractive and Additive Mixing of Colors . . . . . . . . 2.4.4 Tristimulus Color-Matching Experiments . . . . . . . . .
11 11 12 14 18 23 25 34 38 43 43 48 51 57 59 63 65 69 76 82 85 91 101 104 109 110 114 116 120
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2.4.5 Determination of Tristimulus Values . . . . . . . . . . . . 2.4.6 CIE 1931 and CIE 1964 Standard Colorimetric Observers . References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 Systems of Standardized Tristimulus Values, Color Qualities, Chroma of Effect Pigments . . . . . . . . . . . . . . . . . . . 3.1 Systems of Standardized Tristimulus Values . . . . . . . . . 3.1.1 CIE 1931 Tristimulus Values . . . . . . . . . . . . 3.1.2 Chromaticity Coordinates and Chromaticity Diagram 3.1.3 CIE 1976 Color Spaces . . . . . . . . . . . . . . . 3.1.4 DIN99o Color Space . . . . . . . . . . . . . . . . . 3.2 Color Difference Metrics and Color Tolerances . . . . . . . 3.2.1 CMC(l:c) Color Difference Formula . . . . . . . . . 3.2.2 CIE94 Color Difference Expression . . . . . . . . . 3.2.3 CIEDE2000 Color Difference Equation . . . . . . . 3.2.4 Efficiency of Color Difference Formulas, CIE Color Appearance Models . . . . . . . . . . . . . . 3.2.5 Color Tolerances . . . . . . . . . . . . . . . . . . . 3.3 Color Constancy and Metamerism . . . . . . . . . . . . . . 3.3.1 Chromatic Adaptation and Color Constancy . . . . . 3.3.2 Index of Color Inconstancy . . . . . . . . . . . . . 3.3.3 Kinds of Metamerism . . . . . . . . . . . . . . . . 3.3.4 Special Metamerism Indices . . . . . . . . . . . . . 3.4 Specific Qualities of Colorants . . . . . . . . . . . . . . . . 3.4.1 Build-up and Coloring Potential . . . . . . . . . . . 3.4.2 Strength and Depth of Color . . . . . . . . . . . . . 3.4.3 Covering Capacity . . . . . . . . . . . . . . . . . . 3.4.4 Transparency and Coloring Power . . . . . . . . . . 3.4.5 Color Fastness and Turbidity . . . . . . . . . . . . . 3.4.6 Stability of Effect Pigments . . . . . . . . . . . . . 3.5 Chroma of Effect Pigments . . . . . . . . . . . . . . . . . 3.5.1 Coloristic Quantities of Effect Pigments . . . . . . . 3.5.2 Color Difference Equation for Metallics . . . . . . . 3.5.3 Chroma of Pearlesence and Interference Pigments . . 3.5.4 Mixtures of Effect Pigments . . . . . . . . . . . . . 3.5.5 Color Development of Diffraction Pigments . . . . . References . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 Measuring Colors . . . . . . . . . . . . . . . . . . . . . 4.1 Measurement of Reflecting and Transmitting Materials 4.1.1 Measurement of Colors and Visual Judgment . 4.1.2 Measurement Geometries . . . . . . . . . . . 4.1.3 Sample Requirements . . . . . . . . . . . . . 4.1.4 Transparent, Translucent, Opaque Colors . . .
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4.1.5 Color Matching . . . . . . . . . . . . . . . . . . 4.1.6 Acceptability and Tolerance Agreement . . . . . . 4.2 Measuring Methods . . . . . . . . . . . . . . . . . . . . 4.2.1 Tristimulus Colorimeter . . . . . . . . . . . . . . 4.2.2 Spectrophotometer . . . . . . . . . . . . . . . . . 4.2.3 Accuracy of Spectrophotometers . . . . . . . . . . 4.2.4 Reflectance and Transmittance of Layers . . . . . 4.2.5 Auxiliary Optical Methods for Effect Pigments . . 4.2.6 Fluorescent, Thermochromic, Photochromic Colors 4.3 Uncertainties of Spectral Color Measurement . . . . . . . 4.3.1 Qualitative Errors . . . . . . . . . . . . . . . . . 4.3.2 Quantitative Errors and Error Distribution . . . . . 4.3.3 Normal Distribution in Three and More Dimensions 4.3.4 Statistical Testing of Color Differences . . . . . . References . . . . . . . . . . . . . . . . . . . . . . . . . . .
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5 Theories of Radiative Transfer . . . . . . . . . . . . . . . . . . . 5.1 Fundamentals . . . . . . . . . . . . . . . . . . . . . . . . . . 5.1.1 Basic Concepts and Definitions . . . . . . . . . . . . . 5.1.2 Absorption and Scattering . . . . . . . . . . . . . . . . 5.1.3 Single and Multiple Scattering . . . . . . . . . . . . . . 5.1.4 Radiative Transfer Equation . . . . . . . . . . . . . . . 5.1.5 Radiative Transfer in Plane Parallel Layers . . . . . . . 5.1.6 Phase Function for Anisotropic Scattering . . . . . . . . 5.2 Directional Two-Flux Approximation . . . . . . . . . . . . . . 5.2.1 Reflection and Transmission . . . . . . . . . . . . . . . 5.2.2 Optical Special Cases . . . . . . . . . . . . . . . . . . 5.2.3 Optical Triangle . . . . . . . . . . . . . . . . . . . . . 5.2.4 Determination of Optical Coefficients . . . . . . . . . . 5.3 Theory of Kubelka and Munk . . . . . . . . . . . . . . . . . . 5.3.1 Empirical Approach . . . . . . . . . . . . . . . . . . . 5.3.2 Exceptional Optical Cases . . . . . . . . . . . . . . . . 5.3.3 Determination of Optical Constants . . . . . . . . . . . 5.3.4 Boundary Layer Correction . . . . . . . . . . . . . . . 5.3.5 Limits of Kubelka–Munk Theory . . . . . . . . . . . . 5.4 Three-Flux Approximation . . . . . . . . . . . . . . . . . . . 5.4.1 Conception of Three-Flux Theory . . . . . . . . . . . . 5.4.2 Reflection and Transmission . . . . . . . . . . . . . . . 5.4.3 Optically Different Materials . . . . . . . . . . . . . . 5.4.4 Correction of Surface Effects . . . . . . . . . . . . . . 5.4.5 Special Cases of External Reflection and Transmission . 5.5 Approximation of Radiative Transfer by Multi-Flux Theory . . . 5.5.1 Exact Solutions for Internal Reflection and Transmission
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5.5.2 5.5.3 5.5.4
Surface Boundary Corrections . . . . . . . . . . . . Total Reflection and Optical Extreme Cases . . . . . Boundary Conditions, Matrices of Reflection and Transmission . . . . . . . . . . . . . . . . . . Directional and Diffuse Reflection and Transmission Inclusion of Total Reflection . . . . . . . . . . . . . Corrected Optical Triangle . . . . . . . . . . . . . .
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6 Recipe Prediction . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.1 Classical Method . . . . . . . . . . . . . . . . . . . . . . . . . 6.1.1 Calibration Series with Absorbing Colorants . . . . . . . . 6.1.2 Calibration and Reference Colorations for Effect Pigments 6.1.3 Determination of Absorption and Scattering Coefficients . 6.1.4 Optical Path and Albedo . . . . . . . . . . . . . . . . . . 6.1.5 Coefficients of the Phase Function . . . . . . . . . . . . . 6.1.6 Accuracy of Predicted Recipes . . . . . . . . . . . . . . . 6.2 Strategies for Recipe Prediction . . . . . . . . . . . . . . . . . . 6.2.1 Numerical Methods . . . . . . . . . . . . . . . . . . . . 6.2.2 Spectrometric Strategy . . . . . . . . . . . . . . . . . . . 6.2.3 Colorimetric Method . . . . . . . . . . . . . . . . . . . 6.2.4 Balanced Color Differences . . . . . . . . . . . . . . . . 6.3 Realization of Recipes . . . . . . . . . . . . . . . . . . . . . . . 6.3.1 Selection of Suitable Recipes . . . . . . . . . . . . . . . 6.3.2 Sensitivity and Correctability of Color Recipes . . . . . . 6.3.3 Numerical Procedures for Recipe Correction . . . . . . . . 6.3.4 Databases . . . . . . . . . . . . . . . . . . . . . . . . . 6.3.5 Modified Expert Systems . . . . . . . . . . . . . . . . . 6.3.6 Neural Networks . . . . . . . . . . . . . . . . . . . . . . References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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Appendix . . . . . . . . . . . . . . . . . . . . . . A.1 Non-colored Applications of Effect Pigments A.1.1 Metallic Pigments . . . . . . . . . . A.1.2 Pearlescent Pigments . . . . . . . . A.2 Chromatic Adaption Transform CAT02 . . . A.2.1 Forward Mode . . . . . . . . . . . . A.2.2 Reverse Mode . . . . . . . . . . . . A.3 Two-Flux Approximations . . . . . . . . . . A.3.1 Directional Fluxes . . . . . . . . . . A.3.2 Diffuse Fluxes . . . . . . . . . . . .
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Chapter 1
Introduction
Colored objects influence our lives each and everyday. Within physics the term color is used ambiguously and is in no way restricted to the field of optics. In solid-state physics, the origin of the colors of crystals is certainly of interest; in particle physics the so-called quarks carry electrical charges which are astonishingly called red, green, and blue, yet have no relation to any real colors! The well-known colors of light as well as the various phenomena of non-selfluminous colors belong to the field of optics. Non-self-luminous colors result if suitable colorants such as dyes or pigments are mixed into an organic or inorganic medium. This book confines itself to non-self-luminous colors, their physical and colorimetric qualities as well as their typical industrial applications. Modern colorants can be divided into two groups: absorption colorants and effect pigments. Non-self-luminous colors are only perceived when they are illuminated by light or other energy source. Being a perception, the color impression of the observer is thereby of central importance. Amazingly, our vision – from which we obtain about 80% of the information from our surroundings – is provided by nature with the capability of distinguishing more than 10 million colors. At this stage, we must stress that color is a perception; it is not a physical quantity but rather a purely psychophysical response, usually to visual light after entering the eye. It is, therefore, not measurable by normal engineering methods. It is possible, however, to describe colors in an objective manner by quantifying them with three distinct numbers. These numbers are called color values and are dimensionless quantities. The values can be interpreted, for example, as lightness, chroma, and hue of the relevant color. Certainly, the three values are only representatives of a specific color; they do not describe the color perception itself. From a geometrical point of view, these three color quantities can be taken as coordinates of a point in a three-dimensional color space. Hence, a color space can be considered as an isolated part of a three-dimensional Cartesian coordinate system. On the other hand, each space is obviously characterized G.A. Klein, Industrial Color Physics, Springer Series in Optical Sciences 154, C Springer Science+Business Media, LLC 2010 DOI 10.1007/978-1-4419-1197-1_1,
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by the coordinate system and the metrics chosen. Therefore, the so-called colorimetry describes the metrics between the color quantities in a predefined color space. Since color vision arises exclusively from a neural-induced perception and not directly from a physical effect, colorimetry is used to compare colors of similar or nearly identical hue, among other things. Our modern scientific and technical knowledge about colors follows a long historical development. The oldest surviving colored documents created by humans are the rock and cave paintings from the Paleolithic period found worldwide and dating from the time between about 40,000 and 8,000 years ago [1]. Already during this period, humans decorated their skin and cloths with natural colors. In the following epochs until the Egyptians, refinement was limited to merely the application of natural colors. Even from modern antiquity, no fundamental or new findings about color properties are known, simply some unsuccessful attempts for color theories can be found. The first systematic experiments with color phenomenon were made by Newton with sunlight in the year 1671: with a simple prism he proved that sunlight is comprised of colored parts. In 1704, he concluded: “For the Rays to speak properly are not coloured. In them there is nothing than a certain Power and Disposition to stir up a Sensation of this or that Colour”. His knowledge and experience in optics are concentrated in the work “Opticks”, in which he already began treating terms such as refraction, reflection, and interference [2]. In his color theory of 1810, Goethe criticized this apparent overemphasis of the physical aspects of color; in particular, he stressed the physiological components of color vision [3]. However, the physical statements of his theory were subsequently disproved. Fundamental scientific understanding of colors goes back to Young. In 1802, he created the spectrograph for measuring the intensity distribution of light sources. Young additionally introduced the term wavelength of light and established the first physically and physiologically founded trichromatic theory of color vision [4]. A physiologically determined systematic of color sensation was defined by Grassmann in 1853 with four empirical laws of additive color mixing. They form the basis of modern colorimetry [5]. Moreover, Grassmann was the first to characterize colors by quantities. These quantities are composed of numbers for hue, lightness, and saturation, which are similar to the above description. With these, he has introduced the principle of color values – an essential method in modern industrial color physics. The modern trichromatic theory was established already in 1867 by Helmholtz [6]; it is based on the earlier ideas of Young [4] and Maxwell [7]. With the so-called Young–Helmholtz theory, the psychophysically induced color stimulus can be described numerically by physical and physiological factors. The underlying trichromatic theorem – confirmed experimentally in 1964 – is that color stimulus is caused by the fact that the retina in the eye contains three receptors with photopigments of different sensitivities for the primary colors
1 Introduction
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red, green, and blue. Only these three receptors are responsible to initiate color sensation [8]. Independently in 1878, Hering formulated the so-called opponent color theory. According to this model, the rear of the retina contains three different channels for the opponent color pairs of red and green, yellow and blue as well as the opponent achromatic colors black and white, which are able to produce all color sensations [9]. These ideas were finally proven in 1956 [10, 11]. The retinex theory, introduced by Land in 1959, starts from the hypothesis that the retina and the visual cortex (located at the rear areas of both brain lobes) are connected by three separate channels. In these channels, the arriving neural signals are compared according to their trichromatic lightness contribution so that color sensation is stimulated [12, 13]. The three aforementioned color theories outlined here are not only of interest for research of color perception but also for the application of their established results to the evaluation of the visual and colorimetric properties of colors and colorants. Of great importance in this development is the so-called high colorimetry, formulated (in vector algebra) by Schroedinger in 1920, since then it is abbreviated as colorimetry. Our actual colorimetric methods are based on these ideas [14]. With this formalism, it is possible to make statements about the complete identity of color sensation. Moreover, we are able to obtain information about the similarity of visually different color impressions. These phenomena are relevant for color matching and comparison of nearly identical colors [15–17]. There has been great delay in the implementation of most of the above insights and accumulated knowledge into the industrial setting. About 80 years after the beginning of large-scale production of modified natural and increasingly synthetic absorption colorants, in 1931 the first conventions were set out by the Commission Internationale de L’Éclairage (CIE, International Commission on Illumination) to describe colors with uniform quantities [18]. With these decisions, an essential step toward better communication between manufacturers and users of absorption colorants was initiated. In the proposals of the CIE, ideas of the trichromatic theory have been adopted. This concept was thoroughly revised in 1974 and elements of the opponent color theory as well as colorimetry were taken into consideration. Two years later, parts of this program – named CIELAB system – were recommended for global application [19]. On the basis of the experiences achieved with these proposals, the recommendations have been built up and modified since this time [20–23]. Apart from the higher color physical requirements on today’s industrial colorants, their production, improvement, and processing are of primary interest. Among others, important properties are the total miscibility of the utilized colorants, components, and additives, their chemical and physical compatibility, as well as their durability against shear, pressure, or temperature, all of which might depend, for instance, on the chosen process technology. The principally desired characteristics for most technological applications include: high color
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1 Introduction
constancy against different climatic environments, electromagnetic, radioactive, and even cosmic radiation, as well as fastness – meaning resistance – against chemical changes. Beyond these, the innocuousness concerning toxicological and ecological criteria is increasingly important. For testing the aforementioned and additional coloristic properties, spectral and colorimetric methods are used. With the CIELAB system and later adjustments, colorimetric criteria are applied in color industry, for example: – to specify colors and colorants; – to characterize the typical color producing properties of colorants; – to quantify and assess the color differences of similar or nearly equal colors; – for suitable estimation and assessment of the altered color sensation caused by substitution of colorants, change in illumination or observer conditions; – for recipe prediction of colored samples of unknown colorant compositions. The treatment of these and similar applied problems in an economic fashion was realized only during recent decades. Three reasons are responsible for this: first, the development of complex microstructures in semiconductors (actually reduced now to nanodimensions); second, computers with faster computing speed and larger storage density since 1970; and third, the increased accuracy and simultaneously improved reproducibility of the developed components for instruments to measure colors. The resulting progress has led to extensive and fundamental knowledge about color physical problems of absorption and effect pigments. Until now, effect pigments have been intentionally excluded from our considerations. These flake-shaped particles with a diagonal dimension of about 5–100 μm produce exceptional color sensations, differing essentially from those of absorption colorants. Effect colors result optically either from metallic reflection, interference, or diffraction. Effect pigments are produced industrially to an increasing extent only since the middle of the last century. Two main reasons are responsible for this late distribution: first, effect pigments passed through an autonomous technical development in comparison to absorbing colorants; second, the completely unusual colors and optical interactions produced by this kind of colorant. Metallic reflection, interference, and diffraction are not comparable with selective absorption or scattering, which generate the used colors of absorbing colorants. Effect pigments can be divided into four groups: metallic, pearlescent, interference, and diffraction pigments. In Table 1.1 various sorts of modern colorants are listed together with their dominant color producing interactions. Typical for metallic pigments is the metallic gloss, which is absent in traditional absorption pigments. The beginning of metallic pigments goes back to the beating of gold; a skill practiced in Egypt as early as 5,000 years ago [24]. At that time, gold was beaten into foils with minimal thickness of 1 μm (1 μm
1 Introduction
5
Table 1.1 Modern sorts of colorants and main optical interactions Type of colorant
Colorant
Dominant light interaction
Absorption colorants
Dyes Absorption pigments
Absorption Absorption, scattering
Effect pigments
Metallic pigments Pearlescent, interference pigments Diffraction pigments
Reflection Interference Diffraction
corresponds to 10–6 m) for commodities and pieces of jewelry as well as parts of buildings with a precious and protective surface. Since about 200 BC in China, Japan, and India, Buddha statues were embellished with slices of gold. From there, the art of gold-beating reached Rome, where this skill was even mentioned briefly by Plinius Secundus the Elder in the first century AD; the topic is treated in more detail in the Lucca Manuscript. This document is a recipe collection gathered by Greek monks of the 9th century. The most important confirmed last historical discourse on the technology of gold-beating is represented by a manuscript from the 12th century of the German monk Theophilus . Two centuries after the founding of various centers in northern Germany, the town Nuernberg became the primary center of the gold-beating technology. During the period that followed, increasing demand for gold led to ever thinner metallic foils which unfortunately resulted in a greater failure rate. This is why they were embedded in protective binders ever since. From those flakes, the so-called gold flitter, over the last centuries led to today’s gold and metallic pigments. For reasons of economy and excessive demand, it was finally necessary to find a replacement for gold. This led to gold-colored brass, a material which shows an optical behavior similar to gold in the visible range. Brass is well known since the 3rd century BC in Babylon and Assyria, but vanished thereafter and was rediscovered in Roman times. Since the year 1820, brass has been produced on the large scale in Germany by alloying copper (56–90%) with zinc. A similar history is responsible for the replacement of bright silver–bronze, an alloy of silver with tin, by a less expensive metal: aluminum, which shows a metallic reflection comparable to that of silver–bronze. Pure aluminum has been obtained economically using the technology of melt-flow electrolysis since 1886 and can be produced in the shape of metallic pigments. Certainly aluminum pigments have shown an increased acceptance only since 1970, because since that time it has been possible to realize the desired formulations with this kind of effect pigment on the large scale. Aluminum pigments are preferentially applied for mono- and multi-layer coatings, plastics, or printing inks. Metal flakes for colorants – with mean diameters between 5 and 50 μm – have been called
6
1 Introduction
metallic pigments only for some decades. Now, metallic flakes are being produced in various geometrical shapes and even various colors with the addition of absorption pigments fixed on the surfaces of the particles. Pearlescent pigments, the second group of effect pigments, imitate the nacre luster of natural pearls. The colored effect seems to rise from the depths to the surface of the pearl and results from constructive interference at the various internal interfaces. In order to duplicate this color phenomenon, in Paris in 1656 Jacquin produced and processed the so-called essence d’orient (pearl essence) – a suspension consisting of tiny plates of guanine and hypoxanthine – acquired from fish scales [25]. The use of this cost-intensive production process ceased in 1920: during the following two decades some suitable inorganic compounds were crystallized with increasing success in layers of various thicknesses, which completely imitate the luster of pearls. Modern pearlescent pigments mostly consist of metal oxides fixed on natural or synthetic mica substrates. In the middle of the 20th century the economic upturn allowed for the development of pearlescent pigments in a similar range of application as metallic pigments. In addition to mono-layer pearlescent pigments, transparent or opaque twoand multi-layer pigments have also been realized. Their striking chromatic and brilliant colors result mainly from interference at the combined multi-layers: that is why they are called interference pigments. Sometimes the colors of interference pigments change greatly with the angle of observation. This is principally a consequence of the great difference in refractive index of the layers, which consist of different metals, metal oxides, or even liquid crystal structures [25]. The individual films have thicknesses between about 20 and 200 nm (1 nm corresponds to 10–9 m), therefore, on the high side, nearly the size of visible wavelengths, a requirement for optical interference among other things. The typical size of interference pigments extends from some microns to nearly one millimeter. This is about one to three orders of magnitude greater in size compared to absorption pigments. More recently, new types of effect colorants, called diffraction pigments, have been manufactured. Their production is based on knowledge and materials of nanotechnology. The color effect of these pigments is initiated by diffraction – again a consequence of the wave properties of light – and is extremely angle dependent. Compared with interference pigments, they even show extreme color changes ranging from violet up to red – over the entire visible spectrum. The diffraction effect is a consequence of the periodic grating structure engraved in the particles; the pigments have diameters of about 20–100 μm. Without a doubt all kinds of effect pigments increase enormously the available colors in industry, but the methods of characterizing and measuring them are less than satisfactory. This is no surprise given the fact that the methods for measuring and characterization of colors have thus far only be developed for absorbing colorants. These methods are in general unsuited to qualify and
1 Introduction
7
quantify the characteristic color properties and angle-dependent colors of effect pigments. The development of adequate measuring methods for these colorants is ongoing. It is known that new findings and applications in modern natural sciences are improved by interaction between theory and experiment. Since the introduction of digital computers after 1960, the methods of numerical simulation have greatly progressed. Right from the beginning, computers were applied in industrial color physics to simulate the light interactions of colorants. For an adequate optical theory, it is necessary to describe the relevant optical processes in colored materials in a suitable manner. Strictly speaking, the various single or combined optical interactions have to be taken into account. At least two optical principles are used for this: single and multiple scattering. Single scattering was first developed by Mie [26], who postulated that color is caused only by a single interaction of light with the electric charges of the colorant particles. In contrast, in multiple scattering light continues to interact until it is absorbed or it leaves the material. These ideas were finally formulated by Chandrasekhar [27]. Although both concepts of single and multiple scattering produce similar results, the formalism of Mie is to this day much too extensive and time consuming for industrial color applications. In industrial applications, the theory of radiative transfer of Chandrasekhar is mostly used, modified with a well-established method in physics: the continuous radiative field of the light inside and outside of a colored layer is divided into discrete light cones. Two cones represent a two-flux theory and so on, until we get the multi-flux theory with any positive integer number n > 2 of cones. The special case of two fluxes with diffuse radiation corresponds to the theory of Kubelka–Munk [28], which certainly has only limited validity. With finer adjustment of the subdivision, the cone model seems to correspond more closely with reality. At least the multi-flux formalism is a reliable apparatus in color physics and related fields. Although the relevant formalisms are merely approximations, with these and further approximations, the color industry has nonetheless gained economic advantage to a large extent. One of the most important applications of this procedure is the numerical recipe prediction for colorants. Since about 1970, this method has developed itself into an established and particularly efficient tool in the color industry. With this procedure, a color of unknown colorant composition can be matched with available colorants only by calculating their approximate concentrations. Recipe prediction is nowadays an easy and effective aid. This is in contrast to the past, when previous generations were forced to select some suitable samples only visually from extensive series of experiments in a long-term empirical manner. But now, classical recipe calculation delivers a multitude of equivalent or alternative color recipes, and with the added benefit of a considerable shorter development time. The experience with the multitude of varied recipes, generated by this method, has made it necessary to catalog them, for example, with
8
1 Introduction
regard to the constituent colorants. To manage the enormous number of ancient recipes, modern software databases or expert systems are used. Today, these systems are often combined with numerical recipe prediction, in particular, to match colors containing both absorption and effect colorants. Clearly, all existent theoretical concepts aside, the visual sensation of the observer will always be the final authority on all efforts in the color industry. The neural processes in the brain are known to behave nonlinearly; the neural signals coming from the retina are gathered and modulated in different areas of the brain lobes until the signals reach the visual cortex. Consequently they are extremely difficult and complex to detect. It is, without a doubt, desirable to bridge the gap to the understanding of the neurological and the neurophysiological processes in the brain responsible for color sensation. In this context, only interdisciplinary research is able to make a considerable step forward [29]. Otherwise nearly all methods for characterizing, qualifying, or comparing colors remain on the contemporary, empirical level. In any case, it is definite that a perceived color depends on three criteria: the source of light, the illuminated color sample, and the color sensation of the observer. These three factors together constitute the fundamentals of color physics, colorimetry, and relating industrial applications described in this book.
References 1. Guthrie, RD: “The Nature of Paleolithic Art”, University of Chicago Press, Chicago (2005) 2. Newton, SI: “Opticks: or, a Treatise of the Reflections, Refractions, Inflections and Colours of Light; Also Two Treatises of the Species and Magnitude of Curvelinear Figures”, repr edition London 1704; Culture et Civilisation, Bruxelles (1966) 3. Goethe, JW von: “Zur Farbenlehre”, repr 1st vol ed Tuebingen in 1810, Harenberg, Dortmund (1979) 4. Young, T: “On the theory of light and colours”, Philos Trans Lond 92 (1802) 12 5. Grassmann, HG: “Zur Theorie der Farbenmischung”, Annalen der Physik 89 (1853) 69; original translation in English: Philosophical Magazine 7, Ser 4 (1854) 254; further: MacAdam, DL, Ed: “Selected Papers in Colorimetry – Fundamentals”, SPIE Milestone Series MS 77 (1993) 10 6. Helmholtz, H von: “Handbuch der physiologischen Optik”, 2nd rev ed, Voss, Hamburg (1896) 7. Maxwell, JC: “On the theory of compound colours and the relations of the colours of the spectrum”, Philos Trans R Soc Lond 150 (1860) 57 8. Brown, PK, Wald, G: “Visual pigments in single rods and cones of the human retina”, Science 144 (1964) 45 9. Hering, E: “Outline of a Theory of the Light Sense”, (1920), Transl.: Hurvich LM a. Jameson D; Harvard University Press, Cambridge, MA (1964) 10. Svaetichin, G: “Spectral response curves of single cone”, Acta Physiol Scand 39 Supply 134 (1956) 17 11. Hurvich, LM, Jameson, D: “Some quantitative aspects of an opponent colors theory”, I, II, III; J Opt Soc Am 45 (1955) 546, 602; ibid. 46 (1956) 405 12. Land, EH: “Experiments in color vision”, Sci Am 200 5 (1959) 84 13. Land, EH: “Recent advances in retinex theory”, Vision Res 26 (1986) 7
References
9
14. Schroedinger, E: “Grundlinien einer Theorie der Farbenmetrik im Tagessehen I., II., III.”, Annalen der Physik 63 (1920) 397, 427, 481 15. Richter, M: “Einfuehrung in die Farbmetrik”, 2nd ed, W de Gruyter, Berlin (1981) 16. Wyszecki, G, Stiles, WS: “Color Science”, 2nd ed, Wiley Classics Library, New York (2000) 17. Judd, DB, Wyszecki, G: “Color in Business, Science and Industry”, 3rd ed, Wiley, New York (1975) 18. CIE 1931: “Proceedings of the Eighth Session”, Cambridge, England 1931; Bureau Central de la CIE, Paris (1931) 19. CIE No 15.2: “Colorimetry”, 2nd ed, Commission Internationale de L’ Éclairage (CIE); Bureau Central de la CIE, Wien (1986) 20. CIE No 116: “Industrial Colour-Difference Evaluation”, Commission Internationale de L’Éclairage (CIE), Bureau Central de la CIE, Wien (1995) 21. CIE No 142: “Improvement to Industrial Colour-Difference Evaluation”, Commission Internationale de L’Éclairage (CIE), Bureau Central de la CIE, Wien (2001) 22. CIE No 15.3: “Colorimetry”, 3rd ed, CIE, Bureau Central de la CIE, Wien (2004) 23. Schanda, J, Ed: “Colorimetry: Understanding the CIE System“, Wiley, Hoboken, NJ (2007) 24. Humpl, I: “Blattgold”, C Winter, Heidelberg (1990) 25. Pfaff, G: “Special effect pigments”, in: Smith, HM, Ed: “High Performance Pigments”, Wiley-VCH, Weinheim (2002) 26. Mie, G: “Beitraege zur Optik trueber Medien, speziell kolloidaler Metalloesungen”, Annalen der Physik, 25, 4th ser (1908) 377 27. Chandrasekhar, S: “Radiative Transfer”, repr 1st ed 1950, Dover, New York (1960) 28. Kubelka, P, Munk, F: “Ein Beitrag zur Optik der Farbanstriche”, Zeitschr Techn Physik 12 (1931) 593 29. Backhaus, WGK, Kliegel, R, Werner, JS, Eds: “Color Vision: Perspectives from Different Disciplines”, W de Gruyter, Berlin (1998)
Chapter 2
Light Sources, Types of Colorants, Observer
In this chapter, the fundamental conditions for color production are discussed. In simplified terms, the visual color impression of non-self-luminous colors is ultimately due to three independent components: the light source, the colorants of the color pattern, and the observer. The color perception depends, therefore, on the specific properties of these factors. Factors of particular importance are as follows: – the spectral power distribution emitted of the light sources used; – the light interactions with the colorants of the color sample, especially the resultant absorption, scattering, reflection, transmission, as well as interference or diffraction; – the color perception capability of the observer. We will go into these three factors in more detail in the following sections. To begin with, we deal with the most important light sources used for color assessment and the most simple light interactions of colorants. The composition and the typical spectral properties of industrially applied colorant sorts are described in detail. The explanation of color sensation of the observer seems initially to be out of scope; however, this theme is necessary to consider for at least two reasons: first, some phenomena of the human color sense really stand out. These have to be taken into account during color assessment. Second, color perception is affected by the law of additive color mixing, upon which the entire colorimetry and the corresponding applications of industrial color physics are founded.
2.1 Optical Radiation Sources and Interactions of Light Without light there exists no color. The concept of color is bound to visible wavelengths. Therefore, we turn at first toward the typical properties of natural
G.A. Klein, Industrial Color Physics, Springer Series in Optical Sciences 154, C Springer Science+Business Media, LLC 2010 DOI 10.1007/978-1-4419-1197-1_2,
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and man-made light sources because the spectral power distribution of an illuminant affects the color impression. Due to ever-present changes in natural daylight, such a source is unsuited for producing a consistent color sensation with an unchanging non-self-luminous color. On account of this uncertainty, we are forced to rely on man-made sources of constant and reproducible light emission – normally in the visible range. For a reliable assessment of colors in industry, the spectral power distributions of two commonly used man-made light sources have been standardized. The actual physical processes producing color appearances can be described by elements of simple geometrical optics as well as some effects of wave and quantum optics. In this section, these interactions are described in so far as they are significant for better understanding of the color physical properties of modern industrial colorants.
2.1.1 Visible Spectrum and Colors The electromagnetic spectrum covers an enormous range of wavelengths λ from, for example, values such as λ ≈ 1 fm (1 fm corresponds to 10–15 m) for cosmic radiation to λ ≈ 10 km for radio waves, therefore a range of around 19 orders of magnitude; see Fig. 2.1. On the other hand, the visible range of humans is only a small part of the spectrum of electromagnetic waves. Merely wavelengths in the very small interval from 380 to 780 nm are normally perceived by humans as visible light. Wavelengths at the left end of the range between
10–15
10–12
10–9
10–6
10–3
1
λ m
103
1 2 3 4 5
6 7 8 9 10
Violet Green Orange Blue Yellow Red 380 nm
f Hz
1021
1018
780 nm 1015
1012
109
106
Fig. 2.1 Spectrum of electromagnetic waves: 1 cosmic radiation, 2 gamma radiation, 3 Xray radiation, 4 ultraviolet radiation, 5 near-ultraviolet radiation; 6 infrared radiation, 7 radar waves, 8 VHF waves, 9 television waves, 10 radio waves
2.1
Optical Radiation Sources and Interactions of Light
13
380 and 440 nm are perceived as violet. With increasing wavelength, the color impression changes to blue, green, yellow, orange, and finally red. Red is perceived at wavelengths above 600 nm. The associated wavelengths are subject to individual variations in color perception. The so-called spectral colors are the purest producible colors. They are characterized by a wavelength width of less than 1 nm (i.e., with a laser). On the other hand, if the radiation contains nearly all wavelengths of the visible spectrum and of equal intensity, the resulting color impression is white light (e.g., white clouds). For the entire range of visible light between about 380 and 780 nm to be perceived, there must be sufficiently high intensity. Under normal illumination conditions, the wavelength interval that can be seen by humans is restricted to between about 400 and 700 nm. Many modern color measuring instruments work in this limited range [1]. Apart from its wave character, light also exhibits simultaneously particlelike properties. To this day, perhaps, this dualism is not understood in terms of everyday human experience. The corresponding particles of electromagnetic radiation, and therefore of visible light, are the so-called photons. Photons in the visible range carry a sufficient amount of energy for selective stimulation of the photosensitive pigments in the retina of the eye to initiate color impression. The eyes should, however, be protected from dangerous ultraviolet (UV) or infrared (IR) radiation. However, radiation of wavelengths near the visible range which cannot be directly perceived by humans can, in conjunction with suitable colorants, cause different physical effects. Luminescence colorants, for example, absorb energy at UV wavelengths and then emit most of this energy at longer wavelengths – usually within the visible or IR range. The needed transitions from energetic steady states occur either spontaneously by fluorescence or delayed by phosphorescence. The energy surplus is converted into molecular vibration energy and leads macroscopically to a temperature increase. The energy absorption of normal absorption colorants in the visible or IR range is also transformed into molecular vibration energy. If this energy conversion is accompanied by a color change, such kinds of colorants are denoted as thermochromic. Moreover, colorants are termed as phototropic, if the color change is only caused by energy absorption at visible wavelengths. On the other hand, excessively high UV or IR radiation energy is sometimes able to initiate irreversible molecular changes, which result in bleaching or total loss of color. In contrast to the above-mentioned colorants, overall the greatest percentage of industrially used colorants contain absorption and effect colorants. In absorption colorants, the incident energy is sufficiently high to initiate partial absorption or scattering. Physically, light absorption in colorant molecules occurs only for certain transitions between quantum energy levels – therefore, in special wavelength regions of visible light. The corresponding processes are called selective absorption or scattering. On the other hand, scattering of light depends on the electrical charge distribution and the geometry of the colorant
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2 Light Sources, Types of Colorants, Observer
particles. In contrast to absorption pigments, dyes do not normally show any scattering because the size of the isolated molecules in solution is too small for such an interaction. The light reflected in the direction of the eye initiates in the retina signals which are perceived usually as non-self-luminous colors. The color separation of pearlescent, interference, and diffraction pigments is a consequence of the wave nature of light. In order to produce a suited interference effect, the pigment particles are built up of layers with different refractive indices of which the light waves interfere constructively or destructively depending on optical path length. The layer thicknesses are smaller than the interfering wavelengths. In contrast, the particles of diffraction pigments show an embossed regular grating structure at which suited wavelengths are diffracted. The distance between two light-transferring slits is about 1 μm.
2.1.2 Types of Light Sources The perception and assessment of non-self-luminous colors requires illumination with a suitable light source. Depending on the mechanism of light generation, optical radiation sources have different spectral power distributions. On the basis of the emitted spectrum, illuminants can be divided into two categories: temperature and luminescence radiators. The most important luminous sources of both classes are given in Table 2.1. In the following, we discuss details of both categories because the illumination of color samples is our primary context. In the near future, semiconductor diodes and lasers are expected to replace, in part, the light sources used to date. Therefore, we also discuss on these sources even though they are, thus far, rarely applied in color industry despite a multitude of advantages. Table 2.1 Kinds of optical light sources Temperature radiator
Luminescence radiator
Natural
Artificial
Artificial
Sunlight, Scattered light of the Earth atmosphere, stars, galaxies
Blackbody radiator, incandescent lamp, arc lamp
Gas discharge tube, fluorescent lamp, light emitting diode (LED), source of coherent light (laser)
For a common characterization, optical radiation source output distributions are often compared with the spectral energy distribution or temperature of a so-called blackbody radiator – also denoted as blackbody or cavity radiator. At lower temperatures, metals emit heat energy in form of IR radiation; gradually, with increasing temperature, dark-red glow emanates. With a further increase
2.1
Optical Radiation Sources and Interactions of Light
15
of temperature, the color changes to orange and yellow, finally to bluish white. During this process, both the radiation energy and the brightness of the emitted light increase. The wavelength with the most energy shifts to smaller wavelengths, i.e., a blue shift. For an ideal blackbody, this radiation is generated inside the cavity of a blackbody radiator and the outside of the cavity walls absorb all external electromagnetic waves. The ideal situation, therefore, is the emission of only the cavity radiation according to its temperature. The radiation power S(λ,T)dλ of a blackbody radiator at wavelength interval dλ is given by the Planck law of radiation [2]: S(λ,T)dλ =
λ5
c1 dλ. · {exp [c2 (λT)] − 1}
(2.1.1)
The radiation constants c1 and c2 have values of c1 = 2πhc2 = 3.74185 × m2 and c2 = hc/k = 1.43884 × 10−2 m K. In Equation (2.1.1), the wavelength λ should be in units of meters and the temperature T in units of Kelvin. The radiation constants contain the velocity of light in vacuum c and the Boltzmann constant k. For derivation of Equation (2.1.1), Planck introduced h – now called the Planck constant. Figure 2.2 shows the spectral power distribution in wavelength given by Planck’s law. As can be seen, at a temperature of 500 K, the peak of spectral power is in the IR range. For an increase to much higher temperatures, i.e., to greater than 104 K, this peak shifts over the visible range into the UV range. For temperatures of about 7,600 and 3,700 K, the peak of the spectrum lies at the respective edges of the visible range. The Planckian formula (2.1.1) contains 10−16 W
109
Energy density / W.m–2.nm–1
Visual range g
a: 500 K b: 1,000 K c: 2,000 K d: 4,000 K e: 6,000 K f: 10,000 K g: 20,000 K
106 f e d
103
c b
100
a 10–3 101
102
103
104
Fig. 2.2 Spectral power distribution of blackbody radiator of different temperatures
λ
nm
16
2 Light Sources, Types of Colorants, Observer
two limiting cases: for short wavelengths Wien’s law of radiation and for long wavelengths Rayleigh–Jeans radiation formula. Before the quantum hypothesis was established, both laws lead to inconsistent infinite energies in the UV range (“UV catastrophe”). The primary assumption made by Planck is that a radiating system exchanges energy with the surrounding radiation field only with an integer multiple of the quantum energy E=
hc = hf . λ
(2.1.2)
In this formula, f is the frequency of the corresponding wavelength. Both the continuous spectra of temperature radiators and the discontinuous line spectra of luminescence radiators are based on the emission of light quanta that are identical with the already mentioned photons. Because the color of the spectrum emitted by a blackbody radiator changes with temperature, it is useful to introduce the term color temperature. With this quantity, the emitted light of a source is compared with that of a blackbody radiator and thus characterized. The color temperature of an illuminant corresponds to the temperature of the blackbody radiator which emits the maximum of light at the same color as the actual illuminant. Strictly speaking, only a temperature radiator can be assigned a color temperature. Other optical radiators, such as luminescence radiators, are characterized by a so-called similar or correlated color temperature. The most well-known temperature radiator is the Sun. Inside the Sun, at temperatures higher than 107 K, deuterium is converted to helium by nuclear fusion (Bethe–Weizsäcker cycle) [3]. For generation of 1 mol helium, the gigantic energy of 1.55 × 102 GJ is released. The total solar fusion energy results in a Sun surface with a mean temperature of about 5,800 K and an exceptionally high radiation power of about 63.3 MW/m2 . Merely a small fraction of this power, namely the so-called solar constant with value 1.37 kW/m2 , reaches the Earth’s atmosphere. This value reduces to about 1.12 kW/m2 if the Sun is at its zenith and the atmosphere is free of clouds. Already these considerations indicate the necessity of carrying out outdoor exposure tests of industrial colors (Section 3.4.5). Along the way to the Earth’s surface, the light interacts with particles of the atmosphere; its intensity is reduced by absorption and scattering. The light scattering is caused by the molecules in the air and this is responsible, for example, for the blue sky. According to the Rayleigh law J=
V π 2 (n − 1) 2 · · E · cos2 ϑ, N r 2 λ4
(2.1.3)
short wavelength blue light is scattered more strongly than the long wavelength red light because λ is contained in the denominator of this expression. The
2.1
Optical Radiation Sources and Interactions of Light
17
further quantities in Equation (2.1.3) are defined as follows: J the intensity of the scattered light, N the number of scattering particles per unit volume V, n the refractive index of the scattering medium, r the particle radius, E the amount of the electric field strength, and cos2 ϑ the phase function (see Section 5.1.5); ϑ denotes the scattering angle with regard to the incident intensity. The Rayleigh law is only valid for wavelengths λ which are longer than the particle radius r. In contrast to the blue color of the sky, sunrise and sunset are caused by scattering and absorption of light in the atmosphere, more precisely due to the air molecules as well as to aerosols (water drops, dust particles, etc.). On the long and nearly tangential optical path of the light through the layer of air, blue wavelengths are more strongly scattered and absorbed. The remaining blue light, therefore, reaches the observer on the Earth with considerably less intensity as compared with the much less scattered long wavelength red light. The Sun and the sky, therefore, appear reddish. In addition to dependence on daytime, received sunlight changes due to weather conditions, geographical latitude, season, and due to the approximately 11-year sunspot cycle. Accordingly, the color temperature of daylight is subject to substantial variations and takes values in the range of 5,500 K for direct sunlight to more than 14,000 K for blue zenith skylight. Simultaneously, the spectral power distribution changes. This is shown in Fig. 2.3 with curves normalized at the wavelength 555 nm. At this wavelength, the sensitivity of the human eye is at its highest (Section 2.4.6).
a
Relative spectral energy
b
400
c d e
500
600
λ
700
nm
Fig. 2.3 Relative spectral energy distribution curves of daylight, normalized at 555 nm: (a) cloud-free zenith skylight, (b) cloud-free north skylight, (c) overcast skylight, (d) medium daylight, and (e) direct sunlight [4]
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The daylight variations mentioned above create extra complexities for the unambiguous visual and objective assessment of non-self-luminous colors and their typical properties. A single color sample can produce a completely different color impression simply due to a changing illumination condition. In the practice of color physics, it is necessary to use reproducible artificial light sources which have nearly constant spectral power distributions. These artificial light sources are often referred to as technical sources. This corresponds to a constant color temperature if aging effects are neglected. From an economic point of view, the sources should also have a reliable working life of more than 1,000 operating hours. These standards are fulfilled by most of the technical illuminators of importance in the color industry; in the following section, we turn toward such kinds of sources.
2.1.3 Technical Light Sources For solving coloristical problems of non-self-luminous colors, technical light sources are used exclusively. The main reason for this is the high reproducibility of the generated spectrum. In technical temperature radiators, a metal of high melting point is heated up by an electric energy supply to such an extent that a continuous spectrum is emitted in the visible range; this spectrum is similar to that of a blackbody radiator of the same temperature. A temperature radiator in widespread use is the tungsten filament lamp; its color temperature is essentially dependent on the filament thickness, the applied voltage, and the kind of gas filling of the bulb. The so-called tungsten–halogen bulb contains bromine or iodine which increases the light efficacy, the working life, as well as the color temperature from about 2,800 to 3,000 K. The tungsten filament lamp of color temperature 2,856 K is named standard illuminant A by the CIE. The gradual loss of filament thickness in normal tungsten lamps is slowed down by the included halogen: the vaporized tungsten combines with the halogen, cools down at the surrounded quartz bulb, and reaches – by convection – the hot filament surface; there it dissociates so that tungsten is removed. Tungsten filament lamps typically emit light of yellowish color. The accompanying spectral energy distribution is shown in Fig. 2.4. Furthermore, in a tungsten arc lamp with an argon atmosphere, both tungsten electrodes are heated by an arc discharge in such a way that a radiation distribution is produced similar to that of the tungsten filament lamp; the accompanying color temperature amounts to about 3,100 K. A carbon-arc lamp shows a color temperature of 6,000 K and a very high luminance of about 1.6 Gcd/m2 .1
1 The unit candela (cd) is defined as the luminous flux radiated from 1/60 cm2 of a blackbody with temperature 2.042 K.
2.1
Optical Radiation Sources and Interactions of Light
19
200
Spectral energy distribution S (λ)
A
150 D65 100
50
0 300
400
500
600
λ
nm
Fig. 2.4 Spectral energy distribution of a tungsten filament lamp (CIE standard illuminant A) and a UV-filtered xenon lamp (CIE standard illuminant D65)
The term luminescence radiators represents a group of radiators including so-called discharge lamps, as well as photoluminescence radiators [5, 6]. In contrast to temperature radiators, luminescence radiators emit either a line spectrum of discrete wavelengths or a band spectrum of broader wavelength intervals. Line spectra are exclusively generated by gas discharge lamps. The physical mechanisms for generating line spectra are first to accelerate charge carriers by an electric field; during collision with the gas atoms, excitation energy is transferred to the outer electron orbits of these atoms. On the basis of the quantized energy of the electron shells, the electron transition into the ground level results in emission of light with discrete wavelengths λ according to Equation (2.1.2). The actual temperature of luminescence lamps is clearly far lower than the surface temperature of temperature radiators of the same light color. Among the technical gas discharge lamps, only the filtered light of xenon or mercury vapor lamps is of major importance for visual assessment or spectral measurement of colors. The emission of light in gas discharge lamps is based on the same physical mechanisms as in luminescence radiators. At first an electric voltage pulse in a xenon atmosphere causes free charge carriers. In a highpressure xenon lamp under pulsed or constant voltage, the charged particles generate a nearly continuous spectrum in the visible range. This is accompanied by a small amount of UV radiation. The spectral energy distribution shows a flat peak at a wavelength of about 450 nm and the emitted spectrum shows only a
20
2 Light Sources, Types of Colorants, Observer
slight decrease in magnitude for longer wavelengths. Therefore, the perceived light appears slightly but insignificantly bluish; this can be seen in Fig. 2.4, curve D65. The radiation distribution is similar to that of diffuse daylight at midday on cloudless north sky, cf. Fig. 2.3, curve d. For these reasons, a UV-filtered xenon lamp of color temperature 6,500 K is used in the color industry to simulate midday light. The spectral energy distribution of this xenon discharge lamp is standardized; it is termed by the CIE as standard illuminant D65. The CIE recommends the use of xenon lamps with color temperatures of 5,000, 5,500, or 7,500 K, if the standard illuminant D65 is not available. The mercury vapor discharge lamp generates a line spectrum with emission wavelengths of 405, 436, 546, 577, and 579 nm, as well as in the UV range of 254, 314, and 365 nm. Because of the energetically high UV amount, this discharge lamp is utilized in a so-called light booth for visual assessment of fluorescence colorants, artificial color fastness tests, and in fluorescence microscopy. A light booth consists of a small one-sided open compartment with one or two small platforms to lay down the color samples to compare, as well as different non-glare light sources which can be individually switched on. The abovementioned emission wavelengths are also used for wavelength-scale calibrations of color measuring instruments. The UV fraction of the mercury spectrum is furthermore applied to stimulate the phosphorus in fluorescent lamps in order to initiate photoluminescence in the visible range. The spectral composition of the resulting band spectrum or the resulting light color depends on the chemical structure and the mixing ratio of the involved phosphorus. For color assessment of special importance, there is the cold white light of the fluorescent lamp CWF (identical with illuminant FL 2) and the light emission of the so-called three-band lamp TL 84 (identical with FL 11); the three-band lamp has radiation maxima at wavelengths of about 440, 550, and 610 nm; see Fig. 2.5. These wavelengths have spectral colors of blue, green, and red and cause trichromatic a neutral white light color. Fluorescent lamps are in widespread use only because of economic reasons: they have a luminous efficacy and a physical life which are about eight times higher than those of tungsten filament lamps, cf. Table 2.2. Light sources of principle importance in the near future are expected to be light emitting diodes (LEDs) and lasers, which greatly ripened technically in the 1960s. The central component part of an LED consists of a p–n semiconductor junction. A voltage between 1 and 15 V in conducting direction and a current of order 50 mA release photons in the p–n region. These photons are generated by an energy surplus from recombining electrons and defect electrons (holes). Available luminescence diodes doped with suited chemical compounds can emit quite monochromatic light with half-widths of 6–25 nm, for example, at wavelengths of 400 nm (gallium-nitride diode), 600 nm (gallium-arsenicnitride diode), and 660 nm (gallium-phosphide-zinc-oxide diode). The benefits of LEDs are the short switching time of about 5 ns, the small spectral
2.1
Optical Radiation Sources and Interactions of Light
21
Spectral energy distribution S(λ)
80
60
FL 11 40
FL 2 20
0
400
500
λ
600
nm
Fig. 2.5 Spectral energy distribution of fluorescent lamps: cool white fluorescent CWF (illuminant FL 2) and three-band lamp TL84 (illuminant FL 11) Table 2.2 Properties of five selected illuminants Color Correlated color rendering temperature/K index
Light efficacy/ lm/W
2,856
100
12
Tungsten filament lamp
CIE standard D65 illuminant D65, middle daylight
6,500
94
35
UV-filtered xenon lamp
Cold white daylight
FL 2
4,230
64
70
Fluorescent lamp CWF, cool white fluorescent
Bluish white daylight
FL 7
6,500
90
80
Broadband fluorescent lamp
4,000
83
90
Three-band lamp TL84
CIE CIE illuminant abbreviation CIE standard illuminant A, evening light
A
White daylight FL 11
CIE simulator
22
2 Light Sources, Types of Colorants, Observer
half-width of the emitted intensity, the high degree of optical efficiency, and the long working time. Disadvantages up to now have been the low illumination intensity in comparison to traditional light sources. Improvements in these respects, at the time of this writing, are the subject of ongoing research and development. The term laser is an abbreviation of “light amplification by stimulated emission of radiation.” A laser is, therefore, an optical amplifier which is based on the principle of stimulated emission of light. To initiate stimulated emission of light2 , an irradiating field, in some sense, forces the emission of light in atoms, molecules, or ions of gases, liquids, or solids. The incident field of frequency f has photon energy according to Equation (2.1.2). The primary requirement for stimulated light emission is that this photon energy is at least the natural energy difference of the medium. In such cases, the medium that has some population in an excited state has some return to the ground state. This emitted energy is incorporated into the incident field. In order to obtain an amplification of radiation by stimulated emission, the energetically higher levels or bands of a medium should maintain a state with a greater degree of filling. This greater electron number or population in the upper energy state is usually maintained using an energy supply such as flash lamps, other laser pump sources, currents in semiconductor laser, or atom/electron collisions. Typical classification of lasers is along the lines of the physical state of the gain medium: solid state (crystals), semiconductor, liquid (usually organic dyes), or gas lasers, for example. The ruby laser with emission wavelength of λe = 694.3 nm is a solid-state laser. Semiconductor lasers are, for example, indium-gallium-phosphide (In1-x Gax P) or aluminum-gallium-arsenide lasers (Alx Ga1-x As); the emitted monochromatic wavelength of each usually lies in the range 500 and 1,000 nm depending on the content x of the indicated element. Dye lasers are the dominant class of liquid lasers; typical laser mediums are dyes such as coumarin (460 nm ≤ λe ≤ 560 nm) or rhodamine (535 nm ≤ λe ≤ 630 nm). The most well-known gas lasers are the helium–neon laser (632 nm) and the argon-ion laser (wavelengths of highest intensity 488.0 nm and 514.5 nm). The advantages of lasers are clear, considering the outstanding features of the emitted light: constant frequency, highly monochromatic, spatial and temporal coherence, high beam directivity, and adjustable energy density. In the color industry, lasers have been successfully used for the determination of surface gloss, covering capacity and glittering of effect colorants, as well as size distribution of pigment particles in powders, among other things. In the following section, we concentrate on specific properties of light sources which are of special interest for colorimetric applications.
2 The opposite is
absorption, or, more precisely, stimulated absorption.
2.1
Optical Radiation Sources and Interactions of Light
23
2.1.4 Illuminants In the previous section, the physical basics of light emission and the applications in technical light sources have been introduced. Now, we direct our attention toward the special handling of light sources in colorimetry or color matching. Unquestionably, the vast variety of technical light sources complicates the unambiguous visual assessment of colors: colored objects are exposed to changing natural as well as artificial illuminations such as daylight, evening light, or fluorescence light. The change in illumination can alter the visual color impression (see below). The CIE has, therefore, recommended the most representative light sources to use for color assessment applications. For clearness and better communication, four terms should be identified. These terms describe the different kinds of light sources: 1. CIE illuminant: this corresponds to a theoretical source of a tabulated relative spectral power distribution S(λi ); 2. CIE standard illuminant: only two illuminants are standardized by the CIE, illuminant A and illuminant D65; 3. CIE source: corresponds to a technically realized CIE illuminant; 4. CIE simulator: is a technical source which approximately corresponds to the desired CIE illuminant. The first and second terms need some further explanation. The CIE specified several representative illuminants [7], among them are the following: a. three temperature radiators designated D50, D55, D75 with color temperatures of 5,000, 5,500, and 7,500 K, respectively; b. twelve fluorescent lamps designated from FL 1 to FL 12; the illuminants FL 1–6 emit line spectra, FL 7–9 broadband, and FL 10–12 narrowband spectra. Among these, FL 2, FL 7, or FL 11 are preferably used in colorimetry. In Fig. 2.5, only the spectral power distribution of illuminants FL 2 and FL 11 are shown; c. in the end, five high-pressure lamps designated as HP 1–5, of which two are sodium vapor lamps and three metal halide lamps; these are normally not significant in colorimetry but rather in lighting engineering. The two CIE standard illuminants are characterized by the following features: the spectral power distribution S(λi ) of standard illuminant A is given by the Planck law of radiation (2.1.1), whereas that of D65 is given by tabular values [8, 9]. These values correspond to the UV-filtered emission of a high-pressure xenon lamp shown in Fig. 2.4. Standard illuminant A is recommended for simulation of room light in the evening, D65 of midday light of color temperature 6,500 K.
24
2 Light Sources, Types of Colorants, Observer
The tabular values of a CIE illuminant are generally used for computation of color values. The corresponding simulation illuminant serves for visual assessment of color patterns. In other words, the real light source which is used to illuminate a color sample is, for the purpose of calculation, substituted by a theoretical simulation source, consisting of discrete wavelengths and power emission. This can clearly be a reason for deviation between the visual assessment and the colorimetric result. A further deviation can result from the so-called CIE standard colorimetric observers. This is not discussed until Section 2.4.6. The five most commonly used illuminants in colorimetry are D65, A, FL 2, FL 7, and FL 11; a selection of their properties is given in Table 2.2. While the standard illuminant A is assigned a true color temperature, the illuminant D65 and the fluorescent radiators have only correlated color temperatures. These are for the luminescence sources FL 2 –11: 4,230, 6,500, and 4,000 K, respectively. In most cases, the change of illumination also results in a change of perceived color. This can be caused either by the colorants themselves or by the light source used. If the spectral power distribution is responsible for color changes, this is attributed to the color rendering of the illuminating source. The yellowish light of the sodium vapor lamp HP 1, for example, bathes each chromatic color in a pale yellow. This is because sodium emits only two closely spaced wavelengths of 589.0 and 589.6 nm in the visible range. The CIE proposed the dimensionless color rendering index Ra to characterize the grade of color rendering of light sources [10–12]. This index takes values in the range 0 ≤ Ra ≤ 100. The sodium vapor lamp HP 1 has an Ra value of 20; this indicates that colors are quite distorted. In contrast, the CIE standard illuminant A takes the highest possible value of 100. An additionally used characteristic, which has a meaning in terms of energy, is the light efficacy of a radiator. This economic quantity is defined as the ratio of emitted luminous flux of a light source to the input power of unit lm/W.3 As can be seen from Table 2.2, the displayed fluorescence lamps show a higher light efficacy than temperature radiators of equal or lower color temperature. From a comparison of the spectral power distributions shown in Figs. 2.4 and 2.5, it is possible to understand how the change of a source alters the color impression. Consider Fig. 2.4: using source A, the color sample appears more yellow and red compared with illumination of a D65 simulator. This is because of the continuously increasing radiation energy characteristic of the source A from yellow to red wavelengths with quite small values at short wavelengths. Consider now Fig. 2.5: the same color sample is rendered bluish white with FL 2 source, or with FL 11 source, redder in comparison to D65 simulator. Colors 3 By definition, the unit lumen (lm) is the luminous flux which a point light source of emissiv-
ity 1 cd (candela) emanates evenly in all directions in a solid angle of 1 sr (steradian): 1 lm = 1 cd sr; 1 steradian corresponds to a solid angle Ω – of even circular cone with center point in a sphere of radius 1 m – which cuts an area of 1 m2 out of the sphere surface, cf. Fig. 5.1.
2.1
Optical Radiation Sources and Interactions of Light
25
illuminated with a D65 or FL 7 source are rendered and perceived in a similarly balanced way as under midday light. This is because of the nearly constant and high values of the corresponding emission spectra in the visible range.
2.1.5 Geometric Optical Interactions There are various possible interactions between incident light and atoms, molecules, particles, or crystals. Of these interactions, we are primarily interested in the color appearances that result. In a plane electromagnetic wave, the electric and magnetic vectors E and H are perpendicular to one another, and, in addition, mutually perpendicular to the propagation direction. The so-called wave vector k is oriented in the propagation direction. The electromagnetic wave carries the energy flux density in the direction of k, given by vector S (named as Poynting vector) and relation S = E × H.
(2.1.4)
Figure 2.6 shows the connection between the three vectors E, H, and S. In the figure, the electric and magnetic vectors are shifted a quarter wavelength in phase with respect to one another. E
S
H Fig. 2.6 Electric and magnetic field of a stationary wave
The amount of energy flux density S carried by such waves, also termed as flux density, or short flux, is the origin of interactions with the molecules or particles of colorants to produce colors. Color production of non-self-luminous colors can be caused by simple or multiple reflection, refraction, absorption, scattering, interference, and/or diffraction. When the wavelength of the light (order 0.4 to about 1 μm) is much smaller than the size of the objects that it interacts with (i.e., macroscopic objects), the light no longer behaves strongly as a wave, but rather propagates in straight lines according to geometrical optics. Reflection, refraction, absorption, or scattering can occur simultaneously if the light is incident on macroscopic boundary surfaces consisting of mediums with different optical densities. The polarization
26
2 Light Sources, Types of Colorants, Observer
of light can intensify normal color appearance. This can appear especially for some absorption pigments and liquid crystal pigments. Materials can be illuminated by directional, diffuse, or mixed light. Quite simple, but of great importance, is the directional reflection – also denoted as specular reflection. Directed reflection arises from directional light at smooth, polished, or glossy surfaces, for example at organic binders, synthetic polymers, glasses, metals, as well as colorations with absorption and effect pigments. According to the reflection law, the angles of the incident ϑi and reflected light ϑ r , measured with respect to the normal of the reflecting surface, are equal: ϑi = ϑ r . Additionally, both rays and the normal of the reflecting surface lie in the same plane, that of the paper in Fig. 2.7. It is important to note that for visual assessment of colorations of glossy surfaces one must strictly avoid observations in the direction of the specular angle. For visual inspection of absorption colorations with collimated light, the surface should be illuminated from the side and the observation performed perpendicular to the sample surface. In contrast, the visual assessment of effect colorations requires a sophisticated procedure, cf. Figs. 2.29 and 2.30.
ϑi
ϑr
Fig. 2.7 Depiction of the reflection law with incident and reflected beams, as well as angle of incidence, and specular angle, each from normal to the surface
If the medium behind the glossy surface is transparent and of different refractive index than the first medium, the beam is additionally refracted into this medium. The refracted ray deviates from the original direction, see Fig. 2.8a, b, due to the different indices of refraction in the two media. The angle of refraction ϑ 2 depends on the angle of incidence ϑ 1 and the ratio of refractive indices n2 /n1 of the adjoining mediums according to Snell’s law of refraction sin ϑ1 n2 = =n sin ϑ2 n1
(2.1.5)
(original W. Snel van Royen, 1621). In general, the refractive indices are also wavelength dependent, this normally results in violet light being refracted at a steeper angle than red light. This property is called dispersion [2] and results in prism effects.
2.1
Optical Radiation Sources and Interactions of Light
27
ϑ1
ϑ2
n1
n1
n2
n2
ϑ2
ϑ1
a)
b)
Fig. 2.8 Refraction of light at the boundary surface of (a) an optically thinner medium and (b) an optically denser medium
The reflected fraction r(μ, n) of the directional beam at the boundary surface follows from the Fresnel equation 1 μn − w 2 μ − nw 2 r(μ,n) = + , (2.1.6) 2 μn + w μ + nw where μ = cos ϑ ,
w2 = 1 − (1 − μ2 )n2
(2.1.7)
[13, 14]. Equation (2.1.6) can be derived from Maxwell equations of electrodynamics [14]. The reversal of light direction does not change the reflected fraction nor the law of refraction. The reversibility of the light path without change of effect is a general principle of geometrical optics [15]; this principle is used in color measuring methods among other things (Section 4.1.2). In the case of light incident perpendicular to the surface, the special reflected fraction is given by n−1 2 . (2.1.8) r(1, n) = n+1 This follows from Equations (2.1.6) and (2.1.7) using μ = 1. For air with refractive index n1 ≈ 1.0, for example, and plastics or binders with a typical value n2 = 1.5, using n = n2 /n1 , the normal incidence reflected fraction is r = 0.04.4 In other words, under these conditions, 4% of the incident light is immediately 4 The cited refractive indices in this book represent values which – as usual – belong to the wavelength of the sodium line of 589.0 nm.
28
2 Light Sources, Types of Colorants, Observer
reflected from the surface of a colored sample; this amount is not available for further light interactions in the volume of a color sample. The reflectance of pure metals follows from Maxwell’s equations as well, provided that the complex refractive index nˆ is introduced: nˆ = n(1 + iκ).
(2.1.9)
The quantity nˆ is divided into the real part n for the refraction and the imaginary part nκ describing the light absorption at the interface. The quantity κ is √ named attenuation coefficient. In Equation (2.1.9), i is the imaginary unit (i = −1). For directional light incident perpendicular to the metal surface, the reflected total amount is given by r(n, κ) =
(n − 1)2 + (nκ)2 . (n + 1)2 + (nκ)2
(2.1.10)
For κ = 0, this formula reduces to Equation (2.1.8). The product nκ is termed as absorption coefficient; some measured values of n, nκ , and r(n, κ) for metals used for metallic pigments are listed in Table 2.7. A further sort of reflection occurs if a light beam enters an optically thinner medium coming from an optically denser medium. Note that the refracted ray cannot exceed an angle ϑ 2 = 90◦ ; see Fig. 2.9. For a refractive index n = 1.5, the corresponding incidence angle is ϑ 1 = 41.8◦ . In general, from the law of refraction (2.1.5), it follows that rays, with angles of incidence with γcr ≥ arcsin (1/n), are totally reflected back into the optically denser medium. The quantity γcr is called the critical angle of total reflection or in short critical angle. If
ϑ2 n1 n2
ϑ1 γcr
γcr
Fig. 2.9 Critical angle γcr at a boundary surface of different refractive indices
2.1
Optical Radiation Sources and Interactions of Light
29
the total reflected light cannot immediately leave a colored layer, it participates further in the interactions with the color-producing particles until it is absorbed or leaves the layer. Total reflected rays of angles γ ≥γcr are called partly directed in this text. For unpolarized light, a further property follows from the law of refraction with regard to the refracted ray. In the case that the reflected and the refracted rays make a right angle, the light of the reflected ray is linearly polarized, in fact perpendicular to the plane of incidence; see Fig. 2.10. This special angle of incidence is denoted as Brewster angle ϑB and is given from the law of refraction (2.1.5) with ϑ 2 = 90◦ – ϑB : tan ϑB = n.
(2.1.11)
Fig. 2.10 A reflected beam of Brewster angle ϑB is linearly polarized perpendicular to the plane of incidence
ϑB
n1 n2
ϑ2
The Brewster angle depends only on the ratio of the refractive indices at both boundary surfaces. For a ratio of n2 /n1 = n = 1.5, the Brewster angle of ϑB = 56.31◦ results. The critical angle γcr and the Brewster angle ϑB are shown in dependence on n in Fig. 2.11. Polarized light produces always more intensive colors than unpolarized light; polarized light is generated in some absorption colorants and especially in liquid crystal pigments. In addition to that from Equation (2.1.6) and the above considerations, the reflection coefficient of directional light depends on the direction of polarization parallel to the plane of incidence. These properties also follow from Fresnel equations [14]. This is shown in Figs. 2.12 and 2.13 for a refractive index value of n = 1.5 in dependence on the angle of incidence ϑi . The outer reflectance coefficient at the boundary of the optically thinner medium begins to differ from one another for the two rectangular linear polarizations already for small angles
30
2 Light Sources, Types of Colorants, Observer 100
Angle / degree
80
60
γcr
40
ϑB 20
0 1.0
1.2
1.4 1.6 Refractive index n
1.8
2.0
Fig. 2.11 Critical angle γcr and Brewster angle ϑB in dependence of refractive index n
Outer reflection coefficient
1.0
0.8
Polarisation: parallel normal
0.6 n = 1.5 0.4
0.2
0
0
20
40
60
80
Angle of incidence ϑ1
Fig. 2.12 Outer Fresnel reflection factor as function of angle of incidence for polarization parallel and perpendicular to the plane of incidence
of incidence (Fig. 2.12). This difference increases strongly with the angle of incidence. The inner reflection coefficient at the inner boundary of the optically thicker medium shows the same behavior but is compressed into the angle range 0 < ϑ2 < 41.8◦ ; see Fig. 2.13. The high increase of this reflection coefficient is caused by the critical angle of total reflection. Consider now diffuse illumination instead of directional light. This alters the reflection character. The majority of natural and artificial light propagates diffusely. Because of this, it is, perhaps, most reasonable to measure and visually
2.1
Optical Radiation Sources and Interactions of Light
31
Inner reflection coefficient
1.0
Polarisation
0.8
parallel normal 0.6 n = 1.5
0.4
0.2
0
0
20
60 40 Angle of incidence ϑ2
80
Fig. 2.13 Inner Fresnel reflection factor as a function of angle of incidence for polarization parallel and perpendicular to the plane of incidence
judge color samples under diffuse illumination. Ideal diffuse light is in the forward direction inside an angle range of ±90◦ and of equal energy over the entire range of these angles. Because of that the radiation power, the optical interactions, and specially the reflection conditions at the boundary surfaces are changed. The reflection coefficients for diffuse radiation follow from energetic considerations leading to the relation 1 − rd∗ n22
=
1 − rd . n21
(2.1.12)
The quantity rd∗ denotes the reflection coefficient of diffuse light at the boundary of the optically thinner medium with n1 and rd stands for the reflection coefficient of the optically denser medium. In Fig. 2.14, the reflection coefficients for diffuse light are represented schematically by arrows for simplicity. For diffuse illumination from air of n1 ≈1.0 in a layer of refractive index n2 = 1.5, the appropriate reflection coefficients rd∗ = 0.09178 and rd = 0.59635 come from
Fig. 2.14 Reflection coefficients of diffuse radiation at a boundary surface of different refractive indices (schematically)
32
2 Light Sources, Types of Colorants, Observer 1.0 rd
Reflection coefficient
0.8
0.6
0.4
rd∗
0.2 r 0 1.0
1.2
1.4 1.6 Refractive index n
1.8
2.0
Fig. 2.15 Three sorts of reflection coefficients in dependence on refractive index n: r for directional illumination perpendicular to the surface, rd∗ for outer diffuse illumination, and rd for inner diffuse illumination of a material
the literature [13]. The reflection coefficients for diffuse light rd∗ and rd as well as for directional light at perpendicular illumination r are shown in Fig. 2.15 in dependence of the refractive index n. The boundary surface reflection certainly complicates the visual and measuring assessment of colored samples: this surface reflection is superimposed on the entire visual impression as well as the spectrometric measuring results. But the essential and interesting parts of color sensation are generated by the light interactions in the volume of a colored layer. For the following, we define the reflection of an optical medium as the amount of incident radiation energy which is backscattered from the volume and this is superimposed by the surface reflection energy. Correspondingly, the transmission is the amount of the incident light energy which overcomes the interactions in the volume and exits the second boundary surface of the optical medium. The accompanying energies are called reflection and transmission energy; these are abbreviated by WR and WT . The electromagnetic field of a light wave can drive vibrations of suitable charge carriers in atoms or molecules of absorption colorants. This additional absorption of energy leads sometimes to emission of secondary radiation; this process is denoted as scattering. The scattering is elastic if the wavelengths of the incoming and scattered light are equal. This is the case especially within non-self-luminous colors but also for Rayleigh and Mie scattering (Sections 2.1.2 and 5.1.3, respectively). Inelastic scattering, however, produces a change of scattered wavelengths such as in Raman and Brillouin scattering [16].
2.1
Optical Radiation Sources and Interactions of Light
33
In addition to scattering, a part of the incoming light energy is normally absorbed by the charge carriers of the colorant molecules and not scattered. This causes an increased molecular vibration energy and, therefore, a temperature increase of the coloration. The absorption of energy of amount WA is finally absent from the reflected, transmitted or scattered light. In the most colored layers, scattering and absorption occur simultaneously in different amounts, and additionally dependent on wavelength. The three mentioned energy components WR , WT , WA come from the incident energy Wi . Therefore, the energy conservation law, in our case, amounts to Wi = WR + WT + WA .
(2.1.13)
1 = R + T + A.
(2.1.14)
Division by Wi results in
The quantities R, T, A are denoted as follows: R = WR Wi reflectance,
(2.1.14a)
T = WT Wi transmittance,
(2.1.14b)
A = WA Wi absorption.
(2.1.14c)
These quotients are, for simplicity, also denoted as reflection, transmission, and absorption but also reflection factor, transmittance factor, and absorption factor, respectively. The law of energy conservation is an axiom of physics and is of fundamental importance; in the above formulation, it plays a central role in the entire radiative transfer of optical systems. The energy conservation law is even valid for each single wavelength, therefore, valid independent of the irradiated spectral power distribution. Furthermore, this law is independent of any specifications concerning the interacting particles of the optical medium. From that follows a basic realization, which is of great importance for the further discussions in this text: The resulting values of reflection, transmission, or absorption are characteristic quantities of the optical medium; in our case, they are essentially caused only by the colorants of the chromatic color. Reflectance and transmittance are determined with suitable color measuring instruments (Sections 4.2.1 and 4.2.2); absorption and scattering are characterized by corresponding optical constants which follow from optical models (Sections 5.1.2 and 5.1.4). Absorption and scattering are generally the most
34
2 Light Sources, Types of Colorants, Observer
important quantities of absorption colorants. In effect pigments, however, the dominant processes are wavelength dependent such as interference or diffraction. The basic optical laws responsible for color production of pearlescent, interference, and diffraction pigments are discussed in the next two sections.
2.1.6 Interference of Light The colors produced by absorption colorants and metallic pigments are essentially based on processes such as reflection, absorption, and scattering and are occurring at the surface and in the volume of a colored sample. In contrast to that, impressive color effects are generated by interference of light waves in pigment particles composed of an appropriate sequence of layers. Interference is an effect caused by superposition of suitable waves (of, e.g., liquids, gases, electromagnetic fields, elementary particles). Interference of light is, for example, responsible for the colors of soap lamellas, oil films on water, or coated lenses [17]; the colors of opals, natural pearls, insect wings, or bird feathers are in addition based on interference. The colors of interference pigments result from light waves, which are reflected at the inner and outer layer boundaries and which superimpose with the incoming waves. The produced colors are controlled by the thickness and refractive index of the different layers among other things. The layer thicknesses vary from about 10 nm to 1 μm; see Fig. 2.40 [18]. Interference colors can be distinguished from normal absorption colors by the color change in dependence of the observation angle; this is in some way similar to diffraction colors. A necessary requirement for interference is the existence of coherence. Most of temperature and luminescence radiators emit incoherent waves, because the single atoms of the source oscillate independently from each other, only short wave trains are produced; between the single waves exists no constant phase relationship. Waves are coherent, if the time dependence of their amplitude is the same irrespective of a phase shift. In the case of harmonic waves, this means that the frequencies of the waves have to be the same; however, they can have a constant phase difference. Coherent sine-shaped waves must, therefore, be of equal frequency. Coherent waves can result, for example, from the reflection of a radiative field at a mirror. From this perspective, laser light is of nearly perfect coherence because it is amplified during multiple reflections. Interference pigments normally consist of at least two layers of different refractive indices to produce a suitable reflection at the boundary layer, cf. Equation (2.1.6). In Fig. 2.16, there is a simplified illustration of the reflection and interference of light at a plane parallel layer. The reflected waves of beams R1 and R2 interfere above the layer. The waves of R 1 initiated by R1 take a longer way to the surface and, therefore, have an optical path length difference G with regard to the waves of R 2 . In view of the different path lengths, the ratio of refractive
2.1
Optical Radiation Sources and Interactions of Light R1
R2
35 R'1
ϑ1
R'2
ϑ1
n1 n2 d
ϑ2 n3
Fig. 2.16 Interference at a plane parallel layer of different refractive indices
indices n = n2 /n1 , the refraction law (2.1.5), and the phase jump of λ/2 caused by reflection of the waves at the upper layer surface, the difference G is given by
G = 2d ·
λ n2 − sin2 ϑ1 + , 2
(2.1.15)
where d stands for the layer thickness and ϑ1 for the angle of incidence. At some locations, the wave amplitude is increased by the so-called constructive interference of the incident and reflected waves. This occurs if G is an evennumbered multiple 2z of λ/2, fulfilling the condition: (2z − 1)λ = 4d ·
n2 − sin2 ϑz ,
z = 1, 2, 3, ... .
(2.1.16)
Destructive interference occurs for G = (2z + 1)λ 2,
z = 0, 1, 2, ... .
(2.1.17)
The positive integer z is called interference order. The amplifying light waves and, therefore, the corresponding colors can be modified according to Equation (2.1.16) by the material quantities d and n; this is used to a great extent for realization of different kinds of pearlescent and interference pigments. For color sensation, the additional change of color impression in dependence on the observation angle ϑz can be quite strange. The quantity ϑz belongs to the different interference orders z instead of the constant angle ϑ1 . Generally, the intensity of the amplified waves decreases strongly with the number of z.
36
2 Light Sources, Types of Colorants, Observer
Some special interference features result in the case that light is incident perpendicular to the surface of a layer. Colors of pearlescent and simple interference pigments are visually characterized by observation perpendicular to the colored surface; some important technical applications come out of this. From Equation (2.1.16) with ϑ1 = 0 for the dominant first interference order (z = 1), the simple result d = λ/4n follows. Furthermore, if the interference wavelength λ and the refractive index n are constant, the layer thickness for order z, given by d = (2z − 1)λ 4n,
(2.1.18)
leads to constructive interference. A stepwise increase of the layer thickness by the quantity d leads to a distance of Δd = λ/2n between two adjacent intensity maxima. The same distance holds for neighboring minima. These considerations are especially used to reduce the reflection of optical systems by destructive interference. With the so-called optical coating, the optical surfaces are coated with an inorganic layer by physical vapor deposition; the refractive index nC of the coating has to satisfy the condition √ (2.1.19) nC = n1 n2 , where n1 and n2 are the refractive indices of air and of the optical material, respectively. Unfortunately, the effectiveness of reflection reduction is limited to a middle visible wavelength. To achieve a nearly regular reduced reflection of wavelengths in the entire visible range, a multi-layered coating on both sides of the optical element is necessary at the most 10 layers which are tuned with each other. This is a type of dielectric coating called an anti-reflection coating. The so-called dielectric mirror coating relies likewise on interference. For this, multi-layer coatings of alternately higher and lower refractive indices nh and n1 are produced; see Fig. 2.17. If each single layer has a constant optical thickness dh = λ/4nh or dl = λ/4nl , then the reflected waves of first order interfere constructively with the incoming light caused by the additional phase jump at the boundary of the optical denser medium. Therefore, a narrowband mirror results; the reflectivity depends on the difference of the refractive indices of the layers [17]. With change of the layer parameters, the width of the wavelength interval can be controlled. These considerations are also used to achieve suitable layer structures in pearlescent and interference pigments to produce a dominant color component. Interference colors can be further improved by multiple reflection of light between two semi-transparent mirrors at distance d, similar to the placement in a so-called Fabry–Pérot interferometer; see Fig. 2.18. One part of the reflected light is transmitted through the second layer. Multiple reflection leads to a great number of partial beams, which interfere behind the second layer. The layer distance d and the refractive index n of the medium between the layers are chosen in such a way that only a small wavelength band is transmitted; this construction
2.1
Optical Radiation Sources and Interactions of Light
37
Fig. 2.17 Layer sequences of a dielectric mirror with high and low refractive indices nh and n1
nh nl nh nl
dh =
λ 4nh
dl =
λ 4nl
Substrate
operates as an interference filter. For fixed distance d, this construction is also called an etalon. The deciding parameters for the interference efficacy are n and d of the intermediate layer. Because adjacent beams have the same geometrical optical path difference, constructive interference is given by zλ = 2nd cos αz ,
z = ±1, ± 2, ... .
(2.1.20)
The intensified wavelengths become, therefore, smaller with increasing angle of beam incidence α z . For a layer thickness d = 300 nm and refractive index n = 1.5, the wavelengths of violet and red light (400 and 700 nm) are separated for the first order by an angle difference of about 25◦ . Founded on this principle, d
L
LQ P
Q1 n Q
αz
Fig. 2.18 Fabry–Pérot interferometer: the partial waves of points Q, Q1 produce interferences of “equal inclination”
38
2 Light Sources, Types of Colorants, Observer
in particular, is the angle-dependent color effect of multi-layered interference pigments in liquid crystal structures; see Fig. 2.43.
2.1.7 Diffraction from Transmission and Reflection Gratings When light is incident on objects or boundaries with dimensions on the order of the wavelength of the light, the wave characteristics of light become very important. This is the situation, for example, at a diffraction grating. Upon passing through the grating, some portion of the light is deflected and/or is fanned out depending on the grating geometry and the wavelength. This phenomenon is an example of Fraunhofer diffraction if the light beam is incident nearly perpendicular to the grating [19]. In addition to macroscopic structured materials, diffraction pigments can be impressed with such grating structures. This leads to color effects which are also depending on the angle of observation. A simple macroscopic transmission grating is shown in Fig. 2.19, not to scale. The geometry is simply achieved by scratching or etching of equidistant grooves in a thin plane parallel glass sheet. With recent techniques, diffraction pigments can be impressed with nanostructures. Each constant groove gap d, also called grating period, contains a narrow light-transmitting slit. The reciprocal quantity of the grating period, g = 1/d, is denoted as the grating constant; its units are given in lines per millimeter (l/mm). At each of the slits – which are spaced with typically as much as 5,000 l/mm or more – the incident wave front
αz
αi
d
αi G1
αz G2
Fig. 2.19 Diffraction conditions of an optical transmission grating (schematically)
2.1
Optical Radiation Sources and Interactions of Light
39
is diffracted according to the Huygens principle, which means that each point of a wave front is assumed to be the origin of a new elementary wave [19]. Because diffraction occurs at all illuminated grating slits, a pattern of constructively and destructively interfered waves develops behind the grating. The path difference G1 + G2 of waves coming from two neighboring slits follows from Fig. 2.19 as G1 + G2 = d(n1 sin αi + n2 sin αz ),
(2.1.21)
where n1 and n2 stand for the refractive indices in front and after the grating and α i for the angle of incidence. The diffraction maxima occur for a path difference G1 + G2 equal to an integer multiple z of the wavelength λ. With Equation (2.1.21), the relation zλ = d(n1 sin αi + n2 sin αz ), z = 0, ± 1, ± 2, ...,
(2.1.22)
follows. The zeroth-order diffraction, equivalent to z = 0, contains all wavelengths of the irradiated light. Higher diffraction orders for z = 0 are generated on both sides of the zeroth order with symmetric intensity maxima and minima. The wavelengths contained in the incident light fan out by the grating in such a manner that the condition in Equation (2.1.22) is fulfilled. The grating deflects large wavelengths stronger than shorter wavelengths; this is the converse of a prism. Moreover, the diffraction spectrum of the first order is of higher intensity compared to that of a prism spectrum. In order to avoid an overlapping of the diffraction maxima of higher order, the incident angle α i and the grating period d can suitably be tuned with each other (see below). In addition to transmission gratings, reflection gratings are also commonly used – these are especially realized in diffraction pigments. These can be formed by vapor coating both sides of a nontransparent grating structure with an additional layer of a reflecting metal, cf. Fig. 2.20; this has the added bonus of a possible improvement in the mechanical stability of the thin plates. The waves reflected from the periodically arranged mirrors interfere with the incoming waves from the opposite direction. Consequently, the diffraction pattern already known from transmission gratings develops in front of the reflection grating. The cross section of the grooves can be produced as rectangular, triangular, or sine shaped. Reflection gratings are used in modern spectrophotometers and optimized diffraction pigments, among other things. Examples of diffraction particles are shown in Figs. 2.54 and 2.55. Concerning the reflection grating in Fig. 2.20, the path difference G1 – G2 of the reflected waves from adjoining grooves follows from the expression G1 − G2 = d( sin αi − sin αz ) .
(2.1.23)
40
2 Light Sources, Types of Colorants, Observer
Fig. 2.20 Diffraction conditions of an optical reflection grating (schematically)
αi G2
αi d
αz G1
αz
In analogy to the transmission grating, the diffraction maxima are given by zλ = d( sin αi − sin αz ) ,
z = 0, ± 1, ± 2, ... .
(2.1.24)
For z = 0, it follows α i = α 0 and the grating operates like a normal flat mirror, that is, the wavelengths are not separated. Generally, the use of gratings results in spectra of higher light intensity in comparison to prisms, but the incident intensity is distributed among all diffraction orders. Among them, is the maximum for z = 0, which is of highest intensity, and also generally not of interest (see Fig. 2.21). This disadvantage can be bypassed using a so-called echelette grating5 ; see Fig. 2.22. On the basis of the special geometry of such a grating, nearly the entire intensity of the diffracted light can be concentrated into a particular diffraction order, as required. To achieve this aim, the cross section of the grooves has to meet the following requirements: 1. The desired diffraction order zB is not zero; the reflecting grating elements should be tilted by an angle α B above the grating base; this angle is called the blaze angle, after the corresponding production method known as the blaze technique.
5 echelette:
French, small ladder.
2.1
Optical Radiation Sources and Interactions of Light
41
Δα
Δβ
Fig. 2.21 Angle differences of diffraction maxima
2. The angle half-width α of the diffraction fringe, caused by this kind of grating element, has to be matched with the angle distance β between two successive diffraction maxima; see Fig. 2.21. In view of the first condition, it is useful to consider the angles from the grating base normal. The blaze angle is, therefore, given by the simple relation αB = (αi − αz ) 2,
(2.1.25)
where α i and αz are the angle of incidence and the diffraction angle of order z, respectively. In addition, these two angles are combined with Equation (2.1.24), to give zB λB = d · (sin αi − sin αz ) , Grating normal
zB = 0, ± 1, ± 2, ... .
Face normal
αB αi αz b
αB d
Fig. 2.22 Echelette grating with blaze angle α B
(2.1.26)
42
2 Light Sources, Types of Colorants, Observer
The quantity λB is called blaze wavelength and zB denotes the blaze order. According to Equation (2.1.25), the blaze angle depends on the incident and the diffraction angles. For this reason, echelette gratings can be realized with different blaze angles. From the last two expressions, the condition zB λB = d · [ sin αi + sin (2αB − αi )] ,
zB = 0, ± 1, ± 2, ...
(2.1.27)
follows. It is independent of a diffraction angle. For improved understanding, we differentiate now between two types of light incidence – from which consequently follow different blaze angles. In the first case, we assume an illumination in the direction of the grating normal; see Fig. 2.22. In this case, the angle of incidence is α i = 0 and it follows from Equation (2.1.27): zB λB 1 , zB = 0, ± 1, ± 2, ... . αB = arcsin (2.1.28) 2 d In the second case, the light is incident in the direction of the face normal, the so-called Littrow or autocollimation configuration. In this case, then the incident angle is equal to the blaze angle α i =α B given by zB λB (2.1.29) , zB = 0, ± 1, ± 2, ... . αB = arcsin 2d Note that because an echelette grating of sine-shaped cross section can be approximated by a series of successive isosceles triangles, the outlined considerations are also applicable to that geometry. From the second condition above, some further geometrical conclusions result. With the designations given in Figs. 2.20 and 2.22, the relation cos αz b = d cos (αz − αB )
(2.1.30)
can be derived. In other words, the triangle geometry depends on the blaze angle as well as the angle αz of diffraction order z. Additionally, according to Equation (2.1.30), the width b of a step is specified with the groove distance d. If the illumination is carried out parallel to the grating normal, from Fig. 2.22, we have the intermediate result α z = 2α B . The condition b=d·
cos 2αB cos αB
(2.1.31)
therefore follows. On the other hand, for illumination parallel to the face normal, the condition α z = α B is given and the simple formula b = d · cos αB
(2.1.32)
2.2
Absorbing Colorants
43
follows from Equation (2.1.30). In this case, the triangle of the echelette grating is right angled. The utilizable wavelength range of such kinds of gratings is roughly limited to the interval 0.7λB ≤ λ ≤ 2λB . Absorption and scattering dissipation reduce the efficiency of a blaze grating to about 70% [20]. Accordingly, the blaze technique enables the focusing of about 70% of the influx into a desired z = 0 diffraction order. Each diffraction pigment is normally optimized with regard to the first diffraction order z = ±1. This diffraction spectrum can be observed symmetrically with respect to the direction of illumination, and is followed by further orders of lower intensity, cf. Section 3.5.5. These principles apply not only to macroscopic gratings but also to diffractive pigment particles; see Figs. 2.55 and 2.56.
2.2 Absorbing Colorants After considering different light sources and basic light interactions in the previous section, the second fundamental component for color producing of non-self-luminous colors is the color sample containing the colorants. Colorants can be divided into two groups, depending on the dominant mechanism of color production: classical absorption colorants and modern effect pigments (cf. Table 1.1). Industrially applied absorption colorants consist mainly of synthesized colors of inorganic and organic compounds, and in some rare cases of modified natural colors. In this section, we characterize dyes and absorption pigments, describe the most important color attributes and the accompanying coloristic properties as well. Some of these properties are correlated with specific spectral features of the corresponding coloration. Additionally, color-order systems will be outlined. In some application cases, such systems offer an overview of the diverse-generated absorption colors. Each of these color order systems is grouped according to preset characteristic criteria. On one such system is based a special CIE color space. It is also shown that the color impression results from light interactions in the volume as well as at the surface of a color pattern. Properties of effect pigments are described in the next section, which show a typical color development in dependence of the angle of observation, a dependence that is absent in absorption colorants.
2.2.1 Types and Attributes of Absorbing Colorants According to a rough classification, colors can be produced by 15 different physical mechanisms [21]. In the case of non-self-luminous colors, these processes are entirely attributable to energetic interactions of electromagnetic waves with the bounded electrons of atoms, molecules, particles, or crystallites of the color-producing material. With regard to absorption colorants, we first outline
44
2 Light Sources, Types of Colorants, Observer
some typical phenomenological properties of absorption pigments and afterward those of dyes. The color origin of absorption pigments can be reduced to absorption and scattering processes. Such kinds of light interactions are called selective if they are effective in a narrow range of wavelengths in the visible spectrum. Light is scattered by pigment particles if at least two conditions are met: first, the particle dimensions and the wavelengths of the irradiated light are on the same order of magnitude; second, the colorant molecules show spatially separated electric charge distributions – the so-called multipoles. Details of these are given in Sections 5.1.2 and 5.1.3. Chromatic absorption pigments are also called colored pigments or sometimes merely pigments. They consist of inorganic and organic compounds which, in either case, form crystallites of sometimes different types. The crystallite dimensions are typically of the same order of magnitude lesser as the wavelengths of light. Because of the charge separations in multipoles, the morphological non-uniform crystallites sometimes conglomerate to form differently shaped particles with sizes from 10 nm to as much as 1 μm in size. All sorts of pigments – absorption as well as effect pigments – are insoluble in a binder or any polymer matrix. The pigments are usually uniformly dispersible in such materials although some need a suited additive for that. These colorants are used not only, for example, for mass coloration of plastic materials, fibers, paper but also for coloring of lacquers, pastes, and coatings of solids of quite different surfaces. In synthetic high polymers, the pigments tend to congregate in the amorphous regions and, therefore, additionally change the mechanical, thermal, or even electrical properties of the compound. Of great importance – with regard to color physical applications – are the covering capacity (also called hiding power), color strength, and tinting power. Requirements for optimized incorporation of pigments are sufficient wettability, dispersibility, as well as compatibility of the binding materials used, polymers, or additives, among other things. Inorganic pigments consist of oxides, sulfides, sulfates, silicates, chromates, carbonates, and metal complexes, for example [22]. Compared to organic pigments, they are preferentially used on account of their distinct optical scattering power and the typical high hiding power. In comparison with organic pigments, due to their simple and stable molecular structure, inorganic pigments tend to have better rheological behavior as well as increased weather resistance. Characteristically, inorganic pigments are mostly dull colors with lower color strength but with greater hiding power compared to organic colorants. A multitude of absorbing colorations with desired color properties are, therefore, achieved only with mixtures of inorganic and organic pigments. With regard to the chemical structure, organic pigments are divided into azopigments, polycyclic pigments, and anthraquinone pigments. The outstanding feature of organic pigments is their distinctive colorfulness or chroma in comparison to inorganic pigments. This generally comes with a high color strength.
2.2
Absorbing Colorants
45
Compounds of polycyclic structures, compared to molecules with azo-groups, tend to disperse better in polymer binders, have a lower migration tendency, as well as higher weather durability [23]. Table 2.3 shows the most commonly used modern inorganic and organic absorption pigments, differentiated with regard to the kind of the dominant color production mechanism. White and black pigments assume a special role in industrial color physics. White pigments stand out due to their nearly ideal scattering of light in the visible range. They are preferentially used for pure white, increase in the lightness of any coloration, or covering of a background. On the other hand, the characteristic feature of black pigments is the dominant absorption. These pigments are applied mainly in tiny amounts for black colors and for darkening of absorption colors. With calibration series of white and black pigment mixtures, the calibration of the lightness scale is, therefore, carried out between minimal scattering (pure black pigment) and maximal scattering (pure white pigment). An analog consideration holds for the case of absorption (Section 6.1.1). It is further the case that a really tiny amount of a black pigment improves the interference color of transparent pearlescent or interference pigments; this is because the black amount absorbs the complementary color produced of interference pigments. Table 2.3 lists also fluorescence and phosphorescence pigments. These are summarized by the term luminescence pigments. Both sorts absorb light normally at lower wavelengths in the range of X-rays, UV, or the visible spectrum; they often also absorb energy from electron beams. After some short time, a part of the absorbed quantum energy is reemitted but with longer wavelengths (lower energy) according to Equation (2.1.2). Fluorescence radiation is emitted spontaneously and phosphorous radiation, in particular, has a delay in the reemission. In contrast to phosphorescence (Section 4.2.6), fluorescence emission stops immediately after illumination. Unlike absorption pigments, dyes are completely soluble in a solvent or in a polymeric medium. The coloristic properties are essentially based on absorption. On account of the absence of scattering, dyes are normally transparent – notable exceptions are dark dyes in high concentrations. Dyes consist nearly exclusively of organic chemical structures. Typical groups of atoms with covalent bonds such as >C=CC=O, or –N=N– (ethylene, carboxyl, or azo group, respectively), called chromophores, are typically responsible for the coloration of the organic compounds. The π-electrons6 of these covalent bonds absorb a fraction of the incoming light waves. The incorporation of further molecular groups, the so-called auxochromes, causes a color shift either to
6 In chemical compounds π -electrons form a pair of electrons which belong together to two different atoms.
Color production
Selective scattering/ selective absorption
Pigment
Absorption pigment, colored pigment Oxides Iron-II-oxide, iron-III-oxide, chromium-III-oxide, chromium-IV-oxide, chromium-VI-oxide pigments Mixtures with oxide pigments: cobalt blue, cobalt green, zinc iron brown Chromate pigments Chromium yellow, chromium orange, chromium green; chromium titanate, molybdate red, molybdate orange; copper chromate Iron blue pigments Iron cyanide blue Cadmium, bismuth pigments, ultramarine pigments
Inorganic
Typical examples
Table 2.3 Typical modern inorganic and organic absorption pigments
Azo pigments Mono-pigment, disazo-pigment, β-naphthole pigment, naphthole AS pigment, benzimidazolon pigment, disazo condensation pigment, metal complex pigment Polycyclic pigments Phthalocyanine, carbazole, quinacridone, perylene, perinone, pyrrolo/pyrrole, thioindigo pigments Anthraquinone pigments Anthrapyrimidine, flavanthrone, pyranthrone, anthanthrone, dioxazine, triarylcarbonium, quinophthalone pigments
Organic
46 2 Light Sources, Types of Colorants, Observer
Color production
Scattering
Absorption
Selective absorption, emission within 10 ns
Selective absorption, emission after 1 ms
Pigment
White pigment
Black pigment
Fluorescent pigment
Phosphorescent pigment
Pure phosphors Alkaline tungsten salts Other phosphors Alkali halogenoids, alkaline earth oxides, alkaline earth sulfides, Barium oxide: doped with Na, Mn, Ce, Sn, Cu, Ag; zinc phosphide, cadmium phosphide, gallium sulfide, zinc sulfide, cadmium selenide, gallium phosphide
Fluorite, uranylic salts, salts with metals of rare earths
Carbon black, iron oxide black, copper chromate
Titanium dioxide (anastas, rutil), zinc sulfide, zinc oxide pigments
Inorganic
Typical examples
Table 2.3 (continued)
Pure phosphors Carbazoles Other phosphors Fluorescent organic substances, embedded in crystalline matter
Oxinaphthaldazine, disazomethine
Aniline black
White plastic powders
Organic
2.2 Absorbing Colorants 47
48
2 Light Sources, Types of Colorants, Observer
higher wavelengths as with –NH2 and –OH groups (amino and hydroxyl groups, respectively) or to lower wavelengths with –NH–CO–CH3 (ethylene-acid-amide group), for example. Dyes are subdivided into natural and synthetic compounds; see Table 2.4. Dyes found in nature are generally known by common names like indigo, crimson, saffron, or alizarin, although they are prepared partial artificially today. For reasons of product constancy, generally only synthetic dyes are applied. Among synthetic dyes are azo-dye, anthraquinone dye, indigo dye, cationic dye, phthalocyanine dye, polymethine dye, triphenylmethane dye, xanthene dye, and fluorescence dye [24, 25]. Owing to their molecular double bond structures, dyes show a poorer fastness to light and weather resistance in comparison to pigments. The basic molecular interactions of fluorescence dyes and pigments are described in the literature [26]. Table 2.4 Typical examples of natural and synthetic dyes Dye
Typical examples
Natural
Indigo, crimson, saffron, alizarin
Synthetic
Azo-dye, anthraquinone dye, indigo dye, cationic dye, phthalocyanine dye, polymethine dye, triphenylmethane dye, xanthene dye, fluorescence dye
2.2.2 Pigment Mixtures and Light Transmittance The wavelengths of the visible range which are not absorbed by colorants make up a so-called complementary color. This color is the perceived color of the absorbing dye or pigment; see Table 2.5. It can be seen in the table Table 2.5 Spectral range of absorption, light color, and perceived complementary color of absorption colorants Rough spectral range of absorption/nm
Light color of the spectral range
Perceived complementary color of the colorant
380–440 440–480 480–490 490–500 500–560
Violet Blue Green blue Blue-green Green
Yellow-green Yellow Orange Red Crimson
560–580 580–595 595–605 605–750 750–780
Yellow-green Yellow Orange Red Crimson
Violet Blue Green blue Blue-green Green
2.2
Absorbing Colorants
49
that the light and complementary colors reverse their roles at a wavelength of about 560 nm. Over and above that, in Table 2.19 are given some pairs and triples of complementary colors; some of them are partly demonstrated in Color plate 1.7 These relationships concerning complementary colors are valid for uniform spectral power distributions of the irradiated light similar to a xenon discharge lamp. Complementary colors are arranged opposite (according to Hering color opponent theory) in a color plane of the CIELAB system; see Color plate 4. As mentioned in the previous section, the realization of a desired color is normally achieved with mixtures of different sorts of colorants. Apart from coloristic aspects, concerns over the compatibility and color fastness of the components are in the forefront. Colorations of lacquers, plastic materials, or textile fibers consist usually of mixtures with three up to six or more different colorants. Mixtures of different fluorescence dyes can be distorted by fluorescence extinction if the quantum emission of one dye in the visible range causes a fluorescence stimulation of a second dye in this range. For the realization of a great number of different color shades, a selection of at least 25 up to about 130 chromatic, white, and black absorbing pigments has to be made and as much as of 110 effect pigments. Among the colored absorption pigments, normally yellow and red should preponderate in comparison to violet, blue, or green shades; additionally, two to four brown colorants are normally taken into consideration. Similar considerations should be taken into account for dyes. The predicted color should match the reference color as exact as possible. In the majority of cases, there are additional properties, such as high color constancy or low metamerism, which need to be fulfilled. It is, therefore, necessary to have a broad experience with the composition of the colorant components and binding materials for mixing in order to achieve the coloristic, processing, or basic performance conditions required with regard to the reference color. Color samples are termed as transparent, translucent, or opaque in dependence on their light transmittance properties. Requirements for transparent colors are not only pure absorption and complete solubility of the used colorants but also the refractive indices of the applied colorant matrix (e.g., solvents, binding agent, or plastic materials) have to agree with those of the used colorants. Transparent optical media are characterized by the wavelength-dependent absorption coefficient. This coefficient follows from the spectrometric measurements of the transmittance and a suitable approximation of radiative transfer in optical media (Section 5.1). A transparent chromatic layer is perceived by way of not only transmitted light but also reflected light. The accompanying reflectance comes merely
7 Color plates
are inserted between Chapters 3 and 4.
50
2 Light Sources, Types of Colorants, Observer Table 2.6 Light transmittance and spectral quantities of color samples Measuring quantities
Determination quantities
Examples
Transparent
Directed, diffuse reflectance and transmittance
Absorption coefficient K
Liquids, inorganic, organic glasses
Translucent, translucent nonopaque, translucent glimmering
Directed, diffuse reflectance and transmittance
Absorption coefficient K, scattering coefficient S, phase function p
Binders, foils of partially crystalline high polymers, paper, opal glasses
Opaque
Directed, diffuse reflectance
Absorption coefficient K, scattering coefficient S, phase function p
Emulsion paints, lacquers, plastics, textiles, ceramics, leather
Light transmittance
from reflection at the illuminated outer and inner boundary surfaces which is caused by differing refractive indices. The magnitude of the reflected portion follows from Equations (2.1.6), (2.1.7), (2.1.8), (2.1.9), (2.1.10) or (2.1.12). In Table 2.6, three different sorts of color samples with regard to the degree of light transmittance are listed along with some spectral measuring and determination quantities. Translucent color patterns such as turbid films, paper, or opal glass are characterized by selective absorption and simultaneous scattering. Translucent media are only light transmitting on a small scale; nonetheless, a colored background is not completely covered. The light transmittance decreases with increasing layer thickness, this is similar to transparent layers. Some organic pigments of light yellow, orange, or red shade are translucent as are some pearlescent and liquid crystal pigments. The scattering of light occurs at the irregular surfaces or edges of the pigment particles and caused by the electromagnetic interactions with the multipoles of the pigment particles. In general, scattering of translucent colors depends on the pigment sorts used, the chemical structure of the surrounds, the refractive indices, and the structure of the boundary surfaces. Translucent colorations are particularly of interest for such coloristic applications, in which the same hue is to be realized simultaneously in a nearly transparent and almost opaque finish. In addition to reflectance and transmittance, the characteristic quantities of translucent color samples are turbidity and covering capacity (Sections 3.4.3, 3.4.4, and 3.4.5). The theoretical modeling of radiative transfer in translucent systems can actually be quite difficult. These complications are caused by the combined processes of absorption and scattering, where the latter is anisotropic in some
2.2
Absorbing Colorants
51
cases. On the basis of the different optical effects, translucent materials can be subdivided into the following groups: ideal translucent: a directional ray is partly absorbed and diffuse scattered; it exits the medium with lower intensity; translucent diaphanous: the primary ray in the optical medium is surrounded by a halo8 ; the primary ray is more attenuated than in the ideal translucent case; translucent gleaming: the energy of the primary ray is spread out in an intense halo; there is virtually no primary ray remaining at the second boundary surface. These different translucent states are best modeled with a multi-flux approximation. For this, in addition to absorption and scattering coefficients of the optical medium, some additional optical quantities such as the phase function p, for example, need to be taken into consideration (Section 5.1.5). The majority of natural and artificial non-self-luminous colors are opaque; they, therefore, appear impenetrable from the rear – a background is covered completely by this kind of colors. In all opaque systems light scattering is normally the dominant process, and it is accompanied by more or less distinct absorption. Scattering occurs isotropically without a preferred direction or, the other extreme, anisotropic with a specific preferred direction. Increasing scattering lowers the light transmittance and vice versa. The covering capacity of a coloration is, above all, caused by the scattering power of the pigment particles. The single spectrometric measuring quantity of opaque materials is the reflectance. The reflectance, in general, depends on the measuring angle for many kinds of effect pigments. Extreme optical states result in mixtures of absorption and effect pigments with different light transmittance. These are most often implemented in lacquers or plastic materials for consumer goods.
2.2.3 Description of Color Attributes Based on the discussion in the previous sections, it should be clear that the color of absorbing colorants is caused by light interactions such as scattering and absorption. On the other hand, the produced visual color sensation is by no means completely characterized by those. The variety of different combinations of wavelengths as well as the accompanying power distributions reaching the eye results in many colors, which can be described by different color attributes. For better understanding of the context, we use an analogy from acoustics. 8 This is a circular light spot encircling the primary ray; the halo of the Moon, for example, results of light refraction at the ice crystals in the atmosphere.
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2 Light Sources, Types of Colorants, Observer
A pure acoustic tone is unambiguous, physically described by its frequency and amplitude. The same tone, produced from different music instruments, is however surrounded by a typical sound spectrum. In a similar way, each nonself-luminous color is produced not simply by a single light frequency but also from various spectral values of the visible spectrum.9 The different wavelengths simultaneously entering the eye are perceived as a single color impression and not as separate single-colored wavelengths. This entire color impression can be verbally described by characteristic terms. The description or comparison of colors is used in color industry not only from physical or colorimetrical points of view but also according to coloristical attributes [27]. The following enumeration, which is not to be considered complete, gives some conventional terms for characterizing the color impression of non-selfluminous colors. The accompanying definitions and assemblies are, however, not uniformly used in the literature: hue, shade: the color property which is mainly described by adjectives such as red, green, yellow, blue; hue and shade are terms equivalent to color tone, or tint, see below; relative color strength, relative tinting strength: the color economy of an available colorant material relative to an arbitrarily chosen colorant of equal or similar color; color depth, color intensity: the color distinctiveness, which increases with enhancement of the same colorant amount; dullness: a characteristic color feature which can be described by an existing amount of gray or black; it is the converse to brightness. The quantitative determination of relative color strength is standardized based on colorimetric criteria (Section 3.4.2). These instructions underlie the formalism of the CIELAB or DIN99o color spaces. The following terms are also used to denote a color point in color space: lightness: a measure for the reflectance of a non-self-luminous colorant; the reflection ratio of absorption colorants is standardized by the so-called gray scale in which black is assigned to the value of 0 and white to the value 1; fluorescent and effect colorants often have reflectance values greater than 1, caused by the arbitrary fixing of the gray scale; selfluminous sources such as light sources or the sky are characterized by the term brightness rather than lightness; saturation: a quantity describing the colorfulness of colorants which does not change by further increase of the colorant concentration; shade, color tone: this corresponds to hue; equivalent terms are tint or tinge; 9 This metaphor is not to be confused with synesthesia, in which a physiological stimulus induces a further stimulus, for example, colors are associated with music and vice versa.
2.2
Absorbing Colorants
53
chroma: an absorption colorant loses colorfulness with lower saturation; chroma depends on both saturation as well as lightness because a tiny amount of black reduces the colorfulness of a color.10 Common for characterization of color impressions are also adjectives and their comparative forms; their meaning is somewhat equivalent to the terms already given above. Here are listed properties in opposing pairs: colored, chromatic: any color, such as yellow, orange, red, or green; it is analogous to the term hue; uncolored, achromatic: colors like white, gray, or black; light, bright: a color with a high lightness amount; light colors have a high reflectivity; dark: colors of small or even zero reflectance; brilliant, clear, pure: colors of both high hue and high lightness but missing white amount; pale, dirty, dull: colors of both minor hue and minor lightness. A great number of non-self-luminous colors containing absorption colorants can be directly manufactured with properties in the ranges of the last 12 listed extreme color states. Some of the cited characteristics correlate also with typical special features of the corresponding spectral reflection or transmission curve traces. The measured spectrum can sometimes be interpreted as a kind of “finger print” of the accompanying color. Some of these properties can be visualized by characteristic spectral reflection curves of absorption pigments, for example, in Figs. 2.23–2.27. Some of these features can also be found by the angle-dependent spectral reflection of effect pigments. The spectral reflectance of a chromatic absorption color is generally characterized by either a significant maximum (e.g., violet, blue, green) or a steep rise to higher wavelengths (e.g., yellow, orange, red) in the wavelength range of the complementary color or rather natural color; see Fig. 2.23. The highest absorption exists in a wavelength range of a distinct reflection minimum; backscattering, however, dominates in the range of maximal reflection or the plateau region of the relevant pigment. In contrast, an achromatic color shows a nearly constant spectral reflectance; see Fig. 2.24. Ideally scattering white is represented in the visible range by a constant reflection of 1.0 and ideal black of 0.0; gray takes intermediate values depending on the content of white or black. The decrease of spectral reflection for white or gray with shorter wavelengths is due to the tail of the UV absorption of the underlying TiO2 pigment. The impression of white results exclusively 10 These four color terms can be visualized by geometrical quantities in both mentioned color
spaces and further ones; see Sections 3.1.3 and 3.1.4.
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2 Light Sources, Types of Colorants, Observer
R(λ) c 0.8
d e
0.6 b a 0.4
0.2
0
400
500
600
λ
700
nm
Fig. 2.23 Spectral reflectance curves of chromatic pigments: (a) blue, (b) green, (c) yellow, (d) orange, and (e) red
R(λ)
a 0.8
0.6 b 0.4
0.2 c 0
400
500
600
700
λ
nm
Fig. 2.24 Spectral reflectance curves of achromatic colors: (a) white, (b) gray, and (c) black
2.2
Absorbing Colorants
55
R(λ) 2bt 0.8
2dk
1bt
0.6
0.4 1dk 0.2
0
400
500
600
700
λ
nm
Fig. 2.25 Spectral reflectance of bright and dark pigments: 1bt bright blue, 1dk dark blue, 2bt bright yellow, and 2dk dark yellow
R(λ)
0.8 a 0.6 b 0.4 c 0.2
0
400
500
600
700
λ
nm
Fig. 2.26 Spectral reflectance of different gray colors: (a) light gray, (b) middle gray, and (c) dark gray
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2 Light Sources, Types of Colorants, Observer
R(λ) 2br 0.8 2du 1br 0.6
0.4 1du 0.2
0
400
500
600
700
λ
nm
Fig. 2.27 Spectral reflectance of brilliant and dull pigments: 1br brilliant blue, 1du dull blue, 2br brilliant yellow, and 2du dull yellow
from regular light scattering over the entire visible range. This is the case for examples such as water vapor, clouds, or snow. Ideal black, on the other hand, is caused by absorption of entire visible wavelengths. Light (or dark) colors stand out either due to a high (low) reflection maximum or a widened (narrowed) plateau region; a light (dark) gray shows a shift of the reflection level to white (black); see Figs. 2.24 and 2.26. Most of the color-order systems and the colored calibration samples for recipe prediction are based on colored pigment mixtures with white and black colorants. It is remarkable that the human eye provided by nature is more sensitive to color differences between dark colors (violet, blue, green) in comparison to light colors (yellow, orange, red). This is correlated with a low maximum respective high reflectance plateau range. The higher and steeper the rise of the curve to the plateau region or the smaller the half-width of the reflection maximum, the more the color is perceived as brilliant, clear, or pure. Conversely, pale, dirty, or dull colors possess a spectral reflection characterized by a lower and broader maximum or overlapping maxima, compare in Fig. 2.27 curve 1br with 1du for a blue pigment. The spectral reflectance of a dull yellow, for example, shows a more flat peak profile and a lower plateau range compared to a brilliant yellow, cf. curves 2br, 2du in Fig. 2.27. The terms outlined up to now are merely used to describe some typical coloristical properties of classical absorption colors or colorants. This vocabulary
2.2
Absorbing Colorants
57
cannot be directly carried over to effect pigments. Rather than absorption and scattering, effect pigments produce new sorts of colors on account of different optical mechanisms; identical terms have, therefore, different meanings for effect pigments than for absorption colorants. Metallic pigments, for example, produce a characteristic metallic lightness, brilliance, or hue extinction. This ambiguity is discussed in Sections 2.3.3 and 3.5.1.
2.2.4 Color-Order Systems It is quite remarkable that the color sense of humans is capable of distinguishing about 10 millions of colors. It is further important to note that, in addition to the astonishing number of colors, a color can have different attributes; therefore, it seems essential to have systematic classifications for such a tremendous diversity of colors. Such classification systems serve not only as an overview but also as an improved communication about non-self-luminous colors, particularly for their use in difficult applications. From each of the established color-order systems, series of color samples exist for visualization. The antiquated color classifications are certainly not ordered after uniform criteria [28, 29]. The chronologically first systems were arranged based on features, which included the actual knowledge about colors. Among the contemporarily used color-order systems are to differentiate roughly two groups: systems on coloristic and on colorimetric basis. In the following, we sketch the common four representative examples of both groups. The most important coloristic-order system is that of Munsell, established in 1905. It is simultaneously comprised of various companion features such as, for example, precise nomenclature or systematic extension capability for additional colors [30]. The corresponding color patterns are ordered according to the three properties hue H, value V, and chroma C in three dimensions in a cylindrical coordinate system. The true significance of this collection are the colored patterns which display a nearly constant color difference between neighboring colorations. This was developed without any colorimetric background – an amazing for the beginning of the 20th century. In spite of the visually nearly equal color steps, this color-order system was not accepted until 1976 as a basis of the CIELAB system. Experience with the Munsell system has brought out critical disadvantages. Particularly unfavorable are the non-uniform perceived color differences of bright and dark colors. In remedy of these shortcomings, the Munsell system was supplemented by an additional color pattern in 1990. The natural color system (NCS) was worked out in Sweden and is standardized there; it is based on the opponent color theory of Hering and is arranged in pairs of the four chromatic colors red, green yellow, and blue as well as the achromatic colors white and black [31]. The patterns are organized in color
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2 Light Sources, Types of Colorants, Observer
spectra and color triangles after the three criteria blackness s, colorfulness c, and shade Φ. They are grouped in the form of an atlas of 1,741 color patterns. In spite of this great number, the NCS system is restricted in its applicability. It incompletely covers the color space, and additionally, colors with glossy surface are inapplicably marked. Moreover, the arrangement pattern is visually non-uniform. Without a measuring device, this color system is, therefore, only suited for rough orientation in color space. The so-called color index (C.I.) is suited for identification of colorants but represents no real color-order system as in the discussion above. It simply consists of a list with unsystematically assembled dyes and absorption pigments. These are partially denoted according to the origin (generic names) and according to the chemical constitution with natural numbers (constitution numbers) [32]. This listing offers a certain aid only in a few cases, if, for example, some of the colorants listed in the C.I. are to exchange with one another. Strictly speaking, the widely distributed color registry RAL 840 HR in Germany is also not a color-order system in a broader sense. This registry was created to ensure that industrial colors are classified uniformly with defined names and numbers for better communication between public agencies and producers of consumer goods. The color patterns were originally vaguely arranged in view of coloristic criteria; in the meantime, a modification was undertaken using the so-called DIN color chart, see below. It should be added that contemporary color systems also consist of patterns which change uniformly by a suitable technical parameter such as the concentration of the used colorants, for example. The corresponding inconstant changes of hue, lightness, or chroma certainly make color perception and color comparison more difficult. A visual ascertainment of color differences is not ensured by such systems. In contrast to the order arrangements above, the DIN color chart is a colorimetric-based color system [33]. It comes from the CIE chromaticity diagram; see Section 3.1.2 and Color plate 2. The color patterns are arranged with regard to three properties, similar to the Munsell system. These color properties are denoted as darkness D, hue T, and saturation S. They correspond to the ∗ , and chroma C∗ of the CIELAB system (Section 3.1.3). lightness L∗ , hue Hab ab The OSA-UCS system (Optical Society of America Uniform Color Scales) is principally used in the USA. It consists of a total of 588 color patterns, from which 12 colors at a time are positioned in the corners and one in the center of a cubic octahedron [34]. With this system, a multitude of visual equidistant color scales can be established; visually equidistant means that adjacent color patterns always show the same visually perceived color difference independent of color point in color space. This system cannot be directly transformed into the CIELAB system; the same holds for the Munsell system, NCS system, and the DIN color chart. A reliable determination of color differences is impossible on the basis of the OSA-UCS system.
2.2
Absorbing Colorants
59
Accordingly, it is advantageous to fall back on a universal applicable colororder system, which, for chromatic as well as achromatic colors, has the implicit metric of a color space. The RAL design system is organized on such considerations. It is based on the structure of the CIELAB system. The RAL design system enables, with good approximation, the visual determination of color differences. The corresponding color collection is established as RAL design atlas [35]. There exists also a collection of 70 RAL effect colors, which cannot be classified as a definite color-order system.
2.2.5 Surface Phenomenon The color attributes assembled in the next to last section are more or less an expression of a subjective color perception. As already mentioned in Section 2.1.5, the entire color impression is certainly composed of at least two components: the light interactions in the volume and at the boundary surface of a colored sample. In other words, the reflection or transmission from the volume is superimposed on the boundary surface reflection. This reflection is caused by different refractive indices at the boundary surface. Such kinds of boundary surfaces are present in paints, coatings, plastic materials, emulsion paints, or ceramics. This distinction cannot be made for undefined surfaces such as of textiles, uncoated papers, plasters, or suede leather. The kind of surface reflection is also influenced by the structure of the surface. A given color can exhibit a surface structure between two extremes: matt: appears a rough (or structured) surface; this appearance is caused by completely (or partly) diffuse surface reflection; high-glossy: appears a very smooth reflecting surface; such a surface induces only directed reflection, which is called specular reflection, specular gloss, or simply gloss. This behavior is described by the reflection law. Both the above surface properties should generally be interpreted as color attributes. For the illumination of a (color) pattern with directional light, the transition between matt, half-matt, glossy, or high-glossy surfaces can be characterized by the resultant diffuse or directed reflection with the aid of the reflection indicatrix. This is a plane polar diagram which represents the angle-dependent intensity distribution of the light reflected from the surface. In reality, an indicatrix is in three dimensions. Four different indicatrices are shown schematically in Fig. 2.28, each caused by a different sort of surface reflection. The diffuse and directional reflection amounts are given by the shape of the envelope curve and enveloping surface of the intensity distribution.
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2 Light Sources, Types of Colorants, Observer
Fig. 2.28 Reflection indicatrices of different surfaces: (a) matt: purely diffuse reflection, (b) half-matt: dominant diffuse, minor directed reflection, (c) glossy: predominant directed and minor diffuse reflection, and (d) high glossy: exclusive specular reflection
A diffuse reflecting surface of high roughness is achieved by various treatments, for example, with the help of suited polymer matrices or ceramics or pigment crystallites standing out non-uniformly from the boundary surface. In addition, the use of embossing dies is possible with regular geometrical surface forms such as micro-spheres and micro-prisms or irregular linen and other fabric structures. Further methods are sanding, etching, or physical vapor deposition (PVD). Certainly, the realization of ideal matt surfaces is exceedingly difficult. A matt surface appears normally somewhat lighter than a high-glossy surface of the same material. This is caused by the higher reflection coefficient for diffuse light in comparison to that of directional and perpendicular incident light, cf. Equations (2.1.8) and (2.1.12). The higher diffuse reflection is nearly independent of the absorption colorant sort. In the case of directional illumination, however, the reflection is only influenced by the degree of surface roughness. The matt surface of brilliant but dark-colored samples sometimes causes a minimal color shift. This phenomenon comes from the superimposed scattering of pigments near the surface. The entire diffuse reflection at the surface of a colored layer can, therefore, be composed of three components: – immediate reflection at the boundary surface; – scattering from particles near the surface; – anisotropic or isotropic scattering from the volume. The most of color physical problems are associated with the color component originated from the volume because this shows the interesting light interactions with the contained colorants. The result of a color measurement is, of course, composed of the volume and surface components. This result must, therefore, be corrected with regard to the surface boundary effect. This is achieved through the implementation of the various theoretical concepts detailed in Sections 5.3, 5.4, and 5.5, among other things. If the boundary surface contains no colorant particles, then the reflection is given by the refractive index of the binder. The pigments can, however, be
2.2
Absorbing Colorants
61
located in or near the surface, for example, by high pigment volume concentration (PVC), blooming, or flooding. In such cases, the arithmetic mean of the refractive indices of the involved materials is to be used. Such a surface boundary can have further color features, due to the fact that the refractive index of most colorants is dispersive. This effect is named bronzing; it can be present in printing inks, lacquers, plastic materials, or textiles, and can be avoided by appropriate measures. For unambiguous coloristic assessment of matt to high-glossy samples, it is absolutely necessary to avoid the glare caused by specular reflection. Therefore, the sample containing absorption colorants is always illuminated laterally at an angle of 45◦ and viewed perpendicular to the surface; see Fig. 2.29a. The reversed arrangement is also possible, but rarely used. In commercial light booths with lamps of different illuminants (normally D65, A, FL 2, FL 11 simulators), the light sources are arranged laterally and glare-free as shown in the mentioned figure. The color sample should be surrounded directly by a middle gray and the assessment should be performed by keeping the so-called CIE reference conditions, cf. Section 3.2.2. In contrast, the visual evaluation of the surface gloss is achieved with a fixed light source and constant line of vision by tilting of the sample over a specular Light source
Observer
Specular reflection
a)
Color pattern
> 60°
b)
Fig. 2.29 Two different configurations of the three factors for color impression of absorption colors: (a) for coloristical assessment and (b) for evaluation of surface gloss
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2 Light Sources, Types of Colorants, Observer
reflection angle range; see Fig. 2.29b. A light booth should, therefore, possibly have a tiltable support with angle scaling. The quantitative determination of surface reflection is carried out separately using a gloss meter; the reflected intensity is registered at several variable angles between normal to the surface and greater than 60◦ . In the case of curved substrate surfaces, for instance, car body components, cans, bottles, or tubes, it is possible to pursue simultaneously gloss, color blending, and change of gloss in dependence of the observation angle. To achieve comparable results, the radius of curvature of the substrate and the thickness of the coating have to be the same for all color samples of a collection. In contrast, coated curved substrate surfaces are absolutely unsuited for instrumental color measurements. The evaluation of the surface reflection of colorations containing effect pigments is particularly critical. The optical properties of a metallic paint coating, for example, are essentially caused by specular reflection at the flake-shaped metal particles. The flakes are primarily arranged parallel to the substrate surface. Therefore, specular reflection dominates, but it is superimposed by diffuse reflection coming partly from the rough particle edges. For metallic pigments, the angular distribution of the reflection depends also on the illumination angle as well as the angle of observation. As already explained in Sections 2.1.6 and 2.1.7, the color physical properties of effect pigments are also extremely angle dependent. Compared to absorption colorations, the visual assessment of such colorations needs a much more sophisticated procedure, cf. Fig. 2.30. The observation for effect pigments is also normally performed using a fixed light source, but the classical method needs two identical colorations, one kept horizontal and the other rotated by an angle < 45◦ from this position; see Fig. 2.30a. This procedure allows for the observation of the angle-dependent change of lightness intensity. For flake-shaped metallic pigments, this angledependent change in reflected intensity is typical; it is the so-called lightness flop. The color changes of interference and diffraction pigments between the two extreme observation angles is, however, termed as color flop. Figure 2.30b shows the modern arrangement for visual evaluation of effect colorations. In this configuration, the light source and the observer are fixed. Vertical movement of a color sample simultaneously changes both the angle of illumination and angle of observation. Therefore, the observation of the color flop, for example, needs only one color pattern and is carried out at the same surface spot. We have arrived thematically at the transition from absorption to effect pigments. These colorants have been used industrially since about 1970 and to an increasing extent. In the following sections, we discuss the structure, morphology, and the spectral properties of the most important sorts of these modern colorants.
2.3
Effect Pigments
63
Light source Observer
a)
Effect Color pattern
b)
Fig. 2.30 Two different configurations for assessment of colorations containing effect pigments with fixed observer: (a) classical method (tilting): lightness flop and (b) modern method (vertical movement): color flop
2.3 Effect Pigments Effect pigments have broken new ground in color physics, especially with regard to industrial-scale research, development, and application. The color production of effect colorants is predominantly caused by anisotropic processes like single or multiple reflection, interference, or diffraction. These processes are unrealized in absorption colorants. The generic term “effect pigment” is inadequate because colors generated by absorbing colorants are also based on an optical “effect”. However, flake-shaped pigment or shorter flake pigment is an accurate expression for this sort of colorants. The generated color impression of effect pigments is extremely angle dependent. This is a function of both the illumination and the observation direction. Effect pigments result in quite strange color
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2 Light Sources, Types of Colorants, Observer
sensations for human color sense because our sense has evolved to perceive only colors from absorption colorations. In a practical sense, effect colorants need more extravagant manufacture methods in comparison to absorption pigments and also a more extensive characterization, measuring techniques, application, and processing. All types of effect pigments consist of flake-shaped particles with a large range of typical lateral dimensions between 1 μm and 1 mm. This is more than 10 – 1000 times larger than that of absorption pigments. The flake thickness has values between 10 nm and 1 μm. On account of the flake form, the resultant color effect is increasingly distinct with a more uniform morphology and the more the particles are oriented in the binder parallel to the substrate or surface. Like absorption pigments, effect colorants can be of inorganic as well as organic nature. With regard to the processes of color production, they are divided into four groups (cf. Table 1.1). For historical reasons, they are named: – metallic pigment; – pearlescent pigment; – interference pigment; – diffraction pigment. In the literature, pearl luster pigments are often subsumed to the interference pigment classification [36]. The laws used to describe the optical properties of metallic pigments are essentially geometrical optics; all other sorts of effect pigments are generally described by wave optics. Metallic pigments consist normally of a metal or an alloy of metals. The typical metallic gloss is increasingly brilliant the more uniformly the flakes are oriented parallel to the boundary surfaces of a coating. The so-called metallic effect is mainly a consequence of the directional and diffuse reflection at the surface and the edges of the flakes. In contrast, pearlescent pigments consist of two or more layers with a high index of refraction difference; the values normally range from 1.5 to 2.9. The mostly used substrate is mica, but also metals or metal oxides are often applied. The specific pearl luster depends on the permutation of the layers. This luster originates from single or multiple reflections at the layer boundaries followed by interference of the light waves. Differing optical layers are behind the general function of interference pigments; this does not require the use of a mica substrate. An interference pigment subgroup is the so-called optically variable interference pigments. The high ratio of refractive indices, in conjunction with different layer thicknesses, fans out the first or more interference orders in such a way that a variety of interference colors are to observe angle dependence.
2.3
Effect Pigments
65
The grating structure of diffraction pigments deflects the incoming light. The resulting color effect can be attributed also to the wave nature of light. The substrate consists of a highly reflecting or even ferromagnetic substance. The substrate is vapor-coated symmetrically on both sides with several materials known from nanotechnology. The ferromagnetic particles can be oriented with an external magnetic field before the crosslinking of a binder. The produced unusual but often impressive colors require that effect pigments undergo a more subtle and closer examination and handling compared with absorption colorants.
2.3.1 Types of Metallic Pigments Metallic pigments, generally consisting of metal flakes, are employed mainly on account of the metallic reflection from the flake-shaped particles. This kind of reflection consists of superimposed specular and diffuse components which produce unusual color effects compared with absorbing pigments. Conventional metal flakes have mean lateral dimensions ranging from about 5 μm to nearly 50 μm, whereas the thickness varies between roughly 100 nm and 1 μm. In some extreme cases, the particles have dimensions which are up to 10 times higher. The ratio of thickness to diameter of the particle is called the form factor and it extends from 1:50 to about 1:500. Metal flakes are used in paints, lacquers, plastic materials, and inks; they are also employed in chemical products and for sinter metals, building materials, explosives, or pyrotechnics, for instance, as functional or chemically reactive particles. In this text, we are mainly interested in the metallic reflection. This property is caused, in simplified physical terms, by the fact that individual metal atoms can easily release the bonding electrons. In lattice arrangements, the metal atoms completely loose the valency electrons. These electrons form the electron gas which is distributed among the remaining ions so that each ion is fixed on a corresponding lattice position. On account of its interaction with the electrons, an external light wave from a normal source cannot penetrate the very dense electron gas. The majority of the light is rather reflected and the remaining part is absorbed within a very small penetration depth. Reflection and absorption produce the typical metallic brilliance and characteristic natural color of metals [14]. The change in electron gas density at the metal surface results in light dispersion in the visible range, among other things. This causes a light-, gray-, or low-colored metallic effect. The theoretical reflectivity of metals is given by Equation (2.1.10). In Table 2.7, the indices of refraction n, absorption nκ, reflection r(n,κ), and the melting temperature Tm are shown; these are for metals that are most commonly used for metal pigments. In this listing, the metals are arranged according to decreasing reflectivity. The given optical
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2 Light Sources, Types of Colorants, Observer
Table 2.7 Reflectivity, refractive index, absorption index for perpendicular incident light at wavelength of λ = 589.3 nm and T = 293 K as well as melting point of metals used for metallic pigments [37]
Metal
Reflectivity r (n, κ)
Refractive index (n)
Absorption index (nκ)
Melting point Tm /K
Ag Al Au Cu Zn Ni Fe Mo Ti W
0.99 0.912 0.888 0.804 0.768 0.664 0.586 0.575 0.565 0.524
0.052 1.181 0.280 0.493 2.74 1.71 2.91 3.40 2.09 2.83
3.91 6.99 2.91 2.80 5.77 3.61 3.58 3.56 3.11 3.02
1,235 933 1,336 1,356 693 1,726 1,809 2,890 1,933 3,683
quantities are for the middle of the visible Na wavelength of λ = 589.3 nm; they will generally have different values for other wavelengths. The melting temperatures of the given metals are higher than those of the highest flow temperature of normal polymer melts. The refractive index is also subject to dispersion; in cases of Ag, Au, and Cu it is valued n < 1. The phase velocity cp is, on account of cp = c/n, inside these three metals higher than the velocity of light c in vacuum; this is not in contradiction to the special theory of relativity because only the group velocity – with which energy or signals propagate – cannot exceed the velocity of light c. Clearly, the actual reflectivity is lower than the theoretical one. The real reflectivity depends on the details of morphology of the particles, especially the – surface grade and edge roughness; – particle size and particle size distribution; – flake thickness; – pigment orientation in the material of application. In the context of metallic pigments, it is useful to emphasize the fact that historical laxness in naming remains an issue. Terms such as aluminum bronze or silver bronze instead of aluminum pigments, gold bronze or even the more general metal bronzes, are still in widespread use today by pigment manufacturers, colorists, and even in modern literature [38–40]. Actually, aluminum bronze consists of copper alloyed at most 12% aluminum; silver bronze is an alloy of silver and tin; gold bronze is a solid blend of suitable amounts of copper and zinc; genuine bronze, however, consists of copper alloyed with tin.
2.3
Effect Pigments
67
Apart from dispersion and particle size, the character of the metallic color impression is influenced by further details. Among them are the chosen metal or alloy, the manufacturing and processing method of the flakes, and the wettability in binders. In the following, we give a survey of the influence of these parameters with regard to the visual perceived metallic effect. First of all, the chosen metal is responsible for the brilliance of the natural metallic pigment. The metallic colors change from light white (Ag, Ni), white (Al – as a substitute for Ag), bluish white (Zn), orange-yellow (Au), and reddish (Cu) to gray (Fe, Mo, Ti, W). These color attributes relate only to the metal gloss and, therefore, have a different meaning from that which was outlined for absorption pigments in Section 2.2.2. Additional natural metallic colors can be realized using mixtures of metallic pigments: Ni flakes lighten and Fe particles gray the metallic effect. Also alloys such as brass (alloy of Cu and Zn) are suited for gold-yellowish to reddish color, for example. Metallic pigments are manufactured with mixtures or alloys only if the required metallic effect is not achievable using only conventional metal flakes. The most commonly used metallic pigments from modern point of view are given in Table 2.8. Uncoated metal flakes based on natural metals have the most diversity. Particles with especially even surfaces can be manufactured using the PVD method. For this, a polymer foil is vapor coated in vacuum with a metal and afterward crushed at temperatures far below the glass transition temperature of the polymeric material. These flakes are termed as crushed PVD films. Due to modern developments, even colored metallic flakes can be manufactured. In these cases, a colored component is superimposed on the Table 2.8 Classification of metallic pigments Metallic pigment
Typical examples
Uncoated metal flakes
Aluminum (“aluminum bronze”, “silver bronze”), copper, zinc, copper/zinc alloys (70/30, 85/15, 90/10: “gold bronzes”), copper/aluminum alloys (4–12% Al: aluminum bronze), iron (austenitic steel, max. 11% Cr), nickel, tin, silver, gold, titanium
Crushed PVD films
Foils of polyethylene terephthalate, polystyrene, or polypropylene: vapor coated with aluminum, chrome, magnesium, copper, silver, gold (PVD procedure)
Flakes coated with absorption pigments
Inorganic or organic pigments in silicon dioxide or acrylate coating fixed on aluminum or “gold bronze” flakes as substrate (CVD procedure)
Partially oxidized and oxide-coated metal flakes
Partially oxidized from the surface aluminum flakes, copper flakes, zinc/copper flakes (“fire colors”); coated aluminum flakes: iron-III-oxide, tin oxide, zirconium oxide, iron titanate, cobalt titanate
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2 Light Sources, Types of Colorants, Observer
metallic effect. There are two different methods for manufacturing. In the first, absorption pigments are suitably fixed at the surface of the flakes by chemical vapor deposition (CVD) [38, 39]. The second method is based on metal flakes which are partly oxidized from the surface, or coated with metal oxides. Such metal flakes produce an intense color effect, sometimes called “fire colors.” These intense colors are caused by multiple reflections at the transparent outer layers with varying refractive indices; the multiple reflected waves then interfere. Technically, such colorants are not metallic pigments in the strict sense, rather just a multi-layered interference pigment on top of a metal substrate. In most cases, the original metallic brilliance of the metal substrate is lost. It must be noted that the chosen manufacturing method is of great influence to the resultant coloristical properties of metallic pigments. For shaping of natural particles, the melt is pressed through a narrow nozzle of suitable geometry with high pressure. Due to high flow velocities in the nozzle channel, often up to 400 m/s, the velocity gradient leads to an atomizing of the melt into round and contracting tiny droplets outside of the nozzle tip. After cooling, they are transformed into flake-shaped particles; these are the resulting metal flakes. The grinding of the solid particles is performed by two different processes. The wet milling method of Hall uses white mineral thinner for liquid phase. This simultaneously has the benefit of preventing dust explosions. In order to prevent clumping or welding of the particles, long-chained fatty acids are often added, typically 3–6% oleic or stearic acid. The dry milling method of Hametag, however, works in a N2 atmosphere containing at most 5% O2 . For this method, 4–6% palmitinic acid or stearic acid is often used as separators. The mentioned long-chained fatty acids, on the other hand, coat the entire surface of the resulting flakes; this certainly changes their wettability especially against binding materials. Because the end groups of the fatty acids are dependent of surface tension and behave either hydrophilic or hydrophobic, the metal flakes flood or disperse uniformly in the binding agent. Figure 2.31 gives an
Metal flakes
Coating
Substrate a) Leafing
b) Non–leafing
Fig. 2.31 Two different distributions of metallic particles in a painted layer: (a) leafing near the surface and (b) non-leafing or nearly uniform distribution
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illustration of two flake arrangements in a binder, the first is called leafing and the second non-leafing. The tendency to form the leafing arrangement is stronger with the lowering of the wetting with the surrounding polymer. Leafing flakes result from coating with stearic or palmitinic acid; non-leafing particles are usually obtained with oleic acid, for example. It is worth mentioning that the sort of wetting is generally correctable afterward with suitable additives. If the flakes are dispersed in the melt state of plastic materials, the leafing is generally avoided due to the high structural viscosity of the melt.11 A measurement method for determining the leafing behavior is detailed in the literature [41]. Leafing pigments incorporated in transparent binding agents show high brilliance due to a uniform and constant reflection. The abrasion resistance of the surface film is often reduced and, therefore, an additional top coat is usually applied. In contrast, the parallel and compact flake arrangement often behaves like an optical or mechanical barrier: in addition to visible wavelengths, it reflects UV and IR radiation and can also inhibit the diffusion of gases or vapors. Leafing flakes are, therefore, often used for reflection of UV and IR radiation as well as corrosion prevention pigments. Further non-colored applications of metallic pigments are given in Appendix 7.1.1.
2.3.2 Morphology of Metallic Particles As already mentioned, the metallic character is especially influenced by the morphology of the flakes. The wet milling procedure of Hall predominantly produces particles of irregular and uneven surfaces along with high edge errors – they are, therefore, quite accurately called cornflakes. Typical aluminum cornflakes are shown in Fig. 2.32. The picture was taken with a scanning electron microscope (SEM). The irregular particle edges result from fracture from other flakes during the milling process within the ball mill. The uneven surfaces are caused by abrasion of the coarse edges of colliding and pressed particles. At the particle surfaces shown in Fig. 2.32, it is possible to discern some remains of broken edge zones and indentation traces of striking balls. Both the uneven surface structure and the rugged particle edges are responsible for the typically increased diffuse light scattering of cornflakes. The light reflected from such flakes is composed of a directional and a superimposed scattering component. The accompanying indicatrix corresponds to that of Fig. 2.28c. The amount of diffuse reflected light is increased, therefore, with more uneven particle surfaces and rugged flake edges. With increasing particle scattering, there is a reduction of brilliance, that is, “it turns gray.”
11 Structural viscosity means that the viscosity has a nonlinear dependence on shear velocity;
this is in contrast to constant Newtonian viscosity.
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Fig. 2.32 SEM picture of typical cornflake particles of aluminum (source: Eckart Werke GmbH, Velden, Germany)
Sophisticated grinding techniques with metal brushings or polishing pastes have been used since about 1980 to reduce this brilliance loss. These techniques allow for the manufacture of thicker metal flakes with relatively plane surfaces as well as even or rounded edges. Particles of this kind are often called silver dollars, of which an example is shown in Fig. 2.33. These sorts of flakes reflect light with a dominant directional component accompanied by a considerably lower scattering. A paint film with silver dollars and clear top coat is, therefore, lighter and more brilliant than the one with cornflakes of the same metal and identical particle size distribution. Silver dollar pigments are preferentially employed in high-quality systems such as automotive coatings, the so-called metallics. They are also used in high polymer materials and printing inks. Shear stable flakes of upward 10 times the particle thickness of cornflakes can be realized in order to withstand processing techniques of high pressure or high shearing stress (e.g., ring main pumps, injection molding, blow molding, or extrusion). Particles with nearly plane surfaces and high brilliance can also be manufactured by PVD coating of thin polymer foils. They do, however, exhibit an undefined breaking edge. A representative example is shown in Fig. 2.34. In addition, it is possible to produce metallic pigments of constant thickness and of geometric regular shapes. These sorts of particles are called glitter flakes. To describe the glitter effect, the terms sparkle and glittering are also used. Both expressions are often utilized simultaneously, although they have somewhat different meanings.
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Fig. 2.33 SEM picture of silver dollar pigments of aluminum (source: Eckart Werke GmbH, Velden, Germany)
Fig. 2.34 Metallic pigments of PVD metal coated and broken polymer films (source: Eckart Werke GmbH, Velden, Germany)
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Sparkle is the property that single flake particles are directly recognized visually due to their expanded planar reflection surfaces. This is typically the case for mean particle sizes of about 30 μm and larger. The metal flakes are perceived separately on account of the surface reflection contrasting to the darker surroundings. They behave as isolated microscopic mirrors. In contrast to glittering, see below, neither the morphology nor the lateral dimensions of sparkle particles are necessarily uniform. The phenomenon of sparkle (also referred to as sparkling, optical roughness, micro-brightness, glint, or diamonds) is present in quite an assortment of effect pigments and is particularly observable with directional light; see also Section 3.5.1. In contrast, glittering is exclusively due to particles of uniform and regular geometry. These particles are manufactured in the form of squares, rectangles, rhombs, or circles by cutting or punching-out from metal foils or metallized polymer foils. In Fig. 2.35 an example of nearly quadratic aluminum glitter flakes cut from ribbons with a band knife is shown. Glitter flakes are of nearly uniform lateral dimension compared with conventional manufactured metallic pigments in ball mills. They are produced with sizes of 50 μm up to as much as 2 mm. They are generally at least 10 times thicker than usual cornflake or silver dollar particles. With regard to quadratic and rectangular glitter flakes, often specifications such as “2 × 2” or “2 × 4” are used. These can be interpreted as follows:
Fig. 2.35 Almost quadratic glitter flakes cut with a band knife from foil strips of aluminum [38] (source: Rapra Technology Ltd, Shawbury, UK)
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multiplication of each of these numbers with one thousandth inch (2.54 × 10–3 cm) gives the middle lateral extension of the corresponding particles. This means, for the given examples, that the glitter flakes have dimensions of 50 × 50 μm and 50 × 100 μm, respectively. It is also worth noting that with extreme process control in the Hall technique, it is also possible to produce spherical pigment particles with diameters as large as 700 μm. Such particles have, however, not the appearance of glitter flakes [38]. Colored metallic pigments offer an exceptional optical enlargement of usual metal pigments. These consist either of metal flakes covered by absorption pigments or metal flakes partially oxidized from the surface or oxide-coated metal particles. In the first case, the metal particles are coated with silicon dioxide or a polyacrylate containing inorganic or organic absorption pigments. In Fig. 2.36, there is an SEM photograph of aluminum flakes with a silicon dioxide coating of embedded inorganic pigment particles. This picture shows not only the coarse surface structure of the flakes but also the size proportion of the absorption pigments having only a few nanometers to the around two orders of magnitude larger sized metal flakes. From this difference in size, the typically higher scattering power of absorption pigments compared to effect pigments is also understandable. Colored metal effect pigments consist also of partially oxidized or oxidecoated flakes, which are manufactured using the CVD procedure. Partially
Fig. 2.36 Aluminum flakes coated with silicon dioxide and embedded inorganic pigment particles (source: Eckart Werke GmbH, Velden, Germany)
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20
100
10
50
Cumulative frequency curve
Relative frequency %
oxidized flakes of aluminum, copper, or zinc/copper are generally preferred. Iron-III-oxide-coated aluminum flakes are also common. All of these pigments produce particularly impressive reddish colors – and are, therefore, also called fire colors. These unusually striking colors are due to the combination of three effects: first, absorption and scattering of copper, zinc, or iron-III-oxide; second, interference caused by the layer construction; third, metallic reflection of the particles. Already the concept of the glitter flakes suggests that the character of the metallic effect is particularly dependent on the particle size. All particles, however, are not of the same size; therefore, the metallic effect is in general influenced by the particle size distribution. On the other hand, the size distribution can be controlled partly by the milling and sieving process; from these manufacturing steps, an asymmetrical particle size distribution with respect to the mean results. This distribution has a higher amount of smaller particles, cf. Figs. 2.37 and 2.38. The mean, in this context, is usually denoted by the quantity d50 or D[v; 0.5]. This quantity, for example, d50 = 25 μm, indicates that 50% volume of all particles are higher or lower in size than this near center value. The subtle properties of the metallic character even depend on the width of the distribution. In addition to the use of scanning electron microscopy, the laser granulometry method has proven quite useful for the determination of the mean particle size of effect pigments and the accompanying size distribution. The laser method is founded on scattering and diffraction of the particles suspended in a suitable liquid. This so-called laser granulometrical operation is suited only as a relative method, this is, not as an absolute method.
d50 0 10–1
0 100
101
102
d /μm
Fig. 2.37 Curves of particle size distribution and of cumulated frequency of an aluminum cornflake pigment with same value of d50 ≈ 20 μm as in Fig. 2.38
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20
100
10
50
Cumulative frequency curve
Relative frequency %
The size distribution of effect pigments is characterized by the so-called width W, which is given by the quotient W = (d90 − d10 )/d50 > 1. The quantities d10 and d90 mean that 10 and 90% volume, respectively, of the particles have lateral dimensions of Φ ≤ d10 and Φ ≤ d90 . A narrow distribution with low W produces a more brilliant metallic effect in comparison to a broader distribution of equal d50 value; see Figs. 2.37 and 2.38. The concentration of small particles is lower in a narrow distribution than in a broad distribution. However, the greater the number of small-sized particles present, the more gray and paler the metallic effect appears. Of course, with smaller flakes edge scattering preponderates, and in addition, the parallel configuration of the flakes is more distorted than with larger sized particles. The metallic reflection of typically narrowly distributed silver dollar pigments is consequently more distinct than that of traditional cornflakes. Cornflakes show a significantly broader particle size distribution. Among modern metallic pigments, silver dollar flakes of aluminum are the most light and most brilliant particles. According to Figs. 2.37 and 2.38, there is always an elevated number of particles smaller than 5 μm.12 This increased content of fine particles is unavoidably caused by the grinding process and is quite typical for the manufactured metal powders. The fine particles give rise to a scattering component which reduces the metallic brilliance. Finally, the production of the metallic effect is also influenced by the orientation of the particles in the polymeric surrounding medium. The particle
d50 0 10–1
100
101
102
0 d /μm
Fig. 2.38 Curves of particle size distribution and of cumulated frequency of an aluminum silver dollar pigment with same value of d50 as in Figs. 2.37
12 Particles
smaller than 5 μm contribute to particulate (dusty) matter.
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alignment is primarily determined by the processing techniques used. The maximum possible metallic reflection is achieved by complete flake parallelism to the bounding faces of a plane parallel layer; this is equivalent to a mirror. Local perturbations of particle alignment parallel to the paint coating can be caused by turbulent motion of the solvent during evaporation; such kinds of heterogeneity lead to mottling or flocculation. Both kinds of visible non-uniformities are also known from coatings with absorption pigments. Lacquers with low solid-state content display a more distinctive metallic effect than systems with higher solidstate content (so-called high solids). This is because the lower viscosity makes the orientation of the flakes easier. During processing of metallic or other flake-shaped pigments in printing inks, the absorbability of the stock can influence the parallel orientation of the flakes. But the slower the diffusion rate of the solvent, the more time available for parallel alignment of the particles. In high polymer materials, the flake pigments orient themselves according to the prevailing flow conditions. The alignment of the particles direct after surface formation is nearly maintained during cooling time and concurrent volume contraction. The collision of two melt fronts causes a flow line, at which the particles orient – visibly – parallel to the flow fronts. Flow lines can be avoided generally with suitable manipulation of the fusion in the mold [38].
2.3.3 Coloristic Properties of Metallic Pigments The geometry, morphology, and reflection of metallic pigments produce a variety of unusual color effects which need to be described in detail. The most important coloristic characteristics of metallic pigments are given in Table 2.9. From this apparent arbitrary division it is possible to discern two groups: in the first group, the indicated effect properties increase with expanding lateral dimension of the particles and for the second group, they decrease. This inverse behavior and the complex color attributes of metallic pigments demand a closer examination in comparison to the more simple properties of absorption pigments. First, the five special features of the first group will be discussed. The metallic character or metallic gloss depends on the ratio of the directional to the diffuse reflection. Both components are directly proportional to the quotient of the surface to the edge length of the metallic flakes. The higher this ratio, the more distinctly developed the metallic character. Small particles normally give rise to a higher edge scattering and, therefore, produce a poor and gray metallic effect. Conversely, flakes with a lateral dimension greater than 30 μm show a striking metallic character. In general, the narrower the particle size distribution, the more distinct the metallic luster.
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Table 2.9 Correlation between particle size and coloristical properties of metallic pigments (other used terms in brackets) Assessment of characteristic particle diameter d50 , non-leafing pigments Characteristic of metallic pigment
≤10 μm: fine pigments Cornflakes
≥30 μm: coarse pigments Silver dollars, glitter flakes
Metallic character (metallic gloss) Brightness (brilliance) Reflection brightness (whiteness) Sparkle, glittering (optical roughness) Graininess (coarseness, texture)
Insignificant, matt, gray
Quite distinct, brightened
Low Minor
High Enhanced
Invisible
Visually noticeable
Low
Visible
Lightness flop (flop, flip, travel, two-tone) Hue extinction Covering capacity (hiding power, opacity) Distinctiveness of image (DOI)
Light
Dark
Enhanced Enhanced
Low Low
High
Minor
The brilliance of metallic pigments is, in essence, caused by the directional reflection component. Metallic flakes, therefore, appear all the more brilliant the higher the directional reflected light amount and the lower the diffuse reflection component. The brilliance, and consequently the directional reflected component, is reduced with smaller and more uneven surfaces of the pigments, with broader particle size distributions and with greater irregularities in particle orientation in the surrounding polymer material. The reflection brightness or whiteness characterizes the lightness of the metallic effect. This property is a measure of the total reflected light and is composed of the directional and diffuse components. Consequently, reflection brightness differs from lightness of absorption pigments, which is due to scattering and absorption. In connection with effect pigments, the term reflection brightness has, therefore, a quite different meaning from the lightness of absorption colorants (although both quantities are determined with the same measuring and evaluation system). In fact, the spectral reflection of metallic pigments behaves similar to that of white/black mixtures of absorption pigments. Metallic pigments certainly show a key difference: the spectral reflection depends on the angle of illumination and direction of observation. This angle dependence is shown clearly, for example, by the reflectance of an aluminum cornflake pigment in Fig. 2.39. In this illustration, the reflectance
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R (%) 150
100 15 25 50
45 75 110
0 400
500
600
λ /nm
μas /degree
Fig. 2.39 Spectral reflectance of a cornflake aluminum pigment in dependence of the wavelength λ measured at aspecular angles of μas = 15º, 25◦ , 45◦ , 75◦ , 110◦ ; illumination angle β = 45◦
R is plotted in dependence of wavelength λ for five standardized aspecular measuring angles μas and an illumination angle of β = 45◦ .13 With increasing measuring angle, the reflectance behaves similar to that of light white and middle or dark gray, cf. Figs. 2.24 and 2.26. For angles steeper than μas ≈ 75◦ , the reflectance remains at a low level, the metallic effect appears dark gray [42, 43]. On the other hand, the reflectance increases exponentially for the aspecular angle of μas = 0◦ . This drastic change in brightness in dependence on the observation angle is characteristic for metallic flakes; it is termed as lightness flop or short flop (see below). The reflectance increase near the specular angle can be further raised, within limits, with a narrower particle size distribution or altogether larger sized flakes. Measured reflectance values higher than 100% are absolutely usual and produce no inconsistency with conservation of energy. Because of the lack of suited and corrosion-resistant metallic standards, the reflectance scale is based on the reflectance of a white (scattering) standard which is interpreted as a reflectance of 100% (Sections 2.2.3 and 4.1.2). Real effect pigments can have reflectance values up to about R = 800%.
13 For
nomenclature and counting of angles, see Section 4.1.2, Figs. 4.5 and 4.6.
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Metallic pigments of irregular lateral dimension greater than about 30 μm produce a phenomenon termed as sparkle in the last section. This effect is also called sparkling or optical roughness. For particle dimensions of this size or larger, the naked eye can distinguish single flakes of nearly equal orientation at the surface of a coating or plastic material. This is caused by the increased intensity of directionally reflected light at the larger particle surfaces (similar to parallelized crystals of an illuminated snow surface). As a consequence of the distorted orientation of the flakes, sparkling changes in dependence on both the illumination and observation angle. Leafing flakes develop no sparkling in dependence of the particle size because nearly all flakes have an alignment parallel to the surface of the coating or the plastic material. Sparkle is not restricted to metallic pigments and can be present in other sorts of flake-shaped pigments. This striking feature depends, e.g., on the size, the sort, the surface curvature, and the content of the effect pigment in a coloration. If the illumination is switched from directional to diffuse, the sparkling disappears completely and turns into a kind of graininess of the particles. Under this lighting condition, only a kind of fixed snowing picture is observable near the surface of the coating. This phenomenon is also called coarseness, texture, or vivid “salt and pepper” and is independent of observation angle. The impression of graininess depends on the size and type of the flakes, orientation irregularities, or clustering of the pigments during processing. Now, consider the second group of properties listed in Table 2.9. The abovementioned lightness flop (also light to dark flop, flop, flip, travel, two-tone) can be regarded as the most important and visually most striking property of metallic pigments. This term characterizes the decrease in lightness that a metallic coloration shows under diffuse illumination between two extreme angles of observation, especially at angles for perpendicular observation and an angle greater than 60◦ with regard to the normal of the surface (cf. Fig. 2.30a).14 The lightness flop is influenced by three primary factors: first, the flakeshaped pigment morphology, second, the surface and edge formation, and third, how well the flakes are ordered parallel to the surface boundaries of a layer. During observation perpendicular to the surface, the light enters directly the eye after interactions with the flakes. The observer registers the reference lightness. Now, for angles nearly parallel to the surface, the light path through the layer is longer. For this reason more interactions can take place with the particles of the layer, that is, at the surface or edges of the flakes. Due to this, light is increasingly scattered or reflected out of the line of observation and, therefore, only a small amount of the interacting light reaches the eye. This results in a registering of a reduction of lightness in comparison to the perpendicular observation.
14 Perpendicular observation means, in practice, that observation angles of β = ±20◦ , ν referred to the vertical, are permitted.
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This flop is termed as light if only a small lightness difference is observed between both extreme observation angles. It is, however, called dark if a large lightness difference is registered. For finer and irregularly shaped flakes (e.g., cornflakes), for broader accompanying particle size distribution, and for greater particle disorder in the layer, the flop is lighter. Conversely, the flop is the more dark, for greater evenness of the particle surfaces, for more rounded flake edges (silver dollar flakes), for narrower size distributions, and for more consistent parallel orientation of the particles to the surface boundary of the layer. The lightness flop can be altered afterward to some degree by adding inorganic or organic absorption pigments (see Table 2.10). Table 2.10 Lightness and color flop of effect colorations
Flop kind
Flop character
Effect pigment/ absorption pigment
Lightness flop
Light
Metallic pigment
Metallic pigment and absorption pigment Dark
Metallic pigment
Metallic pigment and absorption pigment Color flop
Colored
Absorption pigment
Absorption and pearlescent pigment Interference pigment
Diffraction pigment
Typical examples Fine non-leafing cornflakes, eventually with orientation distortion medium Scattering, inorganic, and organic; for example, titanium dioxide, chromium titanate Coarse non-leafing silver dollar flakes, normal silver dollar flakes, PVD flakes Transparent, inorganic, and organic Blue with green flop: phthalocyanine pigments of neutral color flop; blue with red flop: α/-phthalocyanine pigments Combination of hiding absorption and transparent pearlescent pigments, nano-titanium dioxide Interference pigments with extreme color flop: LCP, flakes coated with silicon dioxide, aluminum oxide, iron-III-oxide, magnesium fluoride Aluminum or nickel substrate PVD coated with chromium/magnesium fluoride or magnesium fluoride/silicon dioxide
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The phenomenon of lightness flop can be examined quantitatively by a gloss meter. The usual measuring angles μν = 20◦ , 60◦ , 85◦ with regard to the normal of the surface are certainly not sufficient. This is already clear from the angle-dependent reflectance measurements in Fig. 2.39. A reliable characteristic value describing the lightness flop of a single-layered metallic formulation is the so-called flop index; however, for clear-over-base paints, the so-called metallic value is used (Section 3.5.1). As mentioned, some metallic systems are mixed with absorption pigments for coloring or covering of the background. These systems have a more or less colored flop; see Table 2.10. Mixtures with absorption pigments always result in a lighter flop compared to the natural metallic pigment. This effect is generally called color flop. Mixtures of pearlescent and metallic pigments normally produce a lighter flop than the corresponding single natural pigments. However, the brilliance is usually raised at perpendicular observation. This behavior can be reversed with suitable pigment combinations. The color flop of interference and diffraction pigments is generally accompanied by a distinct color change. This change is mainly due to the interference or diffraction maximum of first order (Sections 3.5.3 and 3.5.5). A particular kind of color flop is given by a mixture of a metallic flakes with titanium dioxide, provided that nanoparticles of the rutil modification are used. The observable minor color shift caused by the nanoparticles is generated by the selective scattering of waves in the region of blue wavelengths; this special phenomenon is called frost effect [44]. Such a layer has a yellowish color at top view but for a flat angle of observation, a bluish color impression results. Accordingly, the shorter blue wavelengths are more scattered than the other longer wavelengths, in agreement with Rayleigh’s law (2.1.3). This comparatively low effect is also observed with other absorption or pearlescent pigments of lateral dimensions in the nanometer range. Altogether, the color flop of a formulation can be controlled within limits by adding small amounts of nanoparticles. Certainly, the frost effect lowers the entire brightness of the relevant coloration. The next property of interest in Table 2.9 is the hue extinction. This feature characterizes the capability of a metallic pigment to change or to cover completely the natural color of an absorption pigment incorporated into a formulation. In the literature [39], this ability is called “hue saturation,” which is again misleading, because this term implies a saturation of the relevant absorption colorant. The extent of the hue extinction is related to the covering capacity of the metallic particles. In this case, for metallic particles this term has the same meaning as it does for absorption pigments (Section 3.4.3). Both the hue extinction and the hiding power are improved with smaller cross sections of the particles, broader particle size distributions, larger flake thicknesses, and denser packing of the flakes.
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Finally, there is the so-called distinctiveness of image (DOI). In addition to lightness flop and hue extinction, this property lists among the central characteristics of single as well as clear-over-base paints of metallic coatings. The DOI value represents the uniformity of the observable metallic reflection. It depends mainly on the particle size and orientation of the flakes in a layer. The distinctiveness of image is again improved by smaller particles and more highly parallelized grade of the flakes. The DOI value of large-sized flakes nearly correlates with the glittering effect. The determination of the DOI value by measurements is outlined in Section 3.5.1.
2.3.4 Sorts of Pearlescent and Interference Colorants The color production of pearlescent and interference pigments is essentially based on constructive interference. Pearlescent pigments imitate the nacre luster of natural pearls. The brilliant colors and unique luster are due to superimposed light interactions such as absorption and multiple reflection at different boundary surfaces of the particles. Interference pigments generate substantially more brilliant colors than pearl luster pigments. The terms pearlescent and interference pigments are often wrongly used as synonyms for both pigment sorts, although only pearlescent pigments have the typical luster of natural pearls coming from the depths to the surface. The particles of pearl luster and interference pigments consist of layers with different refractive indices. The layer thicknesses are on the order of magnitude of visible wavelengths. The entire flake thickness varies from about 30 nm to 1 μm and the mean lateral dimension of the transparent to opaque pigments extends – similar to metallic flakes – from about 5 to 300 μm. Pearlescent, interference, and diffraction pigments can also exhibit sparkling. This sizedependent phenomenon is, in this case, generally darker than the sparkle of metallic pigments because the reflection is caused only by the difference of refractive indices instead of metallic reflection. The color-producing properties of pearlescent, interference, or diffraction pigments are dependent on the particle geometry, especially on the interfering light interactions, and the color physical conditions in the particle surrounding. According to Equations (2.1.15), (2.1.16), (2.1.17), (2.1.18), (2.1.19), and (2.1.20), the interference laws are functions of the wavelength λ, the refractive index n at the interface, the thickness d of each single layer, and the observation or interference angle α z . These parameters can be tuned in such a way that only the first interference order (z = 1) occurs in the range of normal observation angles. In this case, the higher orders can be neglected or are simply not to observe. The incoming light waves are partly reflected at each boundary surface of a particle, cf. Fig. 2.16. The constructive interference of the waves
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produces the matt to high brilliant color appearance. The interference color is observed at the specular angle on the illumination surface and the complementary color is transmitted by transparent flakes. Each single pigment, therefore, behaves as an interference filter, which the incoming light waves split up into a reflected interference component and a complementary transmitted or absorbed component. As a result of the different refractive indices at the interfaces as well as the morphology of the particles, the following light interactions together contribute to the color appearance of pearl luster and interference pigments: – constructive interference produces the sometimes intense colors which change in dependence of the angle of observation; the different colors and the angle dependence are given by the refractive indices, the thicknesses, and the number of layers; – single reflection at interfaces causes part of the glossiness; – multiple reflection at the different interfaces of the transparent or translucent layers causes the typical luster “from the depths” of pearlescent pigments; – scattering at the edges or rough surfaces of the particles leads to matt interference colors; – absorption reduces the brilliance; it depends on the layer material. Table 2.11 shows the customary substances from which pearlescent and interference pigments are composed. The materials are ordered according to increasing values of refractive index nD . In comparison, air at a pressure of 1.0 bar at room temperature T = 298 K has a refractive index of only n = 1.000272. The pigment particles consist of at least three different Table 2.11 Refractive index n of substances used for pearlescent and interference pigments; λ = 589.3 nm, T = 298 K [40, 45, 46] Substance
Special terms
Refractive index n
Synthetic high polymers MgF2 Proteins SiO2 Alumina silicate CaCO3 Al2 O3 Guanine, hypoxanthine Pb(OH)2 2PbCO3 BiOCl Fe3 O4 TiO2 α-Fe2 O3
Organic materials Magnesium fluoride Proteins Inorganic glasses Mica, muscovite Aragonite Aluminum oxide Natural pearl essence Basic lead carbonate Bismuth-oxide chloride Magnetite Anastas/rutil Hematite
1.35–1.70 1.384 1.40 1.458 1.50 1.68 1.768 1.85 2.00 2.15 2.42 2.5/2.7 2.88
·
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materials. Because the relevant substances are anisotropic crystalline, the indicated n values represent a mean. The refractive indices of the substances given in Table 2.11 are subject to dispersion. Table 2.12 is arranged by pigment classes: pearl luster, interference, and diffraction pigments. In other literature, these are often gathered arbitrarily under the collective name: special effect pigments [18, 40]. Our further discussion relates to the pigment classification and terms given in Table 2.12. This fixes a unified nomenclature for all sorts of pearlescent, interference, and diffraction pigments. Pearlescent pigments of the simplest structure are substrate free and form flake-shaped single crystals. The flakes consist of natural fish scales (75–95% Table 2.12 Effect pigments producing colors founded on wave properties of the light: pearlescent, interference, and diffraction pigments Sort of effect pigment
Unsystematic names
Pearlescent pigment
Platelet-like single crystals
Mica-based pearlescent pigments Interference pigment
Special interference pigments
Liquid crystal pigments (LCP) Optical variable interference pigments (OVIP)
Extended interference films Diffraction pigment
Grating pigments
Typical examples Natural pearl essence, basic lead carbonate, bismuth-oxide chloride, α-iron-III-oxide, titanium dioxide, mixed-phase pigments of aluminum oxide, manganese-iron-III-oxide Substrates: natural or synthetic muscovite layers: titanium dioxide (rutil or anastas), iron-III-oxide, chromium-III-oxide, silicon dioxide (multi-layer principle) Substrates: aluminum oxide, silicon dioxide, iron-III-oxide chromium, silicon–aluminum–boron silicate; Layers of iron-II-oxide-hydroxide, iron-III-oxide, chromium-III-oxide, titanium dioxide, chromium phosphate; chromium, iron-II-/iron-III-oxide, iron titanate, silver, gold, molybdenum Polysiloxanes in cholesteric phase, cross-linked in layers Substrates: aluminum, aluminum oxide, iron-III-oxide, silicon dioxide, glass flakes; Layers: aluminum, chromium, iron-III-oxide, magnesium fluoride, silicon dioxide, titanium dioxide Multi-layer film consisting of polyacrylates, polypropylene with polyethylene terephthalate, polystyrene, or polycarbonate Al substrate with symmetrical PVD layers of MgF2 or Cr/MgF2 Ferromagnetic: Ni substrate with symmetrical PVD layers of MgF2 /Al or Cr/MgF2 /Al
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guanine, 5–25% hypoxanthine), basic lead carbonate, bismuth-oxide chloride, or α-iron-III-oxide, as well as mixed phases of aluminum oxide or manganeseiron-III-oxide. On account of the lack of a mechanically stabilizing substrate, these pearl pigments will not easily survive shear and pressure flow of technical processing. They are similar to ground shells and are, therefore, limited to a small range of applications [40]. However, for the most part, the flake-shaped pearl and interference pigments consist of a symmetrically coated substrate of at least one additional layer. The most used substrates are natural or synthetic mica, aluminum, aluminum oxide, chromium, iron-III-oxide, or synthetic silicon dioxide. The lamellate center should have a great difference in refractive index compared to that of the coated layers. Pearlescent pigments are mostly based on mica substrate. This is a native depositing layer silicate, named muscovite, with total molecular formula KAl2 [(OH, F)2 AlSi3 O10 ]. Instead of natural muscovite, also synthetic mica is increasingly being used. The synthesized material shows a more uniformlayered structure and produces, therefore, more brilliant interference colors. Apart from metal oxides, further coating substances are fluorides or silicon dioxide, also cobalt and iron titanate, chromium phosphate, silver, gold, molybdenum, or chromium [18, 46–48]. The symmetric permutation of layers of the flakes is achieved by normal chemical procedures or vacuum evaporation coating by the PVD or CVD method [49, 50]. Examples of pearl luster pigments based on natural muscovite are shown in Color plates 7 and 8.
2.3.5 Interference Pigments Consisting of Multiple Layers Flake-shaped pigments based on muscovite or other substrates can be modified to produce a variety of further impressive colors. Intensified interference colors and simultaneously selective absorption, analogous to colored pigments, can be achieved by coating mica with two or more metal oxides of different refractive indices. Such kinds of flakes are also called combination pigments. Compared to single-coated mica pigments, they show more brilliant and brighter interference colors, as well as a more distinct color flop. The color flop is called distinct if a variety of interference colors are to observe. Conversely, the color flop is less distinct if only few interference colors are angle dependent to perceive. The color flop is again more distinct than with a mixture of the natural pearlescent and absorption pigments. Because of the underlying two different color production mechanisms, combination pigments are also termed as two-color pigments or color-flop pigments.15 In dependence on the observation angle, 15 Not
only combination pigments produce a color flop but rather interference pigments with other layer combinations as well as diffraction pigments, cf. Table 2.10., Section 2.3.3.
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2 Light Sources, Types of Colorants, Observer
Fig. 2.40 Cross section of a symmetrical multi-layer pigment; permutation of layers from the centered mica substrate: titanium dioxide, silicon dioxide, titanium dioxide; overall layer thickness about 500 nm (source: Merck KGaA, Darmstadt, Germany)
either the gloss is composed of the absorption and interference color or the non-self-luminous color of the absorption pigment is dominant. The most important combination pigments are TiO2 -coated mica flakes vapor-coated with further oxides such as α-Fe2 O3 (hematite modification), Fe3 O4 , or Cr2 O3 . As shown in Fig. 2.40, the muscovite substrate can be covered with two different oxide layers of TiO2 and SiO2 . On account of the six boundary layers with different refractive indices, 15 interference combinations are possible. These produce extreme interference colors which are superimposed by the absorption colors of both oxides. Mica pigments vapor-coated with TiO2 and top-coated with other metal oxides such as TiO2–x , TiOx Ny , FeTiO3 , or nanocarbon particles embedded in TiO2 generate silver gray or black pigments of improved compatibility with colored pigments. Transparent mica pigments can be produced in form of nano-sized particles by a suitable precipitation method of oxides or oxide hydrates; these colorants are called transparent colors. Moreover, modified process engineering allows for the manufacture of pigments of minor gloss [41]. The top-coat of an interference pigment can also consist of a pure metal. A substrate of a metal (Al or Cr) or metal oxide (Al2 O3 , Fe2 O3 , SiO2 ) is coated with a glassy layer of another refractive index (TiO2 , MgF2 ), as well as an evaporated semitransparent metal top-coat (Cr, Ni, or Al). The inner and outer reflecting layers form together a Fabry–Pérot etalon, cf. Fig. 2.18. This structure causes increased interference intensities and a sharp color flop by multiple reflection. An interference pigment showing a distinct color flop is generally named as optical variable interference pigment (OVIP). An example of such an OVIP of layer composition MgF2 /Al/MgF2 is shown in Fig. 2.41. In this SEM picture, it is particularly interesting to see the quite
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Fig. 2.41 SEM photograph of an optical variable interference pigment with symmetrical layer composition of MgF2 /Al/MgF2 ; cf. Color plate 9 (source: Flex Products Inc, Santa Rosa, CA, USA)
even surfaces and the sharp edges of the pigment particles. The even surfaces indicate also internally even surface boundaries and, therefore, brilliant interference colors followed by a distinct color flop. The sharp edges indicate that the flakes are broken at low temperatures and sifted out. The particles shown in Fig. 2.41 have a mean lateral dimension of d50 ∼ = 20 μm and a thickness of about 100 nm. An impression of the color flop produced by this pigment is given by comparing the two pictures of Color plate 9. Both photos show the same image field of a light microscope in bright- and dark-field illumination; bright field means illumination from the top of the surface and dark field means interference from the side of the color sample. In this case, the colored flop changes from green to violet (see also Section 3.5.3). Interference pigments of special shish-kebab layer structures and consisting of organic polymers are termed as liquid crystal pigments (LCP). A liquid crystal state is arranged without exception of rod- or elliptical-shaped polymer molecules consisting of suitable dipole moments or polarizing groups. The corresponding textures are optically anisotropic and are, for example, used in seven segment displays for more than four decades. The accompanying texture is called liquid crystalline or mesomeric phase because the molecular conformation corresponds neither to a random liquid nor to an ordered crystalline state.
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2 Light Sources, Types of Colorants, Observer
There exist altogether three different liquid crystalline textures. The corresponding molecular configurations are termed as nematic, smectic, and cholesteric: – nematic: the molecules are aligned parallel to their longitudinal axes, are arbitrary slidable in the axial direction, and are rotatable around the longitudinal axes independent of one another; – smectic: the molecules are oriented with their long axis perpendicular to each monomolecular sheet; the movement of the molecules is restricted to rotations around the longitudinal axes; – cholesteric: the molecules are arranged parallel to one another and grouped in layers; the layers are systematically turned toward each other by a specific angle; the mobility of the molecules is the same as in the nematic phase. These molecular configurations are schematically sketched in two dimensions in Fig. 2.42, but are to interpret as three-dimensional textures.
Nematic
Smectic
Cholesteric
Fig. 2.42 Schematic representation of rod-shaped polymer molecules in nematic, smectic, and cholesteric phase
The manufacture of liquid crystalline pigments of suitably layered structures normally starts with polymer molecules in the nematic phase. This state is converted into layers of cholesteric texture – for example, with silicones – at higher temperatures in the presence of a chiral additive. The single parallel layers are then cross-linked and fixed using UV radiation; see Fig. 2.43. Each layer is twisted by a constant angle relative to the adjacent layer. The nearly identical molecular conformation with regard to the initial layer is attained after passing the so-called pitch height p of about 100 nm. On account of the systematically twisted molecular conformation inside the pitch, the transmitted light is circularly polarized by this structure. The pigment particles have thicknesses
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Fig. 2.43 Parallel and cross-linked layers of polysiloxane molecules in cholesteric texture forming a half pitch of a liquid crystal pigment (schematically)
of about 5 μm, the lateral dimension normally ranges from about 7 to 90 μm. Liquid crystalline sparkling pigments can be realized up to about 500 μm. An entire pitch works optically like a Fabry–Pérot etalon [51]. The partial reflection at the pitch surfaces and the rotated molecular arrangement causes several optical effects which greatly affect the interference behavior of these pigments: – a kind of gloss coming from the depths, which is attenuated in pearl luster pigments because the light must pass through various pitches and layers; – on account of reflections between adjacent pitch surfaces, the interference wavelength λ changes according to Equation (2.1.20) for z = 1 and p = 2d; the wavelength decreases with increasing angle of observation from the vertical; an example of transparent liquid crystal pigments is shown in Color plate 10; – caused by a low pitch value, only one single interference order is observable within ±90◦ ; it is accompanied by a distinct color flop; – the reflected polarized light increases the brilliance of the interference color; – because the particles are transparent, the total color impression can be influenced by the background color or mixed absorption pigments. Furthermore, modern developments use even pure metals, metal alloys, metal oxides, or borosilicate glass for substrates of interference pigments; see Table 2.13. An example of an uncoated glass substrate and coated with TiO2 is shown in Fig. 2.44. The differences in refractive indices at the interfaces cause not only unusual brilliant and pure interference colors but also sparkle effects which are even colored. Pigments of other compositions, thicknesses, and permutation of layers cause impressive color flops. These occur nearly throughout the entire visible spectrum (see Section 3.5.3). Finally, there are the so-called extended interference films (cf. Table 2.12, previous section). The manufacturing is carried out by co-extrusion of transparent polymer foils with different refractive indices (1.48 ≤ n ≤ 1.60). The films are partly colored with absorption pigments. The original low interface reflectivity is improved by semitransparent silvering of some internal foils. The full foil sequence has a thickness of up to 400 μm and contains a maximum
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2 Light Sources, Types of Colorants, Observer Table 2.13 Some optical variable interference pigments
Substrate
Coating
Peculiarities
Al2 O3
Depending on coating thickness d TiO2 Fe2 O3 Lateral dimension 5 μm ≤ φ ≤ 30 μm
Colors: “Silver,” yellow over blue-green until blue; “Bronze,”, “Copper,” red interference colors; sparkle pigments for φ ≥ 30 μm
Ca–Al borosilicate
TiO2 , Fe2 O3 , SiO2 : SiO2 /TiO2 in multi-layers: d ≤ 1 μm, 20 μm ≤ φ ≤ 200 μm
Substrate of high transparency, “pure” interference colors without scattering, multicolored sparkle effect
SiO2
TiO2
Colored flop: “gold-silvery” to greenish, green-blue to dark-blue; more distinct with rutil compared to anastas
Fe2 O3
Layer configuration: Fe2 O3 /SiO2 /Fe2 O3 / SiO2 /Fe2 O3
Colored flop: violet to orange-“gold”; top coating of Fe2 O3 , corrosion resistant
Metals and metal alloys
Mono-layers: Al, Zn, Cu–Zn alloys; SiO2 /Al/SiO2 , α-Fe2 O3 /Al/α-Fe2 O3 Multi-layers: From the surface partially oxidized and oxides of metal flakes
Fabry–Pérot etalons; cf. Table 2.8
Fig. 2.44 (a) Uncoated borosilicate substrate, (b) coated with titanium dioxide layers; total flake thickness of about 300 nm (source: Merck KGaA, Darmstadt, Germany)
of 70 films. The multi-layer films are crushed at temperatures below the lowest glass transition temperature of the polymers used and are sieved in different fractions.
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2.3.6 Spectral Behavior of Pearlescent and Interference Colorants Pearl luster and interference pigments are either nearly transparent or opaque. The most important representatives of both groups are shown in Table 2.14. In this section, we limit ourselves to describing only transparent particles because these colorants have more interesting color shades. First, we discuss the dependence of the color impression on the background color; thereafter, we explore methods for covering coatings. As already mentioned, the interference color appears in the direction of the specular angle; this corresponds to the interference angle of first order. The complementary color is transmitted by the transparent particles and absorbed by opaque flakes. Table 2.14 Examples of nearly transparent and opaque pearlescent and interference pigments Light transmittance
Examples
Nearly transparent
TiO2 pigment, Fe2 O3 combination pigments on mica substrate; Fe2 O3 coating of Al2 O3 substrate; coated SiO2 flakes; liquid crystalline polysiloxanes
Opaque
Reduced TiO2 on white mica; multi-layer pigments: Al flakes coated with SiO2 , Fe2 O3 ; Al or Cr platelets vapor coated with MgF2 , Cr, or Ni
The total color impression of transparent interference pigments is strongly influenced by the chosen background; this is clearly shown in connection with Fig. 2.45. Because a black background absorbs the complementary color, only the interference color is observed above the coating. The interference color corresponds to the mass tone of the pigment. On account of the additional light scattering, which is generated to a greater or lesser degree by the corners or edges of the pigment particles, the surface of such coatings appears in fact dark, but rarely absolute black. On the contrary, a white background scatters, to a large extent, the transmitted complementary color and is only slightly absorbed. The interference color is then superimposed upon by the scattered amount of the complementary color in direction of the specular angle. In all other directions, only the scattered complementary color is observed. Consequently, over a black background, the natural colors of an interference pigment are observed and over a white background, the covering capacity. These uncolored background surfaces allow also for the determination of the reflectance and transmittance of a transparent or translucent layer from reflection measurements (Sections 3.4.3 and 4.2.4). In the case of a colored background, the interference color is clearly superimposed upon by that color. Because the interference and absorption colors can
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2 Light Sources, Types of Colorants, Observer Interference color
Complementary color
Black
White
Colored
Fig. 2.45 The color impression of colorations with transparent interference pigments is affected by the chosen absorbing or scattering background
be either identical or different, a variety of color flops are possible. At curved surfaces (which are always to be avoided for color measurements), the interference and the absorption color can be observed simultaneously. Transparent interference pigments mixed with colorants of complementary mass tone result in a white color according to the laws of additive color mixing. Mixtures of transparent interference pigments with other pigments of similar color produce more dull colors like the single colorants. As an alternative to a white background, a scattering silver-colored metallic or pearlescent pigment of d50 value less than 10 μm can be used. Such parameters for the pearlescent pigment normally ensure a high DOI value. Preferred bright silvery pigments for this purpose are mica flakes coated with TiO2 or aluminum cornflakes. For light gray layers FeTiO3 -mica pigments are suitable. On the basis of the scattering contribution or broad particle size distribution, the gloss is reduced. Aluminum pigments have also the tendency to reduce the chroma of pearlescent and interference pigments. This is in analogy to white in mixtures of colored absorption pigments. In the following, we consider in more detail the color systematic and the corresponding spectral reflection which result from thickness changes and composition of the layers. For this, we restrict ourselves to the pigments with layer compositions which were already discussed in the previous section, among other things. They are as follows: – titanium dioxide evaporated mica particles; – mica flakes coated with iron-III-oxide;
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Effect Pigments
93
– two mica-based combination pigments of titanium dioxide in rutil modification: top coated with iron-III-oxide or with chromium-III-oxide; – liquid crystal pigments consisting of polysiloxanes.
These pigments are typical representatives of other pearlescent and interference pigments. This goes especially for the accompanying colorimetric behavior of these pigments which show astonishing colorimetric parallels (Section 3.5.3).
2.3.6.1 Titanium Dioxide Evaporated on Mica Substrate An example of a pearlescent pigment on a mica substrate coated with rutil is shown in the upper half of Color plate 7. This picture was taken under bright field illumination. From the top view, the particles produce a yellow color impression over a black background. The non-uniform colors of the particles are caused by different layer thicknesses and by flakes tilted with regard to the image plane. This is further elucidated with the example of the red pearl luster pigment in Color plate 8. In this case, the particles in the same field are recorded in using bright and dark field illumination. The comparatively high-valued refractive index of titanium dioxide (n = 2.5 or 2.7) together with the low value of muscovite (n = 1.5) offers suitable conditions for developing neatly ordered interference colors. However, if the mica substrate is already flake shaped, TiO2 crystallizes in a thin film which is only suited for interference. Among the three possible crystal modifications of titanium oxide – rutil, anastas, and brookit – the rutil structure is preferred in this case. The dependency of the interference color on the titanium-dioxide-layer thickness is given in Table 2.15 (cf. Table 2.5). Each color impression over black background changes with increasing layer thickness from metallic “silver” over copper-red to green. These are no spectral colors because the accompanying colors are, in each case, composed of several adjoining interference wavelengths. The different wavelengths are selected by varied layer thicknesses of the metal oxide and by particles tilted differently toward the image plane (see Color plates 7 and 8). Under diffuse illumination, these pearl luster pigments produce the spectral reflectance over black background shown in Fig. 2.46. With increasing layer thickness, the peak shifts to longer wavelengths and simultaneously broadens. In the figure, this begins in the violet region. The reflectance minimum also moves to longer wavelengths, in the figure starting from the yellow range. The spectral reflectance of the “silver” pigment corresponds to that of a light gray hue or to that of aluminum cornflake pigments. This suggests the substitution of the metallic aluminum pigment by the cheaper pearlescent pigment in suitable cases.
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2 Light Sources, Types of Colorants, Observer
Table 2.15 Interference colors depending on layer thickness of titanium dioxide on mica substrate (cf. Table 2.5)
Layer thickness titanium dioxide/nm
Platelet thickness/nm
Interference color – inherent color over black background
Transmitted complementary color
40–60 60–80 80–100 90–110 120–130 100–140 120–160
120–140 140–160 230–250 250–270 280–300 310–320 370–390
“Silver” Yellow Red Copper-red Violet Blue Green
“Silver” Blue Green Blue-green Yellow-green Yellow Red
Now, assume that the peaks in Fig. 2.46 can be interpreted as interference wavelengths of first order. Clearly, this is not exact, but sufficient for the following estimations. If we use the values of the relevant refractive indices of Table 2.11 and assume perpendicular observation, then Equation (2.1.18) delivers an approximate value for the thickness of the titanium oxide layer. For the R (%) Layerthickness in nm 80
a: 40 – 60 b: 60 – 80 c: 80 – 100 d: 120 – 130 e: 100 – 140 f : 120 – 160
60
40
b a c d
20
e f
0
400
500
600
λ nm
Fig. 2.46 Spectral diffuse reflectance of mica pigments of different TiO2 coating thicknesses; measurements over black background, de:8 geometry16
16 The corresponding de:8 measuring geometry (see Section 4.1.2) simulates diffuse illumination conditions in closed rooms.
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Effect Pigments
95
last five flakes indicated in Table 2.15, this approximate calculation results in values which are in the given thicknesses intervals. The systematic changes in spectral reflectance are characteristic features of the basis pigment series: the spectral reflectance curves measured under diffuse illumination are “fingerprints” of the relevant pearl pigments. This is an analog to absorption colorants. These fingerprints are sometimes utilized for analyzing mixtures with further pigments. Using directional illumination and angle-dependent reflectance measurements, particularly important information about the properties of the relevant interference pigments can be obtained. For the moment, we restrict the discussion to only one illumination angle although the colors of pearlescent, interference, and diffraction pigments depend on the illumination as well as the observation angle. The five spectral reflectance curves in Fig. 2.47 were measured with the green pearlescent pigment, which has a peak at 507 nm in Fig. 2.46, curve (f). The film of pearl luster pigments over a black background is illuminated at an angle β = 45◦ and the spectral reflectance is measured at aspecular angles μas = 15◦ , 25◦ , 45◦ , 75◦ , and 110◦ . As can be seen, the peak reflectance reduces dramatically with increasing measurement angle and it shifts to slightly shorter wavelengths. For observations near the specular angle, the reflectance exceeds values higher than 1.0 or 100%. The chosen five measuring angles are by no means sufficient to gather the entire color dynamics of pearlescent and interference pigments [52, 53].
2.3.6.2 Iron-III-Oxide on Mica Substrate Crystalline α-Fe2 O3 has the highest refractive index of n = 2.88 among the substances listed in Table 2.11. As mentioned in the previous section, the total color impression of the layer composition with mica results from superposition of the layer-dependent interference color and the absorption color of the hematite. Iron-III-oxide produces a red to reddish-brown absorption color which is further modified by the thickness of the outer layer, see lower picture of Color plate 7. The color impression changes with increasing layer thickness from bronze colored to copper to purple or even reddish-green at the highest layer thickness. This is clear from the spectral reflectance curves shown in Fig. 2.48. In the cases of bronze, copper, and red, the reddish-brown absorption color is even amplified by the corresponding, nearly equal interference color like yellow, copper, and red. We return to the hue dependence of the layer thickness in Section 3.5.3. The superposition of interference and absorption leads to brilliant colors in the vicinity of the specular angle. Near this angle, the purple and reddish-green pearlescent pigments have a violet or green interference color caused by the relative high layer thickness of the hematite. With regard to comparable outer
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2 Light Sources, Types of Colorants, Observer 150
R (%)
100
μas = 15°
50
25°
45°
0 400
75°
500
600
110°
λ
nm
Fig. 2.47 Spectral reflectance of the green interference pigment from Fig. 2.46 at five aspecular measuring angles μas ; measurement over black background, illumination angle β = 45◦
layer thickness, the TiO2 -mica pigments produce a broader variety of interference colors, whereas the iron-III-oxide produces diverse types of red hues. The distinct brilliance of the α-Fe2 O3 pigments comes from the slightly higher refractive index of the hematite in comparison to that of titanium dioxide. The increased covering capacity is again a consequence of the typically increased scattering of the inorganic oxide.
2.3
Effect Pigments
97
R (%)
a: Bronce b: Red-golden c: Copper d: Purple e: Red-green
80
Fe2O3Layer thickness
60
a b c
40
d
e 20
0
400
500
600
λ nm
Fig. 2.48 Diffuse spectral reflectance of mica pigments coated with Fe2 O3 of different layer thicknesses; measurement over black background, measuring geometry de:8
2.3.6.3 Combination Pigments Interference with more brilliant colors and higher absorption is generated by coating the substrate with two or more different metal oxides. A multitude of combination pigments are based on titanium dioxide-mica flakes, where the flakes are additionally vapor coated with Fe2 O3 or Cr2 O3 . These sorts of combination pigments show, in comparison to the original single-coated mica pigments, higher brilliance and a more distinct color flop. In the following, we consider the reflection behavior of mica combination pigments composed of layers of titanium dioxide in rutil modification coated with iron-III-oxide. The optical interactions between both metal oxides lead to many brilliant golden colors reaching from pale yellow-gold to rich red-gold to green-gold. With the addition of an oxide layer, a clear color extension with regard to the simple Fe2 O3 -mica particles is achieved. Furthermore, the change of the layer thicknesses of the two metal oxides generates a wealth of superimposed interference and absorption colors. The thicknesses of all three layers can be tuned with each other in such a way that the interaction of the interference and absorption components leads to a demanded coloristical effect, within limits. Similar features result from the substitution of the outer Fe2 O3 layer by Cr2 O3 . The combination of Cr2 O3 with TiO2 in anastas modification results in
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2 Light Sources, Types of Colorants, Observer
R (%) Fe2O3 TiO2 Rutil
80
60
Fe2O3 TiO2 Rutil
40 Cr2O3 TiO2 Anastas Cr2O3
20
TiO2 Anastas
0
400
500
600
λ nm
Fig. 2.49 Diffuse spectral reflectance of two combination pigments Fe2 O3 /TiO2 (rutil), Cr2 O3 /TiO2 (anastas) on mica substrate of different layer thicknesses; measurement over black background, measuring geometry de:8; the curves of Fe2 O3 /TiO2 are shifted 20 units toward higher reflectance values for better overview
high-luster blue-greenish to moss-green colors. Figure 2.49 shows the spectral reflectance curves measured under diffuse illumination of Fe2 O3 /TiO2 pigment and Cr2 O3 /TiO2 -mica pigment. Each has two different outer layer thicknesses, but the total coating thickness is constant in each case. The greater thickness of the outer oxide layer reduces the reflection. This is clearly caused by increased absorption due to greater layer thickness. In the case of a higher layer thickness of Cr2 O3 , this pigment additionally develops a clear peak in comparison to the quite broad peak belonging to the thinner outer layer. The increased influence of the Cr2 O3 layer on the interference development can be ascertained from the reflectance curve (f) in Fig. 2.46 for the green pearlescent pigment together with the two lower curves in Fig. 2.49. Altogether, titanium dioxide is responsible for the brilliance of the colors and the outer layer thickness for the interference color. The included absorption colors of iron oxide or chromium oxide exist otherwise under all observation angles. Nearly equal-colored oxide layers create a pearl luster effect of intensive colors which, at nearly all observation angles, show a noticeable color shift. However, if the color of an absorption colorant corresponds to that of the complementary color of the interference pigment, then a distinct two-colored effect is achieved, especially in the oxide combination of Cr2 O3 /TiO2 . Further inorganic absorption pigments such as Prussian blue, cobalt blue, Fe3 O4 , or carbon
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Effect Pigments
99
black generate, in combination with titanium oxide on mica substrate, unusual color effects as well. 2.3.6.4 Liquid Crystal Pigments The color flop of liquid crystal pigments consisting of polysiloxane depends on the pitch height p and causes, for example, the color pairs violet/blue, blue/turquoise, blue/green, green-blue/gold, and green/copper-red. Flakes with blue/green-flop are shown in Color plate 10 at bright and dark field illumination over black background. The noticeable sparkle particle there is already green from the top view because of the higher pitch height compared to the other flakes. To the present day, mixtures of the transparent particles with absorption or other effect pigments produce unequaled and extremely brilliant colors. As mentioned at the beginning of the section, further shades can be obtained with a suitable background color. With regard to liquid crystal pigments, this concept is underlined by the example in Fig. 2.50. The reflectance curves correspond to background colors of white, red, and black as well as each top coated with a transparent film of the same liquid crystal pigment. The reflectance peak over black at 512 nm corresponds to the green color impression from the top view. The red background leads to a minimal blue-tinged red and the
R (%)
Background alone
White
80
Layer over background
Red
60
40
20
Black 0 400
500
600
λ nm
Fig. 2.50 Spectral reflectance of a transparent liquid crystal pigment with d50 = 30 μm over white, red, and black background, as well as backgrounds alone; wavelengths of maximum reflectance over background: 512 nm (red), 531 nm (black); measuring geometry de:8
100
2 Light Sources, Types of Colorants, Observer
white background creates a very light pink. The flat maximum of the white background at a wavelength of 490 nm is caused by fluorescence emission of the contained optical brightening agent (Section 4.2.6). Figure 2.51 shows the directional reflectance over a black background for illumination angle β = 45◦ and aspecular observation angles μas = 15◦ , 25◦ , 45◦ , 75◦ , 110◦ . With increasing measuring angle, the wavelength of the peak shifts from 483 to 520 nm. Simultaneously, the peak height decreases from R = 108% to about R = 2%. The angle dependence of the interference wavelength corresponds to the cosine function in Equation (2.1.20). R (%)
μas = 15°
β = 45° d50 = 30 μm
100
25° 50
45° 75° 0 400
500
λ nm
110° 600
Fig. 2.51 Spectral reflectance of a liquid crystal pigment with d50 = 30 μm for five aspecular measuring angles; measurements over black background, illumination angle β = 45◦
The brilliance of liquid crystalline pigments depends also on the average lateral dimension of the flake particles. This can be seen from the reflectance maxima in Fig. 2.52. The reflectance curves are measured for three different particle size distributions over the same black background and at constant illumination and aspecular angle of β = 45◦ and μas = 15◦ , respectively. The flakes have size distributions which correspond to the ratios of d50 /d99 = 30/90, 23/60, and 18/50 μm/μm. The reflectance maxima in Fig. 2.52 correspond to the ratios 30:23:18 of accompanying d50 values. In addition, this result is confirmed by measurements over red and blue background. The height of the reflectance maximum of liquid crystal pigments is, therefore, directly proportional to the mean flake size. Clearly, large-sized LCPs orient better to the background surface, in analogy to metallic flakes. These larger particles then show increased brilliance
2.3
Effect Pigments
101
R (%)
β = 45° μas = 15°
d50 = 30 μm 100
23 μm
50
0 400
18 μm
500
λ
600
nm
Fig. 2.52 Directional reflectance at constant aspecular measuring angle μas = 15◦ of a liquid crystal pigment in dependence on particle size d50 ; measurements over black background, illumination angle β = 45◦
compared to smaller sized flakes. The colorimetric properties of the most important pearl luster and interference pigments are outlined in Sections 3.5.3 and 3.5.4.
2.3.7 Opaque Films Containing Absorbing and Effect Pigments From discussions up until now, it is clear that the creation of new colorations by mixtures or films consisting of modern effect and classical absorption pigments represents quite a challenge. Especially needed to meet this challenge are hiding layers which consist of transparent effect pigments and covering absorption pigments. A coating is called covering or hiding, if any colored background can no longer be observed from above the film (Section 3.4.3). Covering layers with coarse metallic, transparent pearlescent, interference, or even diffraction pigments are produced by mixtures of colorants which generate suited scattering or absorption. It is also important to consider the change of the originally desired color effect with the addition of further colorants and also the compatibility with the pure effect pigment. Experience shows that covering coatings with effect pigments can, in the most cases, be manufactured with three different colorants: carbon black, suitable absorption pigments, and fine metallic pigments [54].
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2 Light Sources, Types of Colorants, Observer
A small amount of carbon black turns out to be quite effective for this. The resulting dark and sometimes even intense colors are caused by absorption of the complementary color with carbon black already inside the layer. Only a small volume amount < 1.0% of carbon black is normally sufficient. For larger concentrations, the interference color often appears too dark and the color travel (respectively, color flop) is too small or suppressed. The selective absorption and scattering of mixed in absorption pigments also result in covering layers of additionally impressive colors. Small amounts cause mostly brilliant interference colors. Larger amounts, however, can obliterate the pearl luster and interference effect: on the one hand, the interference intensity is increasingly masked and on the other hand, the complementary and part of the interference color are absorbed depending on the chroma of the absorption pigment. Finally, in the third method, the transparent pearl or interference pigment is mixed with a small amount of a special fine and, therefore, strongly scattering metallic pigment. In this case, the covering formulation is, however, accompanied by reduced brilliance, color saturation, and gloss. In all three mentioned cases, it is important to pay attention to the compatibility of the added components. Furthermore, the added amounts should be as small as possible in order to result in a coloristic effect changed only slightly. Altogether, the level of pigmentation of effect pigments in recipes depends on the desired color effect, the spreading rate of the pigment, and the molecular surroundings. For a few applications the pigment volume content is shown in Table 2.16. Apart from the application, the processability, the light, temperature, or weathering resistance, etc., additionally determine the total pigment amount of a coloration; see also Section 3.4.6. Table 2.16 Pigmentation level of effect pigments in various fields Pigment level % Employment
Metallic pigments
Pearlescent, interference pigments
Lacquers, emulsion paints Thermoplastics, thermosets Printing inks Cosmetics Toiletries
0.5–2 0.5–3 1–45 1–15 0.05–1
0.5–20 0.5–2 1–30 1–50 0.05–1
From color physical point of view, mixtures of effect pigments together or with absorption colorants obey the laws of additive or subtractive color mixing (Section 2.4.3). Mixtures or layers of effect pigments show additive color mixing if the colors of the single pigments are based on the superposition of wavelengths; see Table 2.17. But, as soon as the light interacts only with one
2.3
Effect Pigments
103
Table 2.17 Additive and subtractive color mixing of effect and absorption pigments Pigment combination
Color mixing
Cause
Interference pigment mixed with interference pigment Interference pigment mixed with diffraction pigment
Additive
Interference pigment on absorption pigment
Additive and subtractive
Interference pigment mixed with absorption pigment
Subtractive
Absorption pigment mixed with absorption pigment
Subtractive
Superposition of reflected interference and transmitted complementary color Superposition of interference, diffraction, and transmitted complementary color Superposition interference color, absorption of complementary color and selective absorption of the colored pigment Colored pigment absorbs parts of the complementary and natural color of the interference pigment Each colored pigment absorbs parts of the influx light
Additive
absorption pigment together with any further pigment sort, the resulting color impression is based on subtractive color mixing; see also the literature [54, 55]. Additive color mixing is fundamental in the human color sense and the based on colorimetry of versatile industrial applications. Finally, we return to optical properties of interference pigments which depend on the particle size and morphology. Smaller particles show a reduced pearl luster effect in comparison with those of larger sized. This is because the higher edge scattering reduces the luster. In the case of dominant scattering, the pearl luster and gloss of interference pigments can even disappear completely. An increasing lateral size dimension up to 200 μm improves not only the brilliance but also the sparkle of the pearlescent and interference pigments; furthermore the color travel passes more wavelengths. However, with increasing flake geometry, the hiding power and DOI are reduced. The pigment properties shown in Table 2.18 correlate with related properties of metallic pigments listed in Table 2.9. In other words, comparable color properties of metallic, pearlescent, and interference pigments change in the same direction depending on the flake size. We have, thus far, still neglected opaque multi-layered pigments (Table 2.13). A considerable part of their color physical properties correspond to those of transparent effect pigments. An advantage of these pigments is the fact that the color effect is not distorted by additional colorants, but the absorption and selfscattering of the particles softens the original color. Further similarities between different effect pigment sorts are uncovered in Section 3.5.3.
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2 Light Sources, Types of Colorants, Observer
Table 2.18 Assessment of some properties of pearlescent and interference pigments in dependence of the particle size Particle size Φ/μm Property
Φ 4 ◦ . The 4◦ limit was arbitrarily established although there exists no discontinuity of color perception at this angle. The SCMFs of the 10◦ observer x¯ 10 (λ), y¯ 10 (λ), z¯10 (λ) are distinguished from those of the 2◦ observer by the subscript 10. The values follow from a transformation similar to Equation (2.4.21) using the corresponding CMFs r¯10 (λ), g¯ 10 (λ), b¯ 10 (λ) according to the equation ⎞ ⎛ ⎞ ⎞ ⎛ r¯10 (λ) 0.341080 0.189145 0.387529 x¯ 10 (λ) ⎝ y¯ 10 (λ) ⎠ = ⎝ 0.139058 0.837460 0.073160 ⎠ · ⎝ g¯ 10 (λ) ⎠ . z¯10 (λ) 0 0.039553 1.026200 b¯ 10 (λ) ⎛
(2.4.22)
The numerical values of the components of the matrices in Equations (2.4.21) and (2.4.22) are unequal because they belong to different primaries and different observer fields. The SCMFs of both observers are together represented in Fig. 2.66. The maxima of the functions y¯ (λ) and y¯ 10 (λ) are normalized at λ = 555 nm to 1.0. Due to the different visual field of the observers, the corresponding curves do not match perfectly. For one and the same color, the standard color values corresponding to each observer are also not identical. From the nonlinear wavelength dependence of both CMFs follows that the corresponding standard color values cannot be converted into one another. Although the 10◦ observer is used to an increasing extent in color industry, in order to avoid ambiguity, the observer must be clearly indicated with the results. For the last adjustment criterion of the four listed above, it should be stated that the graph of the function y¯ 10 (λ) agrees with the measured luminous efficiency V(λ) of the human eye
2.4
Observer
127
2° 10°
Standard color matching function
2.0 z (λ) 1.5
x (λ)
y (λ) 1.0
x (λ)
0.5
0 400
500
600
700
λ
nm
Fig. 2.66 Color-matching functions of the 2◦ and 10◦ standard observers (CIE 1931 and CIE 1964 observers, respectively)
y¯ 10 (λ) = V(λ),
(2.4.23)
see Fig. 2.67.20 The standard color value Y is, on account of this adjustment, a measure for the lightness of a coloration. The curves of V (λ) and V(λ) in Fig. 2.67 correspond to the sensitivity of the eye for scotopic and photopic adaption, respectively. The curves are shifted with respect one another by about 40 nm. This is described by the so-called Purkinje effect. From the half-widths of 150 nm, it follows that the middle wavelengths of the visible spectrum are perceived with particular sensitivity under both adaption conditions. Now, the CIE standard color values X, Y, Z are simply given from the previous quantities R, G, B by substituting the discrete color-matching values r¯i , g¯ i , b¯ i of the 2◦ observer in Equations (2.4.18), (2.4.19), and (2.4.20) by the corresponding quantities x¯ i , y¯ i , z¯i :
20 Since
V(λ).
2005, the CIE’s altered recommendation [71]; since 1931 it was accepted y¯ (λ) =
128
2 Light Sources, Types of Colorants, Observer
V(λ)
Relative luminous efficiency
V '(λ) 1.0
0.5
0
400
500
600
700
λ
nm
Fig. 2.67 Relative luminous efficiency of the human eye in scotopic adaption V (λ) and photopic adaption V(λ)
X=
N
Φi x¯ i Δλ,
(2.4.24)
Φi y¯ i Δλ,
(2.4.25)
Φi z¯i Δλ.
(2.4.26)
i=1
Y=
N i=1
Z=
N i=1
The standard color values for the 10◦ observer follow from the same considerations using x¯ 10, i , y¯ 10, i , z¯10, i instead of x¯ i , y¯ i , z¯i and are denoted by X10 , Y10 , Z10 . According to the last three relations, the standard color values of a coloration can be explicitly calculated if the retinal color stimuli Φ i are known from Equation (2.4.11) or (2.4.12). The spectral power distribution S(λi ) of the light source used is known from CIE tables. This means that the spectral power distribution of the real source is substituted by a corresponding artificial source for the determination of color values. The same is the case with regard to the observer: the individual observer is substituted by one of the standard observers. In addition, the measured reflection or transmission of a given color sample can differ in different color measuring devices. The retinal color stimulus values above are, therefore, idealized quantities and it is, therefore, not astonishing that color values can differ from the individual visual assessment. Nevertheless, a given coloration is unambiguously characterized by three corresponding numerical standard color values. Colors of equal standard values are
References
129
perceived as equal, even if they consist of different sorts of colorants (e.g., dyes or absorption pigments). Because of this, it is not possible to infer the constituent colorants from the numerics of the standard color values. At best, with experience, one can estimate the lightness, chroma, or hue of the color. On the other hand, a single color value alone is not of main interest in color physical applications. Of much greater importance is the color difference between two or more similar color shades. Such questions and answers to them for nearly all sorts of colors are discussed in the sections of the following chapter.
References 1. Strocka, D: “Are Intervals of 20 nm Sufficient for Industrial Colour Measurement?”, Colour 73, Adam Hilger, London (1973) 453 2. Pedrotti, FL, Pedrotti, LS, Pedrotti, LM: “Introduction to Optics”, Person Prentice Hall, Upper Saddle River, NJ (2007) 3. Bellan, PM: “Fundamentals of Plasma Physics”, Cambridge University Press, Cambridge (2006) 4. Taylor, AH, Kerr, GP: “The distribution of energy in the visible spectrum of daylight”, J Opt Soc Am 31 3–8 (1941) 5. Albrecht, H: “Optische Strahlungsquellen”, Grafenau (1977) 6. Coaton, JR, Ed: “Lamps and Lighting”, Butterworth-Heinemann, Oxford (2001); Csele, M: “Fundamentals of light sources and lasers”, Wiley-Interscience, Hoboken, New Jersey (2004) 7. CIE No 15.3: “Colorimetry”, 3rd ed, CIE, Bureau Central de la CIE, Wien (2004) 8. ISO 11664-2:2007: “Colorimetry – Part 2: CIE Standard Illuminants”, International Organization of Standardization, Genf, CH (2007) 9. CIE S 014-2E: “Colorimetry – Part 2: CIE Standard Illuminants”, CIE, Bureau Central de la CIE, Wien (2006); ISO 11664-2: 2008 (E), Joint ISO/CIE Standard 10. CIE No 13.2: “Method of Measuring and Specifying Colour Rendering Properties of Light Sources”, 2nd ed, CIE, Bureau Central de la CIE, Paris (1974) 11. CIE No 13.3: “Method of Measuring and Specifying Colour Rendering Properties of Light Sources”, 3rd ed, CIE, Bureau Central de la CIE, Wien (1995) 12. DIN 6169: “Farbwiedergabe” part 1-8, Deutsches Institut fuer Normung eV, Berlin (1976–1979) 13. Kortuem, G: “Reflexionsspektroskopie”, Springer, Berlin (1969) 14. Born, M, Wolf, E: “Principles of Optics”, 7th ed, reprint, Cambridge University Press, Cambridge UK (2006) 15. Ditteon, R: “Modern Geometrical Optics”, Wiley, New York (1998) 16. Bohren, CF: “Absorption and Scattering of Light by Small Particles”, Wiley-VCH, Weinheim (2004) 17. Iizuka, K: “Engineering Optics”, 3rd ed, Springer Series in Optical Sciences Vol 35, Springer, New York (2008) 18. Glausch, R, Kieser, M, Maisch, R, Pfaff, G, Weitzel, J: “Special Effect Pigments”, 2nd ed, Vincentz, Hannover (2008) 19. Tipler, PA: “Physics for Scientists and Engineers”, Freeman, New York (2008) 20. Loewen, GE, Popov, E: “Diffraction Gratings and Applications”, Dekker Inc, New York (1997) 21. Nassau, K: “The Physics and Chemistry of Color”, 2nd ed, Wiley, New York (2001) 22. Buxbaum, G, Pfaff, G, Eds: “Industrial Inorganic Pigments”, 3rd ed, Wiley-VCH, Weinheim (2005) 23. Herbst, W, Hunger, K: “Industrial Organic Pigments: Production, Properties and Applications”, 3rd ed, Wiley-VCH, Weinheim (2004)
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24. Benzing, G, Ed: “Pigmente und Farbstoffe fuer die Lackindustrie”, 2nd ed, expert, Ehningen (1992) 25. Hunger, K, Ed: “Industrial Dyes”, Wiley-VCH, Weinheim (2003) 26. Valeur, B: “Molecular Fluorescence”, Wiley-VCH, Weinheim (2006) 27. Hunt, RWG: “The Reproduction of Colour”, 6th ed, Wiley, Chichester (2004) 28. Smith, KJ: “Colour order systems, colour spaces, colour difference and colour scales”; in McDonald, R, Ed: “Colour Physics for Industry”, 2nd ed, Soc of Dyers and Colourists, Bradford (1997) 29. Kuehni, RG, Schwarz, A: “Color Ordered: A Survey of Color Order Systems from Antiquity to the Present”, Oxford University Press, Oxford (2008) 30. Munsell, AH: “Atlas of the Munsell Color System”, Wadsworth-Howland & Company, Malden, MA (1915); “Munsell Book of Color”, Munsell Color Co, Baltimore, MD (1929) until now 31. Hard, A, Sivik, L, Tonquist, G: “NCS natural colour system from concept to research and applications”, Col Res Appl 21 (1996) 129 32. Colour Index International: “Pigment and solvent Dyes”, Soc Dyers Col, Bradford, England; and American Association of Textile Chemists and Colorists, Research Triangle Park, NC (1998) 33. ASTM E 308 – 08: “Standard Practice for Computing the Colors of Objects by Using the CIE-System”, American Society for Testing and Materials, West Conshohocken, PA (2008); DIN 6164: “DIN-Farbenkarte”, Part 1–3, Deutsches Institut fuer Normung eV, Berlin (1980–1981) 34. Nickerson, D: “OSA uniform color scale samples: a unique set”, Col Res Appl 6 (1981) 7 35. RAL: “RAL-Design-System”, “RAL Effect”; RAL Deutsches Institut fuer Guetesicherung und Kennzeichnung, St Augustin, Germany (2008) 36. ASTM D 16 – 08: “Standard Terminology for Paint, Related Coatings, Materials, and Applications”, American Society for Testing and Materials, West Conshohocken, PA (2008); CIE No 124/1: “Colour notations and colour order systems”, CIE, Bureau de la CIE, Wien (1997); DIN 55943: “Farbmittel – Begriffe”, Deutsches Institut fuer Normung eV, Berlin (2001) 37. Landolt-Boernstein: “Zahlenwerte und Funktionen aus Naturwissenschaften und Technik”, new series II, Vol 15b: “Metalle: Elektronische Transportphaenomene”, Springer, Berlin (1985) 38. Wheeler, I: “Metallic Pigments in Polymers”, Rapra Techn Ltd, Shawbury, UK (2003) 39. Wissling, P et al: “Metallic effect pigments”, Vincentz Network, Hannover (2007) 40. Pfaff, G: “Spezielle Effektpigmente”, 2nd ed, Vincentz Network, Hannover (2007) 41. ASTM D 480 – 88: “Standard Test Methods for Sampling and Testing of Flaked Aluminum Powders and Pastes”, American Society for Testing and Materials, West Conshohocken, PA (2008); DIN 55923: “Pigmente: Aluminiumpigmente und Aluminiumpigmentpasten fuer Anstrichfarben”, Deutsches Institut fuer Normung eV, Berlin (1983) 42. Roesler, G: “Colorimetric characterization and comparison of metallic paints”, Polymers Paint Colour J 181 (1991) 230 43. Rodriguez, ABJ: “Color and appearance measurement of metallic and pearlescent finishes”, ASTM Standardization News 10 (1995) 44. Panush, S: “Opalescent Automotive Paint Compositions Containing Microtitaniumdioxide Pigment”, Patent US 4753829 (1986) 45. Pfaff, G, Franz, KD, Emmert, R, Nitta, K, in: “Ullmann’s Encyclopedia of Industrial Chemistry: Pigments, Inorganic”, Section 43; 6th ed, Wiley-VCH, Weinheim (1998) 46. Teany, S, Pfaff, G, Nitta, K: “New effect pigments using innovative substrates”, Eur Coatings J 4 (1999) 434 47. Sharrock, SR, Schuel, N: “New effect pigments based on SiO2 and Al2 O3 flakes”, Eur Coatings J 1–2 (2000) 105 48. Maile, FJ, Pfaff, G, Reynders, P: “Effect pigments: past, present, future”, Progr Org Coat 54/3 (2005) 150
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49. Droll, FJ: “Just what color is that car”, Paint & Coatings Industry (1998) 2 50. Schmid, R, Mronga, N, Radtke, V, Seeger, O: “Optisch variable Glanzpigmente”, Farbe u Lack 104/5 (1998) 44 51. Heinlein, J, Kasch, M: “LC-Pigmente – Feuerwerk der Farben”, Phaenomen Farbe 7+8 (2000) 18 52. Cramer, WR, Gabel, PW: “Effektvolles Messen”, Farbe u Lack 107 (2001) 42 53. Nadal, ME, Early, EA: “Color measurements for pearlescent coatings”, Col Res Appl 29 (2004) 38 54. Hofmeister, F, Maisch, P, Gabel, PW: “Farbmetrische Charakterisierung und Identifizierung von Mica-Lackierungen”, Farbe u Lack 98 (1992) 593 55. Gabel, PW, Hofmeister, F, Pieper, H: “Interference pigments as focal points of colour measurement”, Kontakte 2 (1992) 25 56. Argoitia, A, Witzman, M: “Pigments Exhibiting Diffractive Effects”, Soc Vacuum Coaters, 45th Ann Techn Conf Proceedings (2002) 57. Dowling, JE: “The Retina: An Approachable Part of the Brain”, Harvard Univ Press, Cambridge, (1987) 58. Kaiser, PK, Boynton, RM: “Human Color Vision”, 2nd ed, Optical Society of America, Washington DC (1996) 59. Birch, J: “Diagnosis of Defective Color Vision”, 2nd ed, Butterwoth-Heinemann, Oxford (2001) 60. Shevell, SK, Ed: “The Science of Color”, Elsevier, Amsterdam (2003) 61. Neumeyer, C:“Color Vision in Lower Vertebrates”, in: Backhaus, WGK, Kliegel, R, Werner, JS, eds: “Color Vision: Perspectives from Different Disciplines”, W de Gruyter, Berlin (1998) 62. Jordan, G, Mollon, JD: “A study of women heterozygous for colour deficiencies”, Vision Res 33 (1993) 1495 63. Mueller, GE: “Ueber die Farbempfindungen”, Z Psychologie, 17/18 (1930) 64. Judd, DB: “Basic correlates of the visual stimulus”, in: “Handbook of Experimental Psychology”, Wiley, New York (1951) 811 65. Grassmann, HG: “Zur Theorie der Farbenmischung”, Annalen der Physik 89 (1853) 69; original translation in English: Philosophical Magazine 7, Ser 4 (1854) 254; in addition: MacAdam, DL, Ed: “Selected Papers in Colorimetry – Fundamentals”, SPIE Milestone Series MS 77 (1993) 10 66. Wright, WD: “A re-determination of the mixture curves of the spectrum”, Trans Opt Soc Lond 31 (1929–1930) 201 67. Guild, J: “The colorimetric properties of the spectrum”, Phil Trans Royal Soc London, Ser A 230 (1931) 149 68. Broabent, AD: “A critical review of the development of the CIE 1931 RGB colourmatching functions”, Col Res Appl 29 (2004) 267 69. Fairman, HS, Brill, MH, Hemmendinger, H: “How the CIE 1931 color-matching functions were derived from Wright-Guild data”, Col Res Appl 22 (1997) 11; Col Res Appl 23 (1998) 259 70. CIE No 15.2: “Colorimetry”, 2nd ed, CIE, Bureau Central de la CIE, Wien (1986) 71. CIE No 165: “CIE 10 degree photopic photometric observer”, CIE, Bureau Central de la CIE, Wien (2005) 72. CIE S 014-1:2006: “Colorimetry-Part 1: CIE Standard Colorimetric Observers”, CIE, Bureau Central de la CIE, Wien (2006); ISO 11664-1: 2008 (E), Joint ISO/CIE Standard 73. Stiles, WS: “The basic data of colour-matching”, Phys Soc London, Yearbook (1955) 44 74. Stiles, WS, Burch JM: “NPL color-matching investigation: Final Report”, Optica Acta 6 (1959) 1 75. Speranskaja, NI: “Determination of spectrum color coordinates for twentyseven normal observers”, Optics Spectro 7 (1959) 424
Chapter 3
Systems of Standardized Tristimulus Values, Color Qualities, Chroma of Effect Pigments
Because the trichromatic color sense of the observer is based on additive color mixture, every color impression can be assigned three numerical color values. These color stimulus specifications are, so to speak, representatives of a color. In this chapter, the previous tristimulus values are extended, specifically in order to better meet some coloristical requirements of color industry. The empirical three color values can additionally be interpreted as points in a color space. We restrict the discussion first to the standardized systems that have been proposed for application by the CIE. The most important empirical color difference formulas in colorimetry follow from these systems. These formulas enable to calculate only the color differences of similar or nearly equal colors. In addition, we discuss the standardized DIN99o color space and the newest color appearance model which offer further methods to solve problems in industrial color physics. These formalisms allow one to better detect numerically such color deviations, which inevitably occur during production, reproduction, repair, or aging. The main focus of the effort relates to properties of absorption colors, such as color constancy, metamerism, color strength, covering power, or transparency, which are described by characteristic values. Experience shows that the related colorimetric procedures are quite efficient; however, they do have limits in their applicability. The limits in applicability of these methods are shown especially with different sorts of colorations containing effect pigments.
3.1 Systems of Standardized Tristimulus Values After introduction of the tristimulus values X, Y, Z by the CIE [1] in 1931, more than 13 different color-value systems were worked out. Each of the accompanying color spaces followed from the intention of broadening the basis of the subjective description for the increasing industrial color requirements of absorption colors. This, in no way arbitrary, variety is an expression of the fact that all of these empirical systems were incapable of sufficiently answering the most G.A. Klein, Industrial Color Physics, Springer Series in Optical Sciences 154, C Springer Science+Business Media, LLC 2010 DOI 10.1007/978-1-4419-1197-1_3,
133
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important questions in the color industry. In the following, we restrict the discussion to the three most applied contemporary color value systems. Although the color physical results with these systems are up to now quite promising, the numerical simulation of the human color sense needs further research.
3.1.1 CIE 1931 Tristimulus Values The standard color values X, Y, Z, also called CIE 1931 tristimulus values, given with Equations (2.4.24), (2.4.25), and (2.4.26), are applicable for opaque, translucent, as well as transparent non-self-luminous colors. However, the following modifications need to be taken into consideration depending on the type of light transmittance. For opaque colors, the color stimulus Φ(λ) from Equation (2.4.1) for each wavelength λi should be inserted in the above-mentioned three equations, which results in X=k Y=k
N i=1 N
S(λi )R(λi )¯x(λi )Δλ ,
(3.1.1)
S(λi )R(λi )¯y(λi )Δλ ,
(3.1.2)
S(λi )R(λi )¯z(λi )Δλ .
(3.1.3)
i=1
Z=k
N i=1
In the case of translucent colors, the additional color stimulus Φ(λ) from Equation (2.4.2) is valid so that three further tristimulus values result. These are simply given by substitution of the spectral reflectance R(λi ) in Equations (3.1.1), (3.1.2), and (3.1.3) by the spectral transmittance T(λi ). For ideal transparent colors, only the transmittance values actually measured should be taken into consideration. The spectral power distribution of the source S(λi ) as well as the SCMFs x¯ (λi ), y¯ (λi ), z¯(λi ) of the chosen standard observer should be taken from standard tables for the relevant Δλ value, which is given by the measuring conditions [2,3].1 The constant k in the above equations depends on the chosen illuminant, the SMCF y¯ (λi ), and the wavelength interval Δλ. This comes from the following consideration. Independent of the wavelength λi in the visible range, an ideally scattering achromatic white field has a constant reflectance R(λi ) = 1.000. For an ideal transparent material, the set value is T(λi ) = 1.000. As explained in Section 2.4.6, the standard color-matching function y¯ (λi ) is accepted as identical to the 1 In addition to previous
recommendations, since the year 2001, the CIE also edits standards, which are designated by CIE S.
3.1
Systems of Standardized Tristimulus Values
135
light sensitivity V(λi ) of the human eye, which is adjusted to the standard color value Y. Consequently, the standard color value is a measure for the lightness of a color. On account of this consideration, the CIE has arbitrarily assigned the ideal scattering field the value Y = 100.000 for every illuminant. Equation (3.2.1), therefore, leads to k=
100.000 N
.
(3.1.4)
S(λi ) · y¯ (λi ) · Δλ
i=1
The choice of the constant k in this equation has a far-reaching consequence: the three standardized color values (and all further ones) are dimensionless quantities, particularly considering that the reflectance and transmittance are dimensionless; see Equations (2.1.14a) and (2.1.14b). Similar considerations are valid in view of the 10◦ observer. The corresponding formalism follows by insertion of the SCMFs x¯ 10 (λi ), y¯ 10 (λi ), z¯10 (λi ) into Equations (3.1.1), (3.1.2), and (3.1.3). In this case the constant k in Equation (3.1.4) simply results from using y¯ 10 (λi ) instead of y¯ (λi ). The accompanying standard color values are denoted as X10 , Y10 , Z10 . It should be pointed out again that for clear interpretation, all color values are to be specified with the underlying illuminant and standard observer. The standard color values X and Z are not subject to further adjustment conditions. Both quantities can, therefore, differ from 100.000. This is shown in Table 3.1 for ideal white (or ideal transparency) and common illuminants. The tabular values of Xn and Zn follow from Equations (3.1.1) and (3.1.3) by insertion of the ideal reflectance or transmittance R(λi ) = T(λi ) = 1.000. For all illuminants and standard observers, the quantity Yn = 100.000 remains. The quantities Xn and Zn are to be consequently interpreted as standard color values of the corresponding illuminant. A careful view of the sums in Equations (3.1.1), (3.1.2), and (3.1.3) confirms the conclusion which was already stated at the beginning of the previous chapter. Table 3.1 CIE standardized color values of different illuminants 2◦ standard observer
10◦ standard observer
Illuminant
Xn
Zn
Xn
Zn
D 65 A C
95.047 109.850 98.074
108.883 35.585 118.232
94.811 111.144 97.285
107.304 35.200 116.145
FL 2 FL 7 FL 11
99.186 95.041 100.962
67.393 108.747 64.350
103.279 95.792 103.863
69.027 107.686 65.607
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Each of the three standard color values X, Y, Z follows from the three external factors, which are responsible for the color impression of non-self-luminous colors: – the light source, approximated by the chosen illuminant of spectral power distribution S(λi ); – the color sample, characterized by the measured spectral reflectance R(λi ) or transmittance T(λi ); – the observer, represented by the standard observer of SCMFs x¯ (λi ), y¯ (λi ), z¯(λi ) or x¯ 10 (λi ), y¯ 10 (λi ), z¯10 (λi ). At this stage, it is necessary to point out a critical fact. Among the three factors, the reflectance and transmittance by the colorants, binders, and additives of the color pattern are clearly given. However, the spectral power distribution and the standard observer are idealized quantities: in most cases, the radiant energy of the light source used deviates more or less from the tabulated values S(λi ). In the same sense, the SCMFs x¯ (λi ), y¯ (λi ), z¯(λi ) or x¯ 10 (λi ), y¯ 10 (λi ), z¯10 (λi ) of the chosen standard observer do not necessarily agree with those of the actual observer. Consequently, the standard color values only represent the color impression of the special standard observer in combination with the chosen tabulated illuminant. In addition, it is important to remember the fact that the experimental quantities of reflectance and transmittance always have measurement errors. These critical connections should always be taken into consideration in order to avoid, for example, confusion during assessment of color values. It was already mentioned at the end of Section 2.4.5 that the sums in Equations (3.1.1), (3.1.2), and (3.1.3) are actually integrals. In reality, the optic nerves integrate over all simultaneously incoming spectral stimuli at the retina. This is independent of the width of the corresponding wavelength intervals. Nevertheless, we maintain the sum notation for the moment because the quantities of reflectance R(λi ) or transmittance T(λi ) have to be measured at a fine number N of discrete wavelengths λi . These are to be combined with corresponding tabular values S(λi ) and x¯ 10 (λi ), y¯ 10 (λi ), z¯10 (λi ), for example. The integrals are ipso facto approximated by N addends. Although the psychophysical knowledge with regard to colors is only based on empirical considerations, the color values enable an approximate quantification of the color impression, of special color properties, or of color differences at least of similar absorption colors. Such color quantities are no longer limited merely to subjective verbal descriptions. The reader should realize that every standard color value is only a representative of three special color components of a color pattern. These are exclusively valid for the chosen illuminant and the underlying standard observer.
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Systems of Standardized Tristimulus Values
137
3.1.2 Chromaticity Coordinates and Chromaticity Diagram In spite of the achieved breakthrough, the CIE 1931 system lacks a level of clarity. However, before the more clear CIE 1976 and DIN99o systems are discussed, it is useful to glance over the so-called chromaticity coordinates x, y, z, which were also introduced by the CIE in 1931. These quantities are based on the standard color values X, Y, Z, upon which the above-mentioned two further systems are also based. The chromaticity coordinates of coloration are defined by the equations x=
X , X+Y +Z
(3.1.5)
y=
Y , X+Y +Z
(3.1.6)
z=
Z . X+Y +Z
(3.1.7)
Each coordinate is given by the ratio of one standard color value over the sum of all three color values of a color pattern. A unity sum of these coordinates follows: x + y + z = 1. This is why two given chromaticity coordinates determine the third quantity. Analogous formulas to Equations (3.1.5) and (3.1.6) follow for the 10◦ standard observer; the chromaticity coordinates are indicated by x10 , y10 , z10 . On the other hand, it is impossible to calculate the three standard color values of a color from two chromaticity coordinates such as x, y. For this calculation, one of the three values X, Y, Z would additionally have to be known. The chromaticity coordinates x and y represent the so-called chromaticity, which combines both terms hue and chroma of a color. The CIE has decided to use the x, y, Y system which is applicable to the 2◦ and 10◦ standard observers. Because the Y value is a measure for the lightness of a color and the primaries X and Z contain no lightness component, the quantities x, y can be taken, for example, as coordinates of a plane triangle. If these coordinates are chosen rectangular, we obtain the CIE chromaticity diagram [1]. In Color plate 2, the chromaticity values x, y of absorption colors with equal lightness are approximately represented.2 The limiting equal-sided triangle of (x, y) corner point coordinates (1, 0), (0, 1), (0, 0) is called the color triangle. Non-self-luminous colors of equal lightness are represented in the chromaticity diagram by the x, y coordinates located inside the sole-shaped area. This area is bordered by the arched spectrum locus and the straight purple boundary. The x, y chromaticity coordinates of visible spectral colors are represented by the spectrum locus. In Color plate 2, some of the corresponding 2
Color plates are inserted between Chapters 3 and 4.
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Table 3.2 Color areas of equal lightness Y in the CIE chromaticity diagram [4] 2◦ standard observer
10◦ standard observer
Illuminant
xn
yn
xn
yn
D 65 A C
0.31272 0.44758 0.31006
0.32903 0.40745 0.31617
0.31382 0.45117 0.31002
0.33100 0.40594 0.31867
FL 2 FL 7 FL 11
0.37207 0.31285 0.38053
0.37512 0.32918 0.37691
0.37928 0.31565 0.38543
0.36723 0.32951 0.37110
monochromatic wavelengths between 380 and 780 nm are indicated. The purple boundary joins the end points of the spectrum locus. The colors represented by the purple boundary are not contained in the visible spectrum, but they can be produced spectrally by additive mixture of monochromatic lights. In the case of the equienergy spectrum, the standard color values X, Y, Z are equal to one another and the chromaticity coordinates are x = y = z = 1/3. The coordinates x = y = 1/3 determine the so-called achromatic point. The quantities of the chromaticity coordinates xn , yn for ideal white or ideal transparency are given in Table 3.2 for various illuminants as well as both standard observers. The values follow from those of Table 3.1 and result from the different spectral power distributions of the sources as well as the slightly different SCMFs of the standard observers. Every point on a straight line through the achromatic point and the spectrum locus represents colors of the same hue. The greater the distance from the achromatic point, the purer the corresponding color. Because the spectrum locus represents only spectral colors, these are the purest colors which are to produce. The third coordinate of the x, y, Y system, represented by the lightness axis, is also arbitrary chosen perpendicular to the color triangle. Its value domain is always between zero for ideal black and 100.000 for ideal white. However, for black, all standard color values vanish. Because of the as-yet not fully defined Equations (3.1.5), (3.1.6), and (3.1.7), it is not so obvious how to represent black in the chromaticity diagram. On the other hand, the area included by the spectrum locus and the purple boundary decreases with increasing lightness. The corresponding entire colors tend to become achromatic until they reach white. This is represented by the chromaticity coordinates of the achromatic point as shown in Fig. 3.1. The volume contained by the surface extending along the lightness axes is called the coloring body. Within this volume, all colors possible to be produced are represented by chromaticity coordinates with the exception of ideal black. The limiting surface, except the base area, represents all pure spectral colors including their mixtures. The chromaticity diagrams in Fig. 3.1 and Color plate 2 belong to the 2◦ observer and illuminant C. In comparison, the spectrum locus for the 10◦
3.1
Systems of Standardized Tristimulus Values
139
520
y
10
540
20 30 40 50
60
560 70
0.6
80 90
580
95
0.4
600 100
620 650 770 nm
0.2 480 470
0
380
450
0
0.2
0.4
0.6
x
Fig. 3.1 Color areas of equal lightness Y in the CIE chromaticity diagram [4]
observer is only marginally shorter. This is caused by the higher and broader maxima of the corresponding SCMFs (Fig. 2.67). The chromaticity points of the illuminants D65, A, and C with correlated color temperatures and of the blackbody radiator are shown in Fig. 3.2. The solid curve section is termed as the Planckian locus. It follows, from Equations (3.1.1), (3.1.2), (3.1.3), (3.1.4), (3.1.5), (3.1.6), and (3.1.7), that this locus has the temperature-dependent Planck law of radiation (2.1.1). The chromaticity coordinates of real temperature or luminescence radiators, however, tend to be located adjacent to the Planckian locus. Although the x, y chromaticity diagram supplies an important contribution to the illustration of color values, it also reveals, however, a serious property of the human color sense which turns out to be a disadvantage in discerning the differences in equal or similar colors. According to the investigations of McAdam, similar colors, which are perceived as equal, lie inside the so-called
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520
y 540
560
0.6 500 580 A 2,000 K 2,856 K 3,500 K D65 4,500 K C 6,500 K 10,000 K
0.4
600
650 770 nm
∞
0.2 480 380
0
450
0
0.2
0.4
0.6
x
Fig. 3.2 Chromaticity coordinates of temperature radiators: standard illuminants A and D65 as well as illuminant C, and blackbody radiator
tolerance ellipses in the chromaticity diagram [4]. Some of these ellipses are shown magnified 10 times in Color plate 3. The length of the ellipse axis and the orientation are not constant; these parameters depend rather on the color locus and lightness. In the area of yellow to green colors, larger ellipses dominate in comparison to those for dark-blue colors. For dark-blue, violet, or dark red colors, the major ellipse axes are oriented nearly parallel to the purple boundary. If this line rotates counterclockwise around the endpoint corresponding to 380 nm, we nearly obtain the new alignment of the major axis in other areas of the chromaticity diagram. Color differences among dark colors are, therefore, more sensibly perceived by the human eye and with improved tolerance than color deviations for brilliant and light colors such as green, yellow, or orange. From colorimetric point of view, the chromaticity diagram gives no consistency in color differences
3.1
Systems of Standardized Tristimulus Values
141
in different color areas. Not only the color sense but even color differences behave in a nonlinear fashion and depend on the color locus in the chromaticity diagram. Consequently, also various color tolerances need to be arranged: a nonnegligible hindrance for industrial color judgment or finding out accurate color tolerance agreement. Brown and McAdam [5] showed, in addition, that Color plate 3 renders only projections of three-dimensional ellipsoids with major axes which are not necessarily located in the x, y plane. The observable lightness differences are also irregularly distributed in the color plane. In a further work, Wyszecki [6] found, however, that the semi-axes of the ellipses are smaller than those given by Brown and McAdam. The shortcomings of the x, y, Y system would really be eliminated, if one could succeed in transforming the X, Y, Z standard color values in such a way that the various ellipsoids change into spheres of equal radii. This would correspond to the uniform chromaticity scale triangle (UCS triangle and corresponding UCS color space). This goal has, until now, not been achieved. As long as it is impossible to quantitatively follow the neural processes of color perception, only the empirical approach of tracking down the so-called visually equidistant color space is possible. This empirical method forms the basis of the modern color value systems and the color appearance model in the following sections.
3.1.3 CIE 1976 Color Spaces The CIE revised several times the x, y, Y system and, in 1978, recommended the so-called CIELAB system, established 1976, for application to non-selfluminous colors [7]. The corresponding three-dimensional color space is based on the Munsell color atlas. These color patterns were characterized by spectrophotometric methods and evaluated visually to be basically equidistant [8]. At the same time, the CIELUV system was published. It is recommended for use with colored light sources and displays. Both systems are united by the term CIE 1976 color spaces. We restrict the discussion to the CIELAB system, which is applied to non-self-luminous colors and to some areas of digital image processing as well. Instead of the Munsell color attributes value V, chroma C, and hue H, the CIELAB color space is based on the following three color values: L∗ : a∗ : b∗ :
lightness or black to white contribution; red to green contribution; yellow to blue contribution.
These correspond to the three color pairs of the color opponent theory of Hering. With this, it should also be taken into account that experience shows that there
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exist no hues of absorption colors such as greenish red, reddish green, or bluish yellow. The term CIELAB is a synonym for CIE and the color values L∗ , a∗ , b∗ . The new color values follow from the empirical transformation equations L∗ = 116 · f (Y/Yn ) − 16,
(3.1.8)
∗
a = 500 {f (X/Xn ) − f (Y/Yn )} ,
(3.1.9)
∗
(3.1.10)
b = 200 {f (Y/Yn ) − f (Z/Zn )} .
These equations contain the previous standard color values X, Y, Z and those of the chosen illuminant Xn , Yn , Zn and standard observer. The values Xn , Yn , Zn are given in Table 3.1 for some illuminants. The three functions f(q) are given by f (q) =
q1/3 for q > (24/116)3 , (841/108) · q + 16/116 for q ≤ (24/116)3
(3.1.11)
where q represents each of the ratios X/Xn , Y/Yn , Z/Zn in Equations (3.1.8), (3.1.9), and (3.1.10) [9]. The existing cubic root in Equation (3.1.11) was determined following the logarithmic change of a physiological stimulus in the Weber–Fechner law. The numbers of the linear term in Equation (3.1.11) are caused by the Pauli extension [10], with which the continuity of f(q) and the first derivative f (q) is achieved at position q = (24/116)3 . The CIELAB color space is based on the three orthogonal L∗ , a∗ , b∗ axes; see Fig. 3.3. The coordinates are arbitrarily chosen perpendicular to each other similar to the x, y, Y system of 1931. The positive L∗ axis represents achromatic colors of values between L∗ = 0 for ideal black and L∗ = 100.000 for ideal white. An a∗ , b∗ color plane of constant lightness represents the chromatic parts of a color stimulus specification. The greater the distance between the color locus and the lightness axis, the more chromatic and saturated the corresponding color. The lightness axis and its vicinity represent the color locus of achromatic colors. The lightness axis itself is, therefore, also named the achromatic axis. The trace point of this axis through any color plane is called the achromatic point. In Color plate 4, for example, a section of an a∗ , b∗ color plane representing absorption colors of middle lightness is shown. In Color plate 5, the central part of the CIELAB color space is depicted as a nearly spherical shape with corresponding achromatic and chromatic colors. The color locus represents the most frequently produced industrial absorption colors. The color values of absorption colors, capable of being manufactured, are by no means distributed over the entire mathematically defined CIELAB space. Such colors are rather limited to a sphere or ellipsoid-shaped volume including the entire achromatic axis. This volume is distorted differently depending on the sort of colorants and chosen color value system. When the McAdam ellipses from Color plate 3 are transformed into the a∗ , ∗ b color plane of the CIELAB system in Fig. 3.4, it is noticeable that the ellipses
3.1
Systems of Standardized Tristimulus Values
143
L∗ 100
White
C(L∗c , ac∗, bc∗)
Lc∗
∗ Cab
–a ∗
∗ Green ac
Yellow
bc∗
∗ hab
0
–b ∗
b∗
a∗ Black
Red
Blue
∗ , a∗ , b∗ ) is Fig. 3.3 L∗ , a∗ , b∗ axes of the CIELAB color space; the color locus C(LC C C ∗ additionally characterized by the chroma Cab and hue angle hab (see below)
are more uniform. The desired circles (respective spheres) of equal radius, however, fail to appear [11]. Although the x, y, Y and the CIELAB color space cannot be directly compared with each other, we get an idea of the effects of the transformation. Visually, the CIELAB and CIE 1931 color spaces are not equidistant. For chromatic colors, the color differences in the CIELAB space a∗ L∗ = 50 100
50
0
–50
–100 –200
–100
0
Fig. 3.4 McAdam ellipses in an a∗ , b∗ plane of the CIELAB system [11]
100
b∗
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have again greater tolerances than for achromatic dark colors. Nevertheless, with the widely accepted and applied CIELAB system, an important intermediate step on discovering the desired UCS is achieved. Properties of industrial colors are often characterized by attributes such as lightness, chroma, hue, or hue angle. The CIELAB system offers now the advantage that these properties can also be visualized and quantified. These quantities follow alternatively – instead of Cartesian coordinates L∗ , a∗ , b∗ – ∗ as the radius from cylindrical with chroma Cab ∗ Cab
a∗ + b∗ ,
=
2
2
(3.1.12)
hue angle hab as the azimuth angle ◦
hab =
180 arctan (b∗ /a∗ ), π
(3.1.13)
and the lightness L∗ for third coordinate; see Fig. 3.3. However, also the cylinder coordinates describe more color points than existing real absorption colors. The ∗ of a color is represented in an a∗ , b∗ color plane by the distance chroma Cab between the achromatic point and the (a∗ , b∗ ) coordinates of a given color. The hue angle indicates the position inside a quadrant of a color plane. Because of this, it is a measure for the corresponding hue, cf. Color plate 4. According to the defining equation (3.1.13), the hue angle is the sole color value with dimensions given in degrees. The hue angle increases counterclockwise. Along the positive a∗ axis lies hab = 0. The CIELAB system has an additional fundamental feature. Because along each of the L∗ , a∗ , b∗ axes opponent colors change, the color difference between a sample color with color values LS∗ , a∗S , b∗S and a reference color with color values LR∗ , a∗R , b∗R is given by the corresponding difference contributions ΔL∗ = LS∗ − LR∗ , Δa∗ = a∗S − a∗R , Δb∗ = b∗S − b∗R .
(3.1.14)
These can now be interpreted in a coloristical sense. The amount and the sign of the so-called color differences ΔL∗ , Δa∗ , Δb∗ mean > 0: lighter ΔL∗ = LS∗ − LR∗ = , (3.1.15) < 0: darker > 0: redder , (3.1.16) Δa∗ = a∗S − a∗R = < 0: greener > 0: yellower ∗ ∗ ∗ Δb = bS − bR = . (3.1.17) < 0: bluer
3.1
Systems of Standardized Tristimulus Values
145
L∗
ΔL∗
CS
∗ ΔEab
CR
Δb∗
b∗
Δa ∗ a∗ ∗ between color locus of a color sample C and reference color Fig. 3.5 Color difference ΔEab S CR in CIELAB color space
∗ follows, as shown in Fig. 3.5, The entire numerical color difference ΔEab from the three-dimensional Pythagorean theorem ∗ = ΔEab
(ΔL∗ )2 + (Δa∗ )2 + (Δb∗ )2 .
(3.1.18)
This color difference equation enables to indicate quantitatively the approximate value of the perceived color difference between two given colors. With the use of Equation (3.1.18), one must certainly take the following aspects into account: 1. The sign of the single color contributions is lost on account of the squares; ∗ alone it is not possible to draw any from the numerical value of ΔEab conclusions with regard to the three individual color differences. 2. As experience shows, Equation (3.1.18) holds – because of the present visually non-uniform color space – merely for small color differences in the range ∗ ≤ 5; the color values change nearly uniformly only in small of about ΔEab regions of the nonlinearly transformed color space. 3. According to the CIE proposal [7], the CIELAB color space should only be applied to non-self-luminous colors of the same size and shape; for visual assessment, the sample and reference color have to be kept in the same surroundings of a middle gray color (Section 3.2.2).
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Standardized Tristimulus Values, Color Qualities, Chroma of Effect Pigments
It seems that some of the mentioned restrictions can be overcome with a color appearance model. A color difference can be alternatively expressed with the aid of the lightness ∗ and the hue difference ΔL∗ in combination with the chroma difference ΔCab ∗ difference ΔHab ; see below. The contribution of the chroma follows due to the defining equation (3.1.12) from ∗ ∗ ∗ = Cab,S − Cab,R . ΔCab
(3.1.19)
From a geometrical point of view, the chroma difference corresponds to the length difference of the cylinder radius between the color locus of the sample and the reference color as seen in Fig. 3.6. Similar to Equations (3.1.15), (3.1.16), and (3.1.17), the chroma difference can be interpreted using color attributes such as ∗ ΔCab =
> 0: more brillant, clearer . < 0: duller, less chromatic
(3.1.20)
b∗
S
b∗S ∗ ΔCab
∗ ΔHab
b∗R
R
Δhab
a∗R
O
a∗S
a∗
∗ , hue ΔH ∗ , and hue angle Δh of sample color S Fig. 3.6 Contributions of chroma ΔCab ab ab ___
___
∗ , OR = C∗ and reference color R: OS = Cab,S ab,R
3.1
Systems of Standardized Tristimulus Values
147
With Equation (3.1.13), the change of hue angle follows as Δhab = hab,S − hab,R .
(3.1.21)
∗ , is shown The change of hue angle Δhab , along with the hue contribution ΔHab ∗ in Fig. 3.6. The quantity ΔHab is defined by
∗ ∗ C∗ ΔHab = 2 Cab,S ab,R · sin (Δhab /2)
(3.1.22a)
and is identical with expression ∗ = ΔHab
∗ )2 − (ΔL∗ )2 − (ΔC∗ )2 (ΔEab ab
(3.1.22b)
∗ corresponds to the arithmetic mean of [29]. Geometrically, the quantity ΔHab the chord lengths belonging to the chroma of the sample and reference color. ∗ leads to Solving Equation (3.1.22b) for ΔEab ∗ = ΔEab
∗ )2 + (ΔH ∗ )2 . (ΔL∗ )2 + (ΔCab ab
(3.1.23)
This is an additional relation for determining a color difference. Equations (3.1.18), (3.1.19), (3.1.20), (3.1.21), (3.1.22), and (3.1.23) give also the hue contribution by ∗ = ΔHab
∗ C∗ ∗ ∗ ∗ ∗ 2(Cab,S ab,R − aS aR − bR bS ).
(3.1.24)
∗ is positive, if the inequality a∗ b∗ − a∗ b∗ ≥ 0 holds; it is The sign of ΔHab R S S R ∗ follow directly otherwise negative [12]. Both the value and the sign of ΔHab from the equation ∗ = ΔHab
a∗R b∗S − a∗S b∗R ∗ C∗ ∗ ∗ ∗ ∗ 0.5 · (Cab,S ab,R + aS aR + bS bR )
,
(3.1.25)
∗ provided the sign of the root is positive. The contributions Δhab and ΔHab have the same sign. Therefore, Equation (3.1.25) can be used for the determination of the correct sign of Δhab , for example, if the color locus of the sample and reference color are located in adjoining quadrants of an a∗ , b∗ color plane. The CIELAB system does not define which of the equivalent color values L∗ , ∗ , h ∗ a , b∗ or respective L∗ , Cab ab are to be used. It is, at least, advisable to
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indicate the L∗ , a∗ , b∗ values from which the further ones immediately follow. It is, furthermore, not specified which of the Equations (3.1.18), (3.1.19), (3.1.20), (3.1.21), (3.1.22), and (3.1.23) is to be used to calculate the color ∗ [7,13]. In any case, it is useful to list the contributions difference ΔEab ∗ , ΔH ∗ , and Δh , which state the color difference ∗ ∗ ∗ ΔL , Δa , Δb , ΔCab ab ab precisely. Although this system does not represent the ideally desirable visually uniform color space, the progressive CIELAB formalism permits, however, to approximately answer further color physical questions which has been impossible in the past.
3.1.4 DIN99o Color Space After the introduction of the CIELAB system, since about the year 1976, international teams have, to a considerable degree, fallen back on the matching of absorption colors, which were selected and disposed of, to get closer to the desired uniform color space. The endeavors lead to the establishment of the DIN99 color space [14, 15], which is more extravagant than the CIELAB system, among other things. The color values of the DIN99 space are indicated by L99 , a99 , b99 or L99 , C99 , h99 and result from a transformation of the already known L∗ , a∗ , b∗ quantities. The revised and actually valid version of the DIN99 space is called DIN99o color space. This system delivers an improved metric, which is expressed by a more effective color difference formula. The color values of the DIN99o system L99o , a99o , b99o or C99o , h99o , likewise, follow from a nonlinear transformation of the L∗ , a∗ , b∗ quantities [14 –16]. The lightness L99o varies in logarithmic dependence on L∗ in the domain 0 ≤ L99o ≤ 100: L99o =
303.67 ln (1.0000 + 0.0039L∗ ). kE
(3.1.26)
The a99o , b99o color values are determined using the following four auxiliary functions: eo = a∗ cos (26◦ ) + b∗ sin (26◦ ),
(3.1.27)
fo = −0.83 · a∗ sin (26◦ ) + 0.83 · b∗ cos (26◦ ),
(3.1.28)
heofo = arctan (fo eo),
(3.1.29)
3.1
Systems of Standardized Tristimulus Values
149
Go = + eo2 + fo2 .
(3.1.30)
For the variable heofo , the following value domains
heofo
⎧ 0 ⎪ ⎪ ⎪ ⎪ arctan (fo eo) ⎪ ⎪ ⎨ π 2 = π+ arctan (fo eo) ⎪ ⎪ ⎪ ⎪ ⎪ 3π 2 ⎪ ⎩ arctan (fo eo)
for for for for for for
eo = fo = 0 eo > 0 and fo ≥ 0 eo = 0 and fo > 0 eo < 0 eo = 0 and fo < 0 eo > 0 and fo ≤ 0
(3.1.31)
should be differentiated. The chroma C99o follows from formula
C99o =
ln (1.000 + 0.075 · Go) . 0.0435 · kCH kE
(3.1.32)
The correction factors kE and kCH in Equations (3.1.26) and (3.1.32) depend on the observation conditions of the color patterns. These are set to 1.0, provided that the CIE reference conditions are fulfilled (Section 3.2.2). The new values of the red to green and yellow to blue proportions follow from relations a99o = C99o cos (h99o ),
(3.1.33)
b99o = C99o sin (h99o ),
(3.1.34)
with the hue angle h99o given by h99o =
180◦ heofo + 26◦ π
(3.1.35)
using the condition in (3.1.31). The original color locus of constant chroma in a CIELAB color plane is, in the new a99o , b99o color plane, rotated and compressed to concentric “ellipses” nearly in the direction of the yellow-blue axis. This is similar to the transformation by the DIN99 system, cf. Figs. 3.7a, b and 3.8. With increasing chroma, the ellipses narrow. The transformed a99o , b99o quantities are smaller than the original values in the domains for a∗ ≥ 20 and b∗ ≥ 20, but larger than comparable a99 , b99 pairs. The up until now visually tolerated higher color differences with the CIELAB system for yellow, orange, and red colors of high chroma have been mostly reduced in the DIN99 and DIN99o color spaces. In the CIELAB as well as the DIN99o space, the metric relations are structured in an analog fashion. The color difference relation
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Standardized Tristimulus Values, Color Qualities, Chroma of Effect Pigments b∗ 80
40
0
a)
–40
–80
–80
–40
0
40
80
a∗
b99 40
20
b)
0
–20
–40 –40
–20
0
20
40 a99
Fig. 3.7 Transformation of color locus of equal chroma from (a) a CIELAB a∗ , b∗ color plane into (b) the accompanying DIN99 color plane
ΔE99o =
(ΔL99o )2 + (Δa99o )2 + (Δb99o )2
(3.1.36)
to apply in the case of DIN99o color values corresponds again to the threedimensional Pythagorean theorem, cf. formula (3.1.18).
3.1
Systems of Standardized Tristimulus Values
151
b99o
40
20
0
–20
–40
–60 –60
–40
–20
0
20
40
a99o
Fig. 3.8 Transformation of color locus of equal chroma from the CIELAB a∗ , b∗ color plane in Fig. 3.7a into the accompanying DIN99o color plane
The differences contained in Equation (3.1.36) between a sample and reference color of indices S and R of lightness ΔL99o , red to green Δa99o , and yellow to blue Δb99o are ΔL99o = L99o,S − L99o,R ,
(3.1.37)
Δa99o = a99o,S − a99o,R ,
(3.1.38)
Δb99o = b99o,S − b99o,R .
(3.1.39)
These are of the same coloristical meaning as in Equations (3.1.15), (3.1.16), and (3.1.17). The chroma difference ΔC99o and the change in hue angle follow from ΔC99o = C99o,S − C99o,R ,
(3.1.40)
Δh99o = h99o, S − h99o, R .
(3.1.41)
The total color difference ΔE99o can be alternatively calculated using the formula ΔE99o =
(ΔL99o )2 + (ΔC99o )2 + (ΔH99o )2 .
(3.1.42)
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The hue contribution ΔH99o and its sign are most simply determined, analogous to Equation (3.1.25), from the relation ΔH99o =
a99o,R b99o,S − a99o,S b99o,R 0.5 · (C99o,S C99o,R + a99o,S a99o,R + b99o,S b99o,R )
,
(3.1.43)
provided that the positive sign of the square root is used as well. As already mentioned for the CIELAB space, Equations (3.1.36), (3.1.37), (3.1.38), (3.1.39), (3.1.40), (3.1.41), (3.1.42), and (3.1.43) are only applicable to small color differences ΔE99o ≤ 5. The new values of the color differences are mostly smaller than those corresponding values of the CIELAB system. The DIN99o color space actually shows a better metric than the CIELAB space, but it is, nevertheless, not visually equidistantly structured [17]. Similar to the CIELAB formalism, the DIN99o color space is also applicable to non-selfluminous colors of colorants, lacquers, plastics, textiles, printing inks, as well as colors of hygiene and cosmetic products. The question remains: Which color space should be applied in colorimetry? This question will be answered in Section 3.2.4. First of all, for simplicity in the following, we leave out the specifying indices and exponents of color values, color differences, and color difference contributions, provided that no confusion is introduced.
3.2 Color Difference Metrics and Color Tolerances The effort of empirically discovering a colorimetrical system, which matches the visually perceived color differences as closely as possible, has created more than 20 contrasting color difference formulas for absorption colorations. Only some of them have survived the constantly rising industrial requirements. In addition ∗ and ΔE to the ΔEab 99o relations, there are three key color difference equations. These are applied in different color fields: the so-termed CMC, CIE94, and CIEDE2000 color difference formulas. These three relations and also the ΔE99o equation are based on the CIELAB formula containing differently weighted color differences. Moreover, the color appearance model CIECAM02 delivers, in addition to new chromaticities, further Euclidian color spaces and color difference relations, in which the observing and surround field conditions are taken better into account than before. Independent of these, the color deviations of effect colorations need especially careful considerations and assessments. Among the color values given until now, because of the lack of suited effect models, few are appropriate for approximate colorimetrical characterization of some angle-dependent effect properties. This is also because the original color spaces were developed only for colored lights and absorption colors. The color differences of effect colors are more complex and are additionally not simply characterized by a
3.2
Color Difference Metrics and Color Tolerances
153
numerical color difference value. Other properties such as the flop, brilliance, distinctiveness, or sparkle, for example, often also deviate. Such kinds of differences should be assessed rather with additional methods that are described in Section 3.5.
3.2.1 CMC(l:c) Color Difference Formula In 1963, the Society of Dyers and Colourists in Britain arranged the Colour Measurement Committee (CMC) for working out a color difference relation for absorption colorations that matches the visually perceived color differences better than the CIELAB formula. Investigations with different color collections confirmed the fundamental insight: perceived color tolerances are represented by ellipses of different axis instead of spheres of equal radii as is expected from color difference Equations (3.1.18), (3.1.23), and (3.1.42). The final results of the committee were published in 1984 and are condensed into the so-called CMC(l:c) color difference formula ΔECMC(l:c) =
ΔL∗ lSL
2 +
∗ ΔCab cSC
2 +
∗ ΔHab SH )
2 ,
(3.2.1)
[18]. This corresponds to the equation of a three-dimensional ellipsoid with axes ∗ , ΔH ∗ . The tolin the direction of the color difference contributions ΔL∗ , ΔCab ab erance parameters l and c in (3.2.1) serve for weighting of the lightness and hue differences. For textile colorations, the values are normally set to l = 2 and c = 1. The corresponding color difference value is specified with the index CMC(2:1). For lacquers and plastic materials, the weighting factors l = 1.3 and c = 1 are used. The empirical functions SL , SC , SH are given by SL =
0.040975LS∗ for (1 + 0.01765LS∗ ) SC =
LS∗ ≥ 16,
∗ 0.0638 · Cab,S
∗ ) (1 + 0.0131 · Cab,S
else SL = 0.511,
(3.2.2)
+ 0.638,
(3.2.3)
SH = SC (f T + 1 − f ),
(3.2.4)
f =
(3.2.5)
where f and T are given by ∗ )4 (Cab,S
∗ )4 + 1900 (Cab,S
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and T = 0.38 + |0.4 cos (35◦ + hab,S )|.
(3.2.6a)
In the hue angle domain 164◦ ≤ hab,S ≤ 345◦ , the equation T = 0.56 + |0.2 cos (168◦ + hab,S )|
(3.2.6b)
∗ , h is valid. The quantities LS∗ , Cab,S ab,S belong to the sample color. If the sample color is not known, then the arithmetic mean of both colors which are ∗ , ΔH ∗ of the color being compared should be used. The differences ΔL∗ , ΔCab ab contributions follow from Equations (3.1.15), (3.1.19), and (3.1.25). The length of each semi axis of the ellipsoid defined by the CMC(l:c) formula in (3.2.1) is given by the correction functions in (3.2.2), (3.2.3), and (3.2.4). In Color plate 6, the sizes and orientations of projected ellipsoids are shown in the range of ΔECMC(1:1) ≤ 2.0 in an a∗ , b∗ color plane for ΔL∗ = 0. The major axis of the ellipses grows with increasing chroma for all colors; the quantity of the minor axis, however, depends on the hue angle hab . The ellipses are smallest in the field of orange near hab = 55◦ and widest in the region of green at ∗ takes extreme values at each hab = 192◦ . The correction function SH for ΔHab ◦ ◦ ◦ ◦ of the hue angles 145 , 164 , 282 and 342 . Since its introduction, the CMC(l:c) formula has been paving the way for the discovery of improved color difference relations. This is underlined in the following three sections.
3.2.2 CIE94 Color Difference Expression Essentially, the CMC(l:c) formula has shown itself to be correct only for textile dyes and synthesized polymeric materials. The CIE, therefore, suggested matching of further absorbent colors in order to find an improved color difference equation. For that, previous data records were used. Those records were selected in view of statistical confidence limits as well as equal measurement and evaluation conditions. Consequently in 1994, a color difference equation was presented. It was termed the CIE94 color difference formula [17, 18]: ∗ 2 ∗ 2 ΔCab ΔHab ΔL∗ 2 ∗ + + . (3.2.7) ΔE94 = kL SL kC SC kH SH With regard to the CMC(l:c) equation, this new relation shows modified correction functions SL , SC , SH . Now, these follow from more simply designed expressions: SL = 1,
(3.2.8)
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∗ SC = 1 + 0.045 · Cab ,
(3.2.9)
∗ , SH = 1 + 0.015 · Cab
(3.2.10)
kL = kC = kH = 1.0
for reference conditions, ∗ ∗ = Cab,R . Cab
(3.2.11) (3.2.12)
These are provided that the reference color is known, otherwise the geometrical ∗ = ∗ C∗ mean Cab Cab,1 ab,2 of colors 1 and 2 to be compared should be used in Equations (3.2.9) and (3.2.10). The coefficients kL , kC , kH depend on the previously mentioned observation conditions, which were introduced at that time. These are set to 1.0 in Equation (3.2.7), as long as the so-called CIE reference conditions are fulfilled [19]. It is suitable to modify the mentioned three constants if one or more criteria deviate from the preset conditions. The CIE reference conditions, together with the experimental realizations, are listed in Table 3.3. These are to be regarded as minimum requirements and are primarily founded on the specific properties of the three factors determining color impression outlined in Sections 2.1 and 2.4. The conditions in Table 3.3 are intended to be used for the comparison and assessment of colors. They follow from these connections: 1. The standard illuminant D65 to simulate middle daylight shows a nearly constant spectral power distribution in the visible range (Fig. 2.4); colors are, to some degree, rendered neutral with this illuminant in comparison to other temperature or luminescence radiators. Change in illuminant possibly exposes nonlinear color changes such as color inconstancy, for example. Table 3.3 CIE reference conditions for assessment of absorption colors No.
Criterion
Realization of CIE reference condition
1 2 3 4 5 6 7
Illumination Illuminance Background field Viewing mode Viewing angle Sample separation Magnitude of color difference Sample structure
D65 simulator 1,000 lx Uniform, neutral gray of L ∗ = 50 Object mode > 4◦ Minimal, with direct edge contact ∗ ≤5 ΔEab
8
Homogeneous, without visible patterns or uniformities
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2. The illuminance should be higher than 500 lx so that all cones of the retina are stimulated for color vision and the rods are switched off. This requirement is definitely achieved above an illuminance level of 1,000 lx; levels higher than 5,000 lx, however, cause blinding glare. 3. According to the color constancy investigations of Land and other groups, the surrounding color changes the color impression (cf. simultaneous contrast, Section 2.4.2). In order to avoid color shifts caused by peripheral colors, in the immediate surroundings of the color pattern (locating surface), a middle neutral gray of lightness L∗ = 50 should be used. It is known that differences between dark colors are resolved to a much lesser degree in a light surrounding than in a dark one. Therefore, a middle gray is a useful compromise. 4. In object modus, by definition, the reflected light of a free field non-selfluminous color is directly observed. In contrast, the assessment can also be carried out in illumination modus (direct light) or in aperture modus (observed field limited by an aperture), so that uncontrolled scattered light hardly contributes to the color impression. 5. The influence of the yellow pigment in the macula of the retina (Fig. 2.60) on color impression is nearly excluded for visual angles greater than 4◦ . Therefore, the need for the application of the 10◦ standard observer is clear. 6. Light or brilliant colors appear darker or duller with edge separation as in direct edge contact; conversely, dark and dull colors are perceived lighter or more brilliant with edge separation. Furthermore, the color assessment is increasingly influenced by the color of the gap between the color patterns; because of this “distraction effect,” higher color differences are tolerated as with perfect formation. These considerations follow directly from the third criterion above. 7. The color values of the color spaces discussed in Section 3.1 change in a nonlinear fashion with regard to color perception. Local changes, however, are assumed to be linear; this is generally valid for color differences ∗ ≤ 5. ΔEab 8. To avoid distorting the color impression from the beginning, only homogeneous, uniform, and optically defect-free color patterns should be employed. A structured surface increases the lightness and non-uniform colored samples distort the chromaticity values. All in all, the CIE reference conditions recommend that the mentioned observation criteria should be met for all sorts of color assessments and are independent of specially used color difference formulas as well. Deviations from the reference conditions or additional premises are to indicate for clarity. In a color appearance model outlined in Section 3.2.4, the color values are calculated directly considering observation criteria.
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3.2.3 CIEDE2000 Color Difference Equation The color difference equation given in the previous section is only roughly appropriate for the varying expectations of different color technological industries. For this reason, the CIE recommended in 2001 an additional color difference formula which was worked out by several groups based on more than 3,600 color patterns [20–23]. This new color difference relation is denoted as CIEDE2000 and delivers the value ΔE00 : ΔE00 =
ΔL kL SL
2
+
ΔCab kC SC
2
+
ΔHab kH SH
2
+ RT
ΔCab kC SC
ΔHab . kH SH (3.2.13)
This expression is again founded on the CIELAB color values and has two innovations in comparison to the previous color difference formulas: and of hue ΔH are transformed by a∗ – the contributions of chroma ΔCab ab ∗ and Cab , instead of the unchanged lightness difference ΔL = ΔL∗ ; – there is a fourth summand which consists of the product of the chroma and hue contributions; the ellipsoid axes are, therefore, not oriented parallel to the , H . coordinates of Cab ab
The original CIELAB chroma and hue differences given in Section 3.1.3 are to modify in the manner that follows. The indices S and R stand for the sample and the reference color: L = L∗ ,
a = a∗ (1 + G),
b = b∗
(3.2.14)
with G=
1 ∗ ∗ ∗ )7 /[(C∗ )7 + 257 ] , C∗ · 1 − (Cab,m ab,m = (Cab,S + Cab,R )/2, ab,m 2 (3.2.15) = Cab
h ab =
(a )2 + (b )2 ,
180◦ · arctan (b /a ), π
(3.2.16) (3.2.17)
ΔCab = Cab,S − Cab,R ,
(3.2.18)
Δh ab = h ab,S − h ab,R ,
(3.2.19)
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a R b∗S − a S b∗R ΔHab = . 0.5 · (Cab,S Cab,R + a S a R + b∗S b∗R )
(3.2.20)
Equations (3.2.14) and (3.2.15) change ellipses located near the lightness axes into circles of the a , b color plane. If the CIE reference conditions of the previous section are met, then the correction parameters in Equation (3.2.13) are kL = kC = kH = 1. The correction functions for lightness, chroma, and hue differences, SL , SC , SH , follow from the relations: − 50)2 1 + 0.15 · (Lm , SL = − 50)2 20 + (Lm
Lm = (LS + LR )/2,
(3.2.21)
SC = 1 + 0.045 · Cm , Cm = (CS + CR )/2,
(3.2.22)
SH = 1 + 0.015 · Cm · T.
(3.2.23)
For the determination of the function values of T in Equation (3.2.23) and RT in Equation (3.2.13), the expressions T = 1 − 0.17 · cos (h m − 30◦ ) + 0.24 · cos (2h m ) + 0.32 · cos (3h m + 6◦ ) − 0.20 · cos (4h m − 63◦ ),
h m = 12 (h S + h R ) (3.2.24)
are used along with RT = (2G − 1) · sin (ΔΘ), ΔΘ = 60 · exp −[(h m − 275◦ )/25◦ ]2 . (3.2.25) , C∗ , C , and h are the arithmetic mean of the correspondThe quantities Lm m m ab,m ing sample and reference values. Equation (3.2.22) is formally equivalent to that of the CIE94 formula in Equation (3.2.9). The function T in Equation (3.2.24) on the hue angle. The takes into account the additional dependence of ΔHab rotation function RT appears in a color difference equation for the first time. It corrects the direction of the major axis of the discrimination ellipses in the blue region of the color plane. To sum up, two different methods have been adopted until now to achieve a better match between numerical color differences and visually perceived color deviations:
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159
– establishing Euclidian color spaces (CIELAB, DIN99o); the color difference expressions correspond to sphere equations; – creation of single color difference formulas which contain weighted and transformed contributions of CIELAB color differences (CMC(l:c), CIE94, CIEDE2000) and follow from assessment of color collections; the corresponding equations describe ellipsoids. Among these approaches, the Euclidian color space is generally preferred: every color locus of the space presents the same metric; furthermore, the color difference follows directly from uncorrected color contributions such as ΔL, Δa, Δb. These five color difference relations discussed here are standardized [24]. Out of these newest formulas at least two further questions show themselves. First, how effectively the individual color difference relations work? And second, are further improvements possible using other empirical methods? Both aspects are discussed in the next section.
3.2.4 Efficiency of Color Difference Formulas, CIE Color Appearance Models The determination of a suitable color difference formula for a special color application requires extensive coloristical experience. Ultimately, it is necessary to decide which of the discussed color difference expressions is at the most accurate. One principal reason for the lack of a generally applicable relation is the incomplete knowledge of the complicated neural sequences which cause the trichromatic color impression in the visual cortex. Furthermore it is not clear whether the postulated visually uniform color space is actually reproducible with mathematical elements. Already from the x, y chromaticity diagram or the CIELAB system, it follows that the visually accepted color difference depends on both the color locus and the direction of the color difference. As is known, the tolerated color deviations of light and brilliant colors are numerically higher than those of achromatic dark ∗ of brilliant coloration is as much colors. The tolerated chroma difference ΔCab ∗ . as four times higher than the corresponding hue difference ΔHab ∗ In comparison to the formulas for ΔEab and ΔE99o , the modified color difference relations such as CMC(l:c), CIE94, and CIEDE2000 result from the assessment of color collections of different chromatic colorant and binder sorts. Consequently, each of these relations is to be applied to the corresponding material as follows: – CMC(2:1) for textile fibers, – CMC(1.3:1) for lacquers and plastic materials, – CIE94 for textile fibers, lacquers, and plastics, ∗ , ΔE – ΔEab 99o , CIEDE2000 for every known base material.
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It goes without saying that the mentioned difference expressions cannot be compared with one another in a direct manner. The corresponding transformations are different, nonlinear, and, furthermore, based on different color collections. The workability or efficiency of such an expression can be estimated by testing additional color patterns followed by a strict statistical evaluation of the results. From this point of view, the five color difference formulas mentioned above were tested with more than 3,600 additional color samples of small color differences [16, 23]. Each spectrometrically determined color difference was divided into its contributions ΔL, Δa, Δb and assigned to an ellipsoid of volume ΔVex ; see Section 4.3.4. Afterward, the visually perceived color differences were evaluated and assigned to a separate ellipsoid of volume ΔVvis . From all of the experimental and visual color differences, a statistical dimension value PF/3 results. This characteristic is an approximate measure of the absolute difference between the ellipsoid volumes: PF/3 ≈ |ΔVex − ΔVvis |.
(3.2.26)
For complete correspondence of the visual and measured color differences, one should expect PF/3 = 0. A value of PF/3 = 30, for example, indicates a statistical deviation between both investigations of about 30%. The results of the above-mentioned five formulas for small differences ∗ ≤ 2.5 correspond to the PF/3 list in the upper half of Table 3.4. From ΔEab these, the advantage of the CIEDE2000 difference equation is clear. This result suggests that the CIEDE2000 or at best the DIN99o color difference formula should be applied for the assessment of small color differences. However, the statistic quantity PF/3 does not indicate if there are systematic deviations in one or more quadrants of the color plane or not. Table 3.4 Effectiveness of color differences from color spaces and color appearance models with regard to the absolute statistical dimension value PF/3 [16, 26] Color collections of small color differences
PF/3 value
Color collections of high color differences
PF/3 value
CIEDE2000 DIN99o CMC(1:1) CIE94 CIELAB
33 35 38 38 52
CIELAB
26
CAM02-SCD CAM02-UCS CAM02-LCD CIECAM02
34 35 47 47
CAM02-LCD CAM02-UCS CIECAM02 CAM02-SCD
23 25 25 27
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161
The other statistical dimension values PF/3 in Table 3.4 each follow from a so-called color appearance model (CAM). The corresponding color difference formula directly contains the surrounding and observation conditions, which are of significance in the color industry and also in image processing. Such a model delivers values of color difference as well as color impression and, additionally, specific color characteristics [25, 26]. The CIE recommends the special model CAM02 for specific applications [27]. As input values, the standard color values X, Y, Z are applied to the test illuminant. With this formalism, three attributes are introduced. These differ in relation to the chromatic content: chroma C, colorfulness M, and saturation s. These color attributes together with lightness J and hue angle h can create three different spaces of color coordinates (J, aC , bC ), (J, aM , bM ), and (J, aS , bS ). The derived color space of color values J, aM , bM shows the most uniform results when tested with the color collection with small color differences as mentioned ∗ ≤ 2.5 and ΔE ∗ ≈ above and a second collection with large differences (ΔEab ab 10). The color collection of small color differences results in a value PF/3 = 47, which is slightly smaller than the corresponding CIELAB value PF/3 = 52; see Table 3.4. Based on CIECAM02, three further systems (CAM02-SCD, -LCD, and UCS) for visually small (SCD), large (LCD), and combined small and large (UCS) differences have been derived [26]. These three formalisms produced the other PF/3 values listed in Table 3.4. Considering these, the CAM02-UCS is suitable for evaluation of both small and large color differences. Because improvements in CAMs are still in progress, we avoid describing the extensive formalisms of the four mentioned models in this text and simply refer to the literature [26, 27]. All in all, the CIECAM02 enables one to determine the above-mentioned parameters and further characteristics such as the color rendering index of light sources, color inconstancy index, or index of metamerism. This CAM is suited for the three major fields in colorimetry, namely color specification, color difference evaluation, and prediction of color appearance. It remains to be seen, whether the CAM02-UCS formalism is really a universal CAM or not.
3.2.5 Color Tolerances The immense effort put into the search for the visually uniform color space follows from the decades-long insight that, roughly speaking, the color differences between absorption colors are of greater significance in color technology than the sign and absolute values of the accompanying color values. Color differences almost inevitably result in production or recipe prediction, among other things. An accurate colorimetry is, however, an essential requirement for arranging an acceptable color tolerance agreement between manufacturer and customer. In
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most cases, the color tolerance agreement is supplemented by further restrictions. In order to obtain an acceptable color tolerance for non-self-luminous colors, we have, in particular, taken into account the different error influences introduced by the three outer factors – light source, color sample, and observer – producing color impression. From the term color difference, we should differentiate between the smallest visually resolvable off shade and the magnitude of the allowed numerical color tolerance [24, 29–33]. For comparison of colors, inevitably, one must consider the sort of binder, surface structures, parameters of manufacture, application, or processing, etc. In addition, it is important to realize that the smallest visually resolvable off shade is non-uniform and color locus dependent: the smallest color difference is about ∗ = 0.3 for achromatic dark absorption colors and about ΔE ∗ = 0.7 for ΔEab ab brilliant green, yellow to red colors; see Table 3.5. In comparison, the short-term ∗ | ≤ 0.02 repetition accuracy of modern spectrophotometers is at least |ΔEab and is, therefore, more than 10 times better than the visual capacity to resolve off shade differences. For series production of coatings with plain lacquers, higher tolerance values compared to the smallest visually discernable color shades are usually applied. In the case of plain colorations of automotive finishes, for example, ∗ ≤ 0.9. The corresponding color tolerances are allowed in the range 0.3 ≤ ΔEab dependence on color locus is standardized [29] and is indicated in the chromaticity diagram of Fig. 3.9. Because the tolerance areas in the diagram are discontinuously separated from each other, it is useful to meet further requirements for the vicinity of the thresholds. A continuous transition between adjoining sectors is realistic (cf. Section 3.5.2). The color tolerances for paint refinishing are twice as high as series coating of automotives; see Table 3.6. Color tolerances for absorption colorants are by no means transferable to metallic or other effect colorations; this is clear by simply considering the angle-dependent color impression. For effect colors, the color tolerances ΔE(μ) should rather be arranged as they depend on the angle of illumination β and of observation μ. As shown in Table 3.6, the tolerance value is ΔED (μ) ≤ 1.0 for delivery and first paint coating; for paint refinishing, a range Table 3.5 Smallest visually perceivable and measurable color differences Coloration, measuring equipment Absorption colorants
Spectrophotometer
Criterion
Minimal color difference value
Smallest visually perceivable color difference Achromatic dark colors Brilliant yellow until orange-red colors
∗ ∼ 0.3 ΔEab = ∗ ∼ 0.7 ΔEab =
Short-term repeatability
∗ ≤ 0.02 ΔEab
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y
0.6
0.7
0.9
0.4
0.5 0.3
0.2
0
0
0.2
0.4
0.6
x
Fig. 3.9 CIE diagram for the 10◦ standard observer showing arbitrary chosen color areas of ∗ for automotive solid paints [29] different color tolerances ΔEab
Table 3.6 Standardized tolerance ranges according to DIN 6175 [29, 30] Kind of paint
Processing
Standard tolerance range
Plain paint
First paint coating Paint refinishing, low-bake paint
∗ ≤ 0.9 0.3 ≤ ΔEab ∗ ≤ 1.8 0.6 ≤ ΔEab
Metallic paint
Delivery and first paint coating Paint refinishing, low-bake paint
ΔED (μ) ≤ 1.0 1.5 ≤ ΔEP (μ) ≤ 3.0
of 1.5 ≤ ΔEp (μ) ≤ 3.0 is permitted. Both tolerance intervals are based on a relatively small number of color samples and, therefore, need additional requirements. Apart from the necessity of color tolerance requirements, it is essential that those involved in the evaluations continuously undertake coloristical and colorimetrical training [34]. Subjective color differences, which have repeated results greater than numerical ones due to insufficient coloristical training, are unsuited for tolerance agreement. Further considerations with regard to color tolerances and their detection are discussed in Sections 4.1.5 and 4.1.6.
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3.3 Color Constancy and Metamerism Color inconstancy and metamerism are color phenomena which are mainly depending on the constituent absorption colorants. These phenomena appear exclusively by illuminant change. Both properties are rarely avoided during manufacturing or matching of colors, but the degree that these appear can be characterized numerically by colorimetrical methods. For this, each of the already mentioned color difference equations is suitable, provided that special restrictions are considered. The resulting color inconstancy value is a measure of the appearance, how much the color impression of one and the same coloration changes due to change in illumination. The fundamental color physical processes are, in fact, only vaguely understood. They can, however, be phenomenologically evaluated with a color difference formula. In contrast to color inconstancy, metamerism is related to a pair of color patterns. Such a pair of same hue at one illumination shows a color change occurring with change of illumination. Also, the extent of this special kind of metamerism is expressed by an additional color difference value. The use of colorimetric methods in this context fundamentally simplifies the manufacture of colors with required high color constancy or low metamerism.
3.3.1 Chromatic Adaptation and Color Constancy Already in Section 2.4.2, we have become familiar with some perplexing phenomena of color perception which should be considered with regard to the assessment of colors. Two further properties of human color sense also belong to this group. These are termed chromatic adaptation and color constancy. The description of both effects in this section can now provide a clearer understanding of color inconstant colorations. Apart from the capability for distinguishing as many as 10 million colors, the human color sense has another astonishing ability: the sense of vision accommodates itself, within certain limits, continuously a previous change of illumination. The corresponding adjustment is generally called adaptation. The accommodation to the altered lighting condition needs a certain time interval. This adaptation phase is nearly independent of the preceding change of light, but – like also of the most other criteria of color perception – depends on the individual constitution and other conditions of the observer. Before any conclusive visual assessment of colors, one should, therefore, wait for a relatively long-time adaptation phase of at least 30 min. This amount of time is generally sufficient to overcome differences in individual delays. We differentiate between four kinds of adaptation: those of absolute sensitivity, discrimination threshold, visual acuity, and chromatic adaptation.
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165
The adaptation of absolute sensitivity occurs if the eye which had been sensitized to a constant illumination then registers a change of lightness. The transition from daylight vision to twilight vision is called dark adaptation; the opposite case is light adaptation. In the case of light adaptation, the visual sensitivity of the eye reduces with increasing luminance, whereas for dark adaptation, the sensitivity increases with lower illumination. Light adaptation takes place at photopic vision for luminance values higher than 10 cd/m2 , dark adaptation at scotopic vision for luminance lower than 0.01 cd/m2 . Both light and dark adaptation are caused exclusively by lightness changes of illumination and not by color differences of sources. Characteristic for adaptation of discrimination threshold is the fact that light adaptation needs shorter time than dark adaptation. Complete dark adaptation needs at least 30 min for the normal eye. In this case, the sensitivity is increased to 105 times that of the daylight sensitivity. The longer adaptation time for dark adaption comes down to the slower-acting rods in comparison to the cones. During light and dark adaptation, the diameter of the pupil changes; this is called adaptation of the visual acuity. The contraction of the pupil during light adaption increases the visual acuity and aberrations are simultaneously reduced. On the other hand, dark adaptation increases the diameter of the pupil and, therefore, the visual acuity worsens and aberrations become more noticeable. The chromatic adaptation is of special importance in our context of color assessment. This phenomenon takes place in photopic vision because the cones in the retina are capable of color vision only in this situation. It is a characteristic of this phenomenon that color sensation is kept nearly constant in spite of illumination change. The explanation for this is that in visual assessment also the illuminated surroundings are included which also change in the same way. The process of chromatic adaption can be divided into two steps: chromatic shift and adaptive shift. The chromatic shift occurs immediately, for example, by the change of a surrounding of daylight to that of a room with fluorescence lighting of illuminant FL 11. Immediately upon entering the room, all colors appear shifted somewhat reddish. This color shift is a consequence of the different spectral power distributions of natural daylight and artificial fluorescence light. During the “short” chromatic adaptation phase of some seconds, the perceived color shift disappears. This is partially a consequence of the effect that the most chromatic colored objects are in reality more or less color constant (see below). After chromatic adaption follows the adaptive shift. The exact process of this phase is not yet completely clear. It is, however, clear from observations that the perceived color impression is controlled by changes in the retina together with the color memory of the observer. In other words, the spectral differences of the sources are nearly balanced by a shift of the spectral sensitivity of the eye. Simultaneously, the perceived color is unconsciously compared to color
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impressions of similar color surroundings stored in the memory. The complete processes of chromatic adaptation needs, as mentioned above, a total time of about 30 min. The phenomenon of color constancy is closely associated with the chromatic shift. A color is considered color constant if it always produces the same color impression, independent of spectrally different illuminations. There is a comparable term, lightness constancy. This term characterizes the situation where the assessment of lightness is nearly independent of the energy level of the source. In reality, this judgment is based on a comparison of diffuse reflecting surfaces. A white sheet of paper is always perceived as white despite light changes, although the color stimulus caused by the sheet is different. It seems that the brain is trained to see colors as if they are always illuminated by white light. But color stimulus is – as discussed in Section 2.4.3 – dependent on the spectral power distribution of the light source. Color constancy is, therefore, an essential reason to characterize colors, color differences, and color appearances by applicable dimensional values rather than simply leaving it entirely up to individual visual judgment. In addition to color constant colorations, there exist a whole host of chromatic absorption colors which change considerably their color under varying illuminants (except monochromatic light sources). Such colors are called color inconstant. A quite unsettling example is a color of reddish hue in daylight which appears greenish under fluorescent illumination. Colors in applications which are subject to frequent illumination changes, therefore, should be generally of low color inconstancy. Dependent on the application field, new colors should be tested with regard to this property. The necessary approach for such tests is described in the next section.
3.3.2 Index of Color Inconstancy A high color constancy is by no means an unusual quality criterion. Safety colors, for example, must always be recognizable as such in daylight, twilight, and night light. Colors of consumer items should also certainly not change under an illumination change. The determination of color inconstancy under a test illuminant is carried out with regard to a reference illuminant, normally D65. The degree of color change, which a single color shows for both illuminants, is given by the index of color inconstancy CIC . Initially, it seems self-evident that the color inconstancy index should be identified as the color difference which appears between both illuminants. Detailed studies show, however, that the change of the corresponding color values is not suitable for an adequate description of color inconstancy. It is particularly important to know the relationship between the color values for colors which look precisely the same to an observer when they are adapted
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167
to different illuminants. Such kinds of colors are called corresponding colors. Given color values R, G, B of a color sample under one illuminant, the color values RC , GC , BC for the corresponding color under another illuminant can be determined by calculation. The second illuminant is the so-called corresponding illuminant. The calculation of the corresponding color values is achieved by a chromatic adaptation transform (CAT). The numerical color difference ΔE between the color values of the corresponding color and the color under the original illuminant is an adequate measure for the degree of color inconstancy CCI (ΔE) = ΔE. For determination of the color values of the corresponding color, von Kries assumed that the three color receptors in the retina are differently affected by chromatic adaptation [35]. Accordingly, chromatic adaptation causes a reduction in sensitivity by constant factors for each of the three cones. The magnitude of each of the corresponding coefficients α, β, γ depends on the stimulus to which the observer is adapted. The von Kries coefficient law can be written as Rc = α · R, Gc = β · G, Bc = γ · B.
(3.3.1)
This law describes the transformation of the cone responses due to chromatic adaptation. Most of the various CATs developed have been founded on the von Kries law (3.3.1). The specific CAT to be used for absorption colors is CAT02. It was improved with a recent color collection of representative absorption colorations in 2002 and forms the basis of the sketched color appearance model CIECAM02 [36, 37]. The relevant transformation equations are given in Appendix A.2. The calculation of the color inconstancy index of a given color using CAT02 is performed in several steps. The input data are the standard color values of the sample, X, Y, Z, in the test illuminant and, XR , YR , ZR , in the reference illuminant. From these, the standard color values Xc , Yc , Zc of the corresponding illuminant are determined. The numerical degree of adaptation of the observer is also included in the process. Finally, the color difference ΔE is calculated with the triplets Xc , Yc , Zc and XR , YR , ZR . From the differences of the three color value pairs, the amount and the direction of the color shift can be seen. A value of CIC (ΔE) = 0 represents a completely color constant coloration for the chosen reference and test illuminant. The application of CAT02 is only for absorption colorants because the corresponding parameters and transformation relations were derived from the above-mentioned color collection. It is advantageous that the value CIC (ΔE) can be calculated in advance for every illuminant change without actually implementing the corresponding lighting. For clearness and comparability, along with the value of the color inconstancy index, the reference and test illuminants, the
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standard observer, the degree of adaption, the observation conditions, and the used color difference equation should also be indicated. As an example, we consider the color values of the reference colors given in Table 3.7. The standard color values X, Y, Z and L∗ , a∗ , b∗ belong to the illuminant/observer combinations D65/10◦ and A/10◦ . In the calculation, the field of the reference and sample is assumed to have a luminance of LA = 200 cd/m2 and presuppose normal observation conditions. In Table 3.8, the corresponding standard color values for the corresponding test illuminant Ac using CAT02 are listed. In the last column, the resulting quantities of the index of color inconstancy for three different color difference formulas are given. The first color sample has values between 6.27 and 6.72 and the second between 2.11 and 2.61. The second color is, therefore, much more color constant than the first. From the difference between the color values, one can estimate the direction and the amount of the color shift. In the special case of the chosen examples, the color inconstancy index is nearly independent of the used color difference formula – which is not typical for other absorption colors.
Table 3.7 Examples of starting values for determination of color inconstancy index in Table 3.8; 10◦ standard observer Sample number
Illuminants 10◦ observer
X
Y
Z
L∗
a∗
b∗
1
D65 A
20.51 24.08
24.09 22.91
26.14 8.99
56.18 54.98
–10.96 –5.64
–0.45 –4.51
2
D65 A
20.29 22.48
23.91 22.74
25.47 8.54
56.00 54.80
–11.26 –11.69
0.30 –2.66
Table 3.8 Color inconstancy index for combinations of reference/test illuminants of Table 3.7 [37] Reference/test illuminant corresponding Sample color; 10◦ observer 1 2
D65/Ac D65/Ac
Normal observation conditions
Color inconstancy index CIC (ΔE)
X
Y
Z
∗ ΔEab
ΔE(CMC1:1) ΔE00(1:1:1)
20.51 20.88
24.09 23.20
26.14 27.30
6.72
6.27
6.56
20.29 19.35
23.91 23.13
25.47 25.95
2.61
2.48
2.11
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Color Constancy and Metamerism
169
3.3.3 Kinds of Metamerism The color property called metamerism is rather undesirable in many areas of color technology; it is, however, in many cases unavoidable. According to Ostwald [38], two colors are called metameric to each other (conditional equal), if they match for one illuminant but show a color difference under a change of illuminant. The metameric behavior is a consequence of additive color mixture of human color sense. It should be pointed out that color inconstancy is a property of one color, whereas metamerism is a property of the comparison of two colors. This effect is of particular importance, for example, in the production of colors in different charges, substitution of one or more colorants in recipes, or recipe prediction of a given color of unknown colorant composition. The degree of metamerism is – apart from color inconstancy and further properties – often the decisive factor for the choice of a desired coloration or suited color recipes among several alternative formulations. As an example, Fig. 3.10 shows the spectral reflectance of a pair of metameric colors which are perceived as nearly equal at midday light. The curve with a relative low maximum at λ = 510 nm for the sample color repeatedly intersects the curve of the reference color. Metameric pairs show generally one further characteristic: the spectral curves have at least three intersection points at different wavelengths in the visible range [20, 39, 40]. If there were fewer intersection points, either the lightness or the hue of the colors under reference illumination do not match. R(λ) R1(λ) 0.3 R2(λ) 0.2
0.1
0
400
500
600
Fig. 3.10 Spectral reflectance R1 (λ), R2 (λ) of a pair of metameric colors
700
λ nm
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The occurrence of at least three intersections touches the heart of the methods of color recipe prediction. More than a hundred years of collective experience shows that to match a color of unknown composition requires at least three different colorants. In the simplest case, the accompanying colorant concentrations follow from the condition that the spectral curves of the recipe and reference color intersect for exactly three different wavelengths. Nearly equal spectral curves can only be achieved with greater number of colorations. A completely congruent pair of curves is only obtained with identical colorants and concentrations (Sections 6.3.3, 6.3.4, and 6.3.5). The spectral values of the color pair are only one factor for producing metamerism. The second is the spectral power distribution of the illuminant used. Both are combined in the color stimulus function Φ(λi ) which is interpreted as the original cause of the appearance of metamerism. The combination of this function and the chosen standard observer can lead – despite different spectral values – to equal standard color values X1 = X2 , Y1 = Y2 , Z1 = Z2 for the metameric color pair. For example, with the spectral reflectance R1 (λi ) and R2 (λi ) of each color, the spectral power distribution S(λi ) of the reference illuminant and, for simplified notation, the 2◦ standard observer follows from Equation (3.1.1): X1 = k
N
S(λi )¯x(λi )R1 (λi )Δλ
(3.3.2)
S(λi )¯x(λi )R2 (λi )Δλ.
(3.3.3)
i=1
and X2 = k
N i=1
Although the reflectance values of both colors are unequal at most wavelengths and the individual summands in Equations (3.3.2) and (3.3.3) to the same wavelength are mostly different: for metameric color pairs, equal totals always result and, therefore, identical standard color values X1 = X2 for the reference illuminant. The same holds for the remaining two color values. The existence of equal standard color values, here X1 = X2 , Y1 = Y2 , Z1 = Z2 , signifies always equal color sensation. Because of this, both colors produce the same color impression. The same holds for additional color values, especially of CIELAB or DIN99o color spaces. If the reference illuminant is substituted by another one of new spectral power distribution S0 (λi ), then the individual summands and totals of Equations (3.3.2) and (3.3.3) are different. The summands show now other weighting factors in comparison to those in the reference illuminant. Even all three color values differ, therefore, from one another, the change of illuminant results in two different color impressions.
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Color Constancy and Metamerism
171
The individual contributions of different power distributions S(λ) in dependence of wavelength have already been seen, for example, from Fig. 2.4 for standard illuminants D65 and A. In the range of blue wavelengths, the distribution of D65 is essentially higher than A. In contrast, in the red range, the radiation intensity of A dominates compared to that of D65. Because unequal color values mean different color sensations, metameric pairs typically produce a color difference for a change of illuminant. Although the concept of metamerism was originally introduced by Ostwald for illuminant changes, it has also been extended to include states without illuminant changes. These are more accurately denoted as “conditional equal prerequisites”. Five metamerism kinds are known to this day. In the following survey, the first and second metamerism kinds are directly influenced by the different summand contributions. The last three are caused by the individual conditions of the observer and the measuring equipment used: 1. Illumination metamerism occurs under change of illuminant as described above; this is the most important sort of metamerism. 2. Observer geometry metamerism results from change between the 2◦ and 10◦ standard observers on the basis of the different CMFs x¯ (λi ), y¯ (λi ), z¯(λi ) and x¯ 10 (λi ), y¯ 10 (λi ), z¯10 (λi ), respectively. The consequences are by no means negligible, as is shown in the next section. 3. Observer metamerism is caused by the subjective color sense of different observers and the individual deviations from the underlying standard observer. Such deviations should be clarified between the involved partners in advance of the color tolerance agreement. 4. Geometry metamerism can occur under otherwise equal conditions and equal visual angle by a change in the line of sight. For effect pigments, for example, the color match by change of the angle of illumination or observation can be lost. A special case of geometry metamerism is the so-called silking effect. This effect means that the reflectance changes simply by rotation of an individual sample around an axis perpendicular to its surface. This phenomenon is caused by the nearly parallel needle-, flake-, or rod-shaped pigment particles. 5. Equipment metamerism can be considered due to the general lack of consistency among color measuring instruments of the same or different manufacturers. The variations in measured values are primarily caused by small but largely unavoidable production differences of the component parts or the equipment design. Illumination metamerism is, as already mentioned, practically unavoidable. It occurs during reproduction of a reference color of unknown composition by applying colorants of different batches, other colorants, binders, additives, and a different number of colored components. The chemical analysis is much
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too complex and priority is generally given to the use of available colorants. There should also be sufficient experience related to color inconstancy, color strength, color fastness, compatibility – only to list some of relevant criteria for reproduction of absorption colors. From each sketched type of metamerism above, an indication for its reduction is at the same time revealed. For lowering illumination metamerism, one can carry out a careful selection and tuning of the colorants during visual or recipe prediction. For a recipe with absorption colors, at minimum three and at best six different colorants should be used. This optimum comes because with increasing number, the risk of an “overshoot” instead of an approach of the spectral values is greater. Because of the substantially lower concentrations of the additional colorants relative to the already dominant ones, a minor admixture is often difficult to meter out or to homogenize. A reproduced color often shows an increased metamerism if for the dominant colorant the coloristical “most natural” one is chosen. To achieve recipes with minimal metamerism, each step of the spectral curve trace should be approached with a separate colorant (cf. Figs. 6.15 and 6.16). This aim in most cases, however, is not achieved with the “first best” colorant. The curve trace of the maximum as well as the rise and slope at the start or end of a curve step should be approximated as well as possible. This goes especially for violet, yellow, orange, or red and brown colors which show increased spectral values at wavelengths longer than 500 nm. For blue and green hues, however, the position of the maximum and the slope are well approximated by only few colorant components. One strategy of recipe prediction is based on the criteria that the color difference between the reproducing color and the target color is minimal for a given reference illuminant. This color difference can be calculated in advance without the necessity of implementing the corresponding recipe. A similar consideration holds for the color inconstancy index. It can be determined in advance for every change of illumination without the need of actually performing the lighting change. As a reference illuminant in both cases, D65 is mostly used, although other illuminants are possible. This strategy allows for the possibility of changing the types and numbers of colorants for a recipe in order to pursue the desired effect on the degree of metamerism. The amount of illumination or geometry observer metamerism is characterized by the index of metamerism. This is discussed in the next section.
3.3.4 Special Metamerism Indices The degree of metamerism of a color pair is indicated by the so-called special metamerism index for change of illumination. This index corresponds to the color difference which results from the change between reference and test illuminant for the given color pair [40]. The choice of the color difference formula
3.3
Color Constancy and Metamerism
173
is an option. In the cases of the CIELAB expressions (3.1.18) or (3.1.23), the color contributions are determined from equations ΔL∗ = LT∗ − LR∗ ,
Δa∗ = a∗T − a∗R ,
Δb∗ = b∗T − b∗R
(3.3.4)
or additionally from ∗ ∗ ∗ ΔCab = Cab,T − Cab,R ,
(3.3.5)
a∗R b∗T − a∗T b∗R ∗ . ΔHab = ∗ C∗ ∗ ∗ ∗ ∗ 0.5(Cab,T ab,R + aT aR + bT bR )
(3.3.6)
The indices T and R belong to the test and reference illuminant, respectively. In most cases, D65 is arranged as the reference illuminant and the test illuminant should greatly differ from the reference. The index of metamerism MXilm needs to be determined for approximate illuminants in which the color pairs are subjected to during application. The degree of metamerism remains unchanged under the exchange of the reference and test illuminants, which is a consequence of the squared color contributions (3.3.4), (3.3.5), and (3.3.6) in a color difference equation. The visually perceived and the numeric color differences can definitely be different because, as already explained, the stored values of the spectral power distribution of the illuminants and the standard observers are not identical with those of the sources used or the individual observer. For a clear interpretation and comparability of the metamerism index for illumination change MXilm , in addition to the numerical value, the following must also be specified in the result: the test and reference illuminants, the standard observer, and the color difference formula used. According to a recommendation of the CIE, the special metamerism index for change of observer can also be calculated under the same illuminant [41]. This is the analog of determining the color contributions (3.3.4), (3.3.5), and (3.3.6) of the CMFs of a test person with regard to one standard observer under the same illuminant. Also in this case, the calculated numerical value of the index MX 0 obs can deviate from that for another observer. For correct determination of the special index of metamerism, a peculiarity needs to be considered. In a number of cases, the standard color values of the color pair are not exactly the same as for the reference illuminant, that is, X1 = X2 , Y1 = Y2 , Z1 = Z2 . In such cases, the standard color values X2,T , Y2,T , Z2,T of the sample in the test illuminant need to be corrected using the respective factors: fX = X1 X2 , fY = Y1 Y2 , fZ = Z1 Z2 .
(3.3.7)
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Otherwise, incorrect metamerism values result. The color difference is, therefore, determined between the color values X1 , Y1 , Z1 of the reference illuminant and Y2 = fY Y2,T , Z2 = fZ Z2,T X2 = fX X2,T ,
(3.3.8)
for test illuminant. As an example, in order to determine the special indices for change in illuminant and observer geometry, we use the color pair of reflectance shown in Fig. 3.10. The accompanying standard and CIELAB color values for the combinations D65/10◦ and FL 2/10◦ as well as D65/2◦ and FL 2/2◦ are listed in Table 3.9. The standard color values of the test illuminant are to be corrected using Equation (3.3.8) because the X, Y, Z or L∗ , a∗ , b∗ values already differ for reference illuminant. The resulting special indices of metamerism for change of illuminant MXilm ∗ , are given in Table 3.10. In and MX 0 obs , each based on color difference ΔEab the second row of this table, the respectively used combinations which follow from Table 3.9 are indicated. The description 6 (1/5), for example, means that the color values of number 6 are multiplied by the ratio of the corresponding color values in lines 1 and 5. The results in the last two rows in Table 3.10 show that the index of metamerism for illuminant change is typically higher than that for the change of observer geometry. From comparison of the CIELAB values for reference and test illuminants for the same observer in Table 3.9, it should be clear that metamerism is here mainly caused by differing red to green amounts Δa∗ between both colors. The combinations 1, 6 with 2, 5 as well as 3, 8 with 4, 7 in Table 3.9 are equivalent because test and reference illuminants are exchanged with each other. The same holds for the change of standard observer with regard to the combinations 1, 7 with 3, 5 as well as 2, 8 with 4, 6. The slight deviations of the corresponding index values are caused by measuring and rounding errors. Table 3.9 CIE 1931 and 1976 standardized values of the metameric color pair in Fig. 3.10
No.
Illuminant/standard observer
X
Y
Z
L∗
a∗
b∗
1 2 3 4
Reference
D65/10◦ FL 2/10◦ D65/2◦ FL 2/2◦
16.862 19.096 17.444 18.753
13.577 15.210 14.068 15.491
7.356 4.735 7.473 4.637
43.62 45.92 44.33 46.30
24.20 17.95 24.10 18.44
20.94 24.89 22.13 25.46
5 6 7 8
Test
D65/10◦ FL 2/10◦ D65/2◦ FL 2/2◦
16.573 17.390 17.305 17.232
13.536 13.680 13.894 13.804
7.140 4.543 7.345 4.486
43.56 43.77 44.08 43.95
22.84 18.47 24.42 20.59
21.63 22.30 22.17 22.31
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Specific Qualities of Colorants
175
Table 3.10 Indices of illumination and observer-geometry metamerism following from color values in Table 3.9 Kind of metamerism Illumination metamerism
Observergeometry metamerism
Number in Color Table 3.9 pattern
Illuminant/ standard observer
1 6 (1/5) 3 8 (3/7) 2 5 (2/6) 4 7 (4/8)
Reference Test Reference Test Reference Test Reference Test
D65/10◦ FL 2/10◦ D65/2◦ FL 2/2◦ FL 2/10◦ D65/10◦ FL 2/2◦ D65/2◦
1 7 (1/5) 2 8 (2/6) 3 5 (3/7) 4 6 (4/8)
Reference Test Reference Test Reference Test Reference Test
D65/10◦ D65/2◦ FL 2/10◦ FL 2/2◦ D65/2◦ D65/10◦ FL 2/2◦ FL 2/10◦
Special metamerism index ∗ MXilm = ΔEab
∗ MX 0 obs = ΔEab
4.65 3.84 4.57 3.94 1.77 2.19 1.75 2.18
In this section, it has been shown that two essential properties of absorption colors can be approximately described and numerically compared by colorimetrical methods using color difference formulas. The following sections deal with further colorimetrical procedures, which have been developed especially for numerically characterizing other qualities of absorption colors.
3.4 Specific Qualities of Colorants The color spaces CIE 1976 and DIN99o described as well as the color difference formulas – which were, in particular, intended for the assessment of collections with absorption colors – are designed for application to additional color properties. In the following, quantities such as color strength, spreading rate, covering capacity, transparency, or color fastness of formulations with regard to colorimetric characterization are discussed. Such properties are united under the term color qualities. With these accounts, the fact that the whole of colorimetric methods are only valid for small color differences needs to be considered. In order to have reasonable comparability of results, the same color space and chosen color difference formula should be maintained throughout.
176
3
Standardized Tristimulus Values, Color Qualities, Chroma of Effect Pigments
3.4.1 Build-up and Coloring Potential All colorants can be dispersed in different concentrations in a dye or binder dependent on the desired color. The change of the color values of a single colorant in dependence on concentration is called build-up. This behavior needs to be differentiated with regard to a dye in the same solvent and a colored absorption pigment in white mixtures for constant total pigment loading in the same binder. In the case of a chromatic absorption pigment in white/black mixtures, the dependence of lightness and chroma on the concentration of all three colorants is given by the so-called coloring potential. The build-up is graphically represented by a three-dimensional curve section in a color space. In comparison, the coloring potential is represented by a three-dimensional area in color space. Its shape depends on the concentration of the chromatic pigment in white/black mixtures. From the geometrical representation of the build-up and coloring potential, characteristic features of the corresponding colorants can be obtained. These are discussed in the following. Figure 3.11 shows the projection of the build-up of different dyes in solution in an a∗ , b∗ color plane. The simultaneous change in lightness here is of secondary importance. From this simplified representation, the color development in dependence of dye content directly follows. Each curve starts for b∗ 1 2
80 60
3 40 20
4
0 7 –20 –40
–40
5
6 –20
0
20
40
a∗
Fig. 3.11 Typical build-up of different dyes: 1 light-yellow, 2 yellow, 3 orange, 4 red, 5 blue, 6 dark-blue, 7 blue-green
3.4
Specific Qualities of Colorants
177
minor dye concentration in the immediate vicinity of the achromatic locus. It ends with the coordinates of the mass tone, which is the natural color of the absorption colorant. At first, the chroma changes directly proportional to the dye content. But at certain high dye concentrations, a particularly noticeable change in hue occurs and the chroma lowers. The build-up describes, dependent on color locus, a left-hand or right-hand turn. The amount of the hue angle |hab | changes as shown between about 20◦ and 60◦ . Chromatic pigments in white mixtures show similar shaped projected buildups such as dyes in solution. However, it has not been clarified as to why a build-up describes systematically a right or left-hand curve in dependence on the quadrant of a color plane. For visualization of a coloring potential, Fig. 3.12 shows the change in ∗ of an organic colored pigment. The lightness L∗ dependent on chroma Cab parameters P/W and P/B indicate the blending ratio of pigment to white and black colorants, respectively, at constant pigment loading. On the envelope curve, three points P, W, and B are plotted. These represent the mass tone of the colored, white, and black pigments, respectively. The intermediately located curve sections have the following meaning: – The section from point W to point P represents the build-up of the colored ∗ plane. It extends from the pigment in white mixtures projected in the L∗ , Cab L∗ W 10P/90W 75 50P/50W
1B/99W 50 3B/97W
P
25 B
99P/1B 95P/3B
0 0
25
50
75
C ∗ab
Fig. 3.12 Coloring potential of an organic absorption pigment in white and black mixtures of constant pigmentation
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3
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mass tone of white to the mass tone of the colored pigment. The downward curved slope of this section shows the decrease in lightness with increasing chromatic pigment content, as well as the simultaneous reduction of chroma. This is an analogous behavior to dyes, Fig. 3.11. – The curve element from P to B represents the color loci for mixtures of the colored pigment and the achromatic black pigment. – The last section of the envelope curve WB is a part of the lightness axis L∗ , representing achromatic mixtures between the mass tone of the white and black colorants without a colored pigment. The area enclosed by these three curve sections represents the coloring potential of an absorption pigment. In other words, the coloring potential forms a curved three-dimensional area in color space similar to a blade of a marine propeller. This area is flat in the surroundings of the lightness axes. The coloring potential includes, therefore, all color loci which can be entirely generated with a given chromatic pigment and white/black mixtures for fixed total pigment loading. The coloring potential is an additional fingerprint of a colored pigment. As can be seen in Fig. 3.12, the distances between the plotted points on curve sections WP, PB, and BW change non-uniformly with regard to the indicated mixing ratio values. This behavior signifies that the lightness, chroma, and hue of the colorant change nonlinearly in dependence on concentration. This nonlinearity is typical for all absorption colorants but, moreover, it develops differently. Altogether, this characteristic complicates the entire color physical and coloristical handling of all colorant sorts. It forces, for example, one to carry out the dosing or weighing of colorants with the upmost care and accuracy and to perform all manufacturing steps with greatest possible reproducibility. Recipe prediction needs, therefore, nonlinear approximation methods. Generally, the chroma, hue, and lightness respond considerably more sensibly to a fraction of black than white of same amount. This behavior can already be inferred for merely 1 part black from Fig. 3.12. The combination 99P/1B ∗ = 75 by about reduces the chroma of the color-intensive mass tone in P of Cab ∗ ∗ ΔCab = −34. The ratio 1B/99W decreases the lightness L = 92 in W for the mass tone of white, however, by about ΔL∗ = –25. Dark chromatic colorants such as violet or blue behave in a similar manner. This most striking nonlinearity turns out to have a particularly detrimental effect on the assessment, manufacture, and reproduction of colors. The strong change of color for a small fraction of a dark colorant is related to the sensitivity and correctability of color recipes. In comparison to organic colorants, inorganic pigments typically show a less developed coloring potential. This is a result of the characteristically higher scattering and lower chroma of the mass tone of these sort of colorants. For inorganic pigments, the arched curve sections in Fig. 3.12 turn into nearly rectilinear line segments of only slight curvature. The nonlinearity of inorganic pigments,
3.4
Specific Qualities of Colorants
179
in dependence on concentration, is in general similarly strongly developed as for organic pigments. The term coloring potential – in its original meaning – does not apply to effect pigments. This is because for these colorants, the angle-dependent color impression is of primary interest. Slight amounts of carbon black in formulations with effect pigments serve principally to absorb the complementary color of interference pigments, reduce chroma, and occasionally for correction of lightness flop. The natural interference colors of interference pigments emerge more clearly with only a minimal amount of carbon black. A borderline case is represented by mixtures of interference and colored pigments. With such mixtures, a new type of build-up in comparison to that of absorption colorants is combined (Section 3.5.4).
3.4.2 Strength and Depth of Color The concepts strength of color and depth of color are closely linked and are of coloristical as well as economic significance. Both distinguishing features were already established at the beginning of the 20th century for assessment of dyes and in 1930 began to be applied to absorption pigments. Whereas the coloration potential and build-up describe the development of a color in dependence on colorant concentration, the strength and depth of color characterize the coloring efficiency of a colorant. Color strength is defined as that property of a colorant, which acts by coloring upon other materials [42]. In contrast, color depth describes that feature of a colorant, which produces a more intense coloration or rather higher chroma with increasing concentration. It increases, therefore, up to the saturation of the colorant but decreases with rising lightness. The color depth correlates consequently with the color build-up. It is important to point out that color strength is a relative quantity. The color strength of an absorption colorant is a quantity in relation to another (similar) absorption colorant. In Fig. 3.13, the depth of color D for a pair of similar colorants in dependence on concentration c is plotted. For small and moderate values of c, the depth of color D changes linearly for the reference and sample colorant. At higher concentrations, the so-called saturation depth of the reference DS,R and sample colorant DS,S is attained. These depths are not necessary at the same level. The two straight lines through the origin have different slopes. The slope, however, is directly proportional to color strength. From this plot, it can be inferred that the color strength of the sample is related to the same level of color depth DSD as that of the reference color. Apart from a constant k, the slope of the straight line through the origin for moderate concentrations is a direct measure for the color strength P of a colorant. Using the notation in Fig. 3.13, the general equation of a straight line through the origin is
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Reference
DS,R DS,S Depth of color D
Sample
DSD = const.
0 0
cR
cS
Concentration c
Fig. 3.13 Schematic representation of color depth D in dependence on concentration c of a pair of similar absorption colorants
D = k · P · c,
(3.4.1)
where P is the absolute color strength. However, it should be noted that it is the relative color strength rather than the absolute that is relevant in practice. Under the condition of equal color depth level DSD for the sample and reference colorants, the relations DSD = kPS cS ,
(3.4.2)
DSD = kPR cR ,
(3.4.3)
follow. If the ratio of PS and PR is defined as the degree of relative color strength Prp of an absorption pigment, it follows that Prp =
PS cR = . PR cS
(3.4.4)
The relative color strength of an absorption pigment follows consequently from the quotient of the concentration cR of the reference pigment to the concentration cS of the sample pigment at equal color depth level DSD . The quantities Prp and D are dimensionless. In the case shown in Fig. 3.13, the initial slope of the reference colorant is twice that of the slope of the sample colorant. Following the definition in Equation (3.4.4), the sample pigment has a color strength of 1/2 related to the reference pigment, and consequently half that of the reference. On the other hand, both pigments are only at equal color depth if the condition cS = 2cR is met. Procedures for determining equal level DSD are described below.
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Specific Qualities of Colorants
181
For dyes in solution, the same considerations hold, but with the difference that the relative color strength Prd is then determined from the quotient of the extinction coefficients εS and εR at the absorption maximums of the reference and sample dyes Prd =
εS εR
(3.4.5)
at equal level of DSD [43]. The determination of relative color strength for pigments follows from brightening mixtures with a white pigment [42]. Instead of the concentration ratio, the mass ratio mR /mS of the reference and sample pigments is now inserted into Equation (3.4.4). First of all, the weighed portion mR is chosen so that the previously fixed color strength level DSD is achieved. At this step, it is necessary to pay attention to insure that the weight fraction of the white pigment mW is the same in the mixture of reference and sample pigments. Afterward the mass mS of the sample pigment is altered as long as both mixtures show nearly no difference with regard to the previously chosen adjustment criterion FAC , so ΔFAC ∼ = 0 (see below). If these conditions are fulfilled, the relative color strength Prp of the sample pigment follows from relation Prp =
mR mS
(3.4.6)
for secondary conditions: DSD = const., mW = const., and ΔFAC ∼ = 0. In addition to the value of relative color strength Prp , it is always necessary to indicate the reference colorant, the level SD of color depth, the sort of white pigment, respectively solvent, as well as the accompanying fraction, and the chosen matching criterion FAC . For comparability of the resulting relative color strength values with those of other colorants, the so-called standard color depth (SD) first for dyes and later geared to pigments was established. The standardized SDs for textile dyes are denoted as 1/25 SD, 1/12 SD, 1/6 SD, 1/3 SD, 1/1 SD, and 2/1 SD. For pigments, there are four standard depths: 1/25 SD, 1/9 SD, 1/3 SD, and 1/1 SD [44]. The production and testing of standard deep colors are described in [45]. Above and beyond the mentioned parameters DSD = const., mW = const., and ΔFAC ∼ = 0, it needs to be considered that the color strength of pigments additionally depends on the chosen reference pigment, the mean particle size, the sort and concentration of the white pigment, and a possible added black pigment. For dyes, the relations are simpler because only the reference dye, the solvent, and the concentration need to be indicated in addition to the chosen standard color depth and matching criteria. For absorption colorants, various effective matching criteria FAC exist. The perhaps obvious idea of using the visual assessment for determination of color
182
3
Standardized Tristimulus Values, Color Qualities, Chroma of Effect Pigments
strength certainly must be ruled out. In particular, this approach is overtaxed if similar reflection or transmission spectra are present. The color matching needs to be carried out exclusively with measuring methods. Some widespread criteria founded on either spectral or colorimetrical quantities follow. The spectral-matching criteria are based on the term Kubelka–Munk function F(λ) = K(λ)/S(λ). It corresponds to the ratio of the absorption and scattering coefficient K(λ) and S(λ), respectively, in dependence on the wavelength λ, cf. Equation (5.3.14). Both coefficients have to be known with regard to the sample and reference colorants at the same wavelength. This quotient is, however, useless if the scattering coefficient tends to zero – especially for highly transparent or dark colorants. In such cases, it is necessary to switch to other criteria. The four most commonly used spectral-matching criteria are as follows: 1. The difference of the Kubelka–Munk functions between the sample and the reference colorant FS , FR , respectively, each at the accompanying wavelength λmax,R of the function maximum of the reference colorant: ΔFmax, R = FS (λmax, R ) − FR (λmax, R ) ∼ = 0.
(3.4.7)
2. The difference of the reflectance between the sample and the reference colorant, each at the accompanying wavelength λmin,R of the reflection minimum of the reference colorant: ΔRmin, R = RS (λmin, R ) − RR (λmin, R ) ∼ = 0;
(3.4.8)
this criterion is equivalent to the previous one. 3. The minimum of the sum, which results from the weighted differences of the Kubelka–Munk function values between sample and reference colorant, each determined at i = 1, 2, . . . , N measured wavelengths λi : N i=1
ΔFi =
N
αi [FS (λi ) − FR (λi )] ≡ minimum;
(3.4.9)
i=1
the weighting factors α i correspond to the sum of the CMFs αi = x¯ (λi ) + y¯ (λi ) + z¯(λi )
(3.4.10)
for the chosen 2◦ or 10◦ standard observer; this criterion leads to unsatisfactory results if the summands in Equation (3.4.9) are simultaneously of high and low values. In this case, it is opportune to apply the next criterion. 4. The minimum of the sum which follows from the squared deviation of the Kubelka–Munk function of the sample and reference colorant at N measured wavelengths λi
3.4
Specific Qualities of Colorants N i=1
(ΔFi ) = 2
N
183
[FS (λi ) − FR (λi )]2 ≡ minimum,
(3.4.11)
i=1
probably with other weighting factors as in the third criterion. The spectrophotometric matching of the sample to the reference colorant should certainly be performed with the same illuminant, standard observer, and spectrophotometer for each. These conditions need to be indicated along with the value of the relative color strength in addition to the employed reference colorant. Relative color strengths are only to be compared with each other if the same reference colorant and the mentioned three conditions had been used. For colorimetrical-matching criteria, one should alternatively take into consideration: 1. One of the differences ΔX = XS – XR , or ΔY = YS – YR , or ΔZ = ZS – ZR between the standard color values of the sample XS , YS , ZS and reference XR , YR , ZR , which contains the smallest value min (XR , YR , ZR ) of the reference colorant: ⎧ ⎫ ⎨ ΔX if XR = min(XR , YR , ZR ) ⎬ ΔY if YR = min(XR , YR , ZR ) ∼ (3.4.12) = 0. ⎩ ⎭ ΔZ if ZR = min(XR , YR , ZR ) 2. The difference of the standard color values YS , YR or lightness values LS , LR of the sample and reference colorant ΔY = |YS − YR | ∼ =0
(3.4.13)
ΔL = |LS − LR | ∼ = 0.
(3.4.14)
or
3. The smallest color difference ΔE with regard to the sample and reference colorant ΔE ≡ minimum;
(3.4.15)
the color difference formula is optional. 4. The depth of color Di at standard color depth SD; this matching method should be applied to dyes as well as pigments.
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There exist empirical formulas, especially for matching of color strength with pigments. We restrict ourselves to these in the following discussion. Historically, these have been found in a similar manner as for dyes. A relation in widespread use is given by ΔDi =
√ Y[s · ai (ϕ) − 10] + bi ∼ = 0.
(3.4.16)
The quantities in this expression are as follows: ΔDi : difference in depth of color for standard color depth level i; i: level of standard color depth, one of 1/1 SD to 1/25 SD as mentioned above; Y: standard color value of the CIE 1931 system, a measure for lightness; s: measure of saturation, it corresponds to 10 times the distance in the CIE chromaticity diagram between color locus of the sample pigment (x, y) and the achromatic locus (xn , yn ) s = 10 ·
(x − xn )2 + (y − yn )2
(3.4.17)
for the chosen illuminant and standard observer, cf. Table 3.2 and Color plate 2; ai (ϕ): empirical function for weighing of s; it depends on hue angle ϕ = arctan [(y − yn )/(x − xn )] and the chosen level i of standard depth SD; empirically determined constant corresponding to the level i; it takes bi : values of b1/3 = 29, b1/9 = 41, b1/25 = 56. The added mass of the sample pigment mk+1 on the kth iteration step, k = 1, 2, 3, . . . , follows from the additional empirical relation mk+1 = mk · 0.9ΔDi ,
(3.4.18)
the exponent ΔDi following from Equation (3.4.16). Often the numerical value of the relative color strength Prp is emphasized alone for the argument for colorant substitution in color reproduction or color recipe prediction. But it needs to be taken into consideration that the replacement usually brings in changes in hue or lightness or other coloristic features with consequences for color constancy, metamerism, among other things. Provided that the new pigments are transparent or translucent, also the light transmission or the covering potential can change. In any case, such consequences must be thoroughly checked before the colorant exchange. Also, as normal in material sciences, it must be ensured that the replacement of one component has no negative effect on other components or system properties.
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185
In summary, we point out that both spectrometric and colorimetric procedures are quite efficiently applied to determine and characterize the relative color strength of absorption colorants. The productive potential of colorimetry up until now is used, in the following, for a quantitative description of further color properties of absorbing colorants.
3.4.3 Covering Capacity Whereas the color strength, in some sense, indicates the coloristical effectiveness of an absorbing colorant, the covering capacity is a measure of the capability of a coating to hide a colored background [46]. This property is called hiding power in ASTM standards [47– 49]. For constant pigment loading, there exists a minimum coating thickness dC for which the color of a substrate can no longer be visually discerned. On the other hand, given a layer thickness d, there is a minimal colorant concentration cmin for which the background color is also not visible. In both cases, the inverse of the minimal covering thickness dC is a measure for the covering capacity of a scattering and absorbing coating, as in D = 1 dC .
(3.4.19)
The quantity D is called the covering capacity value and is in units of reciprocal length. This dimension can be modified in such a way that it has an economical meaning. If the unit of film thickness dC is given in mm and multiplied by the ratio m2 /m2 , then for covering capacity value D, the quotient m2 /l follows; 1 l ≡ 103 cm3 is the volume unit liter. More precise, the quantity Dv = D relates to the volume. The corresponding numerical value of Dv indicates the area in square meters, which 1 l of color can totally cover at film thickness dC . On the other hand, if the mass density ρ m is given in dimensions g/cm3 , then the unit liter l can be substituted by the expression ρm−1 kg. If the numerical value D is given in the units mm–1 or m2 /l, then the multiplication with the value of mass density ρ m in unit g/cm3 results in dimension m2 /kg for Dm = ρm · Dv . The quantity Dm now relates to the mass, it indicates the area in square meters, which one kg of color can totally hide at film thickness dC . Therefore, the value of Dv or Dm is a realistic measure for the covering spreading rate of a formulation with absorption pigments. The quantity of the covering capacity can be simply verified from the dry film thickness. Now, the question needs to be answered as to which method can be used to find out the minimal covering film thickness dC . Just as for the color strength, the covering capacity value of absorption colorations is experimentally determined with the help of a colorimetrically defined criterion. For this purpose, there exist two methods of operation [46 – 50]. The first of them is based on the so-called
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contrast ratio; it follows from the standard color values Yw and Yb which result from the measured reflectance of the film over white and black backgrounds (contrast substrate). According to this criterion, a minimal covering layer is achieved if the condition Yb ≥ 0.98 Yw
(3.4.20)
is fulfilled, for example, for the standard illuminant/observer combination D65/10◦ . The contrast ratio should, accordingly, attain a minimum value of 98% to indicate a covering film thickness. The second procedure uses the color difference ΔEbw which results also from the spectrophotometric measurement of the film over black and white backgrounds of known reflectance. A covering coating satisfies the condition
ΔEbw =
(ΔLbw )2 + (ΔCbw )2 + (ΔH bw )2 ≤ 1,
(3.4.21)
where ΔLbw , ΔCbw , ΔHbw are the difference in lightness, chroma, and hue, respectively, each over both backgrounds. For opaque colors, the values are (Yb /Yw ) = 1 or ΔEbw = 0. Due to the color locus-dependent visual discrimination of color differences, it may be necessary to fix, in dependence of hue, a color difference in the value domain 0.3 ≤ |ΔEbw | ≤ 0.9. In the case of achromatic or nearly achromatic colors, Equation (3.4.21) reduces to |ΔLbw | ≤ 1 because the distribution of chroma and hue is now of secondary importance. In all cases, the spectral reflectance of the black and white backgrounds Rbg,b (λ) and Rbg,w (λ), respectively, should be constant and meet the conditions Rbg,b (λ) ≤ 0.2 and Rbg,w (λ) ≥ 0.8. The actual determination of the volume- or mass-related covering capacity value D from the color difference method can be achieved either graphically or numerically (for simplicity, in the following we leave out the corresponding indices v and m of D). The graphic method requires at least three colorations of different film thicknesses d, each over the black and white substrate. The layer thickness should be known to an uncertainty of ±1%. From the graph of ΔEbw in dependence of 1/d, the value D follows by extrapolation. It is represented by the slope point of coordinates (ΔEbw , 1/dC ) to which the color difference ΔEbw = 1 belongs; see Fig. 3.14. In contrast, the numerical procedure is based on the calculation of the reflectance spectra over both backgrounds. It has the advantage that only one control coloration needs to be manufactured. On the other hand, this method requires various known spectral quantities as input data: the optical constants of the pigments, binder, perhaps additives, and the reflectance of both backgrounds; in addition, the pigment loading and the single concentration ratio of
3.4
Specific Qualities of Colorants
187
ΔEbw
3.0
2.0
1.0 D ≈ 18 m2/l D 0 0
10
20
1/d/mm–1
Fig. 3.14 Determination of covering capacity value D of a pigmented coloration by extrapolation
the inserted colorants have to be known. This set of quantities is used to calculate the spectral reflectance over both backgrounds with the aid of a suitable radiative transfer approximation (see Chapter 5). Afterward, the covering capacity value D follows from iteration as given in Fig. 3.15. The process starts with an estimate for a non-covering film thickness dk = 1/Dk , which leads to the color difference value ΔEk (for simplicity, the exponent ws is left out in the following). In the next step, a suited value Dk+1 < Dk of corresponding color difference ΔEk+1 is determined. If for the sought after covering capacity value (3.4.19), the given color difference obeys ΔEC ≤ 1, then an improved value Dk+2 follows from equation Dk+2 = Dk+1 −
Dk+1 − Dk (ΔEk+1 − ΔEC ). ΔEk+1 − ΔEk
(3.4.22)
This relation results from the method regula falsi. According to this, at each iteration step, a curve section is approximated by a secant line. After a few iteration steps the covering capacity value D = 1/dC is obtained. The graphical and numerical methods do not necessarily result in same values. Covering capacity values can, consequently, only be compared with each other if they are determined using the same method. The determination of the value D runs, however, more elegantly, if this procedure is directly included in color recipe prediction. This is because the optical
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3
Standardized Tristimulus Values, Color Qualities, Chroma of Effect Pigments ΔE bw k=0
6.0
4.0
k=1 2.0
k=2 k=3 D ≈ 22.9 m2/l
0 10
20
30
40
1/d/mm–1
Fig. 3.15 Iterative determination of the covering capacity value D
constants of the inserted colorants and the concentration ratios are already known as well as the calculated spectral reflectance values (Section 6.2.3). The color recipe prediction even allows for the possibility of fixing a covering film thickness dC = 1/D and determining the corresponding colorant fractions. In fact, this method needs intensive computation, but it requires only one coloration in order to check the calculated covering thickness dC . If another covering thickness dC, x = 1/Dx is required, and this thickness differs not more than about ±10% of dC , then the new pigment loading cx follows from the previous one by the simple approximation cx = c ·
dC Dx . =c· dC, x D
(3.4.23)
For use of the maximal pigment loading cmax (in so-called high solids), the even covering and minimal thickness dC, min = 1/Dmax is determined from dC, min = dC ·
c cmax
;
(3.4.24)
the accompanying quantity Dmax follows from formula
Dmax = D ·
cmax . c
(3.4.25)
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Specific Qualities of Colorants
189
To complete the picture, we point out that the change of film thickness or pigment loading can additionally influence the volume or surface properties, for example, gloss, microhardness, abrasive resistance, color fastness, or weathering resistance. Such features, consequently, should also be checked. Moreover, we mention that the discussed methods will produce incorrect results if measured input quantities are inaccurate (“garbage in, garbage out”). On the basis of this fact, the quantities that we are interested in D, dC , or c should be determined in view of a load factor lf > 1 in order to compensate the consequences of unavoidable production fluctuations.
3.4.4 Transparency and Coloring Power According to the previous section, the transition from translucent to opaque of a colored layer is unambiguously characterized by either the covering capacity value, contrast ratio, or color difference over black and white contrast backgrounds. However, reverse has not yet been clarified as to which characteristic value describes the changeover between nearly transparent and slightly translucent materials. Before we discuss this question, we first have to characterize the real state of nearly transparent colorations. Ideal transparency is characterized by pure absorption and completely absent scattering. The greater the transparency of a real layer, the less the light is absorbed or scattered. In addition, transparency of a real material depends on refractive index, the layer thickness, contained colorants, binder, superstructure, as well as aging processes. Clearly, the spectral absorption influences both the light transmittance and color of the material; normally, color differences as small ∗ ≈ 0.02 are just provable. The color shift of nearly colorless transparas ΔEab ent materials is called the tinting power. This color shade is perceptible over a white background, the scattering component, on the other hand, over a black background. A measure for light transmittance is, apart from spectral transmission, the so-called transparency index. It characterizes the scattering component of a transparent medium. It is consequently determined from the color difference ΔEb which follows from reflectance measurements of the layer over a black background and the background itself. Because transparency depends non-linearly on layer thickness d, samples of various thicknesses are to be manufactured for determining the transparency index. In order to attain a transparency index independent of geometrical influence, the color difference value ΔEb for zero thickness d→0 by extrapolation should be determined. The plot of the difference ΔEb in dependence on d results in a nearly positive parabolic curve through the origin, as shown in Fig. 3.16. The transparency index TN is now defined by the reciprocal curve gradient at infinitesimal thickness difference Δd→0:
190
3
Standardized Tristimulus Values, Color Qualities, Chroma of Effect Pigments ΔE b
ΔE2b
ΔE1b
0 0
d1
d2
d
Fig. 3.16 Determination of transparency index from the slope at the origin
1/TN = lim
Δd→0
Δ(ΔEb ) . Δd
(3.4.26)
The quantity of TN has the unit of d. The greater the transparency of a layer, the smaller the gradient at the origin. Consequently, the transparency index is a quantity which is a real characteristic of an optical material [51, 52]. The slope at the origin can be approximately determined by curve fitting. If we assign the measured value pairs di , ΔEib for i = 1, 2, 3. . . to a polynomial of second order through the origin ΔEb = a1 d + a2 d2
(3.4.27)
with coefficients a1 , a2 , then the transparency index follows from TN = 1/a1 .
(3.4.28)
Also for polynomials of higher order, the transparency index results from the inverse of the coefficient at d. For a rough estimate, two layers of thicknesses d1 and d2 > 1.5 d1 are sufficient. With the accompanying color differences ΔE1b , ΔE2b and using Equations (3.4.27) and (3.4.28), the relation TN =
q · (d2 − d1 ) q2 ΔE1b − ΔE2b
, q = d2 /d1 ,
(3.4.29)
can be derived. The quantity TN is quite sensitive to inaccuracies in the values of d1 and d2 . On the other hand, the relative uncertainty of the transparency index can be estimated by summing up and doubling the relative errors of color
3.4
Specific Qualities of Colorants
191
difference and thickness measurement. The computation of adjustment naturally delivers an enhanced error estimate for TN . The coloring power value CP of a layer is determined in a similar way, but using a white background rather than a black one. The quantity represents a dimensional value for the color of a nearly colorless transparent material. For the determination of the coloring power value, the color difference ΔEw between the layer separately over white background and the background is used, this again in dependence of layer thickness d. The color difference ΔEw behaves similar to ΔEb in dependence on d. Therefore, the formalism for TN can be nearly applied to derive a formula for determination of CP . From similar considerations as above, the quantity of CP follows directly from the slope in the origin CP = lim
Δd→0
Δ(ΔEw ) = a1 , Δd
(3.4.30)
provided that Equation (3.4.27) is applied with ΔEw instead of ΔEb . The unit of CP is the same as of d. The smaller the slope at the origin, the lower the value of CP and the less perceptible the natural color of the transparent material. Both quantities CP and TN can even be simultaneously determined from the same layer thicknesses if the transparent films are each measured over a black/white contrast substrate. With the thickness values d1 , d2 , and the accompanying color differences ΔE1w and ΔE2w ,
CP =
q2 ΔE1w − ΔE2w , q · (d2 − d1 )
q = d2 /d1 ,
(3.4.31)
follows from Equations (3.4.27) and (3.4.30). The error estimates of CP and TN are nearly the same, provided that in both cases the same measuring equipment, layer thicknesses, and contrast substrate are used. For more than three thicknesses, the values are to determine by computation of adjustment. The multiplication of transparency index and coloring power value of the same material leads to the dimensionless varnish power value Γ = TN · CP .
(3.4.32)
As stated at the beginning of this section, with the covering power criteria, it is necessary to differentiate between an opaque and a translucent coating. There does not, however, exist a colorimetrical method for distinguishing a nearly ideal transparent medium from a slightly translucent one. This problem is solved at the end of the next section after the discussion of aging stability.
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3
Standardized Tristimulus Values, Color Qualities, Chroma of Effect Pigments
3.4.5 Color Fastness and Turbidity Despite experience indicating otherwise, until now we have disregarded the fact that components – especially colorants, binders, and additives – are subject to aging effects. The term color fastness is to be considered the resistance of a given coloration to physical or chemical influences during manufacturing, processing, storing, application, or aging [53, 54]. Color changes during such periods, however, are of prime importance for acceptance, quality, profitability, and conventional working life of a colored product. A high color fastness is necessary during manufacturing or processing because of the presence of the prevailing temperatures, IR radiation, pressures, shear rates, and processing auxiliaries [55]. Consequently, the short- or long-term aging stability of colorants and formulations should be known or at least approximated from results of simulation experiments. Aging processes depend on the inner and outer conditions of a material. The inner conditions consist of thermodynamic instable molecular states, which lead (especially in plastic materials) to after effects such as secondary crystallization, embrittlement, diffusion of colorants, plasticizers, or colorant auxiliaries by relief of residual stresses. Aging from the surface is primarily caused by radiation energy, from cosmic and radioactive radiation to radiation in the near-UV and far-IR range (cf. Fig. 2.1). The effects of humidity, liquids like brine solutions, acids, leaches, organic solvents, detergents, and also gases such as oxygen, ozone, carbon dioxide, and exhaust pollutants should not be underestimated. The inner and outer effects can damage both the individual colorants and the net color effect. The examinations for color aging can be divided into practice equivalent and time-lapsed methods. Of special interest among them is the long-term fastness to light under different climates. Economic reasons allow only in rare cases a long continual outdoor weathering in a temperate climate (Central Europe), warm dry (Arizona), or warm humid (Bombay) with solar energy influx between 127 and 150 W/m2 (about 10% of the solar constant). From material science, timelapsed simulation experiments are known and widely applied, from which the real aging stability should follow in a shorter exposure time. During an artificial weathering, the color samples are exposed to a continuous radiant flux and additionally loaded with thermal energy or agents [56]. For radiation sources are used independently of each other or combined: xenon radiators, luminescence and mercury vapor lamps, as well as carbon-arc lamps [57, 58]. The emitted spectra are irradiated directly without or with selective filters. In single cases, a spectral power distribution which corresponds to the standardized middle daylight D65 simulator is generally sought after. Because the higher radiant energy densities also cause an accelerated self-aging of the sources, the artificial radiators and the inserted UV filters should be exchanged no later than after 1,500 operating hours, and for multiple instrumentation this
3.4
Specific Qualities of Colorants
193
is in cyclic order. The overall influence of the radiant power is a measure of the radiation-invoked aging process of the relevant material. The artificially induced degradation should approximately correspond to that which will probably occur during working life of the colored product. During natural or artificial aging of colorants or color formulations, the corresponding color values change constantly. Periodically time-dependent color alterations are quite rare in practice. Only in some cases, the aging caused chalking or efflorescence of colorants and additives are pursued with colorimetrical methods. Also changes of wood substrates coated with varnishes need to be interpreted with some restriction and are at best judged qualitatively. Changes of gloss, microhardness, abrasion resistance, blistering, cracking or crazing as well as edge peeling, etc., are difficult or even impossible to characterize with colorimetrical methods; such kinds of damage are often judged subjectively according to standardized guidelines. Among the multitude of damage influences, we only describe the effects that are addressable colorimetrically, such as turbidity and yellowing of transparent and translucent materials. The color changes compared with the original condition can be established, for example, by the color difference contributions ΔL, ΔC, ΔH. Because the majority of the damage mechanisms proceed in an exponential time-dependent fashion, the color difference measurements need, at first, to be carried out in shorter, logarithmic time intervals. If the aged specimen field is larger than the aperture of the color measuring equipment, then the changes should be taken each time at the same marked measuring area and in the same orientation. In cases of fogging, striations, or grains present in the measuring field, at least three representative spots should be chosen and the arithmetic mean of the measured variables taken. Each measurement should be carried out with the same color measuring instrument and evaluated with the same method, the same color differences, and the same illuminant/observer combination. All of the aging and evaluation conditions need to be documented with the results. For performance evaluation with regard to color changes were developed, apart from color difference quantities, further empirical characteristics especially to use for different colorations or materials. Among them are the gray scale rating (principally of textiles), whiteness index (white pigments, paper), yellowness index (paper, foils), and turbidity or haze (foils, inorganic or organic glasses). The mentioned quantities are now discussed. The gray scale rating GS can be determined for achromatic and chromatic colorations. This quantity follows after the time-dependent degradation action with the special color difference formula ΔEC =
(ΔL∗ )2 + (ΔCC )2 + (ΔHC )2 .
(3.4.33)
The special chroma and hue differences ΔCC and ΔHC are empirical functions ∗ , Δh , ΔH ∗ , which are given by a standard [59]. of CIELAB differences ΔCab ab ab
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The value ΔEC corresponds to a gray scale rating value GS , which is a natural number in the range 1 ≤ GS ≤ 5. The GS value ranking in dependence on ΔEC is somewhat arbitrary and not clearly defined for intermediate ΔEC values outside given tolerance intervals; see Table 3.11. For example, a color difference in the value domain 12.6 ≤ ΔEC ≤ 14.6 corresponds to the lowest possible value GS = 1, the highest GS = 5 corresponds to the color difference interval ΔEC ≤ +0.2, a value in the domain 10.3 ≤ ΔEC ≤ 12.6, on the other hand, cannot be clearly assigned a concrete gray scale rating value. The whiteness index and whitening index were introduced for evaluation of nearly achromatic light colorations and accompanying color changes. The determination of the whiteness index W is founded on the x, y, Y system and follows from relation W=
for D65/2◦ Yn + 800(xn − x) + 1700(yn − y) . (3.4.34) Yn + 800(xn, 10 − x10 ) + 1700(yn, 10 − y10 ) for D65/10◦
It comes from extensive color matching [60, 61]. In Equation (3.4.34), xn , yn and xn,10 , yn,10 denote the coordinates of the achromatic point in the chromatic diagram to the 2◦ and 10◦ standard observers, respectively (see Table 3.2). According to Equation (3.4.34), ideal white has a value W = Yn = 100.000 for each of the standard observers. Colorations containing fluorescent brighteners can exceed this value and need a suitable corrected formula or an entirely different one. For description of near-white shades of paper or textiles, on the other hand, the so-called whitening index Tw is used [62]. In comparison to W, its determination follows from a similar relation: Tw =
1000(xn − x) − 700(yn − y) for D65/2◦ , 900(xn, 10 − x10 ) − 800(yn, 10 − y10 ) for D65/10◦
(3.4.35)
Table 3.11 Gray scale value, corresponding color difference, and color-difference tolerance of gray scale rating Gray-scale value GS
Color difference ΔEC
Tolerance ±δ(ΔEC )
1 1–2 2 2–3 3 3–4 4 4–5 5
13.6 9.6 6.8 4.8 3.4 2.5 1.7 0.8 0
1.0 0.7 0.6 0.5 0.4 0.35 0.3 0.2 +0.2
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Specific Qualities of Colorants
195
where the indexed chromaticity coordinates have the same meaning as in Equation (3.4.34). The test color appears greenish for Tw > 0 and reddish in the case of Tw < 0. Ideal white is represented by the value Tw = 0 for both standard observers. For equal color coordinate values of x, y, Equations (3.4.34) and (3.4.35) show numerically different results. Clearly, the whiteness index is a measure for the lightness including the weighed relative red and green fractions of the sample. In contrast, the whitening index represents the difference between the relative red and green fractions. Both quantities, consequently, cannot be compared with one another, neither colorimetrically nor numerically. Greater color changes of white or brightened materials are characterized by the yellowness index Yness or yellowing index Ying . The yellowing is caused by energy absorption at wavelengths < 490 nm. The determination of the yellowness index Yness is based on a relative equation of type Yness = (α · X − β · Z)/Y,
(3.4.36)
this again comes from extensive color pattern matching. The empirical weighting factors α and β depend on the chosen illuminant and standard observer [61, 62]. The yellowness index is to calculate from Yness =
(1.298 · X − 1.133 · Z)/Y for D65/2◦ . (1.301 · X10 − 1.149 · Z10 )/Y10 for D65/10◦
(3.4.37)
Each of the expressions in Equation (3.4.37) corresponds to the difference of the weighted red and blue fractions relative to the lightness value of the yellowish material. The yellowing index Ying is simply defined as the difference in a o : and at the original condition Yness yellowness index after aging Yness a o − Yness . Ying = Yness
(3.4.38)
Yellowing is accompanied by changes of chroma ΔC and hue ΔH, which characterize the color shift more closely. The yellowing of transparent organic materials like coatings, foils, inorganic or organic glasses is also often accompanied by increasing turbidity or haze. The turbidity of transparent finishes or haze of plastic materials transforms a directional light intensity into an attenuated directed and a diffuse component, as shown in Fig. 3.17. A measure for the diffuse scattering effect in the volume of the layer is the haze index HI [63]. This quantity is defined as the ratio of the diffuse transmissivity Td to the entire transmissivity Te of a layer multiplied by hundred HI = (Td /Te ) · 100.
(3.4.39)
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3
Standardized Tristimulus Values, Color Qualities, Chroma of Effect Pigments
Fig. 3.17 Directional and diffuse intensities determine the haze index of a transparent turbid material
Id Io Ie
jdTe
The entire transmissivity equals the transmission of the material. The diffuse component Td is given by the ratio of the transmitted diffuse intensity Id to the irradiated intensity I0 : Td = Id /I0 .
(3.4.40)
The entire transmission Te follows from an analog consideration by the ratio Te = Ie /I0 ,
(3.4.41)
where Ie stands for the entire transmitted intensity. The value of Id is normally determined with angle dependence. For simplicity, the scattered radiation Jd is determined integrally at an axial angle of ±80◦ with respect to the direction of the incident intensity I0 . The diffuse flux Jd is composed of the transmitted component Id and the scattering jd Te caused by the physical elements of the measurement setup: Jd = Id + jd Te .
(3.4.42)
The diffuse flux jd is determined from an empty measurement in normal operating conditions. The haze index HI is consequently calculated from the relation Jd jd − · 100. (3.4.43) HI = Ie I0
3.4
Specific Qualities of Colorants
197
This measuring principle responds quite sensitively to defects at the surfaces such as dust or scratches. In order to observe the haze coming from scattering centers in the volume, the samples need to be handled quite carefully. Transparent materials with structured surfaces are, therefore, also unusable for this measuring method. This is because turbidity depends on discontinuity of refractive index at the interface only to a small extent. The haze index of transparent real materials is in the domain HI ≤ 0.05 and of translucent mediums in the interval 0.05 ≤ HI ≤ 0.30. The haze index value HI ≤ 0.05 is a suitable criterion for discerning transparent layers from translucent ones. The haze index HI is, according to definition equation (3.4.39), a dimensionless quantity, whereas the transparency index TN , from Equation (3.4.29), has the units of length. Also this comparison shows clearly that both quantities represent different optical properties. The discussed evaluation relations in this chapter have been outlined generally for the representation of typical properties of colorations with absorption colorants. Certainly, colors containing flake-shaped effect pigments need separate considerations with regard to color fastness because some color properties of this pigment sort cannot be characterized by colorimetrical methods. More detailed information about this is given in the next section for colorations especially with metallic pigments.
3.4.6 Stability of Effect Pigments Similar to that which was discussed for absorption colors, colorations with effect pigments lose their initial color physical properties due to physical or chemical influences. Because of the composition, morphology, and greater size of such particles compared with absorption pigments, the effect flakes present – in a real and figurative sense – a bigger target. The effect pigments should have high resistance against shear load, light or heat load and to a large degree against aggressive chemical environments. Formulations with effect colorants generally require more extensive fastness tests than for absorption colorants. From the catalog of possibilities for metallic and interference pigments, we restrict the discussion to some fundamental degradation mechanisms. The mechanical loads which flake-shaped effect pigments undergo during manufacturing or processing should, by no means, be underestimated. The mechanical ring pumps of painting plants or fluid plastic melts through narrow nozzles and spiral channels cause enormous pressure gradients – shear rates up to 105 s–1 . Incorporated effect particles should survive a process with a maximal shear stress of 102 MN/m2 undamaged. Because of shear stress load, preferential thin metal particles are uncontrollably deformed and scratched, outer sections of the flakes fold down or fracture: the metallic brilliance grays. In a similar way, the brilliance of pearl luster and interference pigments is also reduced.
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The degree of shear stability of effect particles is characterized either by the gray scale rating GS or colorimetrical lightness L. For determination of the decrease in lightness, test effect pigments are agitated in a cooled mixer machine of a suited agitator at a speed of 20,000 rpm for 15 min. Afterward a coating with such shear-loaded particles is manufactured in a clear binder and the CIELAB lightness difference ΔL∗ is determined between the damaged flakes LS∗ and the lightness of the reference coloration LR∗ . The measurements are each performed at an illumination angle of 45◦ and fixed aspecular measuring angle of μas = 20◦ . In dependence of the amount of lightness difference value ΔL∗ (20◦as ) = |LS∗ (20◦as ) − LR∗ (20◦as )|,
(3.4.44)
three empirically defined groups can be differentiated. These are listed in Table 3.12: shear stable, low shear stable, and non-shear stable platelets. In order to further characterize the degradation, a higher measuring angle is used to determine the difference of flop index (Section 3.5.1), or the damage time is to increase. The highest shear stability show clearly thick glitter particles, the lowest metallic corn flakes. The stability of pearlescent and interference pigments can be increased by coating with suited interface-active substances. Although metallic pigments show a higher light resistance in comparison to absorption pigments, high-energy radiation, thermal energy, or an unfavorable polymer surrounding can lead to immediate degradation of the flakes. The metallic character is further lowered by such influences. Particles of copper/zinc alloys (brass) turn out to be particularly susceptible. Because of the lower melting point, the flakes become thermally unstable at temperatures higher than about 200◦ C; the flakes are, therefore, suitably stabilized for application in baking finishes or plastic materials of high melting and glass transition temperature, respectively. Water-borne systems or hygroscopic polymers are able to activate decomposing effective zinc and copper ions from brass particles. These can cause considerable color shift and luster decrease. Both ions lead to accelerated disintegration of PVC molecules; already a thermal load at a temperature as low as 80◦ C leads to separation of hydrogen chloride. The combined coloristical variTable 3.12 Connection between change of lightness and shear stability of metallic pigments Lightness difference ΔL∗ (20◦as )
Degree of shear stability
10
Low shear stable Non-shear stable
Examples of metallic pigments Glitter particles of metal foils Silver dollar flakes Cornflakes
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199
ations can be quantified by the previously discussed colorimetrical methods for determination of yellowing. The damaging effects of the copper and zinc ions can be reduced, however, by appropriate polymer coatings of the flakes. In such a way, stabilized particles can have elevated processing temperatures of up to 260◦ C. An additional property of effect pigments, which especially need to be considered for aluminum flakes, is the leafing stability. This particle formation can be unintentionally reduced or altogether time-dependent decay by false additives. The standardized testing value for leafing stability indicates the time during which a leafing pigment is flooded and finally shows visible wetting [64]. Leafing stability can also be determined relative to a reference formulation. It is possible to additionally pursue the leafing decay with the colorimetrical lightness L. The chemically caused influences can induce particularly enormous degradations of the metal particles. For example, the brilliance of aluminum flakes is reduced in the presence of water as in water-based paint systems or in the form of water vapor. The particles are oxidized with the release of hydrogen and lose, therefore, their initial brilliance. The dehydration of polymeric materials with comparably high humidity content such as polyamides, polycarbonates, or polyethylene terephthalates should be performed separately and actually directly before incorporation of the aluminum pigments. Otherwise the particles become partially oxidized from the surface by released water vapor under the formation of Al2 O3 (Appendix A.1.1). This unwanted influence causes a distinct reduction of lightness. Moreover, the surface-oxidized aluminum platelets tend to conglomerate during incorporation in binders or melts of high polymeric materials. The conglomerations in paints lead to local restricted mottlings, which are caused by turbulent solvent evaporation. Such heterogeneities are detected as local lightness fluctuations with a small aperture color measuring instrument and applying the method described above in connection with Equation (3.4.44). Coatings with effect and absorption pigments, which are exposed to high humidity, are indispensable for the examination of the so-called condensation water resistance. This test is performed with colorations containing single or various combined pigment types. For this, effect pigments can be coated with various covering organic substances. In such a way, modified particles are subjected to a saturated water vapor atmosphere of 40◦ C for 240 h [65, 66]. The colorimetrical changes to detect are again followed in logarithmic time steps. In general, these actions produce stronger damages as the standardized salt spray testing [67]. This was originally introduced to control recipes for absorption pigments. With this method, conventional effect paints and water-based systems are controlled with regard to swelling, blistering, adhesion, reduction of brilliance, and distinctiveness of image DOI. For outdoor use, metallic, pearl luster, and interference pigments have to meet the greatest demands concerning color constancy or weather stability. In
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addition to the testing procedures mentioned until now, the exterior weathering is also assessed with the non-standardized Florida test. This test is regarded as passed, if after a 2-year natural weathering – under daytime-dependant strong fluctuations of air humidity and temperature – the color difference of a chromatic color regarding the undamaged reference coloration is less than unity: ∗ 1.0 not only at near specular angles; this also leads to lightness values higher than 100. By definition, a dark lightness flop corresponds to a high lightness difference between small and large aspecular observation direction angles. A light lightness flop is, however, characterized by a small lightness difference (Section 2.3.2). Standard metallic flakes of middle light flop show FI values in the domain 10 ≤ FI ≤ 20, high-quality brilliant formulations with metallic pigments of dark flop attain, however, FI values up to 60. As can be taken from the values listed in Fig. 3.18, in comparison to the change of lightness curves, the FI value is directly proportional to the lightness difference between small and large aspecular measuring angles. This corresponds to the numerator in Equation (3.5.2). From Fig. 3.18, it is to infer that the lightness value L∗ (25◦as ) at angle μas = 25◦ plays a central role – it shows values in the range 95 ≤ L∗ (25◦as ) ≤ 110. The curves seem to be slightly rotated at a point with rough coordinates (μas ≈ 25◦ , L∗ ≈ 100). The steeper the lightness curve in the vicinity of this point, the higher the corresponding FI value and the darker the lightness flop. Metallic pigments of high lightness flop index reach lightness values of L∗ (15◦as ) > 300 at small aspecular angles.
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203
103
L∗
β = 45°
Flop index 11.7 15.5 19.8 37.5 55.4
102
101 0
20
40
60
80
100
μas / o
Fig. 3.18 Lightness L∗ in dependence of aspecular measuring angle μas of metallic pigments with different flop indices
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It seems obvious to use similar considerations for characterization of the color flop index. For that, however, it is necessary to verify if there is a suitable additional formula structured like Equation (3.5.2) with chroma instead of lightness, but at the same aspecular angles and other weighting parameters. Additionally, we need to know if it is necessary to vary the angle of illumination. In each case, both extreme flop colors should be indicated together with the color flop index value(s). An additional property of metallic pigments which can be expressed numerically is the distinctiveness of image DOI, cf. Section 2.3.2. The DOI value more or less represents the uniformity of the visually perceived metallic effect and is correlated with the covering capacity of the metallic formulation. The determination of the DOI value is again carried out under an illumination angle β = 45◦ , the reflection measurement at an aspecular angle μas = 15.0◦ , and slightly varied angles μas = (15.0 ± 0.3)◦ . The source used is normally white light, but illuminations of other spectral composition in the visible range are also possible. The DOI value is given by one of the following relations: ! R(μas = 14.7◦ ) · 100, R(μas = 15.0◦ )
(3.5.3a)
! R(μas = 15.3◦ ) DOI = 1 − · 100 R(μas = 15.0◦ )
(3.5.3b)
DOI = 1 −
[71, 72]. For uniformly parallelized flakes, each of the reflection values in the numerator of both equations should be approximately the same. Both formulas (3.5.3a) and (3.5.3b) limit the DOI value domain to the interval 0 < DOI < 100. The higher the distinctiveness of image, the smaller the reflectance value in the numerator compared to the relative value R(μas = 15.0◦ ) in the denominator. Large-sized flakes show low DOI values, on the other hand, fine particles have high DOI values. These higher values indicate that minimal contrast differences are better reproduced. This property comes down to the smaller edge circumference and the smaller surface area of these flakes. Also high-contrast objects are better imaged against the surroundings by the reflections from the small-sized particles. Moreover, this method can also be applied for DOI determination of pearlescent and interference pigments. The DOI value is related to the covering capacity of a formulation with metallic and interference pigments. Both the sparkle effect and graininess of effect colorations are determined using directional light. Actually, sparkling depends on illumination and measuring angle, but in order to reduce the effort of measuring, three illumination angles of β v = 15◦ , – 45◦ , and –75◦ with respect to the normal to the surface are generally sufficient (the negative sign means that the angle is, as regards the normal, opposite to positive ones). Each of the measurements is performed at an
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205
angle μv = 0◦ with a digital CCD camera.4 The registered gray levels are processed as lightness values of the relevant effect coloration. For evaluation of the sparkle effect, two quantities are used: sparkling area Ask and sparkling intensity Isk . The sparkling area corresponds to the total area, which follows from the summation of each registered particle. But for agreement of the result with visual impression, the only reflecting particles taken into consideration are those lighter than the middle basic lightness of the actual coloration. On the other hand, the sparkling intensity Isk follows from the summation of all individually registered intensities. The sparkle effect is determined separately for each of the three measuring angles. For characterization of this phenomenon, the sparkle grade SG and sparkling intensity Isk are used. The sparkle grade is defined as the geometric mean of Isk and sparkling area Ask : (3.5.4) SG = Isk · Ask . For an effect coating without any sparkle particles with Ask = 0, a sparkle grade of SG = 0 follows. Normal sparkling effect colorations of size 34 μm ≤ d50 ≤ 54 μm show illumination angle-dependent values in the interval 0 ≤ SG ≤ 10. In extreme cases, values up to SG = 30 at β v = 15◦ are attained. On the other hand, for a constant sparkle degree, if Isk is plotted against Ask , then variations in manufacturing or processing with empirical tolerance ellipses follow, those have limits of permissible variations ΔIsk and ΔAsk (for tolerance specifications, see Section 4.3.3). The sparkle grade of a fine and coarse gray effect coating at three illumination angles is listed in Table 3.13. Both colorations are visually perceived as identical. As expected, the sparkle grade decreases with higher value of illumination angle for both colors. This is because smaller particles reflect light in the direction of the sensor at more flat angles. On the other hand, the lower sparkle grade of the fine coloration continues to higher illumination angles. This behavior comes from the orientation distribution of the flakes, although the majority of the particles are orientated parallel to the coating surface. Because the appearance of graininess of a coating can be recognized only at a small distance from the coating’s surface, this property is independent of observation angle. The quantitative determination of this phenomenon is performed by measurement with diffuse illumination. Graininess is mainly seen out of direct daylight. In order to ascertain the graininess, the non-uniformity of the light/dark fields is evaluated. These fields are registered by the CCD chip as gray scales. The more non-uniform the fields appear, the higher the value of graininess Gr ≥ 0. A value Gr = 0 represents a coated area without discernible graininess. The value domain of real colorations extends to about Gr = 30. The 4 CCD: charge
coupled device
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Table 3.13 Sparkle grade and graininess value of fine and coarse, dark gray visual and colorimetric equal effect colorations [73] Sparkle grade SG at illumination angle β v Grain quality
15◦
– 45◦
–75◦
Graininess Gr
Fine Coarse
1.3 6.9
1.2 2.9
0.8 1.6
6.0 9.5
graininess values of the above fine and coarse effect colors are also indicated in Table 3.13. Altogether, it is important to emphasize that only recently introduced experimental methods of sparkle grade and graininess enable the accurate description of additional optical properties of effect colorations. The results are consistent and agree well with visual impressions. On the other hand, the entirety of measuring methods discussed in this section is only to be regarded as complementary to the usual angle-dependent color measurements of effect pigments.
3.5.2 Color Difference Equation for Metallics As already pointed out, the color difference formulas given in Sections 3.1.3, 3.1.4, 3.2.1, 3.2.2, 3.2.3, and 3.2.4 are only applicable to absorption colorants. For formulations with metallic or other flake-shaped pigments, it is necessary to additionally consider the angle-dependent, anisotropic reflection of such coatings. A color difference formula only for use in automotive coatings which contain metallic pigments is subject to a standard [30]. This standard is principally designed for refinishing paintwork and low-bake paints. Comprehensive color difference relations for other effect pigments have not been developed up until now. The need of such relations really depends on further use of those colorants. On the other hand, the change of the unusual color physical properties of such effect pigments can generally not be simply reduced to a color difference expression. For determination of color differences occurring with totally covering metallic colorations, the customary illumination angle of β = 45◦ and aspecular measuring angles μas = 15◦ , 25◦ , 45◦ , 75◦ , 110◦ are normally used. For simplicity, the index of the measuring angle is left out below. The measuring results should only be compared with each other if the sample and reference colors are of similar surface gloss and other colorimetrical requirements are the same for both. The reflectance measurement of a metallic coating is performed at about five different points of the plane patterns of the sample and reference coloration. From each of the resulting CIELAB color values of the sample color
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Chroma of Effect Pigments
207
LS∗ (μ), a∗S (μ), b∗S (μ) and the reference color LR∗ (μ), a∗R (μ), b∗R (μ), the arithmetic mean for each of the five measuring angles is taken. The calculated color difference contributions ΔL∗ (μ), Δa∗ (μ), Δb∗ (μ), ΔC∗ (μ), ΔH∗ (μ) lead to five angle-dependent color differences, denoted by ΔEeff (μ). If the coloration consists of both metallic and absorption pigments, then the color flop can be represented by two color loci which are possibly positioned in different areas of a color plane. In such cases, the local color differences are calculated with different formulas. In the mentioned standard, two extended color difference expressions for uncolored and colored colorations are given: ∗ (μ) < 10 as well as pas1. For achromatic colors with chroma values 0 ≤ Cab ∗ < 18 and lightness tel colors (of high “silver” or white content) of 0 ≤ Cab L∗ (μ) > 27, relation
(μ) ΔEab
=
ΔL∗ (μ) gL SL (μ)
2 +
Δa∗ (μ) ga Sa
2 +
Δb∗ (μ) gb Sb
2 (3.5.5)
is applied. ∗ (μ) ≥ 10, but not including pastel colors, the 2. For chromatic colors with Cab formula (μ) ΔECH
=
ΔL∗ (μ) gL SL (μ)
2 +
ΔC∗ (μ) gC SC (μ)
2 +
ΔH ∗ (μ) gH SH (μ)
2 (3.5.6)
is valid. The visually tolerated color difference for chromatic metallic formulations is non-uniform as well. This is already known for absorption colors or colored lights. This conclusion is particularly clear for dark and pastel shades. The values of the empirical weighting factors gL , ga , . . . , gH in Equation (3.5.6) are given in Table 3.14 for different manufacturing steps. The correction functions SL , Sa , . . . , SH in Equations (3.5.5) and (3.5.6) follow also from the assessment of color collections: (3.5.7) SL (μ) = 0.15 L(μ) + (31.5◦ μ), Sa = Sb = 0.7, SC (μ) = max [0.7; 0.48 C(μ) − 0.35 L(μ) + (42◦ μ)], SH (μ) = max [0.7; 0.14 C(μ) − 0.2 L(μ) + (21◦ μ) + 0.7],
(3.5.8) (3.5.9) (3.5.10)
where L(μ) is the geometric mean of the lightness values of the sample color LS∗ (μ) and reference color LR∗ (μ), each at the same measuring angle μ:
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Table 3.14 Empirical weighting factors for color differences in Equations (3.5.5) and (3.5.6) Empirical weighting factors Condition
gL
ga
gb
gC
gH
Delivery First paint coating, refinishing paint, low-bake paint
1.0 2.0
1.0 1.2
1.0 1.2
1.0 1.8
1.0 1.2
L(μ) =
LS∗ (μ) · LR∗ (μ).
(3.5.11)
Also the function C(μ) is given by a geometric average, now of the chroma of the sample CS∗ (μ) and the reference color CR∗ (μ): C(μ) =
CS∗ (μ) · CR∗ (μ).
(3.5.12)
Concerning the correction functions (3.5.9) and (3.5.10), it is important to point out that, at first, the calculation is based on the algebraic expression. If the calculated value is less than 0.7, then it is set to 0.7, otherwise the relevant value ≥ 0.7 is inserted into Equation (3.5.6). At the switchover between the above-mentioned color areas, discontinuous color differences follow from Equations (3.5.5) to (3.5.6). This discontinuity issue is rectified using the Fermi function σ (μ). It is based on Equation (6.3.21) and given as σ (μ) =
1 1 + e[C(μ)−C0 (μ)]
,
(3.5.13)
where C0 (γ ) = 10 +
8 27−L(γ )] [ 1+e
(3.5.14)
is another angle-dependent correction function. The value domain of σ (γ ) is limited to the interval [0,1], cf. Fig. 6.18. The single valuedness of σ (μ) depends ∗ (μ) on the chroma value Cab σ (μ) =
∗ (μ) >> 10 0 for Cab ∗ (μ) 2, are of quite low luminosity and, due to the technically limited angle adjustment, are not measured. The curve shape in Fig. 3.32 looks altogether like an “unfinished treble clef.” Each diffraction order contains all wavelengths emitted by the applied source, which for a reflecting grating are given by Equation (2.1.24) in dependence of diffraction angle. Correspondingly, in the case of the xenon discharge lamp used, the chroma curve section of each diffraction order z > 0 extends over all four quadrants of the color plane. Because the intensity of the higher diffraction orders decreases quickly (Fig. 2.21), the accompanying chroma becomes also smaller. The spectra of higher orders tend, therefore, to achromatic colors. With increased diffraction order, the chroma curve always traces out smaller “ellipses” until these vanish in the achromatic point. If the illumination angle is increased with respect to the normal of the sample, then the chroma maximum at the specular angle shifts nearer to the start of the curve for μas = –35◦ . The corresponding height of the chroma maximum reduces due to increasing scattering at the grooves and the edges of the particles. However, the chroma curve in Fig. 3.32 includes the majority of the second diffraction order. This indicates that the grating geometry is not optimized because the intensities of the first two orders are each lowered by the higher orders.
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Chroma of Effect Pigments
223
∗ b
0°
40 10° –10° 20
40°
– 20°
78°
60°
0 30°
– 35°
20°
50° –20 –20
–10
0
10
a
∗
Fig. 3.32 Chroma curve respective effect line representing diffraction orders z = 0, 1, 2 of a two-layered pigment; illumination angle β = 45◦ ; parameter is the measuring angle with regard to the specular angle; grating constant 1,000 l/mm
However, in the range until the limiting measuring angle μas = 78◦ , the optimized diffraction particles with linear grating constant of 1,400 l/mm and sine-shaped groove cross section produce a chroma curve, which does not contain the order z = 2, cf. Fig. 3.33. This conclusion is also true for extrapolation to higher measuring angles on account of the curve sections always being smaller for higher angle decades to a maximum of μas = 135◦ . In comparison to the pigment with 1,000 l/mm, the curve section for z = 1 in Fig. 3.33 shows a chroma about double: the intensities of the order z = 0 and z ≥ 2 are mostly transferred to the diffraction spectrum for z = 1. This is achieved by the realized blaze technique for the present diffraction particles (Section 2.1.7). Particles consisting of right-angled crossed groove structure, each of 1,400 l/mm with sine-shaped groove cross section, produce the chroma curve shown in Fig. 3.34. The undeflected (zeroth) order and first diffracted order have lower chroma values than the linear grating of same grating constant compared to Fig. 3.33. This behavior is caused by mutually perpendicular crossed √ grooves, with which an additional grating constant of g˜ = (1,400/ 2) l/mm = 990 l/mm is introduced. Whereas the chroma of diffraction order z = 0 is nearly
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b∗ Linear
40
0°
50°
–10°
10°
60°
20 –20°
0
–35° 20°
–20
70°
40° 78°
30°
–40
–20
–10
0
10
20
a∗
Fig. 3.33 Chroma curve of an optimized linear sine-shaped diffraction pigment; grating constant 1,400 l/mm
the same as in Fig. 3.33, the new grating constant reduces the chroma of the higher orders in magnitude comparable to Fig. 3.32 for grating constant of 1,000 l/mm. Moreover, the combined perpendicular and diagonal grating structures produce an azimuthal anisotropy of chroma, which shows a periodicity of 45◦ for rotation of the sample vertical to its surface [83]. An increased linear grating constant of 3,000 l/mm leads, however, to a reduced chroma; in the chroma curves (not shown), the different diffraction orders are barely distinguishable. The reason for this is the more closely crowded grooves: at the edges and corners the light is increasingly scattered so that the remaining light intensity for diffraction is weakened. In addition, small-sized grating particles reduce the chroma caused by increased light scattering at the particle edges. Though it is inappropriate to arbitrarily extend the dimensions for the given pigments of d50 = 20 ± 2 μm, because the smaller groove distances lead to a stronger notch effect of the brittle particles. Such pigments are, depending on application method or processing, subject to increased mechanical degradation. Mixtures of diffraction pigments with other effect or absorption colorants have not been described in literature until now. On the basis of the correspond-
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225
b∗ Crossed 40
0° 10°
–10°
20 –20°
50° 20° –35° 0 70°
78° 40°
–20
30°
–40
–20
–10
0
10
20
a∗
Fig. 3.34 Chroma curve of a linear diffraction pigment with perpendicular crossed grooves; grating constant in both directions 1,400 l/mm
ing insight with interference pigments it is, however, sufficient to regard only the first-order diffraction and to estimate the chroma changes in dependence on the further added colorant fractions. With increased content of the additional pigment, the “diffraction ellipse” decreases and is pulled back into the color locus of the contained absorption or metallic pigment. As already discussed in Section 2.3.5, the optical anisotropy of diffraction pigments is additionally influenced by a substrate consisting of a ferromagnetic material such as nickel, for example. In a magnetic field, the grooves of elongated grating particles orient parallel to the lines of the field. If the particles are simultaneously subject to a shear gradient parallel to the direction of the magnetic field, then this alignment is preferentially fixed during crosslinking time of the binder. The particles are orientated similar to a smectic texture (Fig. 2.42). Ferromagnetic diffraction pigments of symmetrical permutation of layers MgF2 /Al/Ni/Al/MgF2 with a 400 nm thick coating of magnesium fluoride and linear grating constant of 1,400 l/mm appear brilliant metallic under diffuse illumination. With directional illumination however, these particles develop an
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impressive chroma. This chroma depends on the orientation of the grooves perpendicular or parallel to the optical measuring plane. The optical measuring plane is built from the illuminating and measuring beam. In the case of grooves preferentially oriented normal to the measuring plane, ∗ ≈ the first diffraction order shows an increased maximal chroma of about Cab 85 at an orange color of high brilliance; see outer curve in Fig. 3.35. In this alignment, the particles enhance the diffraction effect. This conclusion is clear by comparing Fig. 3.33: for the ferromagnetic pigment, the chroma values of the first diffraction order are in the domain 30◦ ≤ μas ≤ 78◦ . This is more than two times greater than that of the previously optimized non-ferromagnetic pigment. The chroma scale between both pigment orientations can be influenced by magnet field strength and exposure time. However, if the grooves are aligned parallel to the measuring plane, then the previous brilliant chroma development is almost lost. This is represented by the inner curve in Fig. 3.35. This chroma curve is shrunk. Only the specular color can be identified and the chroma of the first diffraction order degenerates to achromatic. Because the influx is oriented parallel to the grooves and not in the normal direction, nearly no real diffraction develops. In this case, the b∗ Measuring plane normal parallel
80
60°
0° 40
10° 50°
–10° –20°
20°
–35°
0
70°
30° –40 78°
–80 40°
–120 –60
–40
–20
0
20
40
a∗
Fig. 3.35 Chroma curves of a three-layered ferromagnetic diffraction pigment; grating grooves perpendicular and parallel to the measuring plane; grating constant 1,400 l/mm
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Chroma of Effect Pigments
227
incident light is attenuated by the covering MgF2 and essentially reflected off the aluminum layer. For diffuse illumination and right angle observation, ferromagnetic diffraction pigments with an additional cover layer of chromium Cr/MgF2 /Al/Ni/. . ./. . ./Cr produce a yellow-golden color impression. For directional illumination and measuring, however, the accompanying chroma curve changes dramatically, if the grooves are normal to the measuring plane, as can be seen in Fig. 3.36. Both particle alignments produce no “ellipses” around the achromatic point; furthermore, the chroma curves travel through at least two adjacent quadrants. This means that the zero and first diffraction orders are missing corresponding colors such as yellow-green, green, or blue. In the case where the grooves are normal to the measuring plane, the color impression oscillates with increased measuring angle only between yellow to orange-red to red-violet with increasing chroma. This particle alignment acts as an interference filter for blue to yellow-green wavelengths caused by the reflecting chromium and aluminum layers spaced by dielectric MgF2 , cf. Fig. 2.18. With the alignment parallel to the measuring plane, the first diffraction order is degenerated again near the achromatic point. This particle orientation behaves b∗
Measuring plane normal parallel
60
0° 60°
0° –10°
40
10°
–20°
–30° 20
–35°
50° 20°
–35°
70° 30°
78°
0
30°
78°
–20 40° –20
0
20
40
60
a∗
Fig. 3.36 Chroma curves of a four-layered ferromagnetic diffraction pigment; grating grooves perpendicular and parallel to the measuring plane; grating constant 1,400 l/mm
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like a dielectric mirror with a specular color of orange red. The brilliance and the diffraction colors as well as the filtered or reflected wavelengths are influenced by the thickness of the nonmetallic layer and the grating structure. To complete this picture, diffraction and interference are superimposed for these pigments and this gives rise to the extreme chroma curves restricted to the first quadrant of the color plane in Fig. 3.36. With the above description of ferromagnetic diffraction pigments, we finish the colorimetrical characterization of some special color physical properties of both absorption and effect colorants. The fact that the color development of effect colorants, which changes with illumination and observation angle, is mainly reproduced by different chroma curves is actually quite astonishing. However, the necessarily large extent of measuring brings a degree of impracticality. On the other hand, the methods for detailed coloristical description of colorations with flake-shaped effect pigments are by no means completed.
References 1. CIE 1931: “Proceedings of the Eighth Session”, Cambridge, England 1931; CIE, Bureau Central de la CIE, Paris (1931) 2. CIE S 014-1: 2006: “Colorimetry – Part 1: CIE Standard Colorimetric Observers”, CIE, Bureau de la CIE, Wien (2006) 3. CIE S 014-2: 2006: “Colorimetry – Part 2: CIE Standard Illuminants”, CIE, Bureau de la CIE, Wien (2006) 4. McAdam, DL: “Visual sensitivities to color differences in daylight”, J Opt Soc Am 32 (1942) 247 5. Brown, WRJ, McAdam, DL: “Visual sensivities to combined chromaticity and luminance differences”, J Opt Soc Am 39 (1949) 808 6. Wyszecki, G, Fielder, FH: “New color-matching ellipses”, J Opt Soc Am 61 (1971) 1135 7. CIE 1978:Supplement to CIE publication 15 (1971): “Recommendations on uniform colour spaces – colour difference equations; Psychometric Colour Terms”, CIE, Bureau Central de la CIE, Wien (1978); CIE S 014-3:2007: “Colorimetry – Part 4: 1976 L∗a∗b∗ Colour Space”, CIE, Bureau Central de la CIE, Wien (2008); ISO 11664-4: 2008 (E), Joint ISO/CIE Standard 8. “Munsell Book of Color”, Munsell Color Co, Baltimore, MD, USA (1929) until to day 9. CIE No 15.3: “Colorimetry”, 3d ed., CIE, Bureau Central de la CIE, Wien (2004) 10. Pauli, H: “Proposed extension of the CIE recommendation on ‘Uniform color spaces, color difference equations, and metric color terms’”, J Opt Soc Am 66 (1976) 866 11. Robertson, AR: “The CIE 1976 Color-Difference Formulae”, Col Res Appl 2 (1977) 7 12. Stokes, M, Brill, MH: “Efficient Computation of”, Col Res Appl 17 (1992) 410 13. DIN 6174: “Farbmetrische Bestimmung von Farbabstaenden bei Koerperfarben nach der CIELAB-Formel”, Deutsches Institut fuer Normung eV, Berlin (1979) 14. DIN 6176: “Farbmetrische Bestimmung von Farbabstaenden bei Koerperfarben nach der DIN99-Formel”, Deutsches Institut fuer Normung eV, Berlin (2001) 15. Cui, G, Luo, MR, Rigg, B, Roesler, G, Witt, K: “Uniform Colour Spaces Based on the DIN99 Colour-Difference Formula”, Col Res Appl 27 (2002) 282 16. Witt, K: “Buntheit mit System”, Farbe u Lack 111 (2005) 86 17. CIE No 116: “Industrial Colour-Difference Evaluation”, CIE, Bureau Central de la CIE, Wien (1995) 18. Clarke, FJJ, McDonald, R, Rigg, B: “Modification to the JPC79 Formula”, J Soc Dyers Col 100 (1984) 128 and 282
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19. CIE No 101: “Parametric Effects in Colour-Difference Evaluation”, CIE, Bureau Central de la CIE, Wien (1993) 20. Luo, MR, Cui, G, Rigg, B: “The development of the CIE 2000 colour difference formula: CIEDE2000”, Col Res Appl 26 (2001) 340 21. Chou, W, Lin, H, Luo, MR, Westland, S, Rigg, B, Nobbs, J: “Performance of lightness difference formulae”, Coloration Techn 117 (2001) 19 22. CIE No 142: “Improvement to Industrial Colour-Difference Evaluation”, Commission Internationale de L’Éclairage (CIE), Bureau Central de la CIE, Wien (2001) 23. Witt, K: “CIE color difference metrics”, in: Schanda, J, ed.: “Colorimetry: Understanding the CIE System”, Wiley, Hoboken, NJ (2007) 24. ASTM D 2244: “Standard Practice for Calculation of Color Tolerances and Color Differences from Instrumentally Measured Color Coordinates”, American Society for Testing and Materials, West Conshohocken, PA (2005) 25. Fairchild, MD: “Colour Appearance Models”, 2nd ed., repr, Wiley, Chichester (2006) 26. Luo, MR, Li, CJ: “CIE Colour Appearance Models and associated Colour Spaces”, in: Schanda, J, ed.: “Colorimetry: Understandig the CIE System”, Wiley, Hoboken, NJ (2007) 27. CIE No 159: “A colour appearance model for colour management systems: CIECAM02”, Commission Internationale de L’Éclairage (CIE), Bureau Central de la CIE, Wien (2004) 28. Luo, MR, Cui, GH, Li, CJ, Rigg, B: “Uniform color spaces based on CIECAM02 colour appearance model”, Col Res Appl 31 (2006) 320 29. DIN 6175-1: “Farbtoleranzen fuer Automobillackierungen”, part 1: “Toleranzen fuer Unilackierungen”, Deutsches Institut fuer Normung eV, Berlin (1986) 30. DIN 6175-2: “Farbtoleranzen fuer Automobillackierungen”, part 2: “Toleranzen fuer Effektlackierungen”, Deutsches Institut fuer Normung eV, Berlin (2001) 31. McDonald, R: “A Review of the Relationship between Visual and Instrumental Assessments of Colour Difference, Part I, II”, J Oil Col Chem Assoc 65 (1982) 43–53, 93–106 32. DIN Fachbericht 49: “Verfahren zur Vereinbarung von Farbtoleranzen”, Deutsches Institut fuer Normung eV, Berlin (1995) 33. ASTM D 3134–97(2008)e1: “Standard Practice for Establishing Color and Gloss Tolerances”, American Society for Testing and Materials, West Conshohocken, PA (2008) 34. ASTM E 1499–97(2003): “Standard Guide for Selection, Evaluation, and Training of Observers”, American Society for Testing and Materials, West Conshohocken, PA (2003) 35. von Kries, J: “Chromatische Adaption”, Festschrift der Albrecht-Ludwigs-Universitaet, Freiburg (1902) 145–158; reprint in: “Sources of Color Science”, MIT Press, Cambridge MA (1970) 109 36. CIE No 159: “A color appearance model for color management systems: CIECAM02”, CIE, Commission Internationale de L’Éclairage, Bureau Central de la CIE, Wien (2004) 37. Luo, MR, Li, CJ, “CIE Color Appearance Models and associated Color Spaces”, in: Shanda, J, ed.: “Colorimetry”, Wiley-Interscience, New York (2007) 38. Ostwald, W: “Farbenlehre”: Vol 1: “Mathematische Farbenlehre”, 2nd ed., Unesma, Leipzig (1930); Vol 2: “Physikalische Farbenlehre”, Unesma, Leipzig (1923) 39. Kang, HR: “Computational color technology”, SPIE Press, Bellingham (2006) 40. DIN 6172: “Metamerie-Index von Probenpaaren bei Lichtartwechsel”, Deutsches Institut fuer Normung eV, Berlin (1993) 41. CIE No 80: “Special Metamerism Index: Change in Observer”, Commission Internationale de L’Éclairage (CIE), Bureau Central de la CIE, Wien (1989) 42. DIN 55978: “Bestimmung der relativen Farbstaerke in Loesungen, Spektralphotometrisches Verfahren”, Deutsches Institut fuer Normung eV, Berlin (1981) 43. DIN 55603: “Pruefung von Pigmenten – Bestimmung der relativen Farbstaerke und des Restfarbenabstandes von anorganischen Pigmenten in Weissaufhellungen nach dem Helligkeitsverfahren”, Deutsches Institut fuer Normung eV, Berlin (2003)
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44. DIN 53235-1: “Pruefung von Pigmenten – Pruefungen an standardfarbtiefen Proben – Part 1: Standardfarbtiefen”, “Pruefung von Pigmenten – Pruefungen an standardfarbtiefen Proben – Part 2: Einstellen von Proben auf Standardfarbtiefe”, (2005); Deutsches Institut fuer Normung eV, Berlin 45. DIN 53235-2: “Pruefung von Pigmenten – Pruefungen an standardfarbtiefen Proben – Part 2: Einstellen von Proben auf Standardfarbtiefe”, (2005); Deutsches Institut fuer Normung eV, Berlin 46. DIN 55987: “Bestimmung des Deckvermoegenswertes pigmentierter Medien”, Deutsches Institut fuer Normung eV, Berlin (1981) 47. ASTM D 2805 – 96a(2003): “Standard Test Method for Hiding Power of Paints by Reflectometry”, American Society for Testing and Materials, West Conshohocken, PA (2003) 48. ASTM D 6441–05: “Standard Test Methods for Measuring Hiding Power of Powder Coatings”, American Society for Testing and Materials, West Conshohocken, PA (2005) 49. ISO 6504-3:2006: “Paints and varnishes – Determination of hiding-Power – Part 3: Determination of contrast ratio of light-coloured paints at a fixed spreading rate”, International Organization of Standardization, Genf (2006) 50. DIN 55984: “Bestimmung des Deckvermoegenswertes von weissen und hellgrauen Medien”, Deutsches Institut fuer Normung eV, Berlin (1986) 51. DIN 55988: “Bestimmung der Transparenzzahl (Lasur) von pigmentierten und unpigmentierten Systemen”, Deutsches Institut fuer Normung eV, Berlin (1989) 52. ASTM D 1746–03: “Standard Test Method of Transparency of Plastic Sheeting”, American Society for Testing and Materials, West Conshohocken, PA (2003) 53. DIN EN ISO 105 – A01: “Textilien – Farbechtheitspruefungen – Part A01: Allgemeine Pruefgrundlagen (ISO 105-A01:2008)”, Deutsches Institut fuer Normung eV, Berlin (2008) 54. DIN EN ISO 105, A06: “Textilien – Farbechtheitspruefungen – Part A06: Farbmetrische Bestimmung der 1/1 Richttype (ISO 105-A06:1995)”, Deutsches Institut fuer Normung eV, Berlin (1997) 55. Graystone, J: “Journeys into Colorspace”, Surf Coat Int, Part B Coat Trans, 87 (B3) (2004) 221 56. ISO 4582:2007: “Plastics – Determination of changes in colour and variation in properties after exposure to daylight under glass, natural weathering and laboratory sources”, International Organization of Standardization, Genf (2007) 57. ISO 11507:2007: “Paints and varnishes – Exposure of coatings to artificial weathering – Exposure to fluorescent UV lamps and water”, International Organization of Standardization, Genf (2007) 58. ISO 4892-1/4: “Plastics – Methods of exposure to laboratory sources; Part 1: General Guidance; Part 2: Xenon-arclamps; Part 3: Fluorescent and UV-lamps; Part 4: Open-flame carbon-arc lamps”, International Organization of Standardization, Genf (1999–2006); identical with: DIN EN ISO 4892-1/4: “Kunststoffe – Kuenstliches Bestrahlen oder Bewittern in Geraeten”, Deutsches Institut fuer Normung eV, Berlin (2000–2001) 59. ISO 105-J05: “Textiles – Test for colour fastness – Part J05: Instrumental assessment of change in colour for determination of grey scale rating”, International Organization of Standardization, Genf (1997); identical with: DIN EN ISO 105-J05: “Textilien – Farbechtheitspruefungen – Part J05: Instrumentelle Bewertung der Aenderung der Farbe zur Bestimmung der Graumassstabszahl”, Deutsches Institut fuer Normung eV, Berlin (1997) 60. ISO 105-J02: “Textiles – Test for colour fastness – Part J02: Instrumental assessment of whiteness”, International Organization of Standardization, Genf (1998) 61. ASTM E 313–05: “Standard Practice for Calculating Yellowness and Whiteness-Indices from instrumentally measured Color Coordinates”, American Society for Testing and Materials, West Conshohocken, PA (2005)
References
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62. DIN 6167: “Beschreibung der Vergilbung von nahezu weissen oder nahezu farblosen Materialien”, Deutsches Institut fuer Normung eV, Berlin (1980) 63. ASTM D 1003 – 07e1: “Standard Test Method for Haze and Luminous Transmittance of Transparent Plastics”, American Society for Testing and Materials, West Conshohocken, PA (2007) 64. DIN 55923: “Pigmente: Aluminiumpigmente und Aluminiumpigmentpasten fuer Anstrichfarben”, Deutsches Institut fuer Normung eV, Berlin (1983) 65. DIN 50017: “Kondenswasser-Pruefklimate”, Deutsches Institut fuer Normung eV, Berlin (1982) 66. DIN EN ISO 6270-1/4: “Beschichtungsstoffe – Bestimmung der Bestaendigkeit gegen Feuchtigkeit (ISO 6270)”, Deutsches Institut fuer Normung eV; Part 1–4 (2002 – 2007) 67. DIN EN ISO 9227: “Korrosionspruefung in kuenstlichen Atmosphaeren – Salzspruehnebelpruefungen (ISO 9227:2006)”, Deutsches Institut fuer Normung eV, Berlin (2006) 68. DIN EN ISO 2810: “Beschichtungsstoffe – Freibewitterung von Beschichtungen – Bewitterung und Bewertung (ISO 2810:2004)”, Deutsches Institut fuer Normung eV, Berlin (2004) 69. Wissling, P et al.: “Metallic Pigments”, Vincentz, Hannover (2007) 70. Kelly, RJ: “Process for matching color of paint to a colored surface”, US Patent No 4692481, DuPont Nemours and Company, Wilmington, Del (1987) 71. ASTM D 5767 – 95(2004): “Standard Test Methods for Instrumental Measurement of Distinctness-of-Image Gloss of Coating Surfaces”, American Society for Testing and Materials, West Conshohocken, PA (2004) 72. ASTM E 430 – 05: “Standard Test Methods for measurement of Gloss of High Gloss Surfaces by Abridged Goniophotometry”, American Society for Testing and Materials, West Conshohocken, PA (2005) 73. Kigl-Boeckler, G: “Total Color Measurement of Effect Finishes”, ECS Nuernberg, Nuernberg (2007) 74. Gabel, PW, Hofmeister, F, Pieper, H: “Interference Pigments as Focal Point of Color Measurement”, Kontakte (Darmstadt) 2 (1992) 25 75. Cramer, WR, Gabel, PW: “Effektvolles Messen”, Farbe Lack 107(1) (2001) 42 76. Nadal, ME, Early, EA: “Color measurements for pearlescent coatings”, Col Res Appl 29 (2004) 38 77. Droll, FJ: “Stunning Views”, PPCJ 191(4441) (2001) 78. ASTM E 2194–03: “Standard Practice for Multiangle Color Measurement of Metal Flake Pigmented Materials”, American Society for Testing and Materials, West Conshohocken, PA (2003) 79. ASTM WK 1164: “New Standard Practice for Multiangle Color Measurement of Interference Pigmented Materials”, American Society for Testing and Materials, West Conshohocken, PA (2006) 80. ASTM E 2539–08: “Standard Practice for Multiangle Color Measurement of Interference Pigments”, American Society for Testing and Materials, West Conshohocken, PA (2008) 81. DIN 6175-3: “Farbtoleranzen fuer Automobillackierungen”, Part 3: “Messgeometrien fuer Interferenzpigmente”, draft, Deutsches Institut fuer Normung eV, Berlin (2006) 82. Cramer, WR, Gabel, PW: “Dreiecksbeziehungen aus Bunt-, Aluminium- und Interferenz-Pigmenten”, Farbe u Lack 109(10) (2003) 78 83. Argoitia, A, Witzman, M: “Pigments exhibiting diffractive effects”, Soc Vacuum Coaters, 45th Ann Techn Conf Proc (2002) 84. Argoitia, A, Chu, S: “The concept of printable holograms through the alignment of diffraction pigments”, Flex Prods Inc, Santa Rosa, CA (2002)
References
Color plate 1. Top: subtractive color mixture; bottom: additive color mixture
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y
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Color plate 2. CIE 1931 x, y chromaticity diagram
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y 0.8
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Color plate 3. McAdam ellipses of same visual color impression enlarged 10 times
x
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Yellow
Hue
Green
Red
Blue Color plate 4. A color plane of CIELAB space (source: Konica-Minolta, Langenhagen/ Hannover, Germany)
References
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White
Yellow
Green
Red
Blue
Black Color plate 5. Three-dimensional approximate representation of CIELAB color space for absorption colors: color loci of effect colorations for L*> 100 are represented in a higher cylinder (source: Konica-Minolta, Langenhagen/Hannover, Germany)
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Color plate 6. CMC tolerance ellipses in a color plane of the CIELAB space (source: x-rite GmbH, Köln, Germany)
References
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Color plate 7. Light microscopic images of pearlescent pigments with mica substrate in bright-field illumination: top: coated with titanium-dioxide (rutile), the particles appear yellow from the top view; bottom: coated with iron-III-oxide (α-hematite), the particles appear deep red from the top view (source: Clariant Produkte GmbH, Frankfurt am Main, Germany)
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Color plate 8. Light microscopic images of a red pearl luster pigment with mica substrate coated with titanium-dioxide (rutile) of greater thickness than those in color plate 7; top: in bright-field, bottom: in dark-field illumination of the same frame (source: Clariant Produkte GmbH, Frankfurt am Main, Germany)
References
241
Color plate 9. Light microscopic images of an optically variable green/purple interference pigment of aluminum substrate coated with chromium and magnesium-fluoride; top: brightfield, bottom: dark-field of the same frame (source: Clariant Produkte GmbH, Frankfurt am Main, Germany)
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Color plate 10. Light microscopic images of a blue liquid crystalline interference pigment of polysiloxane, both over black background; top: bright-field, bottom: dark-field of the same frame (source: Clariant Produkte GmbH, Frankfurt am Main, Germany)
References
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Color plate 11. Light microscopic bright- and dark-field image of an effect coloration of yellow-gold color impression from the top view; the images show mixed metallic, pearlescent and absorption colorants; top: bright-field, bottom: dark-field of the same frame (source: Clariant Produkte GmbH, Frankfurt am Main, Germany)
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Color plate 12. Light microscopic bright- and dark-field image of a brown effect color coating from the top view; the images show mixed pearl luster and absorption pigments; top: bright-field, bottom: dark-field of the same frame (source: Clariant Produkte GmbH, Frankfurt am Main, Germany)
Chapter 4
Measuring Colors
At the beginning of the previous chapter, empirical color value systems suitable for numerical quantification of color impressions were described. A fundamental requirement for such systems is an accurate and precise measurement of the spectral reflectance or transmittance of the relevant color patterns. This necessity comes down to the fact that the retinal color stimulus is caused by the spectral reflection or transmission of the colored object, among other things. Accordingly, the measuring result should agree with the visual impression as well as possible. Color measuring instruments have been established and used since about 1960. Today, they are indispensable pieces of equipment for industrial color physics. Color measuring and especially the clear interpretation of the results require extensive knowledge and experience with regard to the underlying visual, color physical, and metrological interrelations. The measurement quantities are of importance for answering questions in research and development, quality control, and process control or application techniques. Moreover, the measurement results offer an objective base for realistic color tolerance agreements. For such agreements, the people involved should be familiarized with the measuring conditions, performance features of the instruments used, the meaningfulness, and trustworthiness of the measuring quantities. The technological progress attained with regard to color measuring instruments has, however, often been overrated, especially concerning the measuring uncertainty. Undoubtedly, the improvement of component parts has contributed to an increased reliability of the measured quantities and extent of information. Such components include high-resolution reflection gratings or photodiodes with half-width of about 5 nm, cleverly designed interconnect elements for optical wave guides, high-speed microprocessors, and storage mediums of several terabytes at the time of this writing. On the other hand, for measurement of colors, one must take into consideration three fundamental points. These are perhaps self-evident, but nevertheless pointed out explicitly at this stage:
G.A. Klein, Industrial Color Physics, Springer Series in Optical Sciences 154, C Springer Science+Business Media, LLC 2010 DOI 10.1007/978-1-4419-1197-1_4,
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1. The measured values obtained from a color pattern represent the actual physical state at the moment of measurement; even if the measurement is of the highest quality, it is useless, if the color sample does not maintain the required color physical state. 2. The sensitivity of color measuring instruments is already about an order of magnitude better than the visual color sensitivity of even a practiced colorist! Further reductions in measurement uncertainty below this level are, therefore, unnecessary for color industry. 3. Although the result of a color measurement is at present accurate to at least three digits, the final human visual impression determines if the actually measured color pattern is acceptable or not. Experience shows that the combination of subjective visual judgment and objectively obtained color characteristics can be quite successful. These considerations are the subject to a more detailed discussion in the following. At first, we clarify the double meaning of the term color measurement and describe useful requirements for visual and metrological execution of color measurement. Moreover, the measurement geometries proposed by the CIE and the most important color measuring procedures are discussed [1–8]. In addition, we give suggestions for preparation and conditioning of color patterns. With regard to effect pigments, additional measurement methods are given. Finally, we discuss in detail the assessment of measurement uncertainty and statistics of chromaticities. These are indispensable for visual color matching, tolerance agreement, and quality control, among other things.
4.1 Measurement of Reflecting and Transmitting Materials Among the three factors contributing to the color impression of non-selfluminous colors, the final decision maker, as mentioned previously, is undoubtedly the observer. Simply put, in color measuring techniques, the observer is substituted by the color measuring instrument and computer. This substitution follows, e.g., also by comparison of Figs. 2.29a and 4.1, for example. More precisely, the optical image formation by the eye and the trichromatic elements of the retina are simulated by the optical components and photodiodes of the measuring instrument. The transfer of the trichromatic stimulus to the visual cortex and its assessment by the brain are simulated by analog–digital converters interfaced with a computer using suitable software. These days, this software includes the majority of the colorimetrical relations given in Chapter 3 as well as right designed graphic diagrams. Furthermore, it is important to stress that the characteristics and quantities which result from color measurements are also merely representatives of the special spectral or colorimetric properties of the relevant color pattern. The
4.1
Measurement of Reflecting and Transmitting Materials
Fig. 4.1 Principle sketch of a color measuring equipment; the observer is substituted by the measuring instrument and computer, cf. Fig. 2.29a
235 Computer X, Y, Z, L, a, b
Monochromator, Analog-digital converter Light source
Sample
interpretation and judgment of the numerical or graphical results should be carried out by experienced colorists. Often, the subjective color sensation is the decisive factor, because the colorimetrical formalisms only approximately imitate the nonlinear peculiarities of human color sense.
4.1.1 Measurement of Colors and Visual Judgment To measure means to compare. In the context of colors, to compare has a double meaning, namely metrological and visual. In the first case, a property which we are interested in is compared quantitatively with a suitably chosen reference color or standard; in the second case, the comparison is performed using the subjective color sense. First, we consider the fundamental aspects of quantitative measuring of color characteristics. Then, we go into the peculiarities which need to be taken into account for visual comparisons. Already from the law of energy conservation, it is known that light interactions in optical materials can cause effects such as reflection and transmission. The reflection of a layer is comprised of at least two superimposed principle components: backscattering from the volume and reflection from the interfaces. Reflection can be not only directional or partly directional but also diffuse or mixed such as partly diffuse, depending on the main directed or diffuse component (cf. Fig. 2.28). In some cases, the angle-dependent diffuse reflection of a matt surface obeys the Lambert law I(ϑ) = A · B · cos ϑ,
(4.1.1)
where I(ϑ) is the luminous intensity which is reflected into angle ϑ with respect to the face normal of a completely diffuse reflecting surface of size A and luminance B. A diffuse reflecting field satisfying this law is called Lambert radiator.
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On the other hand, even the specular reflection of a highly glossy color pattern or one with metallic pigments is superimposed with a quite small, but detectable diffuse component. Reflectance measurements are performed with regard to two so-called standards which serve as fixed points on the photometer scale. With the blackbody at absolute zero, the theoretical zero point of the photometer scale is established. At this temperature, the blackbody radiator emits no light but absorbs all entering light (Section 2.1.2). In practice, however, a hollow body of napped black interior called blackbody trap is used. The second fixed point of the photometer scale is given by a white standard, which – ideally – reflects, respectively scatters, the incident light completely. The spectral values obtained from the white and black standards are corrected in a suited manner and interpreted as 0.00 and 100.00% reflectance, respectively. The scale between both points is linearly subdivided and called photometer scale. This scale is applied to all sorts of colorants, the reason why colorations containing effect or fluorescence colorants attain apparent reflectance values of R > 100% or lightness values of L > 100. However, to this day, an ideal white standard does not exist. Such a standard is only realized approximately, e.g., by a freshly pressed layer of powdered BaSO4 or polytetrafluorethylene (PTFE). Both materials show a wavelength-dependent reflectance of about 98.5% in the visible range. This value is determined from the ratio of the reflected spectral energy of the white standard to the emitted spectral energy of the illuminating source. Other materials of high spectral reflectance such as MgO or ZnO are, on account of process reasons, very rarely used as white standards these days [1]. Altogether, there exist three different sorts of standards for measuring colors. The relevant quality levels arise from the following rank order: 1. Primary standard is manufactured and certified by a Bureau of Standards.1 The remarkable features of such a primary standard are the highest possible technical precision and greatest dependability. 2. Transfer standard is calibrated using a primary standard; it is preferentially employed by instrument manufacturers for calibration of reference (master) instruments. 3. Secondary standard is calibrated in turn on the basis of a transfer standard; this type of standard is enclosed within the measuring instrument; its photometric scale is previously calibrated with such black and white standards. Secondary standards are only really designed to use for scaling of the accompanying instrument during operation.
1 For
example: National Institute of Standards and Technology (NIST), Gaithersburg, MD, USA; Community Reference Bureau (CRB) of the European Union, Bruxelles, Belgium; Physikalisch-Technische Bundesanstalt (PTB), Braunschweig, Germany.
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In the case of transparent materials, the determination of transmission seems to turn out easier. Transmission is a measure for transparency of a material; it is reduced by interface reflection, absorption, and scattering. Clearly, the transmission can occur not only directionally or partly directionally but also diffusely or mixed such as partly diffusely. There does not exist a specific standard for the determination of the transmittance of a material. Rather the spectral intensity of the light source – without any sample – receiving the detector for closed and opened aperture diaphragm is simply interpreted as 0.00 and 100.00% transmittance, respectively. However, the measurement of transmittance is often influenced by heterogeneities at the interfaces of the relevant material. For non-self-luminous colors, there also does not exist unambiguously defined color standards. Certainly it is useful within itself to check the linearity of the gray scale of color measuring instruments with regard to the reflective factors in the domain 0 ≤ R(λ) ≤ 1.0 with tiles of so-called BCRA II ceramic.2 This consists of an entire set of 12 colored and hueless tiles which, for years ahead, have turned out to be almost color constant in appropriate storage conditions. Actually, the reflection of these patterns depends slightly on azimuthal angle. This influence can be excluded by repeated measurements in which the same measuring spot at the same orientation is always used. Otherwise gonio spectrophotometers can fake a falsely calibrated angle scale. Known and reproducible wavelengths of illuminant sources are used for calibration of the wavelength scale of a color measuring equipment. Such sources are also used to characterize light colors of sources, LEDs, screens, or panels. In order to cover the range of interest, devices such as the gas discharge of helium, mercury, and sodium vapor lamps are used. These sources emit different numbers of sharp spectral lines of known wavelengths in the visible range: He emits 18 lines in the interval 365.0 nm ≤ λHe ≤ 690.7 nm, Hg shows 12 lines in the domain 370.5 nm ≤ λHg ≤ 728.1 nm, and Na merely the pair of lines 589.0 and 589.6 nm. For inspection of the angle scale of gonio spectrophotometers, there exist no obligatory standards until now. As experience shows, each scaling depends on temperature and humidity of the surroundings, the instrument construction, and the standards used. The calibration should, therefore, be performed in operating conditions. Furthermore, the instrumentation and the secondary standards should not be exposed to higher fluctuations of temperature and humidity than specified by the manufacturer. Generally, the best situation is an installation of the instrument and secondary standards in a constant standard climate at temperature ϑ = 20◦ C and atmospheric humidity of 50%.
2 BCRA Series II Ceramic Standards: previously manufactured by British Ceramic Research Association, nowadays by Ceram Research, Penkhull, UK.
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The visual assessment of colors turns out to be the something more problematic; this can by no means be ignored. After all, the entire coloring efforts are oriented toward the human color sense. Clearly, only people with normally developed color perception should be involved in the assessment of colors. The capability of the individual color perception should be checked at regular intervals, and the test should be passed with the Ishihara color panels [9], even better with the Nagel anomaloscope [10], or with another standard [11]. In addition, also the ability to distinguish colors can be selectively reduced or unequally developed (color amblyopy). This also needs to be checked with a visual color test. Moreover, possibly the CMFs of joined observers differ from each other and deviate from those of both CIE standard observers. This observer metamerism needs to be considered by the involved people. The visual judgment is performed not only between similar colorations but can also include a great variety of special colorations. The systematic comparison of sample colors (sample, test, pattern) with reference colors (reference, standard, target) is called equality method. A sample color can be compared with special own standards of the manufacturer, reference colors, a systematic color collection, a pattern collection selected from manufacturing, or with patterns of a color-order system, among other things. A disadvantage of the equality method is the subjective judgment of the colorist – this often turns out to be too strict. For more objective methods, however, the tristimulus and the spectral measuring methods are available (Sections 4.2.1 and 4.2.2). In case of routine examinations under daylight conditions, it is sufficient to expose the colors to diffuse north skylight in the northern hemisphere and to diffuse south skylight in the southern hemisphere. In each of these cases, the skylight should be incident through windows which are as high as possible. During the visual comparison under artificial illumination, of course, it is necessary to meet at least the CIE reference conditions. In a light booth for color judgment, the illuminants that correspond to the colorations to which the color will presumably be exposed in future are to be activated. The basic equipment of a standardized booth includes simulators of illuminants D65, A, FL 2, FL 11 as well as two UV sources of defined bandwidth for stimulation of fluorescence emission [12, 13]. Due to a general lack of time in practice, often the sources are switched in fractions of a second among the various illuminants which means within the short-termed chromatic adaption phase. This procedure is certainly left for only experienced colorists; otherwise, it is better to wait for the longer adaption phase. Special diligence and experience are necessary, if equal colorations are to be compared with each other in different binders or of different surface structures. Further critical color aspects may arise with colorations containing effect and absorption pigments. In most cases, problems emerge by comparing the angledependent lightness or color flop, brilliance, or covering capacity. These require intensive training in color perception in unusual domains of a color space as well
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239
as a sensitive interpretation of spectral reflectance and transmittance or rather of the relevant color values.
4.1.2 Measurement Geometries Instrumental color measurements are performed with different light sources and detectors for wavelength-dependent measurement of the reflected or transmitted light of a color pattern. The term measuring geometry refers to the kind of illumination of the color sample and the placement of the measuring detector. The choice of the measuring geometry depends on the consistency of the color pattern, the surface structure, and in particular, the sorts of colorants. From the accompanying measurement results, it is expected that they agree with the visual impression. Among the whole host of possible combinations, the CIE proposed four measuring geometries for measurements of opaque materials [14]. These can be gathered into two groups: – directional geometries 45:0, 0:45, – spherical geometries d:0, 0:d. The indication 45:0 stands for influx at 45◦ and measurement at 0◦ , e.g., perpendicular to the sample surface; d:0 means diffuse illumination and measurement at 0◦ . The inverse geometries produce identical results because the reversal of a light path has no influence of the effect – this is a fundamental principle of geometrical optics [15]. For absorption and effect pigments, in addition, there are – variable directional geometries β:μ, μ:β or β/μ, μ/β available, which were not proposed by the CIE until now. Before we discuss further details of these geometries, it is necessary to comment on the nomenclature. The measured quantity of opaque color patterns is assigned to a standardized term which depends on the chosen measurement geometry [16]: – reflection factor ρ: beam focused to conical illumination and semi-spatial observation (0:d, 8:d); – reflectance R: semi-spatial illumination and conical observation (d:0, d:8); – radiance factor β: illumination and observation are directional (45:0, 0:45; β/μ, μ/β).
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Be aware of the fact that β stands for either the angle of illumination or the radiance factor. For measurements of transmittance of transparent materials, corresponding terms such as transmittance factor τ and transmittance T have been introduced (see also end of this section). In the following, we discuss the directional geometries, followed by the spherical geometries, and those proposed for measuring transmittance. 4.1.2.1 Directional Measuring Geometries In the simple case of directional geometry, a light beam is incident at an angle β v = 45◦ to the surface of a colored sample; the measurement is carried out normal to this surface, corresponding to an angle μv = 0◦ . This configuration is denoted as the 45:0 measurement geometry and is shown schematically in Fig. 4.2a. The detector takes on the function of the observer. Permutation of source and detector is indicated by 0:45, as shown in Fig. 4.2b. The designation and way of counting of angles are described below and can be taken from Figs. 4.5 and 4.6.
Fig. 4.2 Directional measuring geometries: (a) 45:0 and (b) 0:45
Instrument manufacturers these days prefer the installation of the 45:0 geometry. This configuration has the advantage that the specular beam or ray cone reflected by an even and glossy sample is excluded from the measurement. Primarily, the reflection coming from the volume is registered. The 45:0 geometry corresponds to the observation method of colorists. Therefore, the measuring result agrees best with visual judgment. This conclusion is also correct for minor glossy, matt, or structured surfaces because this measuring arrangement only registers the outward flux at an angle μv = 0◦ . For a color sample of an incompletely homogeneous surface, illumination from opposite sides, each at an angle of β v = 45◦ , is suitable. This configuration is shown in Fig. 4.3a. Instead of two or more lamps, alternatively only a single source can be used. In this case, the source illuminates the color sample in combination with a circular 360◦ mirror at an angle β v = 45◦ . The sample
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241
Detector
Detector Source
Source
45°
45°
45°
Sample
Sample
a)
b)
Fig. 4.3 Directional measuring geometries: (a) bidirectional 45bi:0 geometry and (b) circular 45c:0 geometry
is, therefore, illuminated circularly. For distinction, this measuring geometry is denoted as 45c:0 and shown in Fig. 4.3b. When applying this geometry, inhomogeneous surfaces have nearly no influence on the spectrometric or colorimetric results. With the 45c:0 configuration, it cannot be determined through the measurement whether the color producing mechanism of the sample is caused by a volume or surface effect or both. However, this differentiation is of particular importance for colorations with optically anisotropic pearlescent, interference, or diffraction pigments. The characterization of the angle-dependent interference and diffraction orders needs a so-called gonio spectrophotometer with variable directional geometry β/μ. In the simplest version, such a color measuring device has an illumination at a fixed angle β v = 45◦ and a detector of variable measuring angle μas with respect to the specular angle. In convenient instruments, the angles of the illumination and measuring are adjustable to a large extent and independent of one another. In Fig. 4.4, the principle of such a gonio spectrophotometer is represented. This configuration has an illumination angle of β v = 45◦ and, for simplicity, only four measuring angles μas = 25◦ , 45◦ , 75◦ , and 110◦ . This device is exclusively used for measurements of colors containing metallic pigments [17, 18]. Recently, standardized reflectance measurements have begun to be carried out at two additional angles of μas = 15◦ and –15◦ , also out of plane. However, these four to six measuring angles are not sufficient for clear colorimetrical characterization of effect colorations. At this stage, it is necessary to explain a clear method for angle counting of measurements with goniospectrophotometers. In ASTM and DIN standards for
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Specular direction
45°
25°
75°
110° 45°
45°
Fig. 4.4 Principle of a gonio spectrophotometer of variable directional geometry with only four standardized measuring angles following DIN or ASTM [17, 18]
measuring interference pigments [19, 20], the measuring geometry is denoted for given illumination and measuring angle in the form β v /μas ; see Fig. 4.5. Illumination angles β v are with respect to the normal to the sample surface; however, the measuring angle μas is with respect to the specular angle. The sign of μas is positive in direction toward the source. The aspecular angle is sometimes termed the effect angle in the literature, though there exist two nonstandardized ways of angle counting with regard to the horizontal (β h /μh ) and vertical (β v /μv ) for both angles; cf. Fig. 4.6. The instrument industry supplies gonio spectrometers of fixed illumination angles in the range 0◦ < β v < 90◦ , and also variable illumination up to β v = 360◦ . Measurements can be carried out normally at six standardized angles μas = –15◦ , 15◦ , 25◦ , 45◦ , 75◦ , 110◦ , or at variable angles which, in an extreme case, are adjustable with steps of 1◦ in the angle domain –35◦ ≤ μas ≤ 78◦ . Such a large number of independent angles of illumination and measurement are especially needed for pearlescent, interference, and diffraction pigments
μas = 0 + μas
Fig. 4.5 Fixing of the sign for aspecular measuring angle μas with respect to the specular beam following ASTM and DIN [19, 20]
βv
βv
– μas
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Measurement of Reflecting and Transmitting Materials
Fig. 4.6 Non-standardized illumination and measuring angle pairs for angledependent measurements, with respect to the horizontal β h /μh and to the vertical β v /μv of the sample surface
243
βv
μv μh
βh
(Sections 3.5.3, 3.5.4, and 3.5.5 and [21–25]). For approximate recipe prediction and adjustment of color recipes with effect colorants, measurements at one illumination angle and at least five measuring angles are needed. Such multiple angle measuring geometries are also suitable for investigations of azimuthally dependent effects, e.g., orientation of colored particles or flakes in flow direction especially in high viscous states of high solid lacquers or melts of high polymers. This is valid for marbleizing effects with absorption pigments as well as homogenized sparkling flakes. Such investigations by measurement are performed at defined azimuthal angles and at different points of the sample surface. Altogether, the reflection values resulting from measurements with a gonio spectrophotometer are relative quantities provided that the investigations are performed with respect to a BaSO4 secondary standard. This standard shows an angle-dependent radiance factor and, in comparison to the 45:0 geometry, leads to large deviations in the vicinity of the specular direction. The color values following with this standard can be interpreted as dependent quantities of the spectrophotometer used. Color values of different effect pigments can, therefore, only be compared with one another if the measurements are also based on the same reflection standard and the same instrument. In Table 4.1, available devices with directional or diffuse measuring geometries are listed in order of the type of illumination as well as respective application situations.
4.1.2.2 Diffuse Measuring Geometries The measuring configurations d:0 and 0:d, which are recommended by the CIE, are not explicitly itemized in Table 4.1. These are, however, approximated by the measuring geometries d:8 and 8:d. The notation d:0 means diffuse illumination and directional measurement at an angle μv = 0◦ ; see Fig. 4.7. The emitted light of a source is reflected in different directions at the interior surface of a suitable coated Ulbricht sphere (e.g., powder coated with PTFE). The sample
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Table 4.1 Measuring geometries with directional or diffuse illumination and proposed applications
Illumination
Measuring geometry
Directional
45:0 45:0 bidirectional 45c:0 circular β v /μas gonio spectrophotometer
Diffuse
di:8
de:8
Suitable applications or advantages Smooth, slightly brilliant to high glossy surfaces; specular beam excluded; fluorescent materials Non-uniform, structured, dull to high glossy surfaces; Transparent to opaque materials, dependent on measuring method; agreement of colorimetrical with visual impression Anisotropic, transparent to opaque samples with absorption or effect pigments, all sorts of colorant mixtures; determination of reflection indicatrix Smooth, slightly brilliant surfaces of transparent to opaque materials; agreement of colorimetrical with visual impression; numerical subtraction of specular gloss; color recipe prediction Smooth to glossy, transparent to opaque color samples; specular beam excluded
is consequently nearly diffusely illuminated. In modern instruments, the measuring receiver is not positioned at μv = 0◦ , but rather at an angle μv = 8◦ ; the CIE even allows a deviation of up to 10◦ [14]. As can be seen below, this displacement has some metrological advantages. The diffuse measuring geometry d:8 is versatile enough to be used for absorption colorants and also to survey effect colorants. This geometry is schematically represented in Fig. 4.8. An advantage of the d:8 configuration is that light incident with an angle 8◦ regarding the normal of the sample surface can be included in or excluded from the measurement. In other words, the specular component can be incorporated in or eliminated from the result. Therefore, it is necessary to differentiate between the diffuse geometry with included specular reflection di:8 and excluded specular component de:8. With an absorbing specular light trap installed, the specular component can be excluded from the measurement. Without a light trap, the specular reflection at angle μv = 8◦ is included in the result. Consequently, with sphere geometry has always to be indicated the applied measuring modus. The specular component, which is included in the di:8 measurement modus, can be later numerically subtracted from the result. The resulting spectral values of even or glossy color patterns are nearly identical to those of the de:8 modus. The following color values agree well with the visual impression, analogous to
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245
Detector d:0
Source
Sample
Fig. 4.7 Sphere geometry d:0
d:8
Detector
Light trap
Source
8°
Sample
Fig. 4.8 Sphere geometry d:8 with specular light trap
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results with the 45c:0 geometry. However, from semi-matt or matt colors, only a fraction of the specular reflected component at the angle 8◦ reaches the light trap. The measurement results lead to color values of higher lightness in comparison to the visual impression. In this case, the numerical subtraction of the specular reflection leads to false color values. This means that the de:8 geometry is only suitable for measuring of even or glossy color patterns. On account of the included specular component of the di:8 geometry, it is impossible to discern different surface structures, that is, different textures result in nearly equal color values. The measurement results of matt and structured color samples deviate somewhat from the visual impression. In this case, the 45c:0 geometry is more suitable. The spherical geometry with di:8 modus is preferentially applied for color recipe prediction, if matt or structured color patterns of unknown colorant composition are manufactured with smooth or glossy surfaces. In any case, the choice of the measuring geometry should be considered carefully (cf. Section 4.1.5). When in doubt, the possibilities should be examined experimentally beforehand to decide which of the mentioned geometries is at the best suited for the actual problem. The survey given in Table 4.2 can be helpful. It is divided up with regard to the surface or volume properties of the color pattern of interest. Fluctuations occurring during manufacture of optical and microelectronic component parts are a reason that the results obtained with various color measuring instruments often differ from each other. For clear comparison of results which were achieved by different instruments from the same manufacturer or by different manufacturers, every manufacturing company should generally insure that the actual instrument generation fulfills at least the CIE recommendation [14]. Moreover, possibly several of the updated standards [26 –31] should be met. 4.1.2.3 Geometries for Transmission Measurements The reflectance and transmittance of translucent materials are best determined using one of the above-mentioned geometries and applying the measuring method over two different backgrounds (Section 4.2.4). This procedure is not standardized. For measurement of transparent or nearly transparent materials, the CIE proposed altogether one directional and five spherical geometries as follows [14, 32]: 1. directional normal–normal geometry (0:0): each of the incident and outgoing fluxes is perpendicular to the plane parallel sample surface; 2. diffuse–normal geometry (di:0): the color pattern is illuminated diffusely, the measurement is performed normal to the sample surface with specular reflection included;
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247
Table 4.2 Survey over suitable measuring geometries for color measurements of non-selfluminous colors
Optical surface or volume property Surface
Matt
Slightly glossy, structured
Glossy, high glossy
Volume
Transparent
Translucent
Opaque
Suitable measuring geometries and colored materials Three geometries are suitable: di:8 with subtraction of specular reflection, de:8, 45c:0; colors, lacquers, plastic materials, textile fibers, glass, ceramics, fluorescent colorations Smooth and slightly bright color patterns: di:8 with gloss subtraction, otherwise gonio spectrophotometer; more rarely 45c:0; lacquers, embossed or injection molded surfaces of polymeric materials, textile fibers, paper, leather, glass Also with diffuse component: alternative di:8 with gloss subtraction, 45c:0; lacquers, high polymeric materials, foils, backed paper, ceramic Directional transmission: measurement with transillumination: di:8 with gloss subtraction, de:8; directional and diffuse transmission: reflection over two different backgrounds: di:8 with gloss subtraction, 45c:0; dyes, colored and effect pigments, inorganic and organic glass Homogeneous, inhomogeneous, cloudy, or flow structures: as given for transparent sample under directional and diffuse transmission, see above; comparison of measuring geometry Isotropic scattering: di:8 with gloss subtraction, de:8, 45c:0; colors, lacquers, plastic materials, ceramics; anisotropic reflecting or scattering: gonio spectrophotometer; absorption and effect pigments, fibers, high synthetic polymers
3. diffuse–normal geometry (de:0): unlike to 2., the specular reflection is excluded from measurement; 4. normal–diffuse geometry (0:di): this geometry is the inverse of that in 2.; 5. normal–diffuse geometry (0:de): geometry inverse to that in 3.; 6. diffuse–diffuse geometry (d:d): illumination and measuring are each performed with diffuse light.
The third and fourth geometries with included specular component result in transmittance factor τ , the other listed geometries in transmittance T [32]. The
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construction of the Ulbricht sphere corresponds to that for reflectance measurements. Further details for color measurement of optically different materials follow in Sections 4.1.4 and 4.2.4.
4.1.3 Sample Requirements As already mentioned, the measurement result represents an aspect of the actual physical state of the sample. From there, it is essential that the experimental handling of the color pattern is performed with extreme care. All influences, which are able to distort the measurement result, need to be keep away from the colored sample. Apart from this, the result is influenced by the manufacturing, preparation, selection, and storage of the coloration, among other things. Such factors are often underestimated or disregarded. Among the varied aspects to be considered, we restrict ourselves to the most important influences which are caused by the surface, shape, homogeneity, and manufacturing parameters that possibly change the optical properties of the color pattern [33]. Issues of quality control are not considered in this text. During the manufacture of colored samples, the components are mixed, dispersed, or kneaded in such a way that process variables such as shear velocities, temperatures, pressures, and action times are maintained similar to the future production. Loose powders, granulates, or pellets are completely unsuitable for color measurements. From these, indefinable shadowing is superimposed on the backscattering from the volume; this causes, under both directional and diffuse illumination, false color values: in fact, the colors are lighter. Pigmented powders of required particle size distribution should be homogenized in a transparent binder. Powdered materials are otherwise manufactured in stampings with defined smooth, diffuse scattering surface, and without cracking of crystallites. In this case, the natural chroma and brilliance are maintained to the greatest possible extent. Granulates or pellets of plastic materials are transformed by melting into a sample of required size, shape, and surface structure. From the applied procedure for homogenizing absorption pigments in a binder should result optically isotropic color patterns; therefore, spectral values are independent of the sample orientation. The measurement of optical anisotropic materials – like some textile fibers and fabrics, effect pigments in lacquers, injection molded or extruded plastic materials – is performed by systematical rotation of the sample with regard to the aperture. This is in order to investigate whether the spectral values are independent of azimuthal angle. Modern instruments for this are equipped with a sample objective. On the other hand, naturally or artificially aged materials can develop anisotropic properties such as color streaking, chalking, micro- or macro-cracks and other near-surface or volume variations.
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Measurement of Reflecting and Transmitting Materials
249
For all sorts of colorants or binders, defect-free sample surfaces without any scratches, bubbles, blisters, inclusions, fingerprints, etc., should always be used. Otherwise unwanted reflections are created. These uncontrollably falsify the color impression and the color values. In addition, the electrostatic charging of organic materials which often occurs needs to be avoided. Dust particles cause surface scattering: dark hues appear lighter, light hues darker. Rough and coarse surfaces, e.g., of leather, textiles, ceramics, lacquers or plastic materials, behave in a similar way. On the other hand, in some cases, the brightening effect is directly created with suitable additives in lacquers; in the case of plastics, pearl-, conic-, prismatic-, or linen-shaped surface structures are applied. Saturated and dark hues are extremely difficult to handle in this context. For such colorations, and also for matt surfaces of plastic materials, coatings, and lacquer systems, it is recommended to apply a colorless and transparent topcoat. In this case, not only the applicable color impression is attained but also untainted color values. For spectrometric measurement, the di:8 modus with numerical subtraction of specular reflection, alternatively the de:8, or the 45c:0 measuring geometry should be applied. The entire color measurements and visual color difference assessments should be performed exclusively with smooth and plane samples. Curved or undulated surfaces are unusable. Arched surfaces, however, can be suitable for visual judgment of (a) the gloss or roughness of colorations with absorption pigments or (b) the travel of lightness or color flop of effect pigments. Additionally, inhomogeneities such as flat spots or sink marks in the sample surfaces are to be avoided. These occur preferentially in thin layers of lacquers or at the surfaces of unfavorably constructed and manufactured plastic components. The color samples should be dimensioned in such a way that metrological and visual conditions are satisfied. Irrespective of the colorant sort, the measurement aperture is often adjusted to the largest possible diameter with the goal of achieving an averaging of the spectral values over the measurement field. But with regard to the aperture of a measuring instrument, the need can be laid out more precisely: – effect pigments need always the greatest possible aperture; – absorption and phototropic colorants need a middle-sized aperture; – fluorescent and thermochromic colorants need the smallest possible aperture. There is a rule of thumb that the sample diameter should be at least three times that of the adjusted aperture diameter. With that, the influences of edge reflection and edge loss are somewhat reduced. An applicable theoretical description of such edge phenomenon is, however, as yet unpublished. Both the multiple reflection at the side wall and the emerging light fraction there cause false measurement values. This systematic error exists in the entire previous color measurements up to that point and is withhold in most cases in literature.
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Color patterns of rectilinear, orthogonal edges, at which the color samples are aligned without any gap, are indispensable for visual judgment of color differences (simultaneous contrast). Furthermore, the other CIE reference conditions are met during the evaluation of colors. Also, the different color perception phenomena which can affect the judgment need to be considered. The storage of the manufactured color patterns is normally carried out pressurelessly between pH neutral separating paper in a dark surrounding, and possibly in standard climate or at low temperature and middle humidity. The storage of the calibration patterns for color recipe prediction should be considered with special prudence. This also goes for color collections, long-term internal or external standards, or all sorts of calibration standards of the color measuring instruments used.
4.1.4 Transparent, Translucent, Opaque Colors Optical materials can be distinguished depending on the sort of light transmission. As already mentioned, they are termed as transparent, translucent, or opaque. In the color industry, continuous transition between such different optical states is often desired, for example, a given shade may be manufactured with varying degrees of transparency. For precise characterization of these kinds of colorations, colorimetric terms such as transparency index and contrast ratio are used. An optical transparent medium absorbs a fraction of the incident light in dependence on the wavelength. The residual fraction is ideally transmitted without any scattering. Such a material appears colored not only in transmitted illumination but also in incident illumination. The reason for color impression at incident illumination is the difference between the refractive index of the binder (n2 ≈ 1.5) and of air (n1 ≈ 1.0). From directional light perpendicularly incident on the interface, 4% of the incident light are immediately reflected, from diffuse incident light about 9.2%, cf. Equations (2.1.8) and (2.1.12). For constant colorant concentration, the measured quantities and the visual judgment of transparent colors also depend on the layer thickness (Sections 3.4.3 and 5.1.2). The spectrophotometric measurement of a transparent color pattern is carried out either with transmitted light or reflected light in one of the measuring conditions and geometries listed in Table 4.2. These decisions depend on the question, as to whether only the directional or both the directional and diffuse components of transmission should be recorded. By definition, a transparent material shows no reflection from the volume due to lack of scatter. With the d:8 measuring geometry, the transmittance can be determined with three different procedures: (a) the colored layer is positioned between source and Ulbricht sphere, (b) between the sphere and aperture of the detector,
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Measurement of Reflecting and Transmitting Materials
251
To detector
Position b)
8° Position a)
Fig. 4.9 Two alternative placements for measuring transparent materials: (a) in front of the illumination aperture and (b) at the measuring aperture
or (c) over two different backgrounds; methods (a) and (b) are shown in Fig. 4.9, method (c) in Fig. 4.14. Both sample placements (a) and (b) result in slightly different measurement values, provided that a scattered component from the interfaces appears in position (b). The measurement of transparent materials is often complicated by inhomogeneous surfaces and multiple reflections at the interfaces of a plane parallel layer. In order to exclude such reflections from the measurement result, it is generally not appropriate to simply tilt the layer a few degrees from normal to the beam. Refraction causes not only dispersion but also a shift of the sample beam. A better method for quantitative characterization of transparent or translucent layers, which avoids such disadvantages, is given by the method of reflection measurements over two different backgrounds. From a physical point of view, the color measurement of translucent materials is more complex than for transparent or opaque systems: in this case, it is necessary to determine both reflectance and transmittance, which are already listed in Table 2.6. Both quantities of colored layers can be measured with spectrophotometers by two different procedures: either by separate determination of reflection and transmission or by two reflection measurements over two different backgrounds of known spectral reflectance; see Section 4.2.4.
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The measurement of reflection over two different backgrounds can be performed with the 45c:0 or di:8 geometry. Diffuse illumination, however, is preferentially applied. The accompanying geometry is shown in Fig. 4.8. The measuring procedure over the two backgrounds is complicated by a basic physical requirement: the translucent layer and the background have to be in optical contact with each other. The light background of known spectral reflectance reflects the majority of the light which is not absorbed by the particles of the layer. The measured reflectance, therefore, corresponds to the color of the translucent system. Because the dark background absorbs the majority of the transmitted light, then the reflected fraction is caused by the scattering of the translucent material. Opaque colorations of inorganic colored and opaque interference pigments completely cover a colored background. The measured spectral values over different backgrounds are equal within measurement uncertainty of the instrument used. Nevertheless, the two-background procedure is also applied to opaquecolored materials. The reasons for this are either for the determination of the contrast ratio of a covering layer or the precise separate determination of the optical constants of an incorporated colorant. Layers containing effect pigments need more extensive color measurements than translucent samples. The most commonly used diffuse measuring geometry for these sorts of samples, de:8, shows results which agree well for pearl, interference, and diffraction pigments with visual impression perpendicular to the pattern surface. On the other hand, from directional illumination at fixed angle β and directional measurement for at least five aspecular angles μas , for example, chroma, color travel respective flop, or the interference color of the coloration can be observed. In contrast, apart from at short visible wavelengths, metallic pigments show a spectral reflection nearly independent of wavelength which increases with specular angle (cf. Fig. 2.39). Different shear rates and consequently altered structural viscosities of binders or plastic melts additionally superimpose all sorts of optically anisotropic effects on flake-shaped particles. A possible anisotropy with respect to azimuthal angles, often caused by finishing or processing, can be shown by systematic rotating of the sample perpendicular to the surface of the color pattern.
4.1.5 Color Matching The visual comparison of two or more sample and reference colorations of similar shade and their assessment is generally called color matching. Normally, this method is accompanied by colorimetrical measurements. This procedure of drawing comparisons can be applied to all sorts of absorption and effect colorations in research, development, or quality control. The criteria and suitable tolerances to which the results need to comply are selected beforehand. For
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Measurement of Reflecting and Transmitting Materials
253
visual judgment, at least the CIE reference conditions need to be realized. A light booth should be equipped with standard illuminant D65. Additional illuminants such as A, C, FL 2, or FL 11 are necessary in cases for visual assessment of color inconstancy, metamerism, or fluorescence. The evaluation of the computed color values is carried out with the same illuminants as in the visual method. For competitive color measurements, the involved colorists have to employ the same optical instruments, possibly with the same equipment and capacity. This means the use of the same color-matching booths, (gonio) spectrophotometers of the same measuring geometry, gloss meters, etc. Both sides have to agree and meet the measuring geometry, the angles of illumination and measurement, as well as the illuminants and standard observer. Only in such a situation it is possible to clearly compare and interpret the distinct angle-dependent measurement values of effect colorations. Moreover, the spectral power distribution of the sources used needs to be determined beforehand and compared. Deviations should be eliminated by exchanging lamps with those of the same type. The UV or IR range should be included in the comparison only in cases where fluorescent and phototropic or thermotropic colors are to be matched [33]. In addition, the color capability of the involved colorists is to test and systematically to train. Different color capabilities between the colorists should be known and taken into account. The required color measurements should be performed immediately before or after the visual color matching. Producing two measurement series, one direct before matching and one check series afterward, has proven to be effective. A possible time-dependent change of sample and reference colors during the procedure time can, by this method, be nearly excluded from the results. The mean from the results for each color pattern of both measuring series should be taken. The deviations should not exceed twice the measuring uncertainty of the instrument. As mentioned previously, the color impression of an object comes from the superposition of light interactions from the volume and reflection on account of the conditions of the interfaces. Most of misinterpretations of color measuring results come down to the fact that it is unknown whether the surface reflection is included in the measurement result or not. Applying the diffuse measuring geometry di:8 or 8:di, the specular reflection is included in the result. Before determination of color values and color differences, therefore, from each spectral value, the quantity of the directional reflection coefficient r needs to be subtracted. Afterward, the resulting color values and color differences can be calculated. The color differences attained from different measuring instruments should now agree with each other within the measuring uncertainty of the instruments. With the di:8 modus or reverse, the color differences coming from the colorants homogenized in the volume of the sample are essentially measured. Surface structures have no effect on
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the resulting color difference. These are the reasons why measurements with included specular reflection are preferentially used for colorant tests. On the other hand, subtraction of the directional reflection coefficient of a highly glossy color pattern shows a result which agrees with the visual impression. For a matt sample, the numerical subtraction of the specular component leads to a fictitious color. In this case, an unaffected and realistic color impression is achieved by a highly glossy clear coat of the sample and aspecular observation. The corresponding measurement results are, therefore, valid especially for highly glossy and unstructured color patterns. In addition, the results agree with the visual color impression. The interface reflection of distinctly structured matt to glossy colors such as emulsion paints, plastic materials, and textile fibers needs to be determined by empirical methods. In all other cases, the spectral values are taken without subtraction of the specular component. In the second measurement modus with the diffuse geometries de:0, de:8 and the directional geometries 45:0, 45c:0, the specular reflection is excluded from the result. In reality, the specular reflection is excluded from the measurement only if plane, ideally glossy samples are used. However, fractions of the specular reflection can unintentionally be included in the result. This depends on the construction of the light trap, optical shielding, or the conical divergent light beams with half angles > 5◦ . Measurement results from different instruments are, therefore, not necessarily comparable with each other. The specular excluding modus leads to measurement results which are due to light interactions in the volume of the colored pattern. These results agree with the visual impression excluding specular reflection. However, if the specular component is reduced by color fastness tests, the diffuse surface reflection increases and also, consequently, the entire reflection. Changes in the surface and volume are, therefore, registered together. Consequently, in color fastness tests, it is useful to follow the surface influence in dependence on time separately with a gloss meter. On the other hand, in cases of extreme changes of surface reflection with the observation angle, the measuring geometry de:8 produces differences with regard to the visual color impression. Except of effect colorations, this influence is especially well developed not only for semi-glossy and structured samples but also for patterns showing coat blooming. Such colorations result in even higher deviation of the measurement result if the 45:0 geometry is not exactly realized and the observation is unintentionally performed with partly diffuse illumination. With absorption colorations, a nearly perfect agreement between measurement and observation is only achieved with the 45:0 geometry. Diffuse and directional measurements with the specular component excluded are preferentially employed for color patterns of nearly same hue, which, however, differ with regard to the: – geometrical shape (plane parallel, undulated); – surface (even, structured);
4.1
Measurement of Reflecting and Transmitting Materials
255
– interface reflection (partial directed, partial diffuse, diffuse); – degree of gloss (matt to high glossy). In cases of colorations of the same color, which are manufactured with quite different surfaces – e.g., for textile fibers, foils, interior, and exterior fittings of automotives –, an agreed “secondary standard” for each surface of interest is normally fabricated for assessment. In general, the present considerations are valid for opaque materials containing absorption colorants. Similar ideas can be transferred to transparent and translucent colors of plane parallel layers with glossy surfaces. For such color patterns of different light transmission, it is necessary to take into account the reflections at the outer and inner interfaces. In this context, the method of reflection measurement over two different backgrounds requires that both backgrounds are in optical contact and have the same high-glossy surface. If these conditions are not met, the spectral values will be incorrect (cf. Figs. 5.26 and 5.27). The measurements of the backgrounds alone or together with a chromatic layer should be performed with the same measurement geometry and instrument. It is possible to maintain the above-mentioned criteria for opaque materials for visual assessment of transparent and translucent colored patterns of the same color but of different surface structures.
4.1.6 Acceptability and Tolerance Agreement In the context of color matching, the verbs agreed and tolerated have already been used. The terms acceptability and tolerance agreement are closely interconnected with each other and, moreover, with the procedure of color matching. A color tolerance agreement precedes an extensive color matching, accompanied by the intension of finding the visually accepted color patterns from a given color collection. The experimental and additional numerical evaluation conditions with which the color matching and assessment are to be performed should first be clarified by the involved people. A representative collection of color patterns, which is possibly pre-selected by various independent colorists in groups such as “accepted,” “only just accepted,” or “excluded,” needs to be available for ascertaining acceptability. The sets of accepted or conditionally accepted colorations constitute an ensemble for the succeeding more strict color matching. The pattern collections are either assembled by (a) specifically produced new colorations which show systematic hue error or color deviations from the reference color (possibly in each of the three directions in a color space); (b) selected colorations of the production with random color differences with respect to the reference color. During matching, it is always necessary to distinguish between the smallest visually discernable color difference and the acceptable color difference:
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– the smallest visually discernable color difference is a psychophysical quantity; – the acceptable color difference, however, is a technically or economically reasoned value. However, if the reference threshold of acceptability is set too low and fluctuations of production, for example, always cause systematic crossing of this threshold, then an acceptable serial production is illusive to obtain. Furthermore, a threshold lower than the – color locus dependent – visual capability of discerning color differences is an excessive and unrealistic demand. The analog is true with regard to the stochastic variations in the color measurement instruments used. An acceptability threshold which is below the measurement uncertainty is not experimentally obtainable. The well-configured tolerance agreement comprises arrangements with regard to the sort and extent of deviations which are to accept or to tolerate between sample and reference color(s). In addition, the experimental, numerical, and visual methods are fixed, with which the tolerance parameters are determined and currently checked in future. Apart from that, the random and also systematic errors are taken into account, which occur by changeover from laboratory to production scale. In general, a tolerance agreement includes such parameters, which allow tolerating visual and colorimetrical differences between sample and reference colors regarding agreed thresholds. The criteria to find out are so varied that only some ideas can be given here for that intention: – the magnitude of the tolerance ranges of the different color contributions which are to determine and to fix depends on the sort of colorant, color range, or color point, surface structure of the pattern, binder, etc.; – the measuring and evaluation conditions are unambiguously to arrange; – permissible variations of color difference values are definitely to restrict; – the agreed color difference formula for evaluation use is to apply; – the statistical test of a current production is in detail to arrange and to meet: the formulation of the time frame, the parent population or sample size, test parameters, etc.; – the color tolerance values can include not only color physical criteria but also application-specific or economic aspects; – completely inappropriate is a color tolerance smaller than the visual color discrimination; – on the other hand, it is to consider that too large color tolerances are strictly to avoid, in order to achieve product acceptance by the consumer. Already this short enumeration elucidates the impossibility to formulate a universal valid tolerance agreement for each special case. The partners should rather realize that each current case requires a separate, individually tuned
4.2
Measuring Methods
257
color tolerance agreement. Finally, the concluding document with the tolerance agreement is to enclose with all measuring and evaluation protocols.
4.2 Measuring Methods Altogether, there exist three different procedures for measuring colors: the equality, the tristimulus, and the spectral methods. The equality method is identical to visual color matching described previously, whereas the tristimulus and the spectral methods are based on technical measurement principles. In the following, we describe the construction and interaction of the most important components of color measuring instruments upon which the tristimulus and spectral methods are based. Just to sum up, the tristimulus colorimeter uses three filters of light transmission with which the three standard color-matching functions (SMCFs) are simulated in the range of visible wavelengths. The more precise and versatile spectrophotometers allow for the measurement of reflectance or transmittance of a color pattern at discrete wavelengths in the visible range. Whereas the tristimulus method simply delivers color values, with the last mentioned measuring procedure, the spectral reflectance or transmittance of transparent, translucent, and opaque colorations is determined in different ways. Among these methods is an often applied technique the special measurement over two different backgrounds. This procedure is now discussed in detail. As already explained, the varied color properties of effect pigments are not fully characterized simply with angle-dependent color measurements. Therefore, we give some supplementary and industrially used optical methods. Finally, aspects for color measuring of fluorescent, thermochromic, and phototropic systems are discussed. On the basis of selective absorption mechanisms, these need modified measurement procedures.
4.2.1 Tristimulus Colorimeter The tristimulus technique is carried out with the so-called tristimulus colorimeter. Among the established color measuring instruments, this equipment has the simplest optical structure. The essential optical components consist of an illuminant and three separately positioned color filters in front of connected photocells; see Fig. 4.10. The first filter has a spectral transmittance nearly of the SCMF x¯ (λ), the second nearly of y¯ (λ), and the third of z¯(λ) with respect to the 2◦ or 10◦ standard observer. For simplicity, these colored glasses are also named R, G, B filters. In reality, however, four or more filters are usually inserted. On the one hand, the short- and long-wave fractions of the SCMF x¯ (λ) cannot only be imitated with just a single filter with excessive effort; on the other hand, the
258
4 Measuring Colors Broad band – diode
Source
X
Y Z
Sample
Grating
R, G, B Filter
Computer
Fig. 4.10 Principal configuration of a tristimulus colorimeter for determination of color values
edge steepnesses of usual filters deviate to a large extent from those of the three SCMFs. By comparison of Figs. 4.10 and 2.29a, it can be recognized that the observer in the second mentioned figure is substituted by the color measuring instrument in Fig. 4.10. In order to have the best agreement between the measurement and the visual color impression, the optical construction of a tristimulus colorimeter is kept as simple as possible and is mostly realized in the 45:0, 45bi:0, or 45c:0 geometries. The light emission of a high-pressure xenon lamp is filtered in order to simulate standard illuminant D65. The sample is illuminated at an angle of 45◦ in a linear, bidirectional, or circular manner. The spectral reflection of the color sample supplies the three R, G, B filters, which transmit only wavelengths in the red, green, or blue range with regard to the SCMFs. Afterward, the separate filtered optical signals reach each of the broadband semiconductor photodiodes. These transform the incident light into an equivalent electrical current. Each current is amplified and read in by a microprocessor which calculates the standard, CIELAB, DIN99o, or color values of a color appearance model. For color difference measurements, color differences are computed with various formulas. The color values and differences correspond to the illuminant used and to the observer which is simulated by the three filters. In most cases, the 10◦ observer is simulated. Some manufacturers offer tristimulus colorimeters of selectable illuminants and exchangeable R, G, B sets of filters for both standard observers. It is doubtless that the functional range of the tristimulus colorimeter is quite restricted. However, the clear construction constitutes an economic solution to determine the simplest colorimetrical quantities with sufficient approximation. Certainly, the three-filter photometer measures no single spectral values but
4.2
Measuring Methods
259
produces and registers only three photoelectric currents corresponding to the installed illuminant. Therefore, color inconstant or mutually metameric colors are not detected. Moreover, this method is really restricted to colorations containing absorption colorants and is absolutely unsuited for the characterization of all optical properties of effect pigments. Finally, color recipe prediction for absorption colorations using this instrument should be carried out only with great restrictions, especially in cases of missing spectral values and those given only single color values for the reference color. The simple instrument construction causes also a low absolute accuracy and reproducibility – both properties are, for the most part, five to ten times worse than those of a spectrophotometer; values are given numerically in Table 4.4. The application of this instrument is, therefore, restricted to colorations with absorption colorants in fields of quality control and product information. Compared to this method, the spectral procedure is more complex but versatile for solutions to the majority of color physical problems.
4.2.2 Spectrophotometer The spectral method can be realized in directional, diffuse, and variable directional measuring geometries as discussed. The technical construction of a spectrophotometer of d:8 geometry is shown schematically in Fig. 4.11. The approximate D65 filtered and pulsed light of a high-pressure xenon lamp is reflected many times and scattered at the surface of coarse white inside of a
Measuring beam
Photodiode arrays
Measuring signal
Light trap
Xenonsource
8° Reference beam Reflection grating
D 65-, UV-Filter
Reference signal
Sample
Fig. 4.11 Diagram of a dual-beam spectrophotometer: d:8 geometry with measuring and reference beam (source: Datacolor AG, Dietlikon/Zürich, Switzerland)
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4 Measuring Colors
Ulbricht sphere. The aperture of the xenon lamp has a shielding and the light is emitted parallel to the surface of the color sample which is, therefore, diffusely illuminated. The UV fractions of the xenon spectrum are filtered in such a way that one of the four possible daylight sorts is simulated or rather the stimulation and measurement of luminescent colorants can be performed. The light reflected by the sample under an angle of 8◦ is, through an objective and optical waveguide, directed onto a concave diffraction grating. Similar to diffraction pigments, the grating diffracts the incident light and breaks it into its individual constituents. The concave curved reflection grating collimates the diffraction spectrum which is diverted onto an array of silicon photodiodes. The number of light-sensitive diodes depends on the relevant wavelength resolution and the bandwidth of the measurement spectral range. Instruments of first generation possessed 16 diodes for covering the range between 400 and 700 nm at equidistant interval width of 20 nm. Modern spectrophotometers are equipped with at least 40 diodes and register wavelengths from 360 to 750 nm with interval width of 10 nm. For security, there are sometimes two or three such arrays in the instrument. Such a collection of semiconductor elements with extremely narrow photoelectric tolerances enhances the accuracy and dependability of the spectrometer, but this comes at cost. In Table 4.3, typical characteristics and specifications of a modern reference spectrophotometer are given. The so-called abridged spectrophotometers with spectral range from 400 to 700 nm of equidistant interval width of 10 or 20 nm (31 or 16 measuring wavelengths, respectively) are common these days. Such instruments are absolutely sufficient for a wealth of colorimetric applications with regard to absorption colorants such as quality control, documentation, determination of color values, color differences, inclusive color inconstancy index, metamerism index, covering capacity, and recipe prediction. For colorations with effect pigments, gonio Table 4.3 Characteristics and specifications of a modern reference spectrophotometer Characteristic
Specification
Measuring geometry Spectral range Number of wavelengths Bandwidth Wavelength accuracy Inter-instrument agreement
de:8, di:8 360–750 nm 40 10 nm 0.05 nm ∗ ≤ 0.3 , ΔE∗ ≤ 0.15 average ΔEab ab BCRA II tiles 0–250% 0.001% ∗ ≤ 0.01 ΔEab 3s
Photometric range Photometric resolution Measurement repeatability Measurement time
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Measuring Methods
261
spectrophotometers of variable directional geometry (β/μas or μas /β) of at least five different measuring angles μ are often applied. Spectrophotometers of high-wavelength resolution of Δλ < 5 nm or extended wavelength range from 360 to 780 nm sometimes use a numerical interpolation method with the measurement values. This is for adjustment with regard to the tabular values for illuminant and standard observer of interval widths of 1 or 5 nm given by the CIE. In cases of unequal measurement and standardized spectral ranges, the tabular values are to modify in such a way that for every illuminant, the given standard color values Xn , Yn , Zn of ideal white result (cf. Table 3.1). The narrow interval widths might be necessary for color physical aspects in basic research for precise determination of narrowband extinction or transmission spectra of dyes. However, such spectrophotometers are often overkill for purely colorimetric questions, including for effect colorations. In addition to the main sample beam, spectrophotometers are often equipped with a further reference beam, as shown in Fig. 4.11. This is for enhancement of accuracy and reliability. In such a dual-beam spectrophotometer, the reference beam serves as a measure for the incident light intensity at the sample surface. The reference beam is collected from the diffuse reflected light inside the sphere and supplied to a second optical system – identical to that of the measuring beam. Either the same photoarrays are used for measurement and reference beam and the signals are appropriately time-shifted or two or more arrays are installed. The separately produced photocurrents of measurement and reference beam are amplified, digitized, and numerically edited. The ratio of the measurement and reference signal for each of the wavelengths λi corresponds to the reflectance R(λi ) or transmittance T(λi ) of the sample. In the data storage device of the integrated microprocessor, the tabular values of different illuminants and standard observers to each measured wavelength are stored. In the evaluation unit, routines are implemented for determination of spectrometric and colorimetric quantities. The required evaluation quantities are stored for reference measurements [14, 27, 30]. Additional software should have appropriate algorithms available for performing recipe prediction. Repeatedly, we have pointed out that the measured reflectance or transmittance of a color pattern is independent of the applied light source. The reason for supplying a modern tristimulus meter or spectrophotometer with a xenon lamp is, however, primarily to reduce to two random aspects: first, the spectral power distribution of xenon light is roughly the same at each wavelength in the visible range and second, it corresponds nearly to that of middle daylight with color temperature 6,500 K. Both properties together lead to the fact that standard illuminant D65 is regarded as a kind of universal reference illuminant. If, on the other hand, a tungsten filament lamp of low emission power in the violet and blue range is used, then the relative measuring error rises seriously – especially for dark color samples. This can be avoided by using a xenon
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lamp. Additionally, the nearly constant emission energy of a xenon lamp over more than 5×105 measuring flashes is of economic advantage. The output light impulse of 1 ms duration brings only a minor thermal effect to a normal colored sample (cf. Section 4.2.6). Furthermore, the emitted light energy of only few milliwatts is not a major influence on the instrument drift or aging of optical elements. A major effect contributing to the long-term drift occurring during instrument operation is thermal – due to ohmic heating of electrical components. This may lead to slight thermal variations in the elements. These elements are used for both the measurement and reference lights. Even the aging of the source, the inner reflecting surface of the Ulbricht sphere, and the optical waveguides are experienced equally by both beams. For a well-constructed spectrophotometer, such drifts and aging do not affect the measuring result, due to the fact that the measurement and reference beams experience these effects the same. Nevertheless, it is important to periodically keep an eye on the interior coating of the sphere because the absolute reflection of the coating material can be reduced by aging and, therefore, also the measuring sensitivity. The main advantage of the dual beam concept is the improved and nearly constant accuracy. For reliability, the endpoints of the gray scale of the color measuring device should be calibrated regularly. This might generally occur after the warm-up phase as well as at given regular intervals during operation. Modern instruments automatically ask for calibration if the measurement fluctuations are higher than the measurement sensitivity. If this temporary calibration is neglected, the obtained spectral values are unreliable and reproducible measurements are not ensured. For this, both secondary standards are needed. They are normally delivered with the spectrophotometer and one must be extremely careful working with and storing them. Unusable or lost standards should only be substituted by the instrument manufacturer, who should also perform the necessary new calibration. The calibration of a spectrometer with sphere geometry is carried out each time by reflection measurement with the inclusion of the specular component in the di:0 or di:8 geometry. For temporary calibration of the gray scale, it is assumed that the instrument drift between calibrations is so small that a linear correction is sufficient. This correction can be described as follows. The last obtained calibration values with the black and white standards are denoted as B0 and W0 . From a color pattern, the correct quantity Mcor with regard to B0 and W0 is obtained. In the meantime, instrument drift causes the corresponding new readings Bm , Wm , and Mm for the black and white standards as well as the same color pattern as before, respectively; cf. upper and middle scales in Fig. 4.12. Along with the basic theory of intersecting lines, the valid proportionality relation is given by W0 − B0 Mcor − B0 = . Mm − Bm Wm − Bm
(4.2.1)
4.2
Measuring Methods
263 B0
a) b)
Mcor
W0
Mm
Bm
Wm
c)
0
50
100
Fig. 4.12 Calibration of a spectrophotometer with black and white standards; the scales mean (a) last calibration, (b) before actual calibration, and (c) absolute scale
From this, the correct measurement quantity Mcor follows from the equation of a straight line Mcor = αMm + β
(4.2.2)
of positive slope W0 − B0 Wm − Bm
(4.2.3)
β = B0 − αBm .
(4.2.4)
α= and intercept
The coefficients α and β are separately calculated for each measurement wavelength λ and used for correction of the corresponding measurement value Mm . The original calibration of the manufacturer and the absolute accuracy of the spectrophotometer are not altered by such a calibration procedure. Under careful and normal operating conditions, the calibration of the wavelength or angle scale of gonio spectrophotometers is necessary only in extremely rare cases. Nevertheless as a routine matter, it is reasonable to undertake an inspection or new scaling after about 3 years of continuous operation. For calibration of wavelengths, emission lines of different sources are used (Section 4.1.1). Independent of that, it is recommended that a fundamental reconditioning of the instrument be performed before calibration of new color pattern series for recipe prediction.
4.2.3 Accuracy of Spectrophotometers In addition to the short- or long-term reproducibility issues, all measuring devices are subject to statistical measurement uncertainty. This is independent
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of the temporary calibration. Apart from this, equipment from the same or different manufacturers does not normally give exact the same measuring results. Because the spectrometric procedure is the most important color measuring method in color industry, we deal with its accuracy here in more detail and also the possibilities for enhancement. The more precisely the spectral values Ri = R(λi ) or Ti = T(λi ) are determined, the lower the measurement uncertainty. If we concentrate on the standard color values X, Y, Z given by Equations (3.1.1), (3.1.2), and (3.1.3), the corresponding error increases with increasing number of spectral values i = 1, 2, . . . , N. In some spectral range, apart from the reduction of the wavelength step width Δλ, an increase of N is only useful if the measurement uncertainty of each spectral value is simultaneously reduced. Because the color values of the CIELAB or DIN99o system and further evaluation formulas depend on X, Y, Z in a nonlinear fashion, an analytical representation of the respective error propagation is nearly impossible. The individual and overall error can be estimated with an experimentally determined dependability – which is sufficient for most practical applications. Especially for dyes in solution with erratically changing spectral values, the photometrical resolution should be precise to five valid significant figures. At worst then, this means that the fifth digit is incorrect and the corresponding relative error of one spectral value is in the thousandth range. Modern spectrophotometers meet virtually this condition, cf. Table 4.4. From the given
Table 4.4 Error limits of spectrophotometers Measuring property
Error limit
Photometrical resolution at Ri = 1.0
|ΔRi /Ri | ≤ 20 ppm
Short-term repeatability after calibration for ≤ 30 measurements with intervals of 10 s
White standard: ∗ | ≤ 0.05 |ΔRi /Ri | ≤ 50 ppm or |ΔEab Black standard: ∗ | ≤ 0.01 |ΔRi /Ri | ≤ 20 ppm or |ΔEab
Long-term reproducibility Standards and 12 BCRA II tiles
|ΔRi /Ri | < 0.1% or ∗ | ≤ 0.3 |ΔEab
Temperature drift for Δϑ = |ϑR − ϑN | ≤ 10 K , where ϑ R : room temperature, ϑ N = 20◦ C
|ΔRi /Ri | ≤ 1 × 10−3 × Δϑ/K or ∗ | ≤ 0.05 × Δϑ/K |ΔEab
Inter-instrument correspondence regarding 12 BCRA II tiles and master spectrophotometer
∗ | ≤ 0.15 instruments of same |ΔEab manufacturer ∗ | ≤ 1.0 devices of different |ΔEab manufacturers
4.2
Measuring Methods
265
measuring uncertainties and the color differences in Tables 3.5 and 3.6, it follows that the accuracy of actual spectrophotometers can be well above the given color tolerances. Due to the simpler structure, however, the measuring uncertainty of a tristimulus colorimeter is about five to ten times higher. On the other hand, recall that a color difference is measured up to ten times more precisely using a spectrophotometer than by visual determination. For a color measurement device in continuous operation, the short-term repeatability needs to be checked from time to time. Note that this term is often incorrectly denoted as short-term reproducibility. Suitable internal or external standards, each with marked measuring fields, are normally used to check short-term repeatability. The measuring field is positioned in the indicated direction at the aperture; the spectral and standard color values are then determined repeatedly after time intervals of about 10 s. The resulting spectral values should have a relative error of no greater than ΔRi /Ri = ± 20 ppm for the black standard and ΔRi /Ri = ±50 ppm for the white standard. The color differences ∗ | ≤ 0.01 and |ΔE ∗ | ≤ 0.05, respectively; see Table should show values of |ΔEab ab 4.4. In addition, it is a good idea to determine whether or not the deviations of the spectral values accumulate in different wavelength bands or are uniformly distributed over the entire visible measuring range. The color difference contributions are analyzed in a similar manner with regard to systematic or color locus-dependent deviations from the reference colorations. However, the most important requirement for determination of the short-term repeatability is a stable operating state of the instrument after the warm-up phase. The full warm-up time is attained after the color values of a nonthermochromic sample show no further systematical trend after short-term repeated measurements. In any case, one should strive for constant room temperature and humidity during the measuring phase in order to avoid measuring results influenced by change of surround temperature and humidity. This phenomenon is known as temperature drift (Table 4.4). Color measurement devices are to be placed at a distance from direct heating or cooling sources and at best operated in constant standard climate. Spectrophotometers should additionally have a particularly high long-term reproducibility for several years. This also needs to be ensured for recipe prediction measurements. Verification of this follows using again the same standards as for testing the short-term repeatability as well as the chromatic and achromatic set of BCRA II tiles. The actual measurement values are compared with the previous ones and stored [34]. The long-term repeatability of constantly controlled and readjusted instruments should produce spectral relative devia∗ | ≤ 0.3. tions of ΔRi /Ri < ± 0.1% and color differences in the range |ΔEab Systematical trends need to be pursued over time and need to be eliminated. An expert readjustment is absolutely essential. In this context, for testing of short- or long-term behavior, one must also consider whether to refer to the stored scaling values or those of the actually
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measured reference standards. Experience shows that, in case of doubt, the data stored for many years are preferable over the actual obtained values. To be sure, both records should be evaluated and possibly subjected to a statistical examination (Section 4.3.4). In order to prevent unchecked data loss, a digital storage medium should be exchanged at least every 10 years (the way things are at the moment). A color difference value is used for measure of inter-instrument correspondence or rather absolute accuracy, for orientation. Because it contains no information about the direction or amount of each of the three color difference contributions, this quantity is of low meaning. Experience shows that equal or different instruments of one and the same manufacturer have relative uncer∗ | ≤ 0.15. This range is valid for mean reflection tainties in the range |ΔEab values in the domain 0.2 ≤ R (λi ) ≤ 0.6. Instruments from different manufacturers can show even higher differences, particularly for achromatic, brilliant, and especially for dark shades which frequently attain color differences up to ∗ | = 1.0. In other words, before substitution of an instrument or find|ΔEab ing of a tolerance agreement, it is necessary to perform reliable tests with suited color collections. The efficiency of the relevant instrument in different regions of a color space should be evaluated and be considered only from such measurements. The mentioned differences are somewhat higher than normal color tolerances for classical absorption colors. It is, therefore, useful that the absolute instrument accuracy is enhanced by all manufacturers. With regard to a tolerance agreement value, the visually agreed color difference alone is not sufficient, but also, apart from production fluctuations, above all the short- and long-term measuring uncertainties as well as the absolute accuracy of the measuring device need to be taken into account. Over and above that, with regard to tolerance agreement or color reproduction, one cannot go without exchange of corresponding color patterns between the interested parties: in particular it is not known to the people involved, for example, in what fashion the measured spectral values are accurately and uniformly corrected. In addition, it is not useful for color reproduction simply to convey the spectral values of a reference color pattern. On the basis of these considerations, the requirement for color toler∗ < 0.3 should be evaluated as unrealistically low: a person of normal ances ΔEab color perception ability can perceive such tiny color differences only in very rare cases.
4.2.4 Reflectance and Transmittance of Layers From color physical point of view, translucent colorations are of particular interest for at least three practical reasons: first, often a defined transmittance is required of a colored object, this goes well together with colorant loading
4.2
Measuring Methods
267
and layer thickness; second, the degree of transmittance can be achieved with different sorts of binders or transparent plastic materials; and third, opaque colored layers are often manufactured with minimal covering layer thickness, this can be realized with aid of the two covering criteria. The determination of the reflectance and transmittance of a translucent material fundamentally needs two separate measurements. In the three mentioned cases, the reflectance and transmittance can be determined alone by two separate reflection measurements: the translucent layer is measured separately over a white and a black background of known spectral reflection. This method offers some practical advantages and is, therefore, common: – a spectrophotometer equipped for opaque colorations can additionally, without changing the measurement technology, be employed for translucent and transparent materials; – this method can be directly implemented in recipe prediction in such a manner that the required covering capacity value follows immediately together with the recipe, without the necessity of preparing any coloration in advance; – the covering of the layer over white and black backgrounds and the scattering and absorption of the coloration are directly accessible visually; – from colorations of transparent pearlescent or interference pigments over both backgrounds, the interference and the complementary color can be observed separately; – multiple reflections at various interfaces of the transparent or translucent layers are included in the evaluation formalism. This measuring procedure comes down to the mathematical structure of an accompanying algebraic relation. For derivation, we consider the structure of optically different layers shown schematically in Fig. 4.13. Adjacent interfaces are in optical contact with each other. A set of optically contacted layers means either painted over or pressed as to avoid air gaps. At each interface of different refractive indices, light is refracted, transmitted, and reflected. The relevant single processes at the interfaces of the upper and lower layers are also schematically shown in Fig. 4.13. The contributions to the reflection at the illuminated surface sum up to the quantity R13 . The total transmission T13 follows from the sum of the contributions that are transmitted by all layers. Note that the measured quantities R13 and T13 are composed of reflections and transmissions due to single processes in the volume and at the interfaces which need to be considered. The actual internal reflection and transmission follow, therefore, in an indirect way. Consequently, the evaluation formulas for the so-called external reflection and transmission follow from both reflection measurements.
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4 Measuring Colors
ˆ 1R2 T1T32T
R1
ˆ 1R22Rˆ 1 T1T34T
ˆT1
R1
T1T32R2
ˆ1 R
T1 T1T3
R2
ˆ
T1T32R2R1
T2
ˆ1 T1T2T33R2R
T1T2T3
Fig. 4.13 Reflection and transmission caused by multiple reflections from three layers and single reflection and transmission at both interfaces
For ascertaining of the corresponding expressions, we return to the quantities and single optical processes shown in Fig. 4.13. By summation of all reflection contributions at the upper surface of the layer, the combined reflection R13 is given by the geometric series R13 = R1 + R2 T1 Tˆ 1 T32 (1 + Rˆ 1 R2 T32 + · · · ),
(4.2.5)
which sums to the result R13 = R1 +
R2 T1 Tˆ 1 T32 . 1 − Rˆ R T 2
(4.2.6)
1 2 3
The entire transmission at the lower surface of the permutation of layers is given by the geometric series T13 = T1 T2 T3 (1 + Rˆ 1 R2 T32 + · · · ),
(4.2.7)
which sums to the result T13 =
T1 T2 T3 . 1 − Rˆ R T 2
(4.2.8)
1 2 3
Based on both Equations (4.2.7) and (4.2.8), we consider now two special cases of layer configurations. 4.2.4.1 Two Different Boundary Layers This configuration corresponds to the method of determining the reflection and transmission of a translucent layer by measurement over a black and a white background. In this special case, we assume optical contact of two different
4.2
Measuring Methods
269
interfaces by leaving out the intermediate layer in Fig. 4.13. This leads to the evaluation expressions for determining the reflection and transmission of a layer. Because the middle layer is missing in Fig. 4.13, we set T3 = 1. In addition, we assume an isotropic upper layer, which means R1 = Rˆ 1 and T1 = Tˆ 1 . On account of Equations (4.2.6) and (4.2.8), the entire reflection R12 and transmission T12 of the layer combination are given by expressions R12 = R1 + T12 =
R2 T12 , 1 − R1 R2
(4.2.9)
T1 T2 . 1 − R1 R2
(4.2.10)
Because only reflection R1 and transmission T1 of the upper layer are of interest, we obtain R1 =
2 R12 T22 − R2 T12
(4.2.11)
2 T22 − R22 T12
and T1 =
(R12 − R1 )
1 − R1 R2
(4.2.12)
from Equations (4.2.9) and (4.2.10). However, the determination of R1 from Equation (4.2.11) is impossible because T2 and T12 are unknown; Equation (4.2.12), on the other hand, can only be evaluated if reflection R1 has already been determined. In order to solve this problem, as indicated in Fig. 4.14, we first denote the known reflection of the black and white backgrounds by Rbg,b and Rbg,w , respectively, and the measured layer in optical contact to each background by Rw and Rb, respectively. The spectral reflection values of both backgrounds should fulfill the conditions Rbg,b ≤ 0.2 and Rbg,w ≤ 0.8 for numerical stability. Substitution of the quantities R12 , R2 into Equation (4.2.9) by the respective corresponding pairs results in R = R1 + w
R = R1 + b
T12 Rbg,w 1 − R1 Rbg,w T12 Rbg,b 1 − R1 Rbg,b
,
(4.2.13)
,
(4.2.14)
from which the sought-after reflection R1 of the layer is given by
270
4 Measuring Colors Rb
Rw
T1
Rbg,w
T1
Tbg,w = 0
Rbg,b
Tbg,b = 0
Fig. 4.14 Procedure for determination of reflection and transmission of a layer by reflection measurements over two different backgrounds of reflections Rbg,w and Rbg,b
R1 =
Rbg,w Rb − Rbg,b Rw . Rbg,w (1 + Rbg,b Rb ) − Rbg,b (1 + Rbg,w Rw )
(4.2.15)
Performing the same substitutions for R12 , R2 in Equation (4.2.12), along with Equation (4.2.15), leads to two expressions for calculation of the layer transmission: 1 − R1 (4.2.16) T1 = (Rw − R1 ) Rbg,w and T1 =
(Rb − R1 )
1 Rbg,b
− R1 .
(4.2.17)
From each result for T1 from Equations (4.2.16) and (4.2.17), the mean should be determined so that an error estimate is also possible. Clearly, the calculations of Equations (4.2.15), (4.2.16), and (4.2.17) should be repeated for each measured wavelength. The key to this procedure is the structure of Equation (4.2.9). 4.2.4.2 Transparent Liquid Between Two Equal Transparent Interfaces This case corresponds to the conditions shown in Fig. 4.13 for R1 = Rˆ 1 = R2 and T1 = Tˆ 1 = T2 . Such an optical configuration is given, for example, by a cuvette. The interface reflection R13 and the measured transmission T13 follow now from Equations (4.2.6) and (4.2.8):
4.2
Measuring Methods
271
R13 = R1 + T13 =
T12 T32 R1 1 − T32 R21 T12 T3
1 − T32 R21
,
(4.2.18)
.
(4.2.19)
If the transmission T1 and reflection R1 of the outer layers are known from a measurement of the empty cuvette and setting T3 = 1 in Equations (4.2.18) and (4.2.19), then the transmission of the intermediate material follows from T3 =
T12 2T13 R21
2 /T 4 1 + 4R21 T13 1
−1 .
(4.2.20)
2 /T 4 1.0 can be produced. Color measurements of fluorescent colors are performed with the same measuring geometries which are already used for absorption colors. With regard to the stimulation and fluorescence emission, one should differentiate between two measuring modes from which the fluorescence component results. This procedure is termed two-mode spectroscopy and is based on the following different illumination and measuring conditions [1, 37–39]: First modus: polychromatic illumination and sequential monochromatic measurement; Second modus: sequential monochromatic illumination and polychromatic measurement. In the first modus, the fluorescent colorant is, for example, illuminated with a xenon or mercury high-pressure vapor lamp. The measurement is repeated serially using filters of narrow bandwidth (monochromator) but discrete wavelengths in the visible range. The whole of the measured spectral values correspond, therefore, to the visual impression of the color, provided that
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4 Measuring Colors
the measurements and observation are performed with the same illumination source. In the second modus, a monochromator produces an illumination at each given wavelength. The spectrum of fluorescence emission is measured at all wavelengths in the visible range. From the difference in the spectral values between the first and second modus, a measure of the extent of the fluorescence emission results. In Fig. 4.16, the two reflection curves obtained from the two-mode spectroscopy of a red fluorescence colorant are shown; the curves intersect at wavelength λs . From subtraction of both curves for wavelengths λ ≥ λs , a measure for the actual fluorescence emission results. The fluorescence behavior depends on some fundamental factors which make the handling of such colorants more difficult. For example, the height and width of the emission band of normal fluorescent colorants for wavelengths ≥ λs depend on: – the colorant concentration; initially, the emission intensity increases with increasing concentration, but the intensity is lowered while approaching a saturation concentration; this is caused by intrinsic absorption due to denser
ρ(λ) 1.2
Polychromatic Monochromatic
1.0
0.8
0.6
0.4
0.2 λS 0 400
500
600
λ nm
Fig. 4.16 Spectral reflectance of a red fluorescence colorant at polychromatic and monochromatic illumination; intersection wavelength λs = 600 nm
4.2
Measuring Methods
277
molecular packing; the behavior is similar to chroma reduction of normal absorption colorants, cf. Fig. 3.12; – the sort and chemical structure of the dye or pigment; – the sort and operating mechanisms of additives; these can, by foreign absorption, even lead to total extinction of fluorescence radiation; – the chemical and physical constitution of the binder, e.g., the sort of solvent, polymer, or fibrous material.
During execution of both operation modes further aspects should be considered in order to avoid systematic measuring errors. Reliable and comparable results are only attained using the recommended measuring geometry 45c:0, therefore, the specular component is excluded. Otherwise the excitation energy is additionally – but uncontrollably – increased by the specular reflection. In order to achieve constant excitation, measurements should be performed under stationary operating conditions of the instrument and each with the same illumination and measuring aperture. On the other hand, if fluorescent materials are measured using diffuse geometries such as de:8 or d:0, then the illumination of the sphere interior, which is superimposed by fluorescence emission, can lead to lower reflection factors. This suggests the insertion of the smallest possible measuring aperture. Otherwise the sample field is additionally too intensively illuminated by the emitted fluorescence light [40]. Although the empirical skills for recipe prediction of fluorescent colorants seem to be promising for textiles [41], the experimental realization is – in view of the metrological conditions mentioned – to be judged extremely skeptically. Fluorescent colorants are, therefore, not included in the discussion of recipe prediction in Chapter 6. Similar considerations as the above can also be applied to thermochromic colorants. A reasonable fraction of absorption colorants behave thermochromic, that is, to a high degree the reflection or transmission depends on the temperature of the colorant. The change in temperature can be caused by thermal or optical radiation. Thermally or optically produced color dependence is, however, undesirable for normal absorption colorants. On the other hand, the color changes of thermochromic substances are specifically used, e.g., for determination of surface temperatures to more than 100◦ C. With special liquid crystalline polymers of cholesteric texture, temperature measurements are often accurate to Δϑ = ± 0.1 K. If the color pattern was exposed to undefined illumination or heat release of the instrument, color measurements of thermochromic materials should only be performed after temperature equilibration. For illumination of the sample, only flash lamps of maximum 0.5 ms pulse duration combined with low energy release of no more than 0.1 mW should be applied. Sequential, short-termed
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4 Measuring Colors
monochromatic illumination at discrete measuring wavelengths also turns out to be effective. For systematic investigations of thermochromic behavior, the color pattern is fixed in the instrument and measured in this position several times in a row. After each measurement, the time is recorded and the color differences with respect to the first measurement are determined. The initial and the end temperatures always need to be recorded as well. The specific temperature control of the sample holder is much more well defined. Consequently, the temperature variation can be precisely registered and the thermochromic temperature interval can be determined. Thermochromic behavior, however, can also be mimicked by changing humidity. During measurement and storage one must, therefore, ensure constant air humidity, even better using a standard climate. Measurements on photochromic colorations can be performed just as precisely. Photochromic substances in textile fibers or optical glass are subject to color changes by light absorption in the UV or visible range. Also this sort of color change is reversible; the absorbed energy is dissipated over time in the form of thermal radiation. Phototropy (synonymous to photochromism) can be evoked by different mechanisms such as isomerization of covalent bonds, absorption or emission of photons, tautomerism by proton transfer, cyclo-addition, and dissociation [42]. For measurements of photochromic colorations, the geometries 45c:0 or de:8 installed with smallest possible illumination and measurement aperture are at best suited. The time constant for reaching color saturation and the decay constant result from color measurement in dependence of time under different constant illuminations. The repeated measurements should be performed in the same way as for thermochromic colors. Because of the time-dependent optical behavior and rare demand, thermochromic and photochromic colorants are out of the scope of this text and not included in discussion of recipe prediction.
4.3 Uncertainties of Spectral Color Measurement It is impossible to make a statement about the trustworthiness of a result so long as we have no information about the numerical uncertainty of a measured quantity: if the accuracy of the measurement results is not available, the numerical values are of no meaning. The accuracy, reproducibility, and carefulness with which spectral or colorimetrical quantities are determined are deciding factors for color matching, dependability of covering capacity, color tolerances, acceptability of color differences, and observance of criteria for recipe prediction, among other things. First, we discuss the types and characteristics of errors. Afterward, we give insight into fundamental methods for determining and verifying measurement uncertainty and error distributions of three-dimensional
4.3
Uncertainties of Spectral Color Measurement
279
variables. Finally, we focus on statistical testing of color differences. This is of importance, for example, for color matching or quality control in color industry.
4.3.1 Qualitative Errors Since the beginnings of exact natural sciences, there has been a sobering concept: irrespective of how careful, well considered, or prepared a measurement is performed, the measurement and observational data are unavoidably combined with measurement errors. The combined errors, which occur during measurements, are called deviations. The indicated error of a measurement result is, however, denoted as measurement uncertainty [43]. Because measuring is inevitably accompanied by errors, one always attempts to keep the deviations as small as possible by suitable approaches. This is done in order to obtain the best possible approximate values under the given conditions with regard to the quantity to measure. In addition, as possible, it is useful to estimate the measurement uncertainty. For this, well-established methods of mathematical statistics can be used. These methods of operation are founded on the realization that the error-free measured value is absolutely not known: the range of possible values can only be narrowed with the methods of theory of errors [44 – 47]. Experience shows that the invariably occurring measurement errors are divided into three primary categories which can be considered to be independent of each other: gross, systematic, and statistic or random errors (stochastic uncertainty). Gross errors are to put down to falsely taken readings, confusions, inattentiveness, etc. These are often due to the mistakes of the person doing the measuring. Of course, such errors are not to be treated by the methods of error theory. This type of error is often discernible in a measurement series as socalled anomalies. The nature and way that the anomaly occurs often gives indications as to how such errors can be eliminated. In context of color patterns, gross errors are created, for example, by: – undefined, unequal, defective, or mixed up color samples, binders, backgrounds, or substrates; – employment of color patterns with the wrong surface or surface structure; – manufacturing with inappropriate colorants or incorrect parameters, aged or stored color patterns; – confusion of colorant components, additives, or binders. Systematic errors are based on incorrect conditions which, to a great extent, are due to limitations of the measuring instrument or evaluation method. Among those are:
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4 Measuring Colors
– incorrectly chosen measuring method(s); – incorrect measurement taking with not considering the measurement instructions; – wrongly calibrated measuring instruments; – drift of long-term reproducibility or lack of absolute accuracy of color measuring instruments; – incorrect evaluation methods or inapplicable formulas, approximations; – comparison of incorrect colors in test series.
Systematic errors usually alter the measurement result by the same amount or in the same direction. The detection of systematic errors is sometimes difficult and requires a certain sensibility and experience. This type of error is certainly controllable by supervision and selection. However, discovered systematic errors are also relevant in this context, for example, the edge loss of color patterns especially by measurements using spherical geometry. Random errors are caused by stochastic variations of the measuring conditions or other statistical influence factors. Statistical errors can change the measurement result in the positive and negative directions – in contrast to systematic errors. In accordance with theory of errors, experience shows that random errors can be reduced by either improved measuring conditions, sufficiently high number of repeated measurements, or suitable evaluation procedures. In practice, such methods can be limited by economic constraints. Despite these restrictions, the measuring conditions and extent should be structured in such a manner that the uncertainty obtained can be assessed as acceptable and trustworthy. Now that we have become acquainted with the three categories of measurement errors, we discuss in the following section the determination and reduction of purely random measurement errors by mathematical methods. It is assumed that the measuring uncertainty is influenced only by stochastic errors and all other error types are excluded. Even though the error-free value of a measured variable remains unknown, with these methods it is possible to specify the interval which contains the error-free value within a certain probability.
4.3.2 Quantitative Errors and Error Distribution The uncertainty of a measurement result is most simply indicated by estimation. This method is possible in cases where a computed uncertainty is only for verification of whether the measurement corresponds to the expected aim or not, or if it seems to be successful for orientation in similar problems. Such estimations are somewhat critical with regard to several independent or dependent
4.3
Uncertainties of Spectral Color Measurement
281
measurement variables. The exact determination of such dependent measurement uncertainties with regard to color values is discussed in the next two sections. For the moment, it is useful to concentrate on a single measurement variable. In order to reduce the uncertainty of measurement value x, the measurement is repeated N times – each time under identical conditions. It is self-evident that the result from this series with random (statistical or stochastic) readings is always more trustworthy than a single measurement value. The N values xi , for i = 1, 2, . . . , N, are called parent population. For reduction of the uncertainty of the N measured values, the arithmetic mean value x¯ is determined N 1 xi . x¯ = N
(4.3.1)
i=1
In order to derive the uncertainty of x¯ , the deviations from the mean vi = xi − x¯ are unusable because the sum over all N differences vi vanishes N i=1
vi =
N
(xi − x¯ ) = 0
(4.3.2)
i=1
on account of Equation (4.3.1). Therefore, the sum of squares v2i is summed up as the squared deviations. The expression N 1 v2i (4.3.3) σ = ± N−1 i=1
is the standard deviation of the measurement of the entire parent population of individual measurements for N ≥ 2. The denominator in Equation (4.3.3) contains the quantity N – 1, because a single measurement value has no mean. The value of σ is a measure of the magnitude with which most of the N individual values xi fluctuate around the mean x¯ . It is also called mean deviation or scattering; the quantity σ 2 is called variance. The middle quadratic error of the mean, σAM , is called standard deviation, SD (or root-mean-square error, r.m.s. deviation) and follows with Equation (4.3.3) from σ σAM = √ , N
(4.3.4)
where the subscript AM means arithmetic mean. From Equations (4.3.3) and (4.3.4), it should be clear that the deviations are smaller for a larger number N of the measurement population. This is synonymous with the fact that the accuracy of the mean (4.3.1) increases with the number N of repeated measurements. This dependence on the number N corresponds with hundreds
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4 Measuring Colors
of years of experience and is, in general, called law of large numbers. For reasons of economy and of time, the number N is generally limited to a reasonable value given the measurement time. How much time is necessary to spend on increasing N depends, in a practical sense, on how critical the actual measurement is. In addition, if an excessively long series of N measurements is performed, then a drift can actually make the statistics worse if carried to an extreme. Therefore, there is an additional practical limit to the concept. The quantities σ and σAM are approximates of the real SD σ of the actual parent population. According to the theory of errors, the probable, mean, and ηAM , and σAM , respectively, are in proportion to root-mean-square error γAM , each other: ηAM : σAM = γAM :
2 : 0.8 : 1.0. 3
(4.3.5)
The result of the measured variable is a narrowed value and can be given in the form x = x¯ ± ΔxAM = x¯ ± σAM .
(4.3.6)
The quantity ΔxAM is called the absolute error and has the same unit as the mean x¯ . The relative error of x¯ is given by the quotient ΔxAM x¯ and is dimensionless. Therefore, the measurement result can also be indicated as4 x = x¯ ±
σAM ΔxAM = x¯ ± . x¯ x¯
(4.3.7)
In addition, the probability for which the error-free value of x is in the computed interval x¯ ±ΔxAM can be determined. The probability P is a dimensionless value in the closed interval [0, 1] and it characterizes a statistical event. A value P = 0 means that the event happening is not possible; however, P = 1 represents an absolutely certain event. Although a dimensionless value of, e.g., P = 0.95 means a high probability, it is not for sure that the event actually occurs. Considerations in this regard go back to Gauss. For random errors, the single values xi typically scatter symmetrically about the arithmetic mean x¯ . Because SD becomes smaller with increasing number N according to Equation (4.3.4), the frequency of large deviations from the mean is decreased. In the case N → ∞, the discrete measuring values xi become continuous quantities x. The mean x¯ then equals the error-free value μ = x¯ and the r.m.s. deviation σAM becomes 4 In
connection with expression (4.3.7), the extra terms introduced representing rough accuracy and precision of a measurement result should be differentiated: the fictive quantity of accuracy stands for the difference between the mean x¯ and the error-free, but unknown value; precision is simply a measure for standard deviation σAM .
4.3
Uncertainties of Spectral Color Measurement
283
σ = σAM . The accompanying distribution curve of the measured results is called the Gaussian distribution or normal distribution.5 The corresponding function f(x) is called the distribution function. Now the question should be addressed as to whether it is possible to predict for every experiment the limit distribution f (x). In most cases, it can be assumed that the limit distribution is the Gaussian distribution: ! (x − μ)2 1 . f (x) = √ exp − 2σ 2 σ 2π
(4.3.8)
The graph of the Gaussian distribution takes the form of a symmetrical bellshaped curve. The density function is characterized by both the quantities μ and σ : the maximum is located at the true mean value μ = x¯ and the inflection points are located at x = μ ± σ . From integration of the normal distribution (4.3.8), the normal distribution function, follows "x F(x) =
f (t) dt.
(4.3.9)
−∞
√ The normalizing factor 1/σ 2π in f(x) follows from the plausible condition that the area enclosed by the Gaussian distribution takes the value 1. Accordingly, the normal distribution function F(x) takes for x → ∞ the limit F(x → ∞) = 1. This is synonymous with the fact that the error-free quantity x in Equation (4.3.6) is with absolute certainty, or probability P(x) = 1, found in the infinite interval – ∞ ≤ x ≤ ∞. Now, we assume that an arbitrary random variable X (stochastic variable) obeys the statistics of distribution (4.3.9). In this case, the probability P(X) for X to adopt an arbitrary value within the finite interval a < X ≤ b is given by the relation "b P(a < X ≤ b) = F(b) − F(a) =
f (t) dt.
(4.3.10)
a
If for integration limits in Equation (4.3.10) are used the deviations ΔX = ± lσ from the mean μ, which are given by a = μ – lσ and b = μ + lσ for l = 1, 2, 3, . . . , then the first three probable values are
5 Other distributions like binomial distribution, hypergeometric distribution, or Poisson distribution are not considered in this book.
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4 Measuring Colors
⎧ ⎨ 0.683 for l = 1 P(μ − lσ < X ≤ μ + lσ ) = 0.955 for l = 2 . ⎩ 0.997 for l = 3
(4.3.11)
The first of these cases means that already 68.3% of the N measuring values are located between the inflection points of f(x). The probability of finding a measured value in the interval μ−3σ < x ≤ μ+3σ is already 99.7%. Consequently, nearly all measured values are contained in this extended interval. If a parent population is subject to a Gaussian distribution, then it can generally be assumed that for N ≥ 30, the actual values can be reasonably given by those statistical 2 = σ 2. ones, i.e., μ = x¯ and σAM
4.3.3 Normal Distribution in Three and More Dimensions With regard to colorimetrical aspects, the considerations up to now for one stochastic variable in Section 4.3.2 need to be extended to at least three. The numerical effort is now greater due to two reasons: first, the color values themselves depend on each other and second, the total deviation does not follow only from the deviations that each variable has from its respective mean. For the moment, we concentrate on the general case of n Gaussian random variables xk , for k = 1, 2, . . . , n. These are written in the form of a vector x = (x1 , x2 , . . . , xn )T . Instead of the Gaussian distribution function (4.3.8), the generalized density function 1 1 · exp − (x − m)T C(x − m) Φ(x) = n 2 1 2 / / 2 (2π) ( det C)
! (4.3.12)
[48] is then used. In Equation (4.3.12), m is an n-dimensional vector which contains the means μ1 , μ2 , . . . , μn of each random variable xk , each for infinite number of repeated measurements. The quantity det C is the determinant of the quadratic (n, n) matrix C; the elements of the respective inverse matrix V = C –1 consists of the variances and covariances of the n Gaussian values of vector x. The variance σˆ (xk ) for each random variable xk simply follows from Equation σ 2 . The covariance is composed of the Gaussian (4.3.3) by relation σˆ (xk ) = variables xk , xl , where k = l; see below the case for three variables. Now multidimensional areas with equal likelihood random variables are of interest. These are given by the constant exponent of the generalized density function (4.3.12) without the factor –1/2: (x − m)T C(x − m) = const.
(4.3.13)
4.3
Uncertainties of Spectral Color Measurement
285
This relation written in full corresponds to the equation of an n-dimensional ellipsoid of center point M = (μ1 , μ2 , . . . , μn ), the coordinates agree with the components of vector m. In the special case for colorimetry of n = 3 Gaussian variables x1 , x2 , x3 , the vector x = (x1 , x2 , x3 ) T follows. N repeated measurements comprising (x1i , x2i , x3i ) for i = 1, 2, . . . , N have values scattering around the respective means of x¯ 1 , x¯ 2 , and x¯ 3 . The corresponding single SDs superimpose over each other along the three coordinate axes. This can be illustrated by a three-dimensional ellipsoid with center in about M ≈ (¯x1 , x¯ 2 , x¯ 3 ). In analogy with the case of one dimension, in consequence of Equation (4.3.11), it follows that a longer semi-axis of the ellipsoid results in a higher probability that the result of the kth measurement (x1k , x2k , x3k ) is represented by a point inside of the ellipsoid. The parameters of this ellipsoid follow altogether from six quantities: first, the three variances σˆ (xk ), k = 1, 2, 3, which, with regard to Equation (4.3.3), are given by the squared deviations of the mean (xki − x¯ k )2 for the N single values 1 (xki − x¯ k )2 , N−1 N
σˆ (xk ) =
k = 1, 2, 3;
(4.3.14)
i=1
second, the three covariances σˆ (xk , xl ) for k, l = 1, 2, 3 with k = l. These are given by the combined deviations of two variables xk , xl for k = l: 1 σˆ (xk , xl ) = σˆ (xl , xk ) = (xki − x¯ k )(xli − x¯ l ). N−1 N
(4.3.15)
i=1
It needs to be determined for the covariances σˆ (xk , xl ) whether or not the deviations of both variables xk , xl for k = l are really independent of one another. In cases of dependence, both terms in brackets of Equation (4.3.15) have the same sign, this is the reason why the accompanying variances σˆ (xk ), σˆ (xl ) result in high values. For independent measuring values, covariances virtually vanish. Now, we form the matrix of variances and covariances ⎛
⎞ σˆ (x1 ) σˆ (x1 , x2 ) σˆ (x1 , x3 ) σˆ (x2 , x3 ) ⎠ , V = (vkl ) = ⎝ σˆ (x2 , x1 ) σˆ ( x2 ) σˆ (x3 , x1 ) σˆ (x3 , x2 ) σˆ (x3 )
(4.3.16)
which, due to the commutative factors in Equation (4.3.15), is symmetrical with regard to the main diagonal. From the inverse V–1 , the elements ckl of the new matrix C follow: C = (ckl ) = V −1 ,
ckl = clk , k, l = 1, 2, 3.
(4.3.17)
These elements determine the equation of the accompanying scatter ellipsoid:
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4 Measuring Colors
c11 (Δx1 )2 + c22 (Δx2 )2 + c33 (Δx3 )2 + 2(c12 Δx1 Δx2 + c13 Δx1 Δx3 (4.3.18) +c23 Δx2 Δx3 ) = P(χ 2 ,3). The differences Δxk are given by the deviations Δxk = xk − x¯ k , k = 1, 2, 3.
(4.3.19)
The inhomogeneity P(χ 2 , 3) of the ellipsoid equation in Equation (4.3.18) is, in analogy to the one-dimensional case, the distribution function of the f = 3 Gaussian random quantities x1 , x2 , x3 . The quantity f is called degree of freedom. In the case of vanishing covariances, Equation (4.3.15) and, therefore, coefficients ckl = 0 for k = l vanish; therefore, the axis of the ellipsoid are parallel to the coordinate axis x1 , x2 , x3 , and these variables change independent of each other. The distribution function P(χ 2 , f ) for natural values f is given by
P(χ 2 , f ) =
1 2f /2 Γ (f /2)
"χ
2
ν (f /2)−1 e−ν/2 dν,
(4.3.20)
0
where Γ (f /2) is Euler’s gamma function [46]. The values of P(χ 2 , f ) = (χf ; S )2 with f = 1, 2, 3 are listed in Table 4.5 in dependence on different levels of confidence S = 1 – α, whereas α is the so-called critical value (significance level). The values of P(χ 2 , 3) and, therefore, the length of each semiaxis of the ellipsoid increases exponentially with S. The case f = 1 corresponds to the one-dimensional Gaussian distribution (4.3.8). Table 4.5 Threshold values in dependence on significance level S for two different freedom degrees f of the χ 2 probability distribution [47] (χf ; 1−α )2
χf ; 1−α
S = 1–α (%)
f=1
f=2
f=3
f=1
f=2
f=3
50.0 70.0 75.0 80.0 90.0 95.0 97.5 99.0 99.5 99.9
0.455 1.07 1.32 1.64 2.71 3.84 5.02 6.63 7.88 10.83
1.39 2.41 2.77 3.22 4.61 5.99 7.38 9.21 10.60 13.82
2.37 3.66 4.11 4.64 6.25 7.81 9.35 11.34 12.84 16.27
0.675 1.03 1.15 1.28 1.65 1.96 2.24 2.57 2.81 3.29
1.18 1.55 1.66 1.79 2.15 2.45 2.72 3.03 3.26 3.72
1.54 1.91 2.03 2.15 2.50 2.79 3.06 3.37 3.58 4.03
4.3
Uncertainties of Spectral Color Measurement
287
With regard to color values such as L, a, b, the corresponding quantities of mean, SD, variance, and covariance are only indirectly applicable. This is reasoned from the mathematical point of view that color values are not independent of one another. Nevertheless, the above-mentioned considerations are by no means useless with regard to color values because over a statistical test, it is possible to decide, for example, whether or not the assumed normally distributed color deviations of a special color series are caused by measuring error. The formulation of such questions is not at all restricted to color differences but also for graininess and sparkle area, for example. Furthermore, similar problems occur in a multitude of industrial fields; these would be insurmountable without statistical methods. Such a procedure especially geared to color differences is discussed in the next section.
4.3.4 Statistical Testing of Color Differences Statistical methods are an essential aid not alone in natural and social sciences but also in economics and industrial production. One aim of statistics consists of making a likelihood statement over an interesting property. This is only based on random (stochastic) spot checks. Although the meaningfulness of statistical statements are absolutely unreliable, statistics allows, however, for the possibility of stating confidence levels and testing of a hypothesis by suitable statistical test quantities. The accompanying approach is termed as statistical testing procedure [44, 45, 47]. We now follow the assumptions for examination of color differences of such a statistical test method. With a test method, at any one time it is possible to check an alternative question as to whether or not the mean value of a sample property μS deviates from the mean of the relevant reference property μR . As a rule, the so-called null hypothesis is formulated, which means both average values are assumed to be equal μS = μR , leading to a zero difference. It is then investigated by statistical methods, if the sample property according to this hypothesis turns out to be of high or low probability. For this assumption, as discussed in the previous section, there is a statistical level of confidence S = 1 – α with significance point (critical value) α of, e.g., α = 30, 5, 1, or 0.5%. If the determined probability falls below the given value, it is then assumed that the hypothesis is not true; the hypothesis is rejected. In order to make this decision, a test quantity t is created. This represents itself again a stochastic variable – for example, depending on the color value F to test. With the aid of the distribution of the test quantity and with regard to the chosen statistical security S, a critical value tS can be derived. If the sample property produces a test value |t| ≤ tS , then the hypothesis is not disproved by the sample property and the hypothesis can be accepted. Because of this, t is termed as statistically not significant. However, if |t| > tS , then the hypothesis
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is rejected, t turns out to be statistically significant: |t| =
≤ tS : hypothesis is statistically not significant > tS : hypothesis is statistically significant
.
(4.3.21)
The rejection is synonymous with the fact that the hypothesis is declined with the probability α, although it can still actually be true (the so-called error of first kind). In contrast is if a wrong hypothesis is accepted (error of second kind). Accordingly, application of the statistical testing procedure means that in α% of all cases, the hypothesis is wrongly rejected. Because of that, the quantity α is also termed as producer risk, since in α% of all cases, e.g., a colorant fabrication is rejected as inappropriate, though the production is actually satisfactory. At the latest, the objection should be raised at this stage that chromaticities are not independent of each other and, therefore, are not random variables. After all, the color values depend on – according to Section 3.1 – the standard color values X, Y, Z, those on the overlapping SCMFs x¯ (λ), y¯ (λ), z¯(λ), and the measured spectral values. Certainly, not the absolute values of the chromaticities, but color difference contributions ΔF such as ΔL, Δa, Δb or others are true stochastic variables. For small color differences, so to speak, the mathematical transformation of the spectral values disappears: it remains only the stochastic property of the color differences. The following considerations are consequently only valid for individual, small color difference contributions. These were already assumed to have value |ΔF| ≤ 3 (meaning |ΔE| ≤ 5) considering the non-uniformly scaled color spaces in the previous chapter. This sort of statistical test only answers the question as to whether or not an experimentally determined color difference contribution ΔF is to be considered incorrect due to measurement errors. A critical test quantity tΔF belongs to ΔF. As we will see below, this follows from a coefficient, which is contained in the accompanying equation of the standard deviation ellipsoid (4.3.18). Clearly, the determined ellipsoid coefficients are only valid for the measured sample and reference color patterns, the applied measuring instrument, and the chosen colorimetrical formalism. At least these three conditions need to be indicated with each determined ellipsoid. A previously determined ellipsoid, therefore, is only applicable to a new sample series, if the same conditions were used, such as the same reference colors, manufacturing methods, same spectrophotometer, the same illuminant. The following statistical significance testing (evidence testing) can be applied to colors and colorants as well as to intermediate and final products. For performance of the statistical testing of color differences with the assistance of statistic test values tS , the following procedure has proven to be worthwhile [48 –50]. At first, N ≥ 20 sample and reference color patterns are manufactured. If only one reference color needs to be matched, then it is
4.3
Uncertainties of Spectral Color Measurement
289
assumed that the accompanying mean color differences came from N repeated measurements. The procedure is, in general, divided into four steps: 1. determination of the desired mean color difference contributions ΔF between sample and reference colors ΔL, Δa, Δb, for example; 2. computation of the coefficients of the accompanying scattering ellipsoid ckl with k, l = 1, 2 , 3; 3. calculation of the test quantities tΔF;1 –α concerning the chosen statistical level of confidence S = 1 – α; 4. comparison of the numerical values of |ΔF | and |tΔF; 1−α | . If the condition |ΔF| > |tΔF; 1−α | is satisfied, the color difference contribution ΔF is significant to a statistical level of confidence of S%. However, if it turns out that |ΔF | ≤ |tΔF; 1−α | is valid, then the quantity ΔF is not significant to the same statistical level and the null hypothesis is accepted, cf. alternatives in Equation (4.3.21). In the first step indicated above, the mean color differences between the sample and reference color patterns follow from Sections 3.1.3 and 3.1.4 and Equation (4.3.1), for example, by ΔL = LS − LR , Δa = a¯ S − a¯ R , Δb = b¯ S − b¯ R , ΔC = CS − CR = (¯aS )2 + (b¯ S )2 − (¯aR )2 + (b¯ R )2 , ΔE = (ΔL)2 + (Δa)2 + (Δb)2 .
(4.3.22) (4.3.23) (4.3.24)
In Equations (4.3.22) and (4.3.23), LS , a¯ S , b¯ S and LR , a¯ R , b¯ R stand for the means of the color values of the sample color and reference color patterns, respectively. From both measurement series, the middle difference of the hue angle can also be determined Δh =
% $ %& $ 180◦ # arctan b¯ S /¯aS − arctan b¯ R /¯aR , π
(4.3.25)
and the mean value of the hue contribution ΔH =
a¯ R · b¯ S − a¯ S · b¯ R . + 0.5 · (CS · CR + a¯ S · a¯ R + b¯ S · b¯ R )
(4.3.26)
In the above-mentioned second step, the ellipsoid parameters with the variances σˆ (Δa), σˆ (Δb), σˆ (ΔL) and covariances σˆ (ΔL, Δa), σˆ (ΔL, Δb), σˆ (Δa, Δb) are calculated. These follow from Equations (4.3.14) and (4.3.15) by substituting xk with Δxk :
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4 Measuring Colors
1 σˆ (Δxk ) = (Δxki − Δxk )2 , xk = L, a, b, N−1 N
(4.3.27)
i=1
1 (Δxki − Δxk )(Δxli − Δxl ), xl = L, a, b, (4.3.28) N−1 N
σˆ (Δxk , Δxl ) =
i=1
where Δxki = xki,S − xki,R is the difference between the color value xki,S of the sample and the reference color xki,R and Δxk is the average value of each connected N single color values Δxk1 , Δxk2 , ... , ΔxkN , k, l = 1, 2, 3. With the elements ckl of the inverse matrix, C = (ckl ) = V–1 , the equation of the pattern of dispersion is given by c11 (ΔL)2 + c22 (Δa)2 + c33 (Δb)2 + 2 [c12 ΔL · Δa + c13 ΔL · Δb + c23 Δa · Δb] = 1.
(4.3.29)
The third step is the determination of at best six statistical test quantities tΔF; 1 – α with regard to the various chromaticity differences. These are assumed to be Gaussian and are, therefore, normal distributed. The conditional equations for the single test quantities result from the formulation of the question, what is the likelihood that a color difference contribution ΔF is represented by a point inside the corresponding standard deviation ellipsoid? The equation of the 2 ellipsoid is given by Equation (4.3.33) with inhomogeneity χ3;1−α instead of unity. The test quantity t F;1–α of the color difference contribution F follows from the generally valid expression σΔF tΔF; 1−α = √ · χ3; 1−α , N
(4.3.30)
where σΔF is the SD with regard to the color difference contribution ΔF, N the number of measurements of the parent color population, and χ3; 1−α the distribution quantity of the chosen statistical level of confidence 1 – α (see Table 4.5). The SDs of the various color values are given with the geometrical properties of the scatter ellipsoid, which are represented by the coefficients ckl of the scatter matrix C. The test quantities for the color difference distributions of ΔL, Δa, Δb follow from: χ3; 1−α , tΔL = √ Nc11
(4.3.31)
χ3; 1−α tΔa = √ , Nc22
(4.3.32)
4.3
Uncertainties of Spectral Color Measurement
291
χ3; 1−α tΔb = √ . Nc33
(4.3.33)
In other words, the value of 1/σΔF equals the square root of the corresponding coefficient ckk (k = 1, 2, 3) in the ellipsoid equation (4.3.33). The test quantity for the total mean color difference ΔE is given by χ3; 1−α , tΔE = √ NcE
(4.3.34)
2 whereas, using Equation (4.3.29), the reciprocal squared variance cE = 1 σΔE results in cE =
1 [c11 (ΔL)2 + c22 (Δa)2 + c33 (Δb)2 + 2(c12 ΔL · Δa (ΔE)2 + c13 ΔL · Δb + c23 Δa · Δb )].
(4.3.35)
In addition, the test quantities of moderate contributions of chroma tΔC , hue tΔH , and hue angle tΔh can be derived by consideration of the geometrical context in a color plane (cf. Fig. 3.6): tΔC = χ3; 1−α
1 2N
1 1 , + cS cR
(4.3.36)
where cS is given by cS = c22 cos2 h¯ S + c33 sin2 h¯ S + 2c23 sin h¯ S cos h¯ S ;
(4.3.37)
the quantity cR is immediately given by substitution of the index S with R into Equation (4.3.36), which means that the sample quantities are exchanged with the reference ones. The mean values of the hue angles h¯ S and h¯ R are calculated using Equation (4.3.1). Equation (4.3.36) corresponds to an ellipse in the a, b color plane of curve parameters sin h¯ S , cos h¯ S instead of Δa, Δb. In analogy, the test quantity of the hue contribution is given by χ3; 1−α , tΔH = √ NcH
(4.3.38)
¯ cH = c22 sin2 h¯ + c33 cos2 h¯ − 2 c23 sin h¯ cos h;
(4.3.39)
with
where h¯ is the arithmetic mean of h¯ S and h¯ R . With that, the statistical test quantity for the hue angle can finally be determined from
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4 Measuring Colors
tΔh = arctan
2 · tΔH ΔH
! · tan (Δh 2) .
(4.3.40)
In the preceding formalism, the contributions Δa, Δb can be substituted by the color distributions ΔC, ΔH right from the beginning. In this case, analogous relations to Equations (4.3.30), (4.3.31), (4.3.32), (4.3.33), and (4.3.34) result, but they contain other ellipsoid coefficients c˜ kl . From there, the test values of tΔL , tΔC , tΔH , tΔE follow. The determination of tΔh is unchanged with regard to Equation (4.3.44). Finally, the fourth step is the decisive one. Now, one of the possibilities given in Equation (4.3.21) is true. This means that the hypothesis is either significant or not. The absolute value of the test quantity gives only an indication of how well the assumptions of the null hypothesis are fulfilled. A somewhat better, but always unreliable evaluation is given with the so-called sequential analysis. With this procedure, the double-ended risk of wrongly deciding (errors of first and second kind) is more manageable. The entire parent population N is not directly used, but rather stepwise with numbers of N = 2, 3, . . . . After each step, it is decided if the tested hypothesis is accepted, rejected, or if the procedure is to continue. With that, the number of random tests can often be substantially reduced. Although the formalisms described are complex to program and implement, a large portion of formulation of questions, for example, in quality control can only be answered with the aid of mathematical statistics. At this stage, we conclude this short exposition of measuring uncertainty and statistics of color measurements with respect to color difference contributions. The seemingly trouble-free measurement of color patterns is just compounded by the typical double meaning of the term color measuring. Those are the subjective visual perception and the metrological determination of color values – which are mutually dependent. In principle, the visual non-uniformity of the applied color spaces and, moreover, the nonlinear color development of absorption and effect colorants in dependence on concentration should also be mentioned. The color physical and colorimetrical properties and measurements of colorations with effect pigments are far more complicated to measure and evaluate. It is clear that an accurately applied and correctly performed measurement technique has developed itself into an indispensable instrument in industrial color physics.
References 1. CIE No 46: “A review of publications on properties and reflections values of material and reflection standards”, CIE, Bureau de la CIE, Wien (1979) 2. Hunter, RS, Harold, RW, Eds: “The Measurement of Appearance”, 2nd ed, Wiley, New York (1987)
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3. Berger-Schunn, A: “Practical Color Measurement”, Wiley, New York (1994) 4. Berns, RS, Billmeyer, FW, Saltzman, M: “Billmeyer and Saltzman’s Principles of Color Technology”, 3rd ed, Wiley-Interscience, New York (2000) 5. Hunt, RGW: “Measuring Colour”, 3rd ed, Fountain Press, Kingston–upon–Thames (1998) 6. Hunt, RGW: “The Reproduction of Colour”, 6th ed, Wiley, Chichester (2004) 7. Noboru, O, Robertson, AR: “ Colorimetry”, Wiley, Chichester (2005) 8. Schanda, J, Ed: “Colorimetry: Understanding the CIE System”, Wiley, Hoboken, NJ (2007) 9. Ishihara, S: “The series of plates designed as a test for colour-blindness”, Kanehara, Tokyo (1995) 10. DIN 6160: “Anomaloskope zur Diagnose von Rot-Gruen-Farbenfehlsichtigkeiten”, Deutsches Institut fuer Normung eV, Berlin (1996) 11. ASTM E 1499–97: “Standard Guide for Selection, Evaluation, and Training of Observers”, American Society for Testing and Materials, West Conshohocken, PA (2003) 12. ASTM D 1729–96: “Standard Practice for Visual Appraisal of Colors and ColorDifferences of Diffusely-Illuminated Opaque Materials”, American Society for Testing and Materials, West Conshohocken, PA (2003) 13. ISO 3664: 2000: “Viewing conditions–Graphic technology and photography”, International Organization of Standardization, Genf (2000) 14. CIE No 130: “Practical Methods for the Measurement of Reflectance and Transmittance”, CIE, Bureau Central de la CIE, Wien (1998) 15. Ditteon, R: “Modern Geometrical Optics”, Wiley, New York (1998) 16. DIN 5036-1: “Strahlungsphysikalische und lichttechnische Eigenschaften von Materialien; Begriffe, Kennzahlen”, Deutsches Institut fuer Normung eV, Berlin (1978, 1980) 17. DIN 6175-2: “Farbtoleranzen fuer Automobillackierungen”, Teil 2: “Toleranzen fuer Effektlackierungen”, Deutsches Institut fuer Normung eV, Berlin (2001) 18. ASTM E 2194–03: “Standard Practice for Multiangle Color Measurement of Metal Flake Pigmented Materials”, American Society for Testing and Materials, West Conshohocken, PA (2003) 19. ASTM WK 1164: “Standard Practice for Multiangle Color Measurement of Interference Pigmented Materials”, American Society for Testing and Materials, West Conshohocken, PA (2006); ASTM E 2539: “Standard Practice for Multiangle Color Measurement of Interference Pigments”, American Society for Testing and Materials, West Conshohocken, PA (2008) 20. DIN 6175-3: “Farbtoleranzen fuer Automobillackierungen”, Teil 3: “Messgeometrien fuerInterferenzpigmente”, Project, Deutsches Institut fuer Normung eV, Berlin (2006) 21. Alman, DH: “Directional color measurement of metallic flake finishes”, Proc ISCC Williamsburg Conf on Appearance 53 (1987) 22. Hofmeister, F, Maisch, R, Gabel, PW: “Farbmetrische Charakterisierung und Identifizierung von Mica-Lackierungen”, Farbe and Lack 98 (1992) 593 23. Gabel, PW, Hofmeister, F, Pieper, H: “Interference pigments as focal points of colour measurement”, Kontakte (Darmstadt) 2 (1992) 25 24. Cramer, WR, Gabel, PW: “Effektvolles messen”, Farbe & Lack 107 (2001) 42 25. Nadal, ME, Early, EA: “Color measurements for pearlescent coatings”, Col Res Appl 29 (2004) 38 26. DIN 5033: “Farbmessung”, Part 1-9, Deutsches Institut fuer Normung eV, Berlin (1979–2008) 27. ISO 7724-1: “Paints and Varnishes – Colorimetry – Part 1: Principles”, International Organization of Standardization, Genf (1984) 28. JIS Z 8722/C: “Methods of Measurement of Color of Reflecting or Transmitting Objects”, Japanese Standards Association, Tokyo (1994)
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29. ASTM E 308–08: “Standard Practice for Computing the Colors of Objects by Using the CIE-System”, American Society for Testing and Materials, West Conshohocken, PA (2008) 30. ASTM E 1164–07: “Standard Practice of Obtaining Spectrometric Data for ObjectColor Evaluation”, American Society for Testing and Materials, West Conshohocken, PA (2007) 31. ASTM D 2244–07e1: “Standard Practice for Calculation of Color Tolerances and Color Differences from Instrumentally Measured Color Coordinates”, American Society for Testing and Materials, West Conshohocken, PA (2007); ASTM D 3134 – 97: “Standard Practice for Establishing Color and Gloss Tolerances”, American Society for Testing and Materials, West Conshohocken, PA (2008) 32. CIE No 15.3: “Colorimetry”, 3rd ed, CIE, Bureau Central de la CIE, Wien (2004) 33. DIN Fachbericht 49: “Verfahren zur Vereinbarungen von Farbtoleranzen”, Deutsches Institut fuer Normung eV, Berlin (1995) 34. Rich, DC, Battle, D, Malkin, F, Williamson, C, Ingleson, A: “Evaluation of the longterm repeatability of reflectance spectrophotometers”, in: Burgess C, Jones, DG, Eds: “Spectrophotometry, Luminescence and Color; Science and Compliance”, Elsevier, Amsterdam (1995); ASTM E 2214–08: “Practice for Specifying and Verifying the Performance of Color Measuring Instruments”, American Society for Testing and Materials, West Conshohocken, PA (2008) 35. ASTM E 430–05: “Standard Test Methods for measurement of Gloss of High Gloss Surfaces by Abridged Goniophotometry”, American Society for Testing and Materials, West Conshohocken, PA (2005) 36. DIN 55923: “Pigmente: Aluminiumpigmente und Aluminiumpigmentpasten fuer Anstrichfarben”, Deutsches Institut fuer Normung eV, Berlin (1983) 37. Valeur, B: “Molecular Fluorescence”, repr 1st ed, Wiley-VCH, Weinheim (2005) 38. CIE 76: “Intercomparisation of Measurement of (Total) Spectral Radiance Factor of Luminescent Specimens”, Commission Internationale de L’Éclairage (CIE), Bureau Central de la CIE, Wien (1988) 39. ASTM E 991–06: “Standard Practice for Color Measurement of Fluorescent Specimens”, American Society for Testing and Materials, West Conshohocken, PA (2006) 40. DIN 53145-1/2: “Pruefung von Papier und Pappe – Messgrundlagen zur Bestimmung des Reflexionsfaktors; Messung an fluoreszierenden Proben”, Deutsches Institut fuer Normung eV, Berlin (2000) 41. McDonald, R: “Recipe prediction for textiles”, in: McDonald, R, Ed: “Colour Physics for Industry”, 2nd ed, Soc Dyers Colourists, Bradford (1997) 42. Duerr, H, Bouas-Laurent, H: “Photochromism”, Elsevier, Amsterdam (2003) 43. Kirkup, L, Frenkel, RB: “An introduction to uncertainty measurement”, Cambridge Univ Press, Cambridge (2006) 44. Zurmuehl, R: “Praktische Mathematik fuer Ingenieure und Physiker”, 5th ed, Springer, Berlin (1984) 45. Crawley, MJ: “Statistics”, Wiley, Chichester (2008) 46. Bevingston, PR: “Data reduction and error analysis for physical sciences”, 3rd ed, McGraw-Hill, Boston, MA (2003) 47. Sawitzki, G: “Computational statistics”, Chapman & Hall, Boca Raton, FL (2009) 48. Frieden, BR: “Probability, statistical optics, and data testing”, 3rd ed, Springer, New York (2001) 49. ASTM E 1345–98: “Standard Practice for Reducing the Effect of Variability of Color Measurements by use of Multiple Measurements”, American Society for Testing and Materials, West Conshohocken, PA (2008) 50. DIN 55600: “Pruefung von Pigmenten–Bestimmung der Signifikanz von Farbabstaenden bei Koerperfarben nach der CIELAB-Formel”, Deutsches Institut fuer Normung eV, Berlin (2008)
Chapter 5
Theories of Radiative Transfer
In this chapter, we ask the question as to how closer theoretical examinations could aid the calculation of the spectral values or rather color values which one would obtain experimentally. This is necessary in order to apply them to criteria such as strength of color, covering capacity, or most importantly to numerical recipe prediction. We will describe the optical radiative transfer in layers quantitatively with two different physical approaches: simple and multiple scattering. Although both formalisms achieve nearly the same results, for practical applications multiple scattering is preferred. In particular, for multiple scattering, the formalism is quite simpler, and the measurement geometry – which forms the basis of the experimental results – can be taken into account. In the following, we consider practical methods in order to obtain the interesting spectral and color values with a procedure as simply as possible. We concentrate on the two-, three-, and multi-flux approximations of the radiative field in detail. Within these formalisms, the light at the inside and outside of a colored layer is separated into two, three, or more fluxes. In this way, the interesting parts of reflectance or transmission of the optical material can be assessed. The efficiency of each approximation can be evaluated by means of special optical cases which we illustrate with the so-called optical triangle. The origin of these models basically goes back to questions of physical chemistry, atmosphere physics, and astrophysics. They are summarized by the radiative transfer equation, first formulated by Chandrasekhar [1]. The radiative transfer equation arises out of a basic thermodynamic principle which has fundamental physical meaning and permeates the discussion of this chapter.
5.1 Fundamentals Various interactions of light with the electric charges of involved molecules can occur in optical materials. On a macroscopic level, for example, one can observe reflection, absorption, scattering. These interactions may take place alone or altogether, and they are phenomena which are described by geometric optics. In G.A. Klein, Industrial Color Physics, Springer Series in Optical Sciences 154, C Springer Science+Business Media, LLC 2010 DOI 10.1007/978-1-4419-1197-1_5,
295
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5 Theories of Radiative Transfer
fact, reflection and absorption are formulated on simple physical principles, but they are both included in the radiative transfer equation in a more generalized form. With this fundamental equation, we are able to describe various properties of transparent, translucent, or opaque materials. Moreover, with the phase function, the nature and degree of the light interaction in materials – from isotropic to anisotropic – are characterized. This powerful factor, also called scattering function, indicates the probability of a certain scattering process. Although the radiative transfer equation allows other configurations, the forthcoming explanations are restricted to plane parallel layers and axial symmetric illumination. This restriction is in effort to keep the formalism and results as simple as possible.
5.1.1 Basic Concepts and Definitions In Section 2.1.5, we use the Poynting vector to characterize the energy transferred by an electromagnetic wave. The term radiation energy is closely related to the term intensity. Intensity is a measure of the energy transported through a specific surface during a unit of time and given with dimension W/m2 . In order to express the intensity, we consider a radiation field of energy dEf in the frequency interval between f and f + df. We assume that this energy enters a unit area da and is transferred in the direction of vector s with solid angle element dΩ during the time interval dt; see Fig. 5.1. A vector n perpendicular to da is called the surface normal. The direction of s is defined distinct with the declination and azimuth angles ϑ and ϕ, respectively. These angles can vary independently over the domains 0◦ ≤ϑ ≤ 180◦ and 0◦ ≤ ϕ ≤360◦ . The energy I
n
dΩ
ϑ
da
ϕ
Fig. 5.1 Three-dimensional direction of intensity I
5.1
Fundamentals
297
transferred dEf and the corresponding intensity If are associated by the relation dEf = If · cos ϑ · df · da · d · dt.
(5.1.1)
We regard this expression as the definition of radiation intensity. In general, the intensity If of light is a function of frequency f, time t, position r, and direction s. For our considerations, however, it is sufficient to assume that the intensity is independent of frequency f and time t. Therefore, instead of If we write simply I, and it is given only as a function of position r and direction s I = I(r, s).
(5.1.2)
Consequently, the dimension of intensity is J/m2 . Due to the time and frequency independence of the intensity, the forthcoming formalisms prove greatly simplified. Such simplification readily facilitates the calculation, particularly of the spectral values of reflection, transmission, optical coefficients, or of the phase function separately for each interesting visible wavelength. On the other hand, the calculation of the mentioned variables has to be carried out separately for each wavelength of interest. An additional energy quantity is radiant flux or just flux. Mathematically speaking, the term flux is the product of radiant light intensity I(r, s) and the cosine of the angle between surface normal n and direction s of the light, as in the equation F(r, s, n) = I(r, s) · cos (n, s).
(5.1.3)
Accordingly, the flux is only the component of the intensity aligned perpendicular to the surface of the material. The flux corresponds to the energy which is transferred through a unit area and solid angle of unit steradian1 (sr) in the direction of s; therefore, the dimension of F(r, s, n) is J/(m2 sr). Even though the term directed radiation is simple to imagine (Sections 2.1.5 and 2.1.6), we now give an additional formulation, to which we will return in the following. The directed radiation of intensity I at position r with angles ϑ 0 , ϕ 0 , can be described by the expression I(r, ϑ, ϕ) = I0 (r) · δ( cos ϑ − cos ϑ0 ) · δ(ϕ − ϕ0 ).
1 For definition
of unit Steradian see footnote 1 in Section 2.1.4.
(5.1.4)
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5 Theories of Radiative Transfer
Here, δ(x – a) is the Dirac delta function, which is often used to simplify mathematical expression of functions used in physics and technology.2 The following two characteristics of the Dirac delta function are of primary importance in our context: first, for x = a the function value is infinity and zero for all other x; second, the definite integral of f(x) · δ(x – a) over x has the result f(a), provided that a lies in the integration interval and f(x) is a continuous function in the neighborhood around a. We assume a three-dimensional Cartesian coordinate system with position vector r = (x, y, z), as shown in Fig. 5.2. If we further consider a directed intensity I(z) at coordinate z and angles ϑ = 0, ϕ 0 = 0, from Equation (5.1.4) follows
I(z, ϑ, ϕ) = I(z) · δ( cos ϑ − cos ϑ0 ) · δ(ϕ − ϕ0 ).
(5.1.5)
Integration of this expression over semi-space in the ranges of 0◦ ≤ ϑ ≤ 90◦ and 0◦ ≤ ϕ ≤ 360◦ simply results in the intensity I(z). With these considerations, the intensity of diffuse radiation can be formulated in a practical way. The flux consists of all those intensities included in the angle ranges of ϑ and ϕ; therefore, the entire diffuse flux at position z results from an integration over all angle-dependent intensities I(z, ϑ, ϕ) in the semi-infinite space.
z
I(z, ϑ, ϕ)
ϑ Fig. 5.2 Three-dimensional orientation of the directed intensity I(z, ϑ, ϕ) with angles of declination ϑ and azimuth ϕ in Cartesian coordinates x, y, z
y
ϕ x
2 The Dirac delta function is not a function in usual mathematical sense; it rather belongs to the class of generalized functions known as distributions.
5.1
Fundamentals
299
5.1.2 Absorption and Scattering The first quantitative description of directed light interacting with an optical material goes back to the observations of Beer regarding dilute solutions. The description of his results was based on the theoretical work of Lambert. Assume, for simplicity, direct radiation is incident on a plane parallel optical layer. For this case, according to the theory of Lambert, within the infinitesimal distance dz between positions z and z + dz, absorption of the medium attenuates the incident intensity I0 (z) by an amount dI0 ; mathematically, this is stated by the relation dI0 = I0 (z + dz) − I0 (z) = −K · I0 (z) dz,
(5.1.6)
as shown in Fig. 5.3a. Integration of this expression results in the Beer–Lambert law of absorption I0 (z) = I0 · e−Kz .
(5.1.7)
I0 = I(z = 0) represents the incident directed intensity at z = 0 and K is the wavelength-dependent absorption coefficient of the medium. The Lambert–Beer law is an approximation which is only valid for weak absorption, for instance, in solutions with low dye concentrations. Deviations from this law, for instance, at higher concentrations and reasons for these deviations at a molecular level are out of the scope of the discussion presented here. The Lambert–Beer law is a special case of the Bouguer–Lambert law, which describes further exponential attenuation phenomena in physics, technology, or biology. In the following, we assume that a plane parallel layer contains N pigment particles per unit volume V. The particle number density is defined as n˜ = N/V. Note that in most cases, the incident radiation is not only partially absorbed
I(z + dz, ϑ, ϕ) I0(z)
I0(z + dz)
I0(z)
dz
dz z + dz
z a)
z + dz
z b)
Fig. 5.3 Change of intensity I0 (z) as a result of particle interactions between the positions z and z+dz: (a) pure absorption and (b) absorption and scattering (schematically)
300
5 Theories of Radiative Transfer
but also scattered by the colorant particles in the material. The direction of the intensity I(z + dz, ϑ, ϕ) scattered during propagation from position z to position z+dz is given as a function of angles ϑ and ϕ; see Fig. 5.3b. Now, the change of intensity dI0 due to absorption and scattering within the distance dz is given by dI0 = −(K + S) · I0 (z) · dz.
(5.1.8)
Compared to Equation (5.1.6), this relation now is expanded by the inclusion of the scattering coefficient S. In the case of three dimensions, Equation (5.1.8) changes to (s · grad)I(r, s) = −(K + S) · I(r, s).
(5.1.9)
In this expression, (s · grad)I(r, s) is the vector gradient, which describes the three-dimensional change of I(r, s) between positions r and r + sdr in the direction of s in the material; see Fig. 5.4. Due to Equations (5.1.6), (5.1.7), and (5.1.8), the differential equation (5.1.9) is called the generalized Lambert–Beer law; it represents a special case of the general equation of radiative transfer. Both the absorption coefficient K and the scattering coefficient S can be expressed in terms of the number density n˜ K = n˜ σK ,
(5.1.10)
S = n˜ σS ,
(5.1.11)
with the inclusion of the quantities σK and σS , called cross section per particle of absorption and scattering, respectively; their units are area per number of
sdr
r r + sdr
Fig. 5.4 Light beam at position r traveling the distance sdr in direction of s
5.1
Fundamentals
301
particles. Hence, K and S are expressed in the same units, namely a reciprocal length. The intensity of light I(ϑ, ϕ) scattered in the direction with angles ϑ and ϕ is the product of the incident intensity I0 (z) at position z, the number density n˜ , and the three-dimensional change of the scattering cross section I(ϑ, ϕ) = I0 (z) · n˜ ·
dσS (ϑ, ϕ) dz. d
(5.1.12)
This expression can be interpreted as the general definition of the differential scattering cross section dσS /d. If we integrate the quotient in Equation (5.1.12) over the entire space we obtain the total scattering cross section " σS =
dσS (ϑ, ϕ) d. d
(5.1.13)
Another important quantity in our considerations is the scattering function or phase function p˜ (ϑ, ϕ, ϑ0 , ϕ0 ). In the literature [1], the phase function is introduced by the expression 1 n˜ dσS (ϑ, ϕ) · p˜ (ϑ, ϕ, ϑ0 , ϕ0 ) = · . 4π S d
(5.1.14)
By integrating this expression over the entire three-dimensional space and using Equations (5.1.11), (5.1.12), and (5.1.13), the result is unity: 1 4π
" p˜ (ϑ, ϕ, ϑ0 , ϕ0 ) d = 1.
(5.1.15)
This result shows a first important property of the phase function: the value of the quotient p˜ (ϑ, ϕ, ϑ0 , ϕ0 )/4π corresponds to the probability that light of direction ϑ 0 , ϕ 0 is scattered into the direction of ϑ, ϕ. Further features of the phase function are described in Sections 5.1.5 and 5.1.6. By consideration of Equations (5.1.12), (5.1.13), and (5.1.14), the scattered intensity is given by I(ϑ, ϕ) = I0 (z)
S p˜ (ϑ, ϕ, ϑ0 , ϕ0 ) dz. 4π
(5.1.16)
If we replace ϑ 0 and ϕ 0 by ϑ and ϕ and use Equation (5.1.5), the relation I(ϑ, ϕ) =
S dz 4π
"
I(z, ϑ, ϕ ) p˜ (ϑ, ϕ, ϑ, ϕ ) d
(5.1.17)
follows. The scattered intensity I(ϑ, ϕ) is, therefore, proportional to sum over all intensities of direction ϑ , ϕ at position z multiplied by the accompanying phase
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5 Theories of Radiative Transfer
function. Finally, by integrating this equation in respect of z, we obtain the intensity J(r, s) scattered into direction s at position r; see Fig. 5.4. Consequently, the expression for the so-called source function follows: " S (5.1.18) I(r, s ) p˜ (s, s ) ds . J(r, s) = 4π The source function describes the intensity at position r, which is scattered from direction s into direction s. Both the source function and the Lambert– Beer law are included in the radiative transfer equation. Before discussion of this fundamental equation, it is useful to deal with scattering processes in more detail.
5.1.3 Single and Multiple Scattering Scattering processes can have a variety of origins; phenomenologically they can be caused, for example, by the morphology of the interacting particles, their geometry, packing, or arrangement of electrical charges. Scattering of light can be described quantitatively only if the mean particle size r and the wavelength λ of the incident light are of the same order of magnitude. In contrast to Raman or Brillouin scattering, the incident and scattered radiation normally have identical wavelengths for absorption and effect pigments that we are interested in here, as well as for binders or color additives. The intensity of the scattered light is not necessarily isotropic; it can be anisotropic with angle dependence. Phenomenologically, we can distinguish three concepts of scattering interactions: single scattering, multiple scattering, and dependent scattering. In single scattering, the intensity I(ϑ, ϕ) scattered with declination angle ϑ and azimuth angle ϕ is directly proportional to the product of the number density n˜ and the layer thickness d of the material I(ϑ, ϕ) ∝ n˜ · d.
(5.1.19)
Single scattering takes place at each particle separately and independently of the particle’s neighborhood. A strict theory of single scattering for molecules with r λ. His theory was later extended to particles of other geometrical shapes. The ideas of Mie are described in detail in the literature [4, 5]. According to this theory an incident electromagnetic plane wave excites electric charge vibrations in a particle. The resulting amplitudes and phases are given by the solutions of the Maxwell equations of electrodynamics [6]. In this context, the particle charges
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303
2
3 1
0
Fig. 5.5 Calculated scattering functions for different particle radii: 0: isotropic scattering, particle radius r = 0 nm; 1: 10 nm; 2: 200 nm, 3: 400 nm; refractive index binder n = 1.50, refractive index pigment np = 1.74, wavelength 660 nm
behave as electrical multipoles. With increasing particle diameter, the amount of scattered radiation increases in the forward direction and decreases in the backward direction. In Fig. 5.5, the normalized scattering functions of four different particle radius are projected in a plane, for constant azimuth angle ϕ. The circle in the figure represents therefore a sphere in reality; this amounts to equal levels of isotropic scattering in all spatial directions arising from an infinite small dielectric particle at the center point of the sphere. The dumbbell-shaped diagram 1 shows equal amounts in forward and backward directions, in this case, produced by a dielectric sphere of radius 10 nm. The scattering functions 2 and 3, however, characterize purely forward scattering and are generated by particles with radii 200 and 400 nm, respectively. Forward scattering is in general dominant for particles with radius greater than about 100 nm. The scattering diagram 3 of Fig. 5.5 with dominant forward scattering is enlarged in Fig. 5.6. The angle of declination ϑ varies with respect to the direction of illumination and the azimuth angle ϕ varies perpendicular to the surface. The displayed scattering field with axial symmetry reminds one of the longitudinal cross section of an airship: the fuselage represents the predominant part of forward scattering. Moreover, the scattering field can be approximated by empirical functions. The scattering diagram in Fig. 5.6 is approximated with sufficient accuracy by the Henyey–Greenstein function (Section 5.1.6). Technically, the Mie theory of single scattering is only valid if the distance between particles is at least three times larger than their diameters.
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5 Theories of Radiative Transfer
ϑ
I (ϑ, ϕ)
ϕ Illumination direction
Fig. 5.6 Scattering diagram of a dielectric sphere with predominant forward scattering I(ϑ, ϕ); the angle of scattering ϑ varies parallel to the surface and the angle of azimuth ϕ perpendicular
Unfortunately, this requirement is not fulfilled for the most practical pigment particles fixed in a binder. Nevertheless, the results of this formalism based on electrodynamics are by no means of secondary significance in color physics. For a colored pigment, the reflection spectrum can be calculated approximately if the refractive index, concentration, and distribution of the dielectric particles are known [7, 8]. But this procedure is not pragmatic for practical questions because the calculations are too time-consuming, and, furthermore, the theoretical and experimental results are not identical. This disagreement may be caused by the fact that the geometry of the particles cannot be determined with sufficient accuracy necessary for a reliable model. In comparison to the single scattering of Mie, multiple scattering – the second method describing the scattering processes – has proven to be exceptionally effective for industrial applications. In nearly all pigmented systems single scattering changes into multiple scattering with increasing number density of the particles. Due to the closer particle packing, light is scattered not only once but also several times, provided that it is not absorbed or leaves the medium. According to the scattering of different particles with potentially different orientations, the scattered radiation is not always strictly directed, but rather diffuse and mostly anisotropic. The intensity of the scattered radiation I(ϑ, ϕ) is now a function of the product of particle density n˜ and thickness d of the layer I(ϑ, ϕ) = f (˜n · d).
(5.1.20)
To complete the picture, it is useful to briefly mention dependent scattering. Dependent scattering arises only if the packing density of the particles is so high that their mutual distance is comparable to the incident wavelength (e.g., in high solid paints); here the amount of scattered light is a function of particle density n˜ and layer thickness d, both variables are independent of each other I(ϑ, ϕ) = f (˜n, d).
(5.1.21)
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305
In the case of dependent scattering, the particles no longer scatter independently. This sort of situation means that scattering occurs from about units of particles and therefore requires a more detailed treatment which is beyond the scope of this book. First ideas about multiple scattering were formulated by Schuster [9] and Schwarzschild [10]. Both authors consider an absorptive and scattering medium and divide the internal radiation field into two anti-parallel and diffuse fluxes with intensities denoted as I+ (z) and I– (z); see Fig. 5.7. In the concept of Schuster, a system of two empirical differential equations shows the change of these intensities with z coordinate, +
dI+ = −(2 K + S)I+ + SI− , dz
(5.1.22a)
−
dI− = +SI+ − (2 K + S)I− , dz
(5.1.22b)
where K and S are the coefficients of absorption and scattering of the medium. The subdivision into two fluxes of opposite directions is carried out following the kinetic theory of gases. In this theory of Joule, to simplify matters, the statistical fluctuations of the particles are combined into three directions of movement, which are mutually anti-parallel and perpendicular; in this way, Joule reduced some gas properties such as pressure, temperature, or internal energy to well-known mechanical quantities like momentum or kinetic energy. z=0
I–(z) K, S z
I+(z) z=d
Fig. 5.7 Diffuse intensities I+ (z) and I– (z) within an absorptive and scattering medium
In this context, Kubelka and Munk [11, 12] proceed in a simple and empirical manner. Their approach differs from that of Schuster and Schwarzschild only in the weighting factor of the absorption coefficient, cf. Equations (5.1.22a), (5.1.22b), (5.3.1a), and (5.3.1b). In any case, it remains a fact that the results of this formalism are mathematically quite simple and not surprisingly of only limited applicability. Nevertheless, use of this theory is applied widely in the color industry. The experience of decades with these approximations shows that the real behavior of absorption and scattering in colors is incompletely represented by the empirical assumptions of Kubelka and Munk. Consequently their ideas have been supplemented and modified. Some of those theories, which certainly
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5 Theories of Radiative Transfer
have no further importance for applications in color industry, are given in the literature [13–15]. In the following, we are primarily interested in the radiative transfer equation and the related approximations of the radiant flux.
5.1.4 Radiative Transfer Equation Based on modern understanding, the concept of multiple scattering offers the only real possibility in industrial applications for adequately describing optical interactions inside absorptive and scattering materials. An appropriate basis is offered by the radiative transfer equation (RTE), upon which all known phenomenological theories about light interactions are founded [1]. The RTE results directly from conservation of radiative energy in an isolated system. From another point of view, it can also be derived from the fundamental Boltzmann equation of statistical thermodynamics, which describes with time dependence the collisions of fluctuating particles in three dimensions [16]. If the particles are interpreted as photons then the time-independent Boltzmann equation reduces to the RTE [17]. In order to formulate the RTE, imagine a light ray incident in threedimensional direction s in a medium containing discrete particles such as pigments; see the illustration in Fig. 5.4 (Section 5.1.2). The ray is directed from position r to the infinitesimally distant position r + sdr. Suppose that the path sdr is much greater than the mean particle distance allowing for the assumption that the optical medium is homogeneous and isotropic. Anisotropic optical materials are treated in Section 5.1.6. Fluorescent or phosphorescent colorants are excluded from the following considerations, although it is possible to take them into account. Along the path from r to r + sdr, the beam undergoes repeated intensity alterations due to interactions with particles. Following the considerations in Section 5.1.2, we assume that all of these intensity changes have two contributions. First, the intensity I(r, s) decreases due to absorption and scattering caused by interactions with the particles along the distance sdr. The reduction of intensity can be described with the differential equation (5.1.9) – the generalized Lambert– Beer law. Second, other light incident on the direction s with intensity I(r, s ) is additionally scattered into the direction s. This causes an increase in I(r, s). We recognize that the net radiation transferred into position r + sdr corresponds to the source function J(r, s) in Equation (5.1.18). The entire three-dimensional change of intensity is, therefore, the generalized Lambert–Beer law combined with the source function, S (s · grad)I(r, s) = −(K + S)I(r, s) + 4π
"
I(r, s )˜p(s, s )ds .
(5.1.23)
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Fundamentals
307
This expression is called the general radiative transfer equation (GRTE). Other transport phenomena, such as those in hydrodynamics, thermodynamics, or electrodynamics, lead to balance equations of similar structure: the entire flux is a result of the sink (absorption component) and the source (scattered contribution). The solution I(r, s) of the GRTE characterizes the optical properties of the medium considered. Even with the modified source function J(r, s), which is also called source term or scatter term, various optical materials can be characterized. In the case of pure absorption, the GRTE (5.1.23) becomes the multidimensional Lambert– Beer law (5.1.9). Due to the interaction between the pair of terms in Equation (5.1.23), further special optical cases can be characterized – those such as opaque systems or purely scattering materials. All of these systems may behave as isotropic as well as anisotropic media; this behavior is accordingly represented by the phase function p˜ (s, s ), which is contained in the integrand of the source term. The great importance of this function for various kinds of colorants is elucidated in the two sections that follow. The quantity ds = sin ϑ · dϑ · dϕ
(5.1.24)
in the GRTE (5.1.23) is the solid angle element for the direction of s , given by the angles ϑ and ϕ ; see Fig. 5.8. Integration of expression (5.1.24) over the entire space in the angular intervals 0 ≤ ϑ ≤ π and 0 ≤ ϕ ≤ 2π gives the scale factor 4π in the source function (5.1.18) as well as in the phase function (5.1.14). The three-dimensional position r and the directions s and s are not subject to restrictions. It is, however, useful to adapt these variables in order to realize I(z, ϑ⬘, ϕ⬘)
z
dΩs⬘
ϑ⬘
ϕ⬘
Fig. 5.8 Illustration of the solid angle element ds
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5 Theories of Radiative Transfer
practical applications in color physics, among other things. In the next section, we transform the GRTE to describe the light interactions in a plane parallel layer.
5.1.5 Radiative Transfer in Plane Parallel Layers The primary concern in most situations in industrial color physics is the optical properties of colored layers. In this context, we now intend to cast the GRTE (5.1.23) in a suitable form so that it is directly applicable to coatings. Let us assume a plane parallel layer, extended to infinity in the x, y plane and of finite thickness d in z-direction. In order to simplify the equations, we employ modified polar coordinates instead of the Cartesian coordinates x, y, z, as shown in Fig. 5.2. Thus, the intensity I(r, s) is written as I(z,ϑ,ϕ), a function of the coordinate z, the declination angle ϑ with regard to the z-axis, and azimuth angle ϕ in the plane perpendicular to the z-axis. Furthermore, we replace the path differential dr by dr =
1 dz cos ϑ
(5.1.25)
based on the conditions shown in Fig. 5.9 and introduce the abbreviation μ = cos ϑ.
(5.1.26)
The solid angle element ds in Equation (5.1.24) can now be written as ds = −dμ dϕ . We additionally define the optical path length as τ = (K + S)z ,
dr
(5.1.27)
ϑ dz
z
Fig. 5.9 Relation between the differentials dr and dz in a plane parallel layer
5.1
Fundamentals
309
which is a measure of the attenuation of the incident radiation due to absorption and scattering along the path from z = 0 to z = d. Finally, we introduce the albedo which is defined by the quotient ω0 =
S . K+S
(5.1.28)
In contrast to directed reflection, the albedo indicates the relative amount of attenuation due solely to scattering at the surface or in the volume of a material. Consequently, the albedo is a measure of the scattering of the medium. For example, the surface of the Earth has a mean value of ω0 ≈ 0.3, clouds between 0.7 and 0.9. The albedo has some important properties to keep in mind. The domain is restricted to the interval 0 ≤ ω0 ≤ 1, and both domain boundaries represent special optical cases. The case ω0 = 0 characterizes pure absorption; the expressions (5.1.30), (5.1.31), (5.1.35), and (5.1.37) below turn into the generalized Lambert–Beer law with S = 0. The special condition ω0 = 1, on the other hand, is called the conservative case, which is a synonym for pure scattering. To restate, the boundary values of the albedo can be expressed by ω0 =
0: 1:
pure absorption, Lambert−Beer law . pure scattering, conservative case
(5.1.29)
The term conservative case is derived from mechanical systems: if such a system fulfills the principle of conservation of energy, it is called a conservative system. Pure scattering means no absorption and the energy equation (2.1.14) takes the simple form R + T = 1. Based on this analogy, an optical system without absorption is called a conservative case. Finally the variables μ and ϕ in the GRTE (5.1.23) are restricted to the intervals −1 ≤ μ ≤ 1 and 0 ≤ ϕ ≤ 2π, which consequently determine the corresponding integration limits of μ and ϕ . If we take into account Equations (5.1.25), (5.1.26), (5.1.27), and (5.1.28) as well as the integration limits of μ and ϕ , the RTE (5.1.23) becomes the radiative transfer equation for plane parallel layers dI(τ ,μ,ϕ) ω0 μ = −I(τ ,μ,ϕ) + dτ 4π
"+1 "2π dμ p˜ (μ,ϕ; μ ,ϕ ) · I(τ ,μ ,ϕ ) dϕ . −1
0
(5.1.30) This formulation models all scattering and absorbing cases relevant to the physics and metrology. The optical path length τ is directly proportional to the absorption and scattering. The albedo ω0 characterizes the relative scattering and the phase function p˜ (μ,ϕ; μ ,ϕ ) indicates the degree of anisotropy together with the probability of scattering from direction μ , ϕ into direction of μ, ϕ.
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5 Theories of Radiative Transfer
With the solution I(τ ,μ,ϕ) of Equation (5.1.30), both the reflection and the transmission of the layer can be calculated, provided that the so-called boundary conditions are known. As mentioned before, each required spectral value must be calculated separately for each wavelength of interest. On the other hand, the geometries for measurements are fully specified by the angles of declination and azimuth μ, μ and ϕ, ϕ , respectively; the quantities μ and ϕ correspond to the illumination and μ and ϕ to the measurement conditions. The calculated and correspondingly measured reflection and transmission can, therefore, be compared with one another if the constants for absorption and scattering as well as the phase function and the layer thickness are known. A variety of reasons allow for a simplification of Equation (5.1.30); the formalism and the computing time are reduced. First, we assume that the incoming light at z = 0 is independent of ϕ and ϕ, i.e., axial symmetry (see Fig. 5.10). Therefore, also a rotationally symmetric measurement has to be performed around the z-axis (e.g., 0:45c measuring geometry). In this case, the intensity I = I(τ , μ) is only a function of the optical path length τ and the direction given by μ. Furthermore, the phase function p(μ,μ ) is also independent of ϕ and ϕ; it represents now the amount of incoming light in direction μ which is scattered into direction μ. Integration of Equation (5.1.30) with regard to μ results in ω0 dI(τ ,μ) = −I(τ ,μ) + μ dτ 2
"+1 p(μ,μ ) I(τ ,μ )dμ . −1
z
I(z, ϑ, ϕ)
ϑ ϕ
ϑ⬘ x
y
Fig. 5.10 Coordinates for axial symmetry in a plane parallel layer [18]
(5.1.31)
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Fundamentals
311
This special RTE is specific for plane parallel layers under axial symmetric illumination. It contains only the variables τ , ω0 , μ , and μ, which are proportional to the coordinate z and the angles ϑ, ϑ, respectively. All further explanations and calculations in the text will be based on these assumptions and therefore utilize Equation (5.1.31). Due to its mathematical structure, expressions such as these are called integro-differential equations. The phase function p(μ,μ ) in the source term of Equation (5.1.31) results from integration of the phase function p˜ (μ,ϕ; μ ,ϕ ) over ϕ . Therefore, we write this, from Equation (5.1.15), as the following p(μ,μ )
"2π
1 = 2π
p˜ (μ,ϕ; μ ,ϕ )dϕ ,
(5.1.32)
0
and require the simple normalization condition 1 2
"+1 p(μ,μ )dμ = 1.
(5.1.33)
−1
Based on this result the phase function indicates, as mentioned previously, the probability for light from direction μ is scattered in direction μ. Because Legendre polynomials Pl (μ) form a basis of orthogonal functions, it is possible to write a function such as p(μ,μ ) as a superposition of this basis set as in the equation: p(μ,μ ) =
∞
dl Pl (μ)Pl (μ ).
(5.1.34)
l=0
The quantity dl is the coefficient of the lth Legendre polynomial of the given expansion. Condition (5.1.33) implies d0 = 1. The series expansion of functions is extensively described in the literature; see, for instance, [19]. If we combine Equation (5.1.34) with (5.1.31), we obtain the following: " ∞ ω0 dI(τ ,μ) = −I(τ ,μ) + dl Pl (μ) Pl (μ )I(τ ,μ )dμ . μ dτ 2 +1
l=0
(5.1.35)
−1
In order to give an approximate solution I(τ ,μ) among other things, at least some of the first Legendre coefficients have to be known. For clarity, we summarize here the requirements for the validity of both the ERTs (5.1.31) and (5.1.35):
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5 Theories of Radiative Transfer
– plane parallel layer, extending to infinity in the x, y plane, – the optical path τ depends only on the absorption and scattering coefficients K and S, and coordinate z, – the illumination is axis symmetrical with respect to the z-axis and independent of azimuth angles ϕ and ϕ, – the light is unpolarized before and after interaction, although this can be included in the calculations. In the case of isotropic scattering, all scattering directions are equally likely. From Equation (5.1.33), the phase function becomes p(μ,μ ) = 1.
(5.1.36)
This result represents a sphere with radius r = 1; see Fig. 5.5 in Section 5.1.3. Therefore, from expression (5.1.31) follows the simplest RTE ω0 dI(τ ,μ) = −I(τ ,μ) + μ dτ 2
"+1 I(τ ,μ )dμ .
(5.1.37)
−1
Beyond the requirements mentioned above, Equation (5.1.37) is simultaneously valid for absorptive and isotropic scattering layers. In the following, the twoand three-flux approximations are based on expression (5.1.37) and are mainly applied to samples containing absorptive colorants. The term two- or multi-flux approximation is based on the procedure chosen to determine the intensity I(τ ,μ) in the RTE. Among the various possible solution methods, we chose in the following the procedure to approximate the integral of the source function (5.1.18) by a sum of n ≥ 2 terms (discrete ordinate method). With this approach, the continuous radiation field inside and outside of the layer is divided into n discrete angle ranges, the so-called radiation channels or light cones. Section 5.5 deals with the general case of the multi-flux approximation with up to n = 256 fluxes, respectively, light cones. The accuracy of the approximation increases with finer subdivision of these channels; see also Fig. 5.29. Finally, it is necessary to make a remark concerning Equation (5.1.30) with respect to calculations and measurements of layers containing effect pigments. In these cases, the phase function has to be developed into a series of all four variables μ, μ , ϕ, ϕ ; the integral over ϕ , the source term, has to be approximated by a quadrature equation of 2n terms. The appropriate directed measurement geometry for the effect colorants defines the angle of illumination and several measurement angles. The number i = 1, 2, . . . , N of measurement angle pairs μi , ϕ i defines the number of differential-equation systems that has
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313
to be resolved with respect to I(τ , μi , μ , ϕi , ϕ ). Further work along these lines requires extensive formalism and is beyond the scope of this book.
5.1.6 Phase Function for Anisotropic Scattering The phase function p(μ,μ ) in the ERT (5.1.31) not only corresponds to the probability of light being scattered from direction μ toward direction μ but also its numerical value characterizes the type of scattering. For the simplest case with p(μ,μ ) = 0, the source term disappears; it is, therefore, equivalent to pure absorption. In contrast, the maximum p(μ,μ ) = 1 represents complete isotropic scattering, as explained in the previous section. The series expansion of the phase function can become complicated, if the Legendre coefficients dl do not converge sufficiently fast. In this case, anisotropic scattering is often characterized approximately by using different empirical phase functions [20]. In order to simulate the single scattering of Mie, the Henyey–Greenstein function [21] is used, among other things; for perpendicular illumination, i.e., corresponding to μ = −1, this function reads as
p(μ, − 1) =
1 − g2 . (1 + g2 − 2 gμ)3/2
(5.1.38)
Due to the domain of the phase function 0 ≤ p(μ, μ ) ≤ 1, the coefficient of anisotropy g is limited to values |g| ≤ 1: purely isotropic scattering corresponds to g = 0, whereas values of g > 0 represent anisotropic scattering in forward direction and g = 1 belongs to the case of “extreme anisotropy” of transparent materials. Conventional absorption pigments show frequency-dependent values of g between 0.2 and 0.8 [22]. The expansion coefficients dl of the phase function in Equation (5.1.35) can be calculated in this case by the simple formula dl = (2 l + 1)gl , l = 0, 1, 2, ...
(5.1.39)
[20]. In this case, the smaller the value of g, the faster the values of dl converge to zero with increasing l. Just as before, it follows that the modeling of highly anisotropic materials requires a large number of coefficients. In the case of solely backward scattering with g = –1, the expansion coefficients can be calculated by the equation dl = ( − 1)l (2 l + 1), l = 0, 1, 2, ...
(5.1.40)
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5 Theories of Radiative Transfer
which produces alternating signs for dl . However, these coefficients do not represent the realistic reflection behavior of metallic or reflecting diffraction pigments appropriately. The absolute value |dl | ≤ 2 l + 1 can merely be used to estimate the size of the coefficients. Although the properties of layers containing effect colorants cannot be exactly represented by the Henyey–Greenstein function, the value of g supplies at least an idea of the extent of anisotropy in the present case. For metallic pigments, we are able to acquire an accurate phase function by another consideration. Let us assume that the directed reflection of a metallic flake can be interpreted as an extreme scattering process. This “scattering” corresponds to the effect of a microscopic mirror; see Fig. 5.11. The metallic flake reflects the incident light from direction μ = cos (ϑ/2) toward the main direction μ = −μ ; this process can be described by the Dirac delta function3 as in p(μ,μ ) = δ(μ + μ ).
(5.1.41)
However, in a real layer the metallic particles are not oriented completely parallel to the surface, but rather their alignment is statistically distributed with preference to being parallel to the surface. In that case the phase function can
ϑ 2
ϑ 2
Fig. 5.11 Schematic representation of the reflection of a metallic flake [18]
3 For some
properties of the delta function, see Section 5.1.1.
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315
be approximated by a suitable orientation-distribution function. If the reflecting metallic flakes are distributed rotationally symmetric with respect to the direction of illumination – i.e., independent of azimuth angle ϕ – then the phase function is correlated with an orientation-distribution function f(ϑ). Figure 5.12 shows the plot of a typical phase function in dependence on declination angle ϑ for a sample containing metallic pigments, among other things. The more evenly the flakes are oriented parallel to the substrate surface, the more the phase function approximates a delta function. The maximum of the phase function is decreased if metallic pigments are mixed with scattering absorption pigments. In general, the phase function of a colorant mixture is a linear combination of the phase functions of the respective individual colorants.
p (μ, μ′ = –1)
15
Metallic pigment Absorption pigment Mixture 50/50
10
5
1 0 0
20
40 ϑ/degree
60
80
Fig. 5.12 Typical phase functions of a metallic pigment, an isotropic scattering absorption pigment, and of a mixture of the two [22]
The various contributions of absorptive colorants to either the phase function p(μ, μ ), the optical path τ , or to the albedo ω0 are usually dependent on the wavelength λ. In contrast, the albedo of metallic pigments is nearly independent of λ, because the spectral absorption is practically constant over the entire visible range (cf. Fig. 2.39, Section 2.3.3). This also implies that the phase function of metallic flakes is nearly independent of the wavelength; certainly, due to the individual orientation distribution of the flakes, the phase function can be slightly different for each coloration of the same charge. For pearlescent, interference, and diffraction pigments, the situation is more complex. In these cases, the particles reflect or transmit the light in dependence
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5 Theories of Radiative Transfer
of illumination and observation angles, layer thicknesses, colored background, and other contributions. Apart from the reflection of the interference or diffraction wavelengths, the transmission of the complementary color of interference pigments must also be taken into consideration. The absorption of these kinds of colorants corresponds roughly to that of metallic pigments, in fact it decreases the albedo but does not affect the phase function.
5.2 Directional Two-Flux Approximation In this section, we begin with the version of the RTE (5.1.37) which is valid for plane parallel layers of isotropic scatterers and corresponds to the simple phase function p(μ, μ ) = 1. In order to solve this integro-differential equation for the case of two-flux approximation, we separate the continuous radiation field into two anti-parallel fluxes, this, following the principle of Joule. With this simplification, the integral of the RTE reduces to a sum of two terms, each consisting only of the intensities corresponding to these fluxes. A system of two linear equations is, therefore, obtained. This system is conducive to straightforward calculation of the desired directed intensity quantities. In view of the boundary conditions, the solutions result in useful expressions for the reflection and transmission of a colored layer. In order to obtain these values for the entire visible spectrum, the calculations must be repeated for each wavelength in the desired range given by the measuring conditions chosen for the inward and outward fluxes of directed light. The calculated values of spectral reflection or transmission belong only to the chosen directional two-flux approximation; they are not transferable to any other approximation. We verify the correctness of this directional two-flux approximation with three special cases: a transparent layer, an opaque layer, and a purely scattering layer which corresponds to the conservative case. These special cases can be illustrated quite simply using the so-called optical triangle. The methods developed under the two-flux approximation are further applicable to other approaches of radiative transfer. The spectral quantities obtained from the two-flux approximation are used in three different areas of application (see Chapter 6). The first application is to compare them with the correspondingly measured spectral quantities. The second is to calculate the optical constants of a layer material, for example, the absorption and scattering coefficients or the optical path and albedo. The third is color recipe prediction, that is, to determine the type and concentrations of colorants for a given color of unknown colorant composition. This application is quite important and commonly used in the color industry.
5.2
Directional Two-Flux Approximation
317
5.2.1 Reflection and Transmission As shown in Fig. 5.13, we express the continuous radiation field inside a plane parallel optical medium as two directed intensities written as i(τ ,μ) and j(τ ,μ). These directed intensities are oriented in positive and negative directions with regard to the given z-coordinate axis. The orientation μ is related to the angle of declination ϑ by definition (5.1.26). For the two-flux approximation, the integral of the source term in Equation (5.1.37) is replaced by the sum of the intensities i(τ ,μ) and j(τ ,μ). Most admittedly, this is a quite rough approximation; we do, however, obtain a system of two linear differential equations with constant coefficients μ
di(τ ,μ) ω0 = −i(τ ,μ) + [i(τ ,μ) + j(τ ,μ)] , dτ 2
(5.2.1a)
z ≤ 0: − μ
dj(τ ,μ) ω0 = −j(τ ,μ) + [i(τ ,μ) + j(τ ,μ)]. dτ 2
(5.2.1b)
z ≥ 0:
z=0 j (τ, μ)
ω0, τ z
i (τ, μ) z=d
Fig. 5.13 Illustration of the two-flux approximation with directed intensities i(τ ,μ) and j(τ ,μ) inside a plane parallel layer
Such a system lends itself to solution much easier than the earlier form involving an integral expression. The determination of i(τ ,μ) and j(τ ,μ) leads to the characteristic equation μ2 k2 + ω0 − 1 = 0
(5.2.2)
with roots k1/2 = ±k = ±
1 1 − ω0 . μ
(5.2.3)
The particular solutions of i(τ ,μ) and j(τ ,μ) contain integration constants which are determined from the boundary conditions i(τ = 0, μ) = 1,
(5.2.4)
j(τ = τd , μ) = 0,
(5.2.5)
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5 Theories of Radiative Transfer
with the optical path τd = (K + S)d
(5.2.6)
from Equation (5.1.27) using thickness z = d. The incident flux is normalized as given in Equation (5.2.4). Part of this incident flux is reflected by the medium, part is absorbed in the layer, and the remainder is transmitted. Now, we define the reflection R as the ratio of the reflected to the incident flux; analogously, the transmission T is defined as the ratio of the transmitted to the incident flux, cf. Equations (2.1.14a), (2.1.14b), and (2.1.14c). In every approximation, reflection and transmission have to be put in concrete terms. In the present case the influx and efflux are both directed by an angle μ. Accordingly, the directed reflection Rμμ is the proportion of intensity returning at the upper surface of the optical layer at z = 0 and is written as Rμμ = j(z = 0, μ).
(5.2.7)
The directed transmission Tμμ at position z = d is likewise given by Tμμ = i(z = d, μ).
(5.2.8)
With the solutions for i(τ ,μ) and j(τ ,μ) from Equations (5.2.1a) and (5.2.1b), we obtain expressions for these directed quantities, ω0 , 2 − ω0 + 2μk coth (kτ )
(5.2.9)
2μk . (2 − ω0 ) sinh (kτ ) + 2μk cosh (kτ )
(5.2.10)
Rμμ = Tμμ =
Both formulas have, for simplicity, τ written in place of τ d , cf. Equation (5.2.6); the quantity k corresponds to the characteristic root in Equation (5.2.3) with positive sign. It is to keep in mind that the above expressions are only valid in the relevant two-flux approximation. From the above expressions (5.2.9) and (5.2.10), the simplicity of the result becomes apparent; a mere four parameters, two geometrical and two optical, are necessary to calculate the reflection or transmission of the layer under this approximation. The required parameters, specifically, are the layer thickness d, angle of illumination μ, albedo ω0 , and optical path τ . Moreover, the optical and coloristical properties of the layer are represented only by the values ω0 and τ . These results are of fundamental importance. They follow from the concept of multiple scattering and are valid for all subsequent approximations based on multiple scattering. In the case that all four of the above required parameters are known for the calculation, the obtained theoretical quantities Rth = Rμμ and T th = Tμμ
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319
can be directly compared with those experimentally obtained, Rex , Tex . On the other hand, given the values of the geometrical parameters μ, d, along with measured values of reflection and transmission, Rex , Tex , the optical constants ω0 and τ of the layer can be determined by Equations (5.2.9) and (5.2.10). In order to simplify the evaluation, the illumination of the layer can be carried out perpendicular to the surface, which corresponds to the condition μ = 1. It is possible to use the absorption and scattering coefficients K and S for calculation rather than ω0 and τ . These parameters follow from Equations (5.1.27) and (5.1.28) with z = d: K = (1 − ω0 )τ/d,
(5.2.11)
S = ω0 τ/d .
(5.2.12)
In any case, the above approach is applicable for all approximations within the multiple scattering concept. Equations (5.2.9) and (5.2.10) are approximations for many sorts of optical layers, chromatic or achromatic, provided that only directional rays are considered. In particular, they are considered for three special optical cases in the next section.
5.2.2 Optical Special Cases An unverifiable model is epistemologically worthless. Moreover, the results of the model must be consistent with actual experience and common sense as well as not contradicting other accepted theories. A lack of these consistencies would require the ideas to be modified or rejected. In this section, we do a reality check for the two-flux approximation in three special optical cases: an opaque, a transparent layer, and a purely scattering layer, corresponding to the conservative case. The reasons for these examples are made clear in the next section. These three special cases are applied to further approximations elsewhere in the book. An opaque material is by definition neither transparent nor translucent. It is characterized by zero transmission corresponding to Tμμ = 0. This means that an opaque material completely hides the substrate, which is mathematically equivalent to a layer of infinite thickness corresponding to d → ∞, and therefore likewise τ → ∞. Considering the exponential behavior of the hyperbolic functions in the denominator of Equation (5.2.10), the transmission vanishes: lim Tμμ = 0.
τ →∞
(5.2.13)
The same limit τ → ∞ in Equation (5.2.9) leads to the formula for the reflection of an opaque layer
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5 Theories of Radiative Transfer
Rμμ =
ω0 . √ 2 − ω0 + 2 1 − ω0
(5.2.14)
This is a remarkable result for a variety of reasons: – the reflection of an opaque medium is only a function of albedo ω0 and independent of τ , – Rμμ does not depend on the angle of illumination μ, – it is identical to the corresponding formula for two diffuse fluxes (see Appendix A.3.2). As already shown, the range of albedo values is limited to 0 ≤ ω0 ≤ 1; see Equation (5.1.28). Expectedly, the reflection Rμμ is restricted to the same interval. This follows already from the general definition of the reflection in the last section. The second special case of interest is that of a transparent medium. For a transparent layer, part of the incident light is absorbed and the remainder is transmitted; that is, there is no reflection or scattering. The scattering coefficient S, together with the albedo ω0 , vanishes; in consequence, with Equation (5.2.9), the directed reflection Rμμ also vanishes: Rμμ = 0.
(5.2.15)
The absence of scattering reduces the characteristic root in Equation (5.2.3) to k = 1/μ; from Equation (5.2.10), the transmission then follows Tμμ = e−τ/μ .
(5.2.16)
In this case, the optical path takes the simple form τ = Kd. Expression (5.2.16) is, in fact, the general one-dimensional Lambert–Beer law for absent scattering written in Equation (5.1.7) with μ = 1 and Tμμ = I0 (z = d)/I0 . As a side note, the Lambert–Beer law also follows immediately by integration of Equation (5.2.1a) or one of the RTEs (5.1.30), (5.1.31), (5.1.35), and (5.1.37) when using ω0 = 0. The third special case to deal with is the conservative case. This is an absorption-free case and is specified by ω0 = 1. From the principle of the conservation of energy (2.1.14), in the absence of absorption, the relation Rμμ + Tμμ = 1 must hold. In order to verify this, we insert the expression for the characteristic root (5.2.3) into Equations (5.2.9) and (5.2.10) and determine the limits with ω0 → 1. We, thereby, obtain Rμμ =
τ , 2μ + τ
(5.2.17)
Tμμ =
2μ . 2μ + τ
(5.2.18)
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321
It is clear, therefore, that in the two-flux approximation, the conservation of energy requirement is fulfilled. The bottom line here is that the results of the two-flux approximation above are consistent with experience and common sense. In the next section, these extreme cases are illustrated in particular with the help of the optical triangle.
5.2.3 Optical Triangle By definition in Sections 2.1.5 and 5.2.1, reflection R and transmission T are relative quantities; their values, therefore, are always in the range [0, 1]. Given this, it is possible to characterize the optical system with a representation of these values in Cartesian coordinates. In this case, T is interpreted as a function of R in the usual sense of an x, y coordinate system. The result of this is the optical triangle shown in Fig. 5.14. The legs and corner points of the triangle represent the special cases detailed in the previous section. To jump straight to the most important result here, each point within the area of the triangle represents the characteristics of an optical system and the area of the triangle contains the whole of possible combinations of R and T for all optical systems of linear materials. To elucidate these concepts further, we consider now the optical meanings of various cases. An opaque purely absorptive material without scattering is characterized by a zero albedo (ω0 = 0) and an infinite optical path length (τ →∞). The values Tμμ = 0 and Rμμ = 0 for this case, therefore, follow from Equations (5.2.13) and (5.2.14). These conditions correspond to an ideal black medium represented by the triangle corner labeled B in Fig. 5.14. Now, the case of absent absorption is called the conservative case. This case is represented by the line defined by Tμμ = 1 – Rμμ . This line extends from corner A for Rμμ = 0 to corner C for Rμμ = 1. Corner C is the special case of pure scattering, which, in addition to unity albedo, is characterized by an infinite optical path length (τ →∞). This corner, therefore, represents the case with Tμμ = 0 and Rμμ = 1, meaning all incident light is scattered back, synonymous with an ideal white material. Corner A represents ideal transparency characterized by a zero albedo and optical path length; this means zero reflection and unity transmission. It is a hypothetical material without any absorption or scattering (like vacuum). It is clear that the special cases just discussed should not depend on any particular approximation used to calculate transmission and reflection. We, therefore, leave out the subscripts of R and T in the following. Table 5.1 gives a survey of various values for the corner points. The legs of the optical triangle, not including the corner points, describe the following optical states:
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5 Theories of Radiative Transfer
Transparent materials
Internal transmission T
A (0, 1)
C
on
se
rv at
ive
ca
se
Opaque materials
B (0, 0)
C (1, 0)
Internal reflection R
Fig. 5.14 The area of the optical triangle ABC is the geometric locus of all reflection– transmission combinations characterizing optical linear systems
Table 5.1 Three optical extreme cases, represented in the corner points A, B, C of the optical triangle Corner optical Optical special cases triangle
Internal reflection and transmission
Optical constants
R
T
ω0
τ
K
S
Ideal transparency Pure absorption Pure scattering
0 0 1
1 0 0
0 0 1
0 →∞ →∞
0 →∞ 0
0 0 →∞
A B C
– AB: transparent materials; only absorption, no scattering; ω0 = 0, the optical path changes from τ = 0 at A toward infinity at B; – AC: conservative case; only scattering, no absorption, ω0 = 1; τ = 0 at A, τ → ∞ at C; – BC: opaque materials; absorption and scattering but no transparency, τ → ∞; the albedo changes nonlinearly between ω0 = 0 at B and ω0 = 1 at C. The optical triangle is somewhat analogous to the operating triangle of a machine or circuit where its operating state can be read from the coordinates
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323
A, τ = 0 1.0
τ = 0.3
Internal transmission T
0.8 1.0 0.6
3.0
0.4
0.2
10 102 C, τ → ∞
B
0
ω0 = 0 0
0.5 0.2
0.8
ω0 = 1.0
0.95
0.4 0.6 Internal reflection R
0.8
1.0
R
Fig. 5.15 Optical triangle with families of curves calculated from the directional two-flux approximation; indicated are curves of constant optical path τ and constant albedo ω0 ; μ = 1, n = 1.5
of the working point. In a figurative sense, the “operating points of an optical system”, meaning the spectral (T, R) points, represent not only the values of reflection and transmission but also the accompanying values of albedo and optical path length. As previously mentioned, the coordinates and significance of the corner points are independent of any approximation being used. However, the shapes of any curves plotted with parameters of ω0 and τ within the boundaries of the optical triangle do, in fact, depend on the approximation. In Fig. 5.15, a family of curves for constant albedo and a family for constant optical path are plotted. These curves are calculated using Equations (5.2.9) and (5.2.10) of the twoflux approximation with value μ = 1 (representing perpendicular influx) and a refractive index of n = 1.5. Starting at point A, the triangle is ordered neatly by a set of curves with constant albedo ω0 ; they are intersected by curves of constant optical path τ . Note that at A, the albedo ω0 is mathematically not continuous, but this is unimportant for applications. As a result of the dependencies in Equations (5.2.9) and (5.2.10), the curve shapes in either family depend on ω0 and τ in a nonlinear fashion. It is remarkable that the recipe prediction (based on calculated values of reflection and transmission) gives quite acceptable results at least for absorption colorants.
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It is worthwhile, however, to further improve the methods of recipe calculation, especially by taking into consideration the nonlinear spectral or colorimetric properties of colorants in dependence on concentration.
5.2.4 Determination of Optical Coefficients If accurate values of Rμμ and Tμμ are available from measurements and the quantities μ and d are also known from the measurement geometry and layer thickness, then it is possible to calculate the optical constants ω0 and τ , respectively. To do this, one may use the theory outlines in the preceding sections. It is important to remember that the calculated optical constants are specifically for the measuring wavelength λi and are normally different at other wavelengths. The knowledge of both coefficients, ω0 and τ , of a colored layer facilitates some important applications in colorant industry, such as: – determination of color strength, depth of color, or hiding power of absorption colorants; – comparative characterization of colored pigments; – numerical recipe prediction. With the albedo and optical path given, the absorption and scattering coefficients can also be calculated by using Equations (5.2.11) and (5.2.12). For the two-flux approximation, we now determine the optical constants ω0 and τ for the three special cases treated in Section 5.2.2, and for the general case of a translucent layer. In principle, for an opaque layer, only the albedo can be determined, for which one obtains ω0 =
4Rμμ (1 + Rμμ )2
(5.2.19)
using Equation (5.2.14). In the case of an opaque material, ω0 is only dependent on the measured reflection, whereas the optical path goes to infinity: τ → ∞ or equivalently d → ∞. If Equation (5.1.28) is considered, the following results: (1 − Rμμ )2 K . = S 4Rμμ
(5.2.20)
Note: It is a characteristic of an opaque medium that only the quotient of K and S can be ascertained; this is equivalent to the statement just above that only the albedo ω0 can be determined.
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Directional Two-Flux Approximation
325
According to definition, a transparent material acts as a partial absorber without any scattering. Using the value ω0 = 0 in Equation (5.2.16), the result gives the optical path length in dependence of the transmission τ = −μ ln (Tμμ ).
(5.2.21)
As a result of the fact that a transparent material has zero scattering, S = 0, expression (5.2.11) for τ reduces to τ = Kd; the absorption coefficient is therefore given by K=−
μ ln (Tμμ ). d
(5.2.22)
In the conservative case, using ω0 = 1 in Equations (5.2.15) and (5.2.16), one obtains τ = 2μ
Rμμ . Tμμ
(5.2.23)
In order to determine the optical coefficients of a translucent medium, one needs the values of reflection and transmission from two independent measurements. Often the direct measurement of transmission is quite uncertain due to the possibility of surface reflections or heterogeneities at the boundary layers. For this reason, the method of measuring the reflection over two different colored backgrounds is used quite often. In connection with Equations (4.2.13) and (4.2.14), we can write Rx = Rμμ +
2 R Tμμ bg,x
1 − Rμμ Rbg,x
,
(5.2.24)
where Rx is the measured reflection from the test layer optically contacted on top of background x and Rbg,x is the measured reflection directly from the uncovered background x. The insertion of Rμμ and Tμμ using Equations (5.2.9) and (5.2.10) into Equation (5.2.24) gives Rx =
ω0 − Rbg,x [2 − ω0 − 2μk coth (kτ )] . 2 − ω0 (1 + Rbg,x ) + 2μk coth (kτ )
(5.2.25)
Consider that reflection values for normally plain white and black backgrounds are indicated by Rbg,w , Rbg,b , respectively, and for a test layer covering these backgrounds by Rw , Rb , respectively. Four reflection measurements can determine these. By inserting the respective measured pairs into Equation (5.2.25), it is possible to eliminate the hyperbolic functions and obtain a term for the albedo
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5 Theories of Radiative Transfer
ω0 =
4D , (1 + Rbg,w Rw )(Rb − Rbg,b ) − (1 + Rbg,b Rb )(Rw − Rbg,w ) + 2D (5.2.26a)
where D = (Rbg,w Rb − Rbg,s Rw ).
(5.2.26b)
The right-hand side of Equation (5.2.26a) contains only measured parameters and, in particular, it is independent of μ and τ . Solving of expression (5.2.25) for τ results in ! ω0 (1 + Rbg,x Rx ) − (2 − ω0 )(Rbg,x + Rx ) 1 τ= arccoth . 2μk 2μk(Rx − Rbg,x ) This expression contains only known quantities, particularly since μ is known from the measuring geometry and k from Equation (5.2.3) with positive sign. The corresponding measured pairs Rbg,b , Rb and Rbg,w , Rw can be used in order to determine two values of τ . The reliability of results can be evaluated by error estimation of the measured values. If both quantities of τ differ by less than ±1%, experience shows that the mean is trustworthy. Finally it is important to once again stress that the resulting values of the optical constants depend on the approximation used. That is to say, the various approaches yield different results. Accordingly the question is legitimate, which approximation delivers the correct coefficients for a specified optical system? The question can only be answered empirically. However, experience shows that approximations of more than two fluxes lead to quite reliable results for recipe prediction of absorption and effect colorations. Nonetheless, the next section deals with the two-flux theory of Kubelka and Munk because it is widespread, but of restricted validity – a consequence of the simply structured evaluation formulas.
5.3 Theory of Kubelka and Munk The assumptions made of Kubelka and Munk [11,12] about light interactions in colored scattering materials are essentially identical with those of Schuster and Schwarzschild [9, 10]. This theory is, however, not based directly on the RTE (5.1.37) for plane parallel layers and is, therefore, not directly compatible with any of the further approximations of that equation. Kubelka and Munk work on an empirical premise of two diffuse fluxes – corresponding to a modified approximation which includes absorption and isotropic scattering. Due to the simple handling of this model, during the past few decades, some of the formulas have been implemented in algorithms for recipe prediction; generally, at the time, they were limited by the relatively low computing power for simulations.
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Theory of Kubelka and Munk
327
Simplicity, however, does not mean a completely reliable applicable description for the optical properties of real colorations. The limits of this theory become evident especially when corrections due to the different refractive indexes of a layer are necessary, which is clearly demonstrated with the aid of the optical triangle.
5.3.1 Empirical Approach Following Kubelka and Munk, we assume here that a homogenous, plane parallel layer of thickness z = d is illuminated of diffuse light at position z = 0. The layer is composed of an absorptive and isotropically scattering paint; see Fig. 5.16. The radiation field inside the layer is divided into two anti-parallel diffuse fluxes of intensities I+ (z) and I– (z). During a propagation through a distance dz, these intensities are modified by dI+ and dI– , respectively. The intensity I+ (z) is attenuated by absorption and scattering, but intensified by the scattering component of the oppositely oriented intensity I– (z). This attenuation and intensification is analogous for I– (z). The interplay between I+ (z) and I– (z) is described by Kubelka and Munk [11, 12] with the phenomenological system of two linear differential equations: z ≥ 0: +
dI+ = −(K + S)I+ + SI− , dz
(5.3.1a)
z ≤ 0: −
dI− = +SI+ − (K + S)I− . dz
(5.3.1b)
Wherein K and S denote the absorption and scattering coefficients of the paint layer. In comparison to Equations (5.1.22a) and (5.1.22b), this system only differs with regard to the weighting factor of the absorption constant.
R z=0
I– (z) K, S z
I+ (z) z=d T
Fig. 5.16 Diffuse radiation components in a plane parallel layer after Kubelka and Munk
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5 Theories of Radiative Transfer
In solving system (5.3.1a) and (5.3.1b), one first obtains the roots k of the corresponding characteristic equation k2 − (K + S)2 + S2 = 0.
(5.3.2)
The formalism is simplified introducing the abbreviations a=
K +1 S
(5.3.3)
and b = + a2 − 1.
(5.3.4)
The characteristic roots are, therefore, given by k1/2 = ±k = ±bS.
(5.3.5)
Again, the integration constants follow from the boundary conditions which are, here, given by I+ (z = 0) = 1,
(5.3.6)
I− (z = d) = 0.
(5.3.7)
Using the definition of the reflection R in the irradiated surface R = I− (z = 0)/I+ (z = 0)
(5.3.8a)
and for the transmission T in the second surface T = I+ (z = d)/I+ (z = 0),
(5.3.8b)
cf. Fig. 5.16, the result follows 1 , a + b coth (kd)
(5.3.9)
b . a sinh (kd) + b cosh (kd)
(5.3.10)
R=
T=
Both expressions contain again hyperbolic functions. Equations (5.3.9) and (5.3.10) are, in fact, quite similar to those of the directional two-flux approximation in Section 5.2.1. They allow to calculate the diffuse reflection R and diffuse transmission T, requiring only the optical constants K and S and the layer thickness d. It must be pointed out that R and T, in fact, have different values
5.3
Theory of Kubelka and Munk
329
compared with Rμμ and Tμμ from Equations (5.2.9) and (5.2.10). These values and also K and S depend on the approximation used and are, therefore, not directly interchangeable between different approximations (cf. Section 5.4.2).
5.3.2 Exceptional Optical Cases It is useful now, in the context of the formalism of Kubelka and Munk, to consider the compliance for the three special cases previously considered for the directional two-flux approximation in Section 5.2.2. For this, we begin with Equations (5.3.9) and (5.3.10) and consider again the opaque, transparent, and absorption-free conservative cases. Already from ideas developed in the directional two-flux theory, we know that for an opaque layer the transmission vanishes. Again considering the exponential nature of the hyperbolic functions in Equation (5.3.10), the limiting case d → ∞ gives lim T = 0
d→∞
(5.3.11)
and therefore compliance to requirements for this case. The same condition in Equation (5.3.9) yields, for the reflection R of an opaque layer, the simple expression R=
1 , a+b
(5.3.12)
which, considering Equation (5.3.4), is equivalent to R = a − b.
(5.3.13)
Inserting the expressions for a and b from Equations (5.3.3) and (5.3.4) into the above results in an expression for the ratio of the absorption and scattering constants gives F=
(1 − R)2 K = S 2R
(5.3.14)
This relation is called Kubelka–Munk function. Although similarly structured to Equation (5.2.20), this result is larger by a factor of 2. This results from the empirical weighting of K and S in the system of equations (5.3.1a) and (5.3.1b). Expressions (5.3.14) and (5.2.20) each have a singularity for R = 0 and S = 0, respectively, and are, therefore, undefined in these cases. These special cases correspond to dark colors or colorants such as carbon black or dark violet. In order to avoid this difficulty in reality, a tiny amount of scattering white is added to the corresponding coloration.
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5 Theories of Radiative Transfer
A transparent medium absorbs light without any scattering; therefore, S = 0 holds, which means the reflection vanishes (since reflection means scattering, by definition). This connection follows additionally from Equation (5.3.9) for k=0 R=
1 S = = 0, a K+S
(5.3.15)
provided K > 0. Here, the relations K = bS, a = 1, and b = 0 are valid; therefore, we obtain from Equation (5.3.10) in the limit b →0: T=
1 . sinh (Kd) + cosh (Kd)
(5.3.16)
This is equivalent to T = e−Kd ,
(5.3.17)
which again corresponds formally to the one-dimensional Lambert–Beer law of an absorptive layer, cf. Equation (5.1.7) using T = I0 (z = d)/I0 . Note that the absorption coefficient K here is twice as much as in Equation (5.2.16). Returning to the conservative case originally characterized by ω0 = 1 and K = 0, from Equation (5.3.3), it follows a = 1. The equation of energy (2.1.14) reduces to the simple relation R + T = 1. In order to reassess this expression, we take the limit of the expressions in Equations (5.3.9) and (5.3.10) for a → 1 and obtain R=
Sd , 1 + Sd
(5.3.18)
T=
1 , 1 + Sd
(5.3.19)
clearly complying with the conservation of energy requirement. In addition, for large values of S or d, the results from Equations (5.3.18) and (5.3.19) approach R = 1 and T = 0, respectively. This corresponds to the coordinates of corner point C of the optical triangle in Fig. 5.14. The coordinates of corner point A follow from expressions (5.3.18) and (5.3.19) for d = 0. On the other hand, the coordinates of the special points A and B, as well as the quantities K and S, follow directly from Equations (5.3.11), (5.3.12), (5.3.13), (5.3.14), (5.3.15), (5.3.16), and (5.3.17); all parameters mentioned agree with those listed in Table 5.1. Therefore, the special cases just discussed are again in agreement with experience and expectations.
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331
5.3.3 Determination of Optical Constants The methods outlined in Section 5.2.4 can be applied directly to the results of the Kubelka–Munk formalism. From Equations (5.3.9) and (5.3.10) and those that follow, it is possible to determine the coefficients K and S. In order to obtain the albedo ω0 or optical path τ , we refer to Equations (5.1.27) and (5.1.28). To begin, for the case of a transparent material, the absorption constant K follows immediately from Equation (5.3.17): 1 K = − · ln (T), d
(5.3.20)
with known layer thickness d and measured transmission T. The unit of K is an inverse length; this is in accordance with the considerations in Section 5.1.2. In the case of an opaque medium, only the ratio K/S can be calculated, that, using Equation (5.3.14). This ratio vanishes for R = 1; physically, this is because the incoming flux is completely backscattered and not absorbed at all (the conservative case represented by corner point C in Fig. 5.14). For translucent systems, it is possible to ascertain both coefficients K and S separately and, additionally, by way of known two different methods: either by single measurement of reflection and transmission or, most often applied, by measuring the reflection over two known but differently colored backgrounds. For the first of these methods, one can base calculations on Equations (5.3.9) and (5.3.10) suitably combined with (5.3.3) and (5.3.4) and solve for K and S. The second method refers to Equations (4.2.13) and (4.2.14), in which R1 stands for reflection R and T1 for transmission T. Together with Equations (5.3.9) and (5.3.10), the following formulas are obtained: Rw =
1 − Rbg,w [a − b coth (kd)] , a − Rbg,w + coth (kd)
(5.3.21)
Rb =
1 − Rbg,b [a − b coth (kd)] , a − Rbg,b + coth (kd)
(5.3.22)
where Rbg,w and Rbg,b are the measured reflection of the plain white and black background substrates, respectively, Rw and Rb are the reflection of the test layer over the white and black backgrounds; layer and background substrate have to be in optical contact (cf. Section 4.2.4). Combining Equations (5.3.21) and (5.3.22) results in a=
(1 + Rbg,w Rw )(Rb − Rbg,b ) − (1 + Rbg,b Rb )(Rw − Rbg,w ) . 2(Rbg,w Rb − Rbg,b Rw )
(5.3.23)
The parameter a, therefore, can be determined from four measured reflection quantities Rbg,w , Rbg,b , Rw , and Rb . If the black background substrate is really
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5 Theories of Radiative Transfer
black, i.e., Rbg,b ≈ 0, Rbg,b