information to users...4.2 reflected luminance measurements as a function of azimuthal detector...
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REFLECTION FROM IMPERFECT CHOLESTERIC LIQUID CRYSTALS: BASIC PROPERTIES AND APPLICATIONS
A dissertation submitted to Kent State University
in partial fulfillment of the requirements for the degree of Doctor of Philosophy
by
William Joseph Fritz
August, 1995
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Dissertation written by
William J. Fritz
B.S., Kent State University, 1980
M.S., Case Western Reserve University, 1982
Ph.D., Kent State University, 1995
Approved by
_, Chair, Doctoral Dissertation Committee
Members, Doctoral Dissertation Committee
't/C * - — ;
Accepted by
hair, Department of Physics
— , Dean, College of Arts and Sciences
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TABLE OF CONTENTS
LIST OF FIGURES......................................................................................................vii
LIST OF TABLES........................................................................................................ xii
ACKNOWLEDGMENTS............................................................................................. xiii
1. Introduction...................................................................................................................1
2. Optical Properties of Chiral Nematic Liquid Crystals................................................8
2.1 Introduction: General Properties of Liquid Crystals.......................................... 9
2.2 General Optical Properties of Chiral Nematic Liquid Crystals......................... 10
2.3 Reflection at Normal Incidence from a Perfect Cholesteric Liquid Crystal.... 122.3.1 Kinematic Theory of Reflection (Single Scattering)................................142.3.2 Dynamical Theory of Reflection (Multiple Scattering)...........................20
2.4 Reflection at Oblique Incidence from a Perfect Cholesteric Liquid Crystal 252.4.1 Two-wave Approximation (Analytic Solution)........................................262.4.2 4x4 Berreman Method (Numerical Solution)........................................... 28
2.5 Reflection from Imperfect Cholesteric Liquid Crystals......................................322.5.1 General Approach.....................................................................................32
2.5.1.1 Single-scatter Two-wave Approximation (Arbitrary Domain Shape)..................................................................................................... 35
2.5.1.2 4x4 Berreman Method (Imperfect Planar Domain)............................40
3. Reflection from Imperfect Cholesterics: Experiment and Calculation.................... 42
3.1 Introduction........................................................................................................ 42
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Table of Contents (continued)
3.2 Sample Preparation.............................................................................................. 433.2.1 Domain Structure as a Function of Polymer Concentration..................... 473.2.2 Domain Structure as a Function of UV Illumination Time........................523.2.3 Domain Structure as a Function of a Different Monomer.........................59
3.3 Physical Model of Domain Structure.................................................................62
3.4 Measurement and Model for Reflected Intensity Versus Polymer Concentration and Detection Angle.................................................................... 643.4.1 Introduction............................................................................................... 64
3.4.2 Measurement o f Reflected Intensity versus Polymer Concentrationand Detection Angle................................................................................... 66
3.4.3 Model of Reflected Intensity versus Polymer Concentration and Detection Angle..........................................................................................70
3.4.4 Comparison of the Model to the Data.......................................................78
3.5 Measurement and Model o f Reflection Spectra Versus Polymer Concentration and Detection Angle.................................................................... 80
3.5.1 Measurement o f Reflection Spectra............................................................803.5.2 Model of Reflection Spectra Utilizing 4x4 Berreman Method................. 843.5.3 Comparison of Calculated to Measured Reflection Spectra..................... 87
4. Illumination and View Angle of Reflective Cholesteric Displays..........................88
4.1 Introduction........................................................................................................ 884.1.1 Measurement Conditions..........................................................................89
4.2 Reflected Luminance Measurements.................................................................924.2.1 Reflected Luminance Measurements...................................................... 924.2.2 Reflected Luminance about the Zero Degree Polar Plane.................... 944.2.3 Physical Model for Measured Reflected Luminance Results................944.2.4 Luminance Polar Plots............................................................................104
4.3 Contrast Ratio Measurements...........................................................................1044.3.1 Contrast Ratio Measurements................................................................104
4.3.2 Physical Model for Measured Contrast Ratio Results........................... 1074.3.3 Contrast Ratio Polar Plots...................................................................... 111
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Table of Contents (continued)
4.4 Chromaticity as a Function of Incident Light and Detection Angle...............1114.4.1 Chromaticity........................................................................................... I l l4.4.2 Physical Model to Describe Angular Hue Dependence........................1164.4.3 ChromaticityMeasurements................................................................... 120
4.5 Optimal Illumination Conditions...................................................................... 122
5. Study on Color Quality o f Chiral Nematic Liquid Crystals....................................125
5.1 Color.................................................................................................................1265.1.1 Reflected Color from a Chiral Nematic Liquid Crystal.........................126
5.2 Effect of Absorption on the Reflection Spectrum from CholestericLiquid Crystals..................................................................................................127
5.3 Reflection Spectrum and Color Quality of CLCs with Dichroic Dyes 1315.3.1 Dichroic Dyes.........................................................................................131
5.3.2 Measured Reflection Spectrum from Absorbing Cholesteric Liquid Crystals with Different Dyes.................................................................. 138
5.3.3 ChromaticityMeasurements.................................................................. 143
5.4 Calculation of the Reflection Spectrum from Cholesteric Liquid Crystals with Dichroic Dyes.......................................................................................... 146
5.5 Comparison of Calculated Reflection Spectra to Measured Results.............147
6. Multi-color Displays.................................................................................................151
6.1 Introduction....................................................................................................... 1516.1.1 Additive Color Mixing.............................................................................1526.1.2 Pixelization............................................................................................... 155
6.2 Mechanical Approach.......................................................................................1566.2.1 Lithographic/Etch Technique for Rib/Channel Formation..................156
6.3 Photochemical Approach................................................................................. 159
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Table of Contents (continued)
6.4 Hybrid Approach.............................................................................................164
7. Conclusions............................................................................................................ 168
References................................................................................................................. 174
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LIST OF FIGURES
Figure Page
1.1 Perfect (a) and imperfect (b) planar texture o f a cholesteric liquid crystal...........2
1.2 Schematic representation of the three possible states of a chiral nematicLC with the application of a suitable electric field.................................................4
2.1 Schematic representation of chiral nematic liquid crystal material showing the twist in the liquid crystal director as a Sanction o f position along thez-axis.........................................................................................................................11
2.2 Schematic representation for light that is Bragg reflected from (a) cholesteric liquid crystal material and (b) from a crystalline solid...........................................13
2.3 Diagram showing paths traversed by an em wave with X=np (1,2,3) and for A,=np+ne (1,,2',3I)..................................................................................................... 15
2.4 Diagram showing incident em wave undergoing only one reflection withinCLC material............................................................................................................ 17
2.5 Schematic diagram showing multiple scattering within a CLC..............................21
2.6 Reflection and transmission from r* layer in dynamic theory of scatteringfrom a CLC is shown in (a). Calculated reflection curves using the dynamic theory of reflection for (b) 3 )tm and (c) semi-infinite thick sample.....................23
2.7 Schematic representation showing a multi-domain CLC....................................... 33
2.8 Schematic representation of an imperfect CLC showing domains of (a)arbitrary shape and (b) with imperfect planar texture............................................37
3.1 Top micrograph (1 OOx) showing texture before polymerization (a) andbottom micrographs (lOOx) showing the texture of samples with 0.47%(left) and 0.72% (right) polymer concentrations, respectively (b)........................48
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List of Figures (continued)
3.2 Plots of average domain size versus BAB polymer concentration. Upperplot has line drawn through data as an aid to the eye. Solid line in bottom plot is a fit to the data with a function that varies as the inverse of the concentration............................................................................................................50
3.3 SEM micrograph showing approximate cylindrical areas o f anisotropicallyoriented polymer...................................................................................................... 51
3.4 Reflection spectra from samples with different polymer concentrations............ 53
3.5 Micrographs (lOOx) showing the texture of samples with 0.63% and 1.3%BAB polymer concentration after (a) 0.5, (b) 2.0 and (c) 30.0 minuteso f UV illumination................................................................................................... 56
3.6 Plot of domain size versus illumination time showing the domain sizedecreases as the UV illumination time increases................................................... 57
3.7 Reflection spectra as a function of UV illumination time.................................... 58
3.8 Micrographs (lOOx) showing the texture of samples with (a) 0.38, and(b) 0.8 and (c) 1.1% of the BAB6 monomer......................................................... 60
3.9 Log plot o f average domain size versus BAB6 concentration............................ 61
3.10 Reflection spectra of samples with different BAB6 concentrationsbefore and after polymerization............................................................................... 63
3.11 Schematic of perfect cholesteric (a) and schematic of imperfect cholestericcreated by the polymer studied in the experiments................................................65
3.12 Geometry of measurement set-up where P is the incident light angle, <)> theazimuthal and 0 the polar angle of the detector.................................................... 67
3.13 Log plot of luminance versus azimuthal angle for four samples with differentpolymer concentrations............................................................................................. 69
3.14 Plot of luminance versus polymer concentration for the three detector angles40, 35 and 30 degrees, respectively.........................................................................71
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List o f Figures (continued)
3.15 Schematic representation of the geometry of the domains created by thepolymer used in the experiments............................................................................ 74
3.16 Gaussian distribution as a function of the variable y for different standarddeviations................................................................................................................. 77
3.17 Comaparison of measured data (points) to the model (solid line)....................... 79
3.18 Measured (solid line) and calculated (dashed line) reflection spectra for theincident light angle of 5 degrees and detector angles indicated.............................82
3.19 Measured (solid line) and calculated (dashed line) reflection spectra for theincident light angle of 22 degrees and detector angles indicated...........................83
4.1 Measurement geometry (a) and the effect of refraction on the incident lightas a result of the air-glass interface (b)................................................................... 91
4.2 Reflected luminance measurements as a function of azimuthal detector angle for the incident light angles shown from the yellow sample (upper) andthe green sample (lower)......................................................................................... 93
4.3 Reflected luminance measured as a function of azimuthal and polar angle foran incident light angle of 29 degrees.......................................................................95
4.4 Schematic representation of helical axis orientation and incident light angle.The helical axis orientation is the same for diagrams (b) and (c) whilethe incident light angle differs between (b) and (c)................................................ 97
4.5 Comparison of calculated (solid line) and measured (points) luminance...............101
4.6 Comparison of calculated (solid line) and measured (points) luminance...............102
4.7 Two-dimensional polar plots of reflected luminance for the yellow sample..........105
4.8 Two-dimensional polar plots of reflected luminance for the green sample............106
4.9 Contrast ratio measurements as a function of incident and detector angle..........108
4.10 Measured luminance from the yellow sample in both the imperfect planar and focal conic states for 10° (upper plot) and 65° (lower plot) incidentlight angles............................................................................................................... 109
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List of Figures (continued)
4.11 Two-dimensional contrast ratio polar plots for the yellow sample........................112
4.12 Two-dimensional contrast ratio polar plots for the green sample......................... 113
4.13 Color circle (a) and 1976 CEE color chromaticity diagram (b)..............................115
4.14 Schematic representation of helical axis orientation and incident light angle with the helical axis orientation and incident light angle in (a) reversedfrom that in (b)..........................................................................................................117
4.15 Schematic diagram of helical axis orientation and incident light. While the helical axis orientation is the same in both (a) and (b), the incidentlight angle is different................................................................................................119
4.16 Chromaticity coordinates as a function of incident light and azimuthal angle..... 121
4.17 Upper two plots are maximum luminance (left) and maximum CR (right)and lower plot is viewing angle, all versus incident light angle............................. 123
5.1 Plot of absorption coefficient (y-axis left) for constant k values 0.2, 0.1 andBragg reflection band (y-axis right) of a CLC with pitch to reflect yellow..........129
5.2 Calculated reflection spectra using the dynamic theoiy of reflection froma CLC with the k values shown (a) and using the two-wave approximation for the k values 0.0, 0.02 and 0.2, respectively (b)................................................ 130
5.3 Measured absorption curves along the extraordinary (e) and ordinary (o)axes for the dyes DR-13, R4, and C6......................................................................133
5.4 Upper plot is modelled absorption spectrum for the three dyes along the extraordinary axis while the bottom plots show both the calculated(solid line) and measured (points) absorption spectra............................................136
5.5 Plots for the different dyes showing the absorption spectra (y-axis left) and Bragg reflection spectra from a CLC (y-axis right) with pitch toreflect yellow.............................................................................................................137
5.6 Reflection spectra from a CLC with a chiral concentration of 27.2% andone with 26.5%..........................................................................................................141
x
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List of Figures (continued)
5.7 Upper plot shows collectively the measured reflection spectra from samples with the various dyes while lower plots show the individual spectra forsamples with the dyes DR-13, R4, C6, respectively...............................................142
5.8 Upper three plots show measured chromaticity coordinates from samples with the three dyes at the various concentrations shown. Lower plotshov/s general area on the CIE diagram where measured data is located.............144
5.9 Upper plot shows collectively the calculated reflection spectra with thevarious dyes while lower plots show the individual reflection spectra................... 148
5.10 Comparison of the measured (solid line) to the calculated (dashed line)reflection spectra for samples with the three dyes................................................... 149
6.1 Several examples of additive color mixing................................................................153
6.2 View of rib/channel layout (a) and method to fill alternating channelswith different pitch material (b).................................................................................158
6.3 Sample using ribs for two-color display.................................................................... 160
6.4 Color change as the result of UV illumination on samples with (lower)and without (upper) polymer....................................................................................163
6.5 A three color hybrid display........................................................................................167
xi
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LIST OF TABLES
Table Page
la. Relevant parameters for the nematic liquid E48 (EM chemicals).........................44lb. Relevant parameters for the chiral compounds...................................................... 44
II. The chiral compounds CB15, R1011 and CE1 are mixed in a ratio of 3:1:3 with a relative concentration of 28% in the nematic E48. The relative concentrations of the monomer BAB with the chemicalstructure as shown are listed............ in the table................................................... 45
III. A listing of times at which samples are removed from UV illumination.Samples are examined with optical microscopy and then reflection spectraare measured............................................................................................................ 54
IV. The table shows standard deviations determined from the measurements and model for helical axis orientation distribution as a function ofpolymer concentration............................................................................................81
V. Table showing a from fitting the model to the measurements for the green sample and comparison to a of chapter 3 (5.8°) as % difference
l< W -° ) /a J .................................................................................................................103
Via. Relevant parameters for the dyes from measurements.......................................135VIb. Relevant parameters for the dyes from curve fit............................................135
VII. Listing of the concentrations of the three dyes used in the experiments...............140
xii
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ACKNOWLEDGMENTS
I would like to express my appreciation and gratitude to my parents for their
support in this effort to pursue an advanced degree. Without their support, it would
have been very difficult, if not impossible.
I would like to thank Dr. J. William Doane for being my advisor in this effort. His
insight and support were critical in completing this work. I would also like to thank
Dr. Nathan Spielberg for his support and encouragement, which made possible the
opportunity to continue my education. Finally, I would like to thank Dr. Dengke
Yang for his technical support.
xiii
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Chapter 1
Introduction
In a cholesteric (also called chiral nematic) liquid crystal (CLC), the director twists
about its optic axis, where the director is the average orientation of the liquid crystal
molecules at a point in space. The twist of the liquid crystal molecules creates a
continuously varying but periodic dielectric function, which results in many interesting
optical phenomena1. One aspect, Bragg reflection, is the subject of investigation of
this research.
When CLC material is filled between two glass pieces that have surfaces treated to
provide strong, homogeneous anchoring (the director lies along one direction near the
surface), the material can form what is called the planar or grandjean texture1. The
helical axes are oriented along a direction normal to the glass surface. If there are no
sharp discontinuities in director configuration (Fig. 1.1a) this can be considered a
perfect cholesteric liquid crystal (or single domain CLC). A polymer network inside
the material will introduce sharp discontinuities and break the planarization into
domains which have the helical axes oriented in different directions (Fig. 1.1b). At the
discontinuity, a defect (point defect or disclination) is formed. Areas of perfect
cholesteric LC surrounded by a disclination or ceil wall surface are called domains.
This situation is called an imperfect cholesteric LC (or multi-domain CLC).
1
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2
(a)
(b)
Fig. 1.1. Perfect (a) and imperfect (b) planar texture of a cholesteric liquid crystal
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3
As illustrated in Fig. 1.2 with the application of an electric field, the material
transforms from the planar into the focal conic state1. In this state, many domains are
formed where the helical axes are primarily oriented parallel to the surface. Upon
removal of the field, the material relaxes back to the planar texture. However, the
inclusion of an anisotropic polymer network stabilizes the focal conic texture, so that
the field can be removed and the material remains in that state2. By using a suitably
pulsed electric field, material with a polymer network can be stabily placed in either
state.
At a high enough electric field, the director unwinds and aligns parallel to the field1.
This is called the homeotropic state. However, it is not possible to stabilize this
texture and upon removal of the electric field, the material relaxes to either the planar
or focal conic state.
Bragg reflection from single domain chiral nematic liquid crystals has been well
studied and is now fairly well understood3'5. Recently, there has been interest in
multi-domain systems generated by their importance in reflective flat-panel displays2.
However, little research has been performed on reflection from multi-domain chiral
nematic material due in part to the difficulty in conducting quantitative experiments.
One goal of this research is to investigate reflection from these multi-domain CLCs
utilizing a polymer network to quantitatively control domain structure.
Because of the selective nature of Bragg reflection from CLCs, reflected color can
be produced without the use of color filters. This property makes these materials
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4
electric field electric field
imperfect planar texture
focal conic texture
m M i '1i i1 1 i1 ]11|
I I I ' l l !
homeotropictexture
(reflecting state) (scattering state) (transparent state)
Fig. 1.2. Schematic representation of the three possible states o f a
chiral nematic LC with the application of a suitable electric field.
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5
attractive for use in display applications. Initial interest for using cholesteric liquid
crystals in display applications occurred in the early lPVOs6"8. Primarily single domain
or poorly controlled multi-domain CLCs were utilized. Displays made in this fashion
had poor spatial and color uniformity, large color change with angle and poor viewing
angle. However, with the advent of polymer modified cholesteric textures, reflective
color displays using chiral nematic liquid crystals have been made feasible2,9. In
addition to improving the optical properties, a polymer network makes the display
bistable, which allows for flicker-free, low power operation. A goal of this research is
to understand the reflective properties of multi-domain chiral nematic liquid crystals to
improve the luminance, viewing angle, contrast ratio and color quality of polymer
modified reflective cholesteric displays and to optimize illumination conditions.
Two methods are investigated for calculating reflection spectra from multi-domain
chiral nematic liquid crystal samples; the two-wave single scatter approximation
method and the 4x4 Berreman method. The 4x4 Berreman method is used for detailed
calculations because it can be more readily applied to the domain structure created by
the polymer network. The calculations take into account domain size, shape, and
orientation distribution of the domains. The domain structure is experimentally
investigated as a function of polymer concentration, ultra-violet (UV) illumination
time, and type of polymer. By varying the polymer concentration, domain structure
can be controlled. A phenomenological model is developed to describe reflected
intensity measurements as a function of detector measurement angle and polymer
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6
concentration. Calculated reflection spectra are compared to measured results with
fitting parameters used to determine domain orientation distribution. There is
excellent agreement between theory and measurements.
A study is conducted to determine the effect of different illumination and detection
conditions on the reflective properties of multi-domain chiral nematic liquid crystal
material. Samples with optimal polymer concentrations are illuminated at four
different incident light angles and the resulting luminance, contrast ratio and
chromaticity measured at different azimuthal and polar angles. A model is developed
to describe the observed results and optimal illumination and detection conditions are
established.
Research on the quality of the reflected color is also conducted. As the pitch o f the
chiral nematic liquid ciystal material is increased, the center wavelength of the Bragg
reflection increases. In addition, there is an increase in the reflected bandwidth as
8X=XSn/n, where X, is the wavelength, 5n is the birefringence and n the average
refractive index.10. This reflection band is a linear function of wavelength, so that the
longer the wavelength, the wider the reflection band resulting in a desaturation o f the
colors yellow, orange and red.
Research is conducted on the use of dyes with absorption bands overlapping the
Bragg reflection spectrum to decrease the bandwidth o f reflected wavelengths and
thus increase the saturation (i.e., quality) of the reflected color. Theoretical
calculations using the dynamic theory of reflection show this absorption overlap causes
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7
a change in shape in the reflected spectra where the primary effect is a decrease in
intensity at various wavelengths within the reflection band. Experimental
measurements with different dyes show good agreement with the theory and result in
varying degrees of improvement in color quality depending on the type of dye, and dye
concentration used.
Finally, experiments are conducted using various approaches to develop a
multi-color display. One approach is to use lithographic and etching techniques on
various materials to form mechanically separated channels. The channels are then
alternately filled with materials o f different pitch to produce a multi-color sample.
Another approach is to use a chiral compound that can have the chirality change under
intense UV illumination. A series o f masks and subsequent UV illumination define the
different color areas. The best results to date utilize a combination of both
approaches.
The research reported here is the first detailed experimental study on the reflection
properties o f multi-domain chiral nematic liquid crystals. The results from this basic
research increase the fundamental knowledge on the optical properties of imperfect
cholesterics in addition to improving reflective cholesteric display properties.
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Chapter 2
Optical Properties of Chiral Nematic Liquid Crystals
This chapter presents the fundamental basis on which the reflective properties of
imperfect cholesterics can be quantitatively described. The chapter begins with a brief
introduction on the general properties of liquid crystals. Next, three approaches are
outlined to calculate the reflective properties for normally incident light on a perfect
cholesteric. Of the three, the dynamic theory of reflection is discussed in detail. The
dynamic theory of reflection is utilized in chapter 5 to quantitatively discuss the effect
of absorption in chiral nematic liquid crystals. Then, two approaches are discussed to
calculate the reflective properties for obliquely incident light on a perfect cholesteric.
Of the two, the 4x4 Berreman method is discussed in detail. Next, a general approach
to calculate the reflective properties of imperfect cholesterics is developed. Within this
approach, two techniques are examined, the single scatter approximation and the 4x4
Berreman method. The general approach using the 4x4 Berreman method is discussed
in detail because this approach is utilized in chapter 3 to specifically calculate the
reflective properties of imperfect cholesterics studied in this research.
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9
2.1 Introduction: General Properties of Liquid Crystals
The term liquid crystal refers to a class o f material that exists in a state between a
pure liquid and a pure solid. In this state the material possesses some properties
common to liquids such as fluidity and other properties common to solids such as
orientational order10. The degree of orientational order is described by an order
parameter which is a function of temperature1. There are two types of liquid crystal
mesophases, thermotropic and lyotropic". Thermotropic liquid crystals undergo a
phase transition from a liquid to a liquid crystal as the result of a change in
temperature. Lyotropic liquid crystals undergo a phase transition as the result of a
change in concentration. The research discussed herein deals solely with thermotropic
liquid crystals.
Thermotropic liquid crystals are usually composed of elongated organic
molecules". Depending on the specific molecule, the material can exist in one of
several possible liquid crystalline states (nematic, cholesteric, or smectic) depending on
the temperature10. The molecular order of a nematic liquid crystal is characterized by
long range orientational order but the nematic phase is still fluid, thus there is no long
range correlation of the molecular center of mass positions1. The average direction the
liquid crystal molecules point at some region in space is described by what is called theA
director, n. Per the discussion by Chandrasekhar10, cholesteric order consists of a
nematic liquid crystal except that it is composed of optically active molecules. As a
consequence, the structure spontaneously twists about an axis normal to the preferred
molecular direction10. Smectic order consists o f a liquid crystal having, in addition to
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10
orientational ordering, a translational ordering that results in a layered structure10.
There are various smectic phases with each phase having a different degree or
character o f spatial ordering.
The following discussion deals with the optical properties (and in particular the
Bragg reflective properties) of chiral nematic liquid crystals, consequently, detailed
discussions on other aspects of liquid crystals such as the order parameter, elastic
energy, flow properties, etc. are listed in the references1,10"12.
2.2 General Optical Properties of Chiral Nematic Liquid Crystals
As mentioned, the director of a chiral nematic liquid crystal rotates about an axis
which is normal to the preferred orientation of the liquid crystal molecules. This axis
is the optic axis of the material. The distance over which the director rotates 360
degrees is defined as the pitch. Figure 2.1 is a schematic representation of the director
configuration for a chiral liquid crystal. The director can be described in a cartesian
coordinate system in the following manner;A
nx = cos(^oz+<p)»>, = sin(9o2+<p) (1)«z = 0
where qo is defined as qo = 2n/p where p is the pitch.
A A
Because n = -n , a chiral nematic liquid crystal is periodic with a spatial period equal
to one half the pitch.
The spatially periodic, helical structure of a chiral nematic liquid crystal results in a
continuously varying, but periodic dielectric function. This dielectric function
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11
' / / / /
z=pA
pitch
/ / / /
z-axis
x-axisy-axis
Fig. 2.1. Schematic representation of chiral nematic liquid crystal material
showing the twist in the liquid crystal director as a function of
position along the z-axis.
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12
produces many different optical phenomena such as Bragg reflection1, strong optical
rotary power11, the Borrmann effect10, etc. In addition, the chiral nematic liquid crystal
structure results in different electro-optic effects than that observed for nematic liquid
crystals as well as modifying the flow properties of the material. The following
research primarily deals with the Bragg reflective properties (i.e., when the wavelength
is comparable to the pitch), consequently, detailed discussions on other properties of
chiral nematic liquid crystals are contained in the references1,10'13.
2.3 Reflection at Normal Incidence from a Perfect Cholesteric Liquid Crystal
A perfect cholesteric is a sample in the planar texture that has all the helical axes
pointed in the same direction and there is a uniformity across the sample. In this
section, the helical axes and the incident light are assumed to be normal to the sample
surface as shown in Fig. 2.2a for (5=0. Bragg reflection from a chiral nematic liquid
crystal is similar to Bragg reflection from a crystalline solid except that the
continuously varying, but periodic dielectric function of the liquid crystalline material
replaces the discretely placed, but periodic planes of the crystalline solid as shown in
Fig. 2.2b. As a result of the differences, the Bragg reflection conditions will be
different. Several approaches can be taken to determine the detailed properties of
Bragg reflection from a chiral nematic liquid crystal. In one approach, Maxwell's
equations are reduced to one dimension (say the z direction)
(2)
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(a) (b)
A, = npcosP Bragg reflective condition for CLC
P = 0 for normally incident light
Fig. 2.2. Schematic representation for light that is Bragg reflected from (a)
cholesteric liquid crystal material and (b) from a crystalline solid.
Note: The increase or decrease in the length of the lines in (a)
indicates a twisting into, or out of the plane by the LC director.
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14
and solved with the dielectric tensor e suitably expressed as a periodic function of z
in the fixed laboratory frame". Then by Floquei's theorem there exist solutions such
that
E(z+p/2)=KE(z) (3)
where K is a constant that may be complex14,15. Another approach is to solve
Maxwell's equations by first transforming into a coordinate system that rotates with
the cholesteric helix. In this rotating frame, e has a simple diagonal form for all values
of z and thus enables a straightforward approach to obtaining a solution". A third
approach is to utilize the dynamical theory of reflection as developed for X-ray
diffraction10,16,17. The dynamic theory of reflection is presented in detail because it is
utilized in chapter 5. First, the kinematic theory is developed from which the
dynamical theory is based.
2.3.1 Kinematic Theory of Reflection (Single Scattering)
Before discussing the kinematic theory of reflection, a brief intuitive explanation
for Bragg reflection from chiral nematic liquid crystals is presented (see Fig. 2.3). The
requirement for Bragg reflection is that all reflected waves have the same phase at the
incident surface10. The phase of an electromagnetic (em) wave propagating through a
CLC can be described as <)> = 2nn(z)zl‘k. For this illustration assume n(z)=n where n is
the average refractive index and is constant. If the incident em wave has a wavelength
A,=riP, then the phase after propagating a distance equal to the pitch P is <)> = 2iuiPlnP = 2jt. Thus, there is no change in phase. After travelling a distance 2P the
phase is 4jt (i.e., no phase change). For a wave that has a wavelength nP+ne and e is
a small number, then no phase change occurs after a distance d=P+e,
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15
o 3'
d=2p
td=p
II
h= np
II
° 2IIII
° 1
o , d=2p+ 2e
! d=p+ e
i I IO 1' T T
k= n(p+e)
note: (1) X = np, X is Bragg wavelength(2) positions 1,2,3 occur in same relative location within cholesteric helix
while positions l',2', and 3' do not.
Fig. 2.3. Diagram showing paths traversed by an em wave with A.=np (1,2,3)
and for X,=np+ne (I1,2',3').
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16
<(> = 2nn(P+ e)/(nP+ we) = 2n. After moving a distance 2(P+e), the phase would be
4k , but as shown in Fig. 2.3, the wave is not at the same relative position within a
pitch as it was for the first P+e distance. Because n is in reality a function of distance,
and the wave did not traverse the same path in the first step as the second step, the
phase will not be 4k but some other value. Consequently, the reflected waves at this
wavelength will have different phases at the incident surface and destructive
interference will occur resulting in no reflection. Because the choice of wavelength
was arbitrary in this case, n(P + e), then the only wavelength that meets the
requirement that all refleced waves at the incident surface have the same phase is for
X=nP, as shown for the first case.
To develop the kinematic theory of reflection, it is assumed that the chiral nematic
liquid crystal can be represented as a medium composed of a large number of
infinitesimally thin birefringent layers with the principal axes of the successive layers
turned through a small angle p10. In this case, mP=2jt where m is the number o f layers
per turn of the helix, and md=P, where d is the thickness of one o f the layers and P is
the pitch. Also, 8n=ne-n0 is the layer birefringence and n=(n+n0)/2.
As discussed by Chandrasekhar10, assume right circular light given by D = * j
referred to the laboratory frame of reference x,y is incident along the z direction. If
the light is incident on a CLC with a right-handed twist, then P is positive. In this
development, it is assumed that the light only undergoes a single reflection (Fig. 2.4).
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17
T
-> incident wave ► reflected wave
Fig. 2.4. Diagram showing incident em wave undergoing only one
reflection within CLC material.
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18
To calculate the reflection coefficient at the boundary between the s+1 and s+2
layer, first the incident light vector is resolved along the principle axes of the s+1 layer
which is at an angle of (s+l)p with respect to the laboratory x,y axes. The resolved
components are
where ^ = 2jtnr(s+l)dA, and nr is the refractive index for right circular light.
At the boundary the component emerges from a medium of refractive index na
and the t | component from a medium of refractive index nb. Because the principle axes
of the s+2 layer are rotated slightly with respect to the s+1 layer, as the wave
propagates into the s+2 layer, one component will travel into a medium with a slightly
smaller index of refraction and the other into a slightly larger index of refraction. As a
consequence, one component is reflected without a change in phase while the other
with a phase change o f jc. This accounts for the observed fact that the sense of
circular polarization reflected from a CLC remains the same.
The reflected components £',r|' from the wave propagating from the s+1 layer to
the s+2 layer with respect to the principle axes of the s+2 layer are as follows17. The
reflected ^ component is along the t | direction with magnitude sinP (na - nb )/(na + n,, )
= P5n/2n where fin is the birefringence, n the average refractive index, and sinp is
approximately p because p is small. Similarly, the reflected r| component is along the
exp(/'{(j+l)P-<j»rt-i})
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19
% direction with magnitude sinf^n,, - n, )/(n, + n,, ) = -p8n/2n. Thus the reflected
components from the s+1 layer can be written;
Transforming back to the laboratory frame x,y, the reflected wave (note the
assumption of single scattering so the wave propagates back without further
reflection) on reaching the incident surface is
between this wave and the wave between the first and second layers is as follows. For
the first and second layers the phase is (<J>=(s+-1 )|3—<))s and with s=l) (|>=2P+27tnrdA,.
The phase difference between the s+1 layer and the s=l layer is 2(sP-<j)s). When A^n^,
then 27tnrd/X= 2jinrd/n1P=2rcd/P=P because md=P and mP=2rc, so «j> =sp. The phase
factor exp(2i(sp-<{)s)) becomes unity irrespective o f the value o f s because
sP-<l>=sp-sp=0. For right circular polarized light incident on a left-handed twist
material, the phase term ( s p -^ does not vanish because P is negative. Therefore the
waves from the different layers will not be in phase and destructive interference occurs
resulting in no Bragg reflection, and as a consequence, the wave will be transmitted
through the material virtually unchanged. The reflection coefficient per turn of the
helix as determined from Eq. (5) is (with mP=2rc)
ex p (i{ (j+ l)P -4*i}) (5)
exp(/'{(2s+2)P - 24»j+i})
This is right circular light traveling in the negative z direction. The phase difference
|Q|=mP8n/2n=rc8n/n. (7)
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20
Note how the reflected amplitude per turn of the helix is dependent on the
birefringence. The greater the birefringence, the greater the reflected amplitude.
Intuitively this indicates that for an equivalent amount o f total reflected light from a
given CLC sample, the CLC sample could be made thinner if its birefringence is larger.
The kinematic theory of reflection shows that Bragg reflection occurs only when
the wavelength of incident light is equal to the index of refraction times the pitch
(X=nP). It also shows that only right (left) circularly polarized light will be reflected
from material with a right-handed (left- handed) twist without a change in the sense of
circular polarization.
2.3.2 Dynamical Theory of Reflection (Multiple Scattering)
In the preceding development only single scattering was considered. However,
a complete description of the reflective properties from a CLC requires taking multiple
reflections into account. Before presenting the dynamical theory o f reflection,an
intuitive description of the effects of multiple scattering on the reflection from a CLC
is discussed.
As shown in Fig. 2.5, after reflection from the s layer, the backward propagating
wave can have some fraction of the wave reflected back in the forward direction, and
then some fraction of that wave reflected back in the original direction. This extra
distance can arbitrarily change the phase as (J>=27cn(d,-t-d2+d3)/A.. Consequently, if the
incident wavelength were X.=nP, this wave could arrive at the incident surface out of
phase with single scattered waves. A slight change in wavelength, X=np+e, could
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21
incident wave -> i reflected wave i=l, 2, or 3
Fig. 2.5 Schematic diagram shows multilple scattering within a CLC.
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22
adjust the reflected wave's phase to that o f other multiply scattered waves and
constructive interference (Bragg reflection) could occur. The greater the number of
multiple reflections, the greater the change in wavelength that would be required to
adjust the phase correctly. For a sample of a given thickness, the more reflections a
wave underegoes, the lower the total reflected intensity at that wavelength. And as
mentioned previously, the farther in wavelength from the single scatter wavelength
A=nP, the more reflections a wave must undergo to interfere constructively at the
incident surface.
To quantitatively take into account the multiple reflections within a CLC, the
dynamic theory of reflection is utilized. The CLC is divided into a series o f thin layers.
The layers are taken thin enough that within the layer the kinematic (single scattering)
description is valid. Then multiple scattering is considered between the layers10.
The reflection coefficient for normally incident right circular polarized light on each
layer is -iQ because of the kinematic assumption for scattering within each layer.
Difference equations can then be written for reflection and transmission between the
layers as shown in Fig. 2.6a. In Fig. 2.6a, Tr (T^,) is the complex amplitude of all
transmitted waves incident on layer r (r+1) and Sr (S^,) is the complex amplitude of all
waves reflected from layer r (r+1). The difference equations for the amplitudes as the
result of wave propagation across the r layer can be written
Sr=-iQT+exp(-i(t))Sr+, (8)
TrH=exp(-iQ)Tr-iQexp(-2i()))Sr+1 (9)
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23
Tr ^ t s r— — — — — — r layerTi+I ^ f S ,+t------------- 7X------------------- r+1 layer
0.5
0.4
> 0.3*->ocu0.2
0.0400 500 600 700
wavelength (nm) (b)
0.5
0.4
>u<D
0.0400 500 700wavelength (nm)
Fig. 2.6. Reflection and transmission from rlh layer in dynamic theory of scattering
from a CLC is shown in (a). Calculated reflection curves using the
dynamic theory of reflection for (b) 3 pun and (c) semi-infinite thick
samples, respectively.
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24
where <j)=27cnrP/X. Difference equations can be written for adjacent layers and an
iterative expression written for an arbitrary number (v) o f layers to describe the
complex reflected amplitude at the incident surface as (and putting Sv=0)
S0=(yv-1-(v-2)yv'3+(v-4)(v-3)yv'5/2!-.....)SV.,
(10)
where
y=exp(i<(>)+exp(-i<|>)+Q2exp(-i<t>) (11)
A similar expression can be developed for the complex transmitted amplitude as
To=(fv(y)exP(i<!>Kv.i (y))Tv (12)
By a suitable substitution, expansion around the reflection condition X=nP and
reduction o f the series f(y) (in Eqs. (10) and (12)) to a closed form, the ratio of the
total reflected amplitude to the incident amplitude is approximatelySo -)gexp(ie)To /e+^cothui; (13)
where
and
e= -2n(l-X0)/X (14)
(Q2-e2),/z (15)
and v is the number of layers and Q is as before.
The reflectivity is then
r> _ 1 So I ̂ _ Q1 fifV\| To | “ ^ J c o t h ’vl; K )
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25
For a semi-infinite medium v goes to infinity andSo _ Q___ (17)
(18)
Figure 2.6b is a plot o f reflectivity versus wavelength using Eq. (16) for a sample
with a thickness o f 3 microns. Figure 2.6c is a plot of reflectivity versus wavelength
using Eq. (17) for a semi-infinite medium. The results from the intuitive discussion are
in qualitative agreement with these calculations.
As shown by these results, not only is there Bragg reflection o f light at the
condition X=nP, but there is a range of Bragg reflected wavelengths around this
wavelength (X=np) which are the result of multiple scattering within the CLC. The
magnitude of this reflection band can be determined by setting Q=e, and by
substituting the quantities for these expressions, then 8A,=X8n/n. The range of
reflected wavelengths is proportional to the birefringence.
2.4 Reflection at Oblique Incidence from a Perfect Cholesteric Liquid Crystal
There exists no analytic solution for the reflective properties from a perfect
cholesteric when there is an angle between the incident light and the helical axis of the
cholesteric (see Fig. 2.2). As a consequence, other techniques need to be developed to
obtain a solution. In the following, a technique utilizing a suitable approximation
enables an analytic solution to be obtained'8'24. This approach will be briefly outlined.
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26
Next, a detailed description of a numerical solution using the 4x4 Bereman method for
obliquely incident light on a perfect cholesteric will be discussed25'27.
2.4.1 Two-wave Approximation (Analytic Solution)
The dielectric tensor for a chiral nematic liquid crystal with helical axis
oriented normal to the sample surface (the normal to the surface will be the z axis in
the laboratory frame) can be expressed in the laboratory frame as
^e+eScos2<t>(r) ±e5 sin 2§(z) 0 ^e= (19)±eSsin2<j>(z) e - e 8 cos2<j>(z) 0
0 0 e3 jwhere e = (ei + e 2)/2, 5 = (ei - e 2)/(ei + e 2>, and ei, e2 ande3 = e2
are the principal values o f the CLC dielectric tensor18. The z axis is directed along the
cholesteric axis and <j)(z)=xz/2 where x=47t/P and P is the pitch.
The Fourier expansion of this dielectric tensor can be written
e ( r ) = 2 e ,exp(m *r)J=0,±1
where
(20)
"e 0 o ' „ <-» r \ ±i o'0 e 0 ,e i =e_i = f - ±i -1 0 (21)
,0 0 e3,
000e0 =
where T is the reciprocal lattice vector.
The general Fourier expansion of the periodic three dimensional dielectric tensor for a
CLC can be written- v 1
(22)e ( r ) = 2exexp(/x»r)X
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27
To obtain an analytic solution for this expression of the dielectric tensor the amplitudes
ez for x not equal to zero are required to be small compared to e019. This condition
can be met when 5n is small.
Using Maxwell's equations and the dielectric tensor in Eq. (22), then the electric
field vector for an arbitrary direction of light propagation may satisfy
ed2E/dt2 = - c 2V x V x l (23)
where e is defined by Eq. (22).
Because the medium is periodic, the solution of Eq. (23) is a Bloch wave
E (r, t) = er ? • r (24)X
Substituting Eq. (24) into Eq. (23) results in the homogoneous set of equations for
’ '2 E f + (co2/c2)E e ? _?/ • • E-*) = 0 (25),X
where k-^-ka + x and are defined by Eq. (22).
To obtain an analytic solution to Eq. (25), the two wave approximation is utilized.
It is assumed that if the Bragg condition is satisfied, that generally, the set of equations
(Eq. (25)) has only two amplitudes,E0 and ET whose values are as large as that of the
incident wave. All remaining amplitudes are of the order of at least le^e^ which is a
small number on the order of 10'2 for most CLC systems23.
Writing explicitly the two equations from Eq. (25) in the two wave approximation,
the two vector equations for waves E,= Et and E0 with wave vectors
ko andki = kx = ko + x are ̂ ̂ —> 2 —> ^ —>
e0 *£o-(c/(0)2 k 0 E q E i =0
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28
ex» E0 + e o • E i - (c/to)2I 2
Jfc,| E i = 0 (26)
The accuracy of the approximation makes negligible small quantities on the order of
|, which show how the waves E0 and E, differ from a transverse one. Therefore,
it is possible to assume they are orthogonal to kj, and k„ respectively23.
The solution of Eq. (26) results in 4 eigensolutions and the general solution of Eq.
(26) is a linear combination of all 4 eigensolutions
E(r,t) = ̂ C jE j(r ,t) ,j=i
Ej(r, t) = (E0Jeikv '7 + Eyeik̂ ) e ~ m
where the coefficients Cj and the quantities k^ and k,j in each eigenwave are
determined by the boundary conditions. Upon solving for these quantities, the
reflective properties for obliquely incident light on a perfect cholesteric can be
determined.
2.4.2 The 4x4 Berreman Method (Numerical Solution)
Another approach to calculating the reflective properties for light incident
at an oblique angle on a perfect cholesteric is to use numerical techniques. The
following presents the 4x4 Berreman method for numerically calculating the reflective
properties.
Maxwell's equations in gaussian units and rectangular coordinates can be written in
6x6 matrix form as
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Equation (27) can be abbreviated as
(28)
where R is a symmetrical matrix with nonzero elements only in the off-diagonal
positions of the first and third quadrants26. Ignoring nonlinear optical effects, a linear
relation may be written between G and C as
where the first and third quadrants of M are nonzero in optically active media and the
third quadrant is the dielectric tensor.
In situations where M is only a function in one dimension (which generally is the
case for the dielectric tensor of a chiral nematic liquid crystal), say the z direction, then
the dependence of the fields on x is described by exp^il^x), therefore,
Then, with some algebraic manipulation 4 first order linear differential equations can
be written in 4x4 matrix form as26
M » G = C (29)
^ —> -iko sin p and -> 0.
(30)
Defining a new vector y as
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30
¥ =
'E x 'EyHx
(31)
then Eq. (30) becomes
$Ldz = / Q(z) (32)
where the appropriate matrix elements for a chiral nematic liquid crystal are
substituted in Q, then Q becomes
Q-
0 rio(£rsin2p - l )
(33)
0 0 ■ ' - ‘-jj0 0 Tlo 0
eu/fto (e22-w 2sin2p)/rio 0 0x-en /r|o - e i2/rio 0 0
wkere n o = ^ r 377a 5 = E = 2-(e" + Q=fn = \{ n e+n0), An = {ne - n 0), ne = JzJJ, nQ = Je±
a (is the handedness): a= + l(-l) for right-handed (left) helical structure
eii = e + e 8 cos#z 612=621 = ae 8 singz 622 = e - e8 cos qz 633 = 6j.
Equation (32) can only be solved numerically. For a small increase 8z, then Eq. (32)
is approximately
?(z+A z) = e I M e(z)Az • »p(z) (34)
In the computation the chiral nematic liquid crystal cell is divided into M layers with
thickness given by 8z=d/M where d is the cell thickness. With the definition
(35)i \ k 0\Q(z)AzB(z) = e
and the approximation given by Eq. (34) then
'P(Az) = 5(0) • 'F(O)
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31
vF(2Az) = 5(Az) • 'F(Az) = 5(Az) • 5(0) • ¥(0)
¥ (5) = B [{M - l)Az] • B [(M - 2)Az] • .......• 5(0) • T(0)= F« 'P(0)
At the boundaries z=0 and z=d the following conditions hold,
(36)
4 ',+ 4V = 4'( 0) iF, = 'P(5)
(37)(38)
where i,r, and t are the incident, scattered or reflected and transmitted waves,
respectively.
From Eqs. (36), (37), and (38) then
Vi is given and it is necessary to find t|fr to determine the reflectivity. In Eq. (39) there
are 8 unknown variables (4 for y r and 4 for xjrJ. At this point there are only 4
equations. However, outside the liquid crystal, the 4 magnetic field components can
be expressed in terms of the 4 electric field components, thus giving 4 more equations.
Solving these equations gives t|fr in terms of the incident fields which determines
the reflectivity.
The matrix B can be calculated from Eq. (35) by a Taylor series expansion.
However, a better technique which allows for larger values of 8z and thus results in a
faster calculation (hence the name, the faster 4x4 Berreman method) can be used27.
In this approach, use is made of the Cayley-Hamilton theory which shows that B
can be expressed by a finite series of order 3 as,
(39)
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32
(40)
where ft (i=l,...,4) are determined by the equations
= P i + P2?/ + P3g,? + p4?/ { i - l , . . . , 4 } (41)
where are the eigenvalues o f Q. This can increase the value of 8z by as much as 100
and thus obviously increase the speed of the calculation by the same factor.
2.5 Reflection from Imperfect Cholesteric Liquid Crystals
The following sections develop the basis on which the reflective properties can be
calculated for an imperfect cholesteric. First, there is a general development to
calculate the reflective properties for any type of imperfect cholesteric28. Then, a brief
outline to specifically calculate the reflective properties for a domain of arbitrary shape
using the single scatter approximation is presented29-30. Finally, a detailed treatment
using the 4x4 Berreman method for an imperfect planar texture is discussed31.
2.5.1 General Approach
The basic approach in calculating the reflective properties from an imperfect
cholesteric is to subdivide the sample into a series of thin layers (Fig. 2.7). The
thickness of the layer is on the order of the average diameter of the domain. A
scattering matrix is used to take into account multiple reflections between the layers.
The elements o f the matrix describe the reflected and transmited waves across an
individual domain. The total reflection and transmission is the matrix product across
all the layers (which is the thickness of the sample).
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33
Fig. 2.7. Schematic representation showing a multi-domain CLC.
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34
The first step is to define some matrices R and T (the exact form will be discussed
later) that relate either the Stokes parameters (if using intensities) or the field
amplitudes o f the reflected I,, and transmitted waves I, to the incident wave I; across an
individual domain as
W i , It==T»Ii (42)
Then the matrix F relating the vectors ^ and I, of the reflected and transmitted waves
at the boundaries (z and z-z+h)
C S M i S )is expressed in the matrix that takes into account multiple scattering between the layers
as
g _ ( T , - R , T ? R , R .T; ' )M -T ? R , 7? J (44)The matrix FN for the whole sample is then the product of the individual matrices over
the number of layers the sample has been divided into28,«•» n <->
Fn = YIF, (45)
The matrices RN and TN that relate the total reflected and transmitted wave from
the sample to the incident wave are found by using the boundary conditions and
solving for R N and TN by28
Rn = ~~{F22 )_1-^ 21 <-> <->Tn =F\\ ~ F u (F22)~1F2\ (46)
where the submatrices take the form
F n = rF u F n ̂F2i F n
(47)
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35
Calculation of the reflective properties of the sample reduces to calculating the R and
T matrices for the individual layers, and then calculating the total reflection and
transmission from Eqs. (45), (46) and (47).
Calculation of the individual matrices for a domain depend on the detailed structure
of the domain. A general expression for the R and T matrices for a given domain can
be expanded as28<-> ooRs ~ n (48)
and
Ts — ̂ n=QQntn (49)
The index n denotes the multiplicity of scattering in the layer and the coefficients
determine the fractional contribution of that n-multiple scattering to the total reflection
or transmission. Methods to calculate R and T are discussed in detail in sections
2.5.1.1 and 2.5.I.2.
Due to the potential randomness or distribution in properties of the domains (e.g.,
the orientation o f the helical axis), some type of averaging may be required. The exact
form of the averaging depends on the specific details of the domain properties and the
manner of scattering that is involved. For the situation where the domain properties
are completely random, then averaging of the R and T matrices reduces to averaging
expressions for the individual layers.
2.5.1.1 Single-scatter Two-wave Approximation (Arbitrary Domain Shape)
In this approach it is assumed that only single scattering occurs and the
conditions for the two-wave approximation as previously discussed are valid. Because
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36
of the single scattering approximation, this approach will determine the second term,
r„ in the expansion of Eq. (48). Only the first two terms in Eq. (48) are kept when
using this approach in the general procedure.
Consider an electromagnetic wave incident on the material at some arbitrary angle
and the refractive index of the outside medium is equal to the average refractive index
of the CLC material. The relevant situation is shown in Fig. 2.8a. As previously
discussed for the two-wave approximation, the wave field inside the liquid crystal is
represented as the superposition of two waves,
where k° is the wave vector of the incident wave and kT =k°-Fr is the wave vector of
the diffracted wave (here T is the CLC recoprocal lattice vector equal to 27t/P)18.
When there is an absence of correlation between phases o f the scattered waves due
to the random properties of the domains distributed through the material, intensities
instead of field amplitudes are used. The polarization tensor contains all possible
quantities that are quadratic in the amplitudes of the fields where the polarization
tensor can be represented as
The description of the waves propagating through the domain can be described as23
E(r) = E (z)eu , r + £ e ' t , r (50)
(51)
&r =A0J ° -B ° J <> + C0zJxV- «-»«-» <-><-» «-»<->
(52)
(53)
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(a)
(b)
Fig. 2.8. Schematic representation of an imperfect CLC showing domains o f (a)
arbitrary shape and (b) with imperfect planar texture. Note: |5 is the incident
light angle, <)> the detector angle and y the angle between the helical axis and
sample normal.
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38
The first equation (Eq. 52) describes the change in the incident wave as the result
of scattering through the domain. The operator A in this equation describes the
polarization tensor change due to absorption and birefringence o f light. The operator
B describes the decrease in J° due to scattering into J* and the operator C describes
the scattering into J° from the «T wave. The second equation describes analogously
the change of the polarization tensor «P.
The tensors A, B, and C are determined in the following fashion with the dielectric
tensor expressed as in Eq. (22). The tensor A can be derived from transport theory
and is given by
A °ikim = fK[(eo)//Sfe» - 5i/(eo)ton]/sina (54)
where e0l is the transverse (relative to the wave vector) part o f the zeroth Fourier
component of the dielectric tensor, and K={e)m w/c is the average wave vector of the
light in the CLC.
The form of the tensor operator C is determined from the fact that the change SIT
of the x'th wave as a result of the Bragg scattering o f the wave E0 can be expressed
with good accuracy in terms of the amplitude for scattering in the kinematic (Bom)
approximation23. With this approximation (i.e., single scatter), the change in the x'th
wave is
AE, - /{[e?(e - 7 ) 4 ]• exp[i(£ - ? ) • r]}dVA
~ M e % e l)E l = hFfkE l
(55)
(56)
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39
where the integration is over the volume of the domain, e are the unit vectors of the 0
and x waves, and E° and ET are the amplitudes of the 0 and x waves. The parameter
that determines the applicability of equation (56) is that 8t d i« l where h is the
dimension of a domain.
In the approximation considered, the scattering amplitude represented in equation
(56) is the product of two factors. The tensor quantity F is determined by the CLC
structure and is the analog of the structure amplitude of X-ray scattering. The factor f,
determines the dependence of the amplitude on the shape, size, orientation and other
properties of the domain. The tensor quantity C can then be determined from the
factor f, and the tensor F. The tensor quantity B is determined in a similar fashion
using the second Bom approximation.
The key result of this approach is the determination of the term f, because the
reflectivity is directly established from this term. As discussed, this term contains the
effects of all properties of the domain such as size, shape, etc. Also, as discussed, the
term f, comes from an evaluation of the integral in Eq. (55).
For this approach to be useful, the assumption of single scattering must be valid
and the dielectric anisotropy small. Even if these conditions are valid, in general, the
evaluation of the integral in Eq. (55) can be very difficult. The great advantage of this
approach is that it can determine the reflectivity for any arbitrarily shaped domain.
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40
2.5.1.2 4x4 Berreman Method (Imperfect Planar Domain)
When the shape of the domain is planar in nature, the 4x4 Berreman method
can be used to calculate the reflected and transmitted fields from the domain. In the
general procedure, the n-multiple scattering series of Eq. (48) can be replaced directly
with the 4x4 Berreman method because it inherently accounts for all scattering. The
4x4 Berreman method is developed as previously discussed, however, with some
modification because of possible different axis orientations with respect to the sample
normal.
As shown in Fig. 2.8b, the helical axis of the CLC within a domain (in addition to
the incident light) can have some angle with respect to the sample normal. For this
case, preliminary analysis indicates the CLC takes the director configuration shown in
Fig. 4.8b to minimize the free energy of this system31. In this situation, the 4x4
Berreman method cannot be used if the laboratory z axis is chosen because the
dielectric function is no longer a function of one variable. A workable approach is to
solve the 4x4 Berreman in the CLC frame where the helical axis lies along the z1 axis
of the local coordinate system, and then transform the fields back to the laboratory
frame. In the z' frame, the dielectric function is a function of one variable, z', and the
4x4 Berreman method is then applicable. The transformation is more than a
transformation between two coordinate systems but rather a transformation for the
fields expressed in the two coordinate systems. It should be noted this approach is not
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41
an exact solution because the transformation results in the k* component to be no
longer parallel to the sample surface.
So, from section 2.4.2, Eqs. (31) through (36) should have the vector field
expression iff, and the z coordinate replaced with primes, to denote the local
frame and everything procedes as discussed in section 2.4.2. The fields are found in
the laboratory frame by the following transformation,
*¥ = A • ' F /
where
cosy 0 0 rniosin(p-y)siny/e330 1 0 00 — wt|o sin(p - y) sin7/633 cosy 00 0 0 1
(57)
(58)
and n is the average refractive index of the dielectric medium and r)0 is the impedance
in vacuum. Now, using Eqs. (37) and (38), Eq. (57) and the usual boundary
equations, Eq. (39) of section 2.4.2 is replaced by
yVi = - xVr+A*F~x • A -x*'V, = -'V r + H*'Vt (59)
where r,i, and t represent the reflected, incident and transmitted waves, respectively.
Then, all fields can be expressed in terms of the k and a polarizations and utilizing the
procedures discussed in sections 2.4.2 and 2.5.1.2 a matrix Z can be written so that
the reflected and transmitted fields can be expressed in terms of the incident fields as
(60)
(E r 'I f a )E ra •
INII E'aE'k E‘a
[e 'c)
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Chapter 3
Reflection from Imperfect Cholesterics: Experiment and Calculation
3.1 Introduction
The reflection properties of perfect cholesterics have been studied for over 30 years
and are now fairly well understood3'5. However, there has been little work on
developing a detailed understanding of the reflection properties of imperfect
cholesterics which are of importance in flat panel reflective displays. One difficulty is
controlling the domain size and orientation distribution. In the following, preparation
of samples with polymer networks formed by ultra-violet light induced polymerization
is discussed, where domain properties are determined by the polymer concentration.
Physical analysis of the domains and a description of the domain structure is presented.
The angular dependence of reflected intensity is measured and the results compared to
a phenomenological model describing reflectivity as a function of domain axis
orientation. Finally, measured reflection spectra as a function o f incident light angle,
detector angle and domain structure are compared to theoretical calculations using the
4x4 Berreman method.
42
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43
3.2 Sample Preparation
The liquid crystal mixture used consists o f the nematic liquid crystal E48 and the
chiral compounds CB-15, ZLI-4535(R1011) and CE-1. The relevant parameters are
shown in Table I. By varying the concentration of the chiral compounds, the pitch of
the cholesteric is changed. For low concentrations, the relation describing pitch, P, as
a function of chiral concentration is given by P=l/H% where H is the helical twisting
power and % the chiral concentration11. So, the larger the chiral concentration, the
smaller the pitch; and by the Bragg reflection condition for cholesterics, X=nP, the
smaller the pitch, the shorter the wavelength that is reflected. For the work discussed
in this chapter, a chiral concentration of 28% is used. This concentration produces a
pitch of 0.33 pm and results in a center Bragg reflected wavelength of approximately
0.54 pm, which produces a green color.
To form the polymer network, a small amount o f laboratory synthesized monomer,
4,4-bisacryloyl-biphenyl (BAB) is added into the liquid crystal mixture with a small
amount (around 0.02%) of the photoinitiator, benzoin methyl ether (BME). The
chemical structure of the monomer is shown in Table II. The monomer has an active
double bond at each end which is polymerized to form a cross-linked network under
UV irradiation. Because the central part of the monomer is rigid, similar to a liquid
crystal molecule, it is believed the monomer has an alignment similar to that of
the liquid crystal molecules2,33. After LTV illumination, the polymer network has some
degree of orientation similar to the orientation of the liquid crystal when the polymer
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44
Table la. Relevant parameters for the nematic liquid crystal
E48 (EM chemicals)
K-N N-I r| 8n
-19° C 87° C 43.5 (cSt) 0.231
Table lb. Relevant parameters for the chiral compounds
utilized in the experiments
chiral mpt Ch-I PmaterialCE-1 99.5°C 195.5°C 0.15pmCB15 -30.0°C 4.0°C 0.15pm
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45
Table EL The chiral compounds CB15, R1011 and CE1 are mixed in a ratio
of 3:1:3 with a relative concentration of 28% in the nematic E48.
The relative concentrations o f the monomer BAB with the chemical
structure as shown are listed in the table.
H C = C H - . C - 0 - Q ^ p - 0 “ C - C H = C HII IIo o
_________ BAB polymer concentration_(%)__________OO 025 047 072 090 U 2 L40
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46
network was formed. In other words, the liquid crystal influences the orientation of
the monomer, and after polymerization, the polymer network affects the texture for
director configuration33'35.
Samples are prepared by vacuum filling indium tin oxide (ITO) coated glass pieces
separated by 5 micron spacers with the chiral nematic liquid crystal/monomer mixture.
The inner surfaces of the glass have a rubbed polymide layer for parallel surface
alignment of the liquid crystal molecules. With this type of cell, after filling, the liquid
crystal is in the planar texture, which is the perfect cholesteric illustrated earlier in Fig.
2.2a.
To form a multi-domain cholesteric sample, the cell is irradiated with UV light to
form the polymer network. While the sample is irradiated, an electric field is applied
to place the material in the homeotropic state, which produces an anisotropic polymer
network. One result of forming the polymer network in this fashion is to stabilize the
focal conic texture for bistable operation. Another consequence of the polymer
network is that it creates defects in the planar texture so that domains are formed. The
domains provide for wide angle viewing and grey-scale addressing of a flat panel
display.
The following three subsections discuss in detail experiments to determine domain
structure as a function of polymer concentration, UV irradiation time and type of
polymer.
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47
3.2.1 Domain Structure as a Function of Polymer Concentration
Seven samples are prepared as discussed in section 3.2 with polymer
concentrations varying from 0.0 to 1.4% by weight. The specific concentrations and
other data is shown in Table II. The samples are illuminated with UV light at an
intensity of 5 W/cm2 for 45 minutes while biased with an electric field to form an
anisotropic polymer network. Before and after polymerization, the samples are
examined using a Nikon optical microscope with crossed polarizers in both the
transmission and reflection mode at magnifications of lOOx and 400x. Also, reflection
spectra are measured for each sample before and after polymerization. The
measurements are made by illuminating the samples with unpolarized light at 22°
incidence with a 50W tungsten-halogen light source and measuring the resulting
reflection spectra with a Spectrascan PR704 camera.
The top micrograph of Fig. 3.1 shows the typical texture of all samples before
polymerization. The bottom micrographs show the results of examination after
polymerization for two representative samples with 0.47 and 0.72% polymer,
respectively. The dark areas in the micrographs are defect regions primarily created by
the polymer networks and basically represent domain wall boundaries. As shown in
the bottom micrographs of Fig. 3.1, the domains are smaller for the 0.72% sample than
the sample with 0.47% polymer.
The average domain size is determined for all the samples. Domain sizes are
greater than 100 microns for polymer concentrations less than 0.4%. The upper curve
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(b) |- | 20 |im
Fig. 3.1. Top micrograph (lOOx) showing texture before polymerization (a)
and bottom micrographs (lOOx) showing the texture o f samples
with 0.47% (left) and 0.72% (right) polymer concentration (b).
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49
in Fig. 3.2 is a plot o f the average domain size versus polymer concentration with a
line drawn through the data. As shown in the data, as the polymer concentration
increases, the domain size decreases. No reasonable model could be fit to all of the
data. However, as shown in the bottom curve of Fig. 3.2, a quantitative analysis of the
data for polymer concentrations 0.6% and greater shows that the domain size is
inversely proportional to the polymer concentration as:
d = (0.12/x)-5 for 0.6% < x < 1.4% (61)
where d is the average domain diameter and x is the polymer concentration.
Examination of the domain features by optical microscopy shows irregular,
circularly shaped areas o f apparent perfect planar texture surrounded by defects
created by the polymer network. Within a domain, optical microscope examinations
show a single reflected color with no shading. This indicates the domains have a
planar boundary at the top and bottom surface. If the domains had an irregular
boundary, light would be reflected differently at various depths in the sample and thus
produce regions with different shades.
Samples are examined with a scanning electron microscope (SEM) to determine
the structure o f the polymer network and are prepared for SEM analysis by first
removing the liquid crystal and carefully separating the top glass piece from the
bottom one36. SEM examinations of samples prepared in a similar fashion as those
discussed in section 3.2 show discrete areas of large concentrations of polymer
oriented perpendicular to the surface as illustrated in Fig. 3.3. The shape of the areas
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dom
ain
size
50
60
50
30
20
0.4 0.80.6 1.0 1.2 1.4 1.6% p o ly m e r c o n c e n t r a t i o n
20
<uN' t o
Fh' H(0aoX)
0.6 0.8 1.21.0 1.4 1.6% p o ly m e r c o n c e n t r a t i o n
Fig. 3.2. Plots of average domain size versus BAB polymer concentration.
Upper plot has line drawn through data as an aid to the eye. Solid line
in bottom plot is a fit to the data with a function that varies as the
inverse o f the concentration.
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51
Fig. 3.3. SEM micrograph showing approximate cylindrical areas of anisotropically
oriented polymer.
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52
where there is little or no polymer correspond to the shape of the areas of perfect
planar texture identified in the optical microscope analysis.
The SEM analysis indicates the domains are single layer. For multilayer formation,
some polymer is expected to be required to stabilize defect areas forming the layer
boundaries. After removing the liquid crystal for SEM analysis, the polymer required
for multi-layer formation would collapse into the areas surrounded by the large
concentrations of anisotropically oriented polymer. However, as shown in Fig. 3.3,
there is virtually no polymer in these areas indicating the domains are single layer.
Figure 3.4 shows the reflection spectra of the samples with the differing polymer
concentrations after UV illumination. The top curve is the typical reflection spectra
from a sample with no polymer. As shown in these curves, the reflection spectra
change significantly from before, to after polymerization, and there is distinctly
different reflection spectra between samples with different polymer concentrations.
There are changes in shape, magnitude, and peak Bragg reflected wavelengths. These
changes in reflection spectra as a function o f polymer concentration are discussed in
detail in section 3.4.
3.2.2 Domain Structure as a Function of UV Illumination Time
A study is conducted to determine domain structure as a function o f UV
illumination time. Optical examinations and reflection spectra are measured for two
samples with polymer concentrations of 0.63 and 1.3%, respectively, after the times
indicated in Table III.
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refl
ecti
vit
y
53
in c id e n t and d e te c te d ligh t un po lar izedin c id e n t l ig h t a n g le 22
0.5
0.0 % p o ly m e r c o n c .
0.250.4
0.47
0.30.72
0.90.2
1. 12
0.0400 500 600 700
w a v e le n g th (n m )
Fig. 3.4. Reflection spectra from samples with different polymer concentrations.
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54
Table III. A listing o f times at which samples are removed from
UV illumination. Samples are then examined with optical
microscopy and then reflection spectra is measured.
BAB polymer concentration (%)
time(minutes)
0.63 and 1.3 0.00.51.01.52.05.010.030.0
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55
Figure 3.5 shows micrographs of the texture for the two samples at 0.5 minutes, 2
minutes and 30 minutes UV illumination time, respectively. The texture of these
samples with little UV illumination time is similar to the samples with low polymer
concentrations. As UV illumination time progresses, the domain size decreases.
Figure 3.6 shows the plot o f average domain size versus UV illumination time. In the
first two minutes, the domains rapidly approach the size identified in samples with
extended illumination time. In the first two minutes, the curves are nearly linear on the
log plot of Fig. 3.6 indicating an exponential process. From 2 minutes to 30 minutes
there is a continued slight decrease in domain size. The curves are also linear from 2
minutes to 30 minutes but with a much smaller slope than in the first two minutes of
UV illumination time. This indicates a different exponential process after the initial
formation for the final structure of the domains. However, because it is difficult to
clearly distinguish, the entire polymerization could be a multiple exponential process in
time. The final domain size of the sample with 0.63% polymer is approximately 12
microns, larger than the approximate 4 micron final size for the sample with 1.3%
polymer. The final domain sizes for the two samples are consistent with the values
found in section 3.2.1.
Figure 3.7 shows the reflection spectra for the samples as a function of UV
illumination time. The curves show a change in shape, wavelength and intensity. For
short UV illumination times, the curves are consistent with the reflection spectra
measured for the samples with the low polymer concentration samples of section
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Fig. 3.5. Micrographs (lOOx) showing the texture of samples with 0.63% and
1.3% BAB polymer concentration after (a) 0.5, (b) 2.0 and (c) 30.0
minutes of UV illumination.
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57
cuN
C• rH
BoX)
<uW)c0QJ>td
(dowuoo
% p o ly m e r c o n c e n t r a t io n
10 20 30 40
UV e x p o s u r e t im e (m in u te s )
Fig. 3.6. Plot of domain size versus illumination time showing the domain size
decreases as the UV illumination time increases.
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refl
ecti
vity
re
flec
tiv
ity
58
in c id e n t and d e te c to r an g le 22 (u n p o lar ized light)0 .5
0.63% polym er conc.no polym er0.0
UV exposure tim e (m in) _0.41.5
5.00.3 10.0
/ 30.00.2
0.1
0.0400 500 600 .
w a v e le n g th (nm )700 800
0.5no polym en 1.3% polym er conc.
UV exposure tim e (m in)0.00.4
0.50.3
5.02.00.2
30.
0.0400 500 600 700 800
w a v e le n g th (n m )
Fig. 3.7. Reflection spectra as a function o f UV illumination time.
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59
3.2.1. For extended UV illumination times the curves are consistent with the
reflection spectra from samples with similar polymer concentrations from section
3.2.1.
3.2.3 Domain Structure as a Function of a Different Monomer
An examination of domain structure using a different monomer is conducted.
The monomer used is a laboratory synthesized derivative of BAB called BAB6. This
monomer is similar to BAB but has the reactive double bonds attached to the end of
two flexible six carbon chains extending from the central monomer core.
Samples are prepared as before, but with the monomer BAB6 substituted for BAB
at concentrations of 0.38, 0.8, and 1.1%, respectively. Figure 3.8 shows the texture
of the samples after polymerization. There is a slight change in domain features as
compared to the BAB samples. The domains o f the BAB samples are irregularly
shaped circular regions, while for the BAB6 samples, the domains appear to be
irregularly shaped rectangular areas. Figure 3.9 is a log plot o f average domain size
versus BAB6 concentration. Because this plot is not completely linear, the domain
size decrease is only approximately exponential with polymer concentration. SEM
examinations of similar samples after the liquid crystal had been removed indicates
nearly vertical fiber-like strands extending from the top to the bottom. It is suspected
that the flexible chain o f this monomer accounts for the difference in polymer structure
and domain shape than that found for the samples made with BAB. The extended
flexible chain o f the BAB6 monomer could facilitate cross-linking around the rigid
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60
(a)
(c)
Fig. 3.8. Micrographs (lOOx) showing the texture of samples with (a) 0.38,
(b)0.8 and (c) 1.1% of the BAB6 monomer.
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aver
age
dom
ain
size
(j
um)
0
20
0
o00.0 0.2 0.4 0.6 0.8 1.0 1.2
% BAB6 p o ly m e r c o n c e n t r a t io n
Fig. 3.9. Log plot o f average domain size versus BAB6 concentration.
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62
liquid crystal molecules, and thus reduce diffusion as a growth mechanism. This
would then tend to result in the quick formation of a complete network in one (in this
case vertical) direction, as opposed to the accumulation of polymer in discrete regions.
Figure 3.10 shows the reflection spectra of the three samples made with BAB6
before and after polymerization. There are significant changes in shape, wavelength
and intensity. This research deals with the change in reflective properties as the result
o f different BAB polymer concentrations and thus no detailed analysis of the reflection
spectra from the BAB6 samples is presented
3.3 Physical Model of Domain Structure
As shown in section 3.2, changes in polymer properties (concentration, etc.) results
in changes in the reflection spectra. Physical analysis shows the polymer changes
resulted in changes in the domain structure. The theoretical development discussed in
chapter two to describe the reflective properties is based on the domain structure.
Consequently, to calculate the reflective properties of imperfect cholesterics, a detailed
knowledge of the structure of the domains is required.
Analysis of the texture o f samples with the BAB polymer by optical microscopy
discussed in section 3.2.1 shows approximate circular shaped areas o f planar texture
surrounded by large defect regions. SEM examinations of similar samples with the
liquid crystal removed shows significant polymer concentrations only in the defect
areas identified in the optical microscope examinations. In the areas corresponding to
the defect regions, the polymer primarily extends from the top to the bottom of the
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refl
ecti
vity
63
incident and detector angle 22 (unpolarized light)0.5
% BAB6
0.4 0.38a
0.38b
0.3
0.8a0.2
0.1
400 500 600 700
wavelength (nm)
Fig. 3.10. Reflection spectra of samples with different BAB6 concentrations
before and after polymerization.
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64
sample with little extension in the horizontal direction. The material is polymerized
with the liquid crystal molecules oriented in a vertical direction because of the applied
electric field, thus the observed results are consistent with the way the samples are
prepared.
The model for the structure of the domains (see Fig. 3.11b) then is one where
there are approximately cylinder-like areas of nearly perfect planar texture extending
from the top to the bottom of the sample. The cylinder-like domains are separated in
the horizontal direction by defect areas created by the polymer network. The physical
analysis thus determines the size, shape and texture of the domains. The helical axis
orientation of a particular domain, the pitch of a particular domain and the
corresponding distribution of these quantities in a sample can be (and, in fact, as
shown in the following sections are) affected by the polymer network.
The exact nature of anchoring to the polymer network and the cause of the tilt in
helical axis orientation are the subject of future investigation.
3.4 Measurement and Model for Reflected Intensity
3.4.1 Introduction
Optical observations of samples with polymer show a much greater viewing
angle than samples without polymer. Also, it is generally found that the higher the
polymer concentration, the larger the viewing angle. The following is a qualitative
explanation for this observation.
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65
(a)
v v y \
(b)-> incident wave -► reflected wave
Fig. 3.11 Schematic o f perfect cholesteric (a) and schematic of imperfect
cholesteric created by the polymer studied in the experiments (b).
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66
Consider a sample with the helical axes all oriented in the same direction (i.e., a
perfect cholesteric). Due to the one dimensional periodicity of the cholesteric
dielectric function, light can only be Bragg reflected into one angle. This reflected
angle is equal to the angle the incident light makes with the helical axis ( Fig. 3.11a).
However, for an imperfect cholesteric, there can be domains with the helical axes of
the chiral nematic liquid crystal oriented in many different directions. Consequently,
for a given incident angle, light can be Bragg reflected in many different directions and
thus greatly improve the viewing angle (Fig. 3.11b).
3.4.2 Measurement of Reflected Intensity versus Polymer Concentration and
Detection Angle
Measurements are conducted to determine the reflected intensity versus
detection angle for the samples with different polymer concentrations. From these
measurements and using a model developed in the next section (3.4.3), the distribution
function describing the orientation of the helical axes as a function of polymer
concentration is established.
The measurement set-up is shown in Fig. 3.12. The samples are illuminated with a
50W tungsten-halogen light source at an incident angle of 48 degrees with respect to
the sample normal. Reflected luminance (luminance is the integrated reflected
intensity times the photopic response weighting function) is measured at different
angles in the azimuthal plane with a Spectrascan PR704 camera. The samples with
polymer concentrations varying from 0.0 to 1.4% as shown in Table II are measured.
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67
detector
sample
lightsource
x
Fig. 3.12 Geometry of measurement set-up where p is the incident light
angle, <|> the azimuthal and 6 the polar angle of the detector.
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68
The camera is swept through a total angular range of 68 degrees. The first
measurement is taken at 48 degrees, the next at 45 degrees, then 42 degrees and then
40 degrees, while subsequent measurements are taken in 5 degree intervals to -20
degrees.
Figure 3.13 is a log plot of luminance versus detector angle for four representative
samples. As shown in this data, at the specular angle 48 degrees, the sample with the
least polymer has the highest luminance, the sample with next lowest polymer
concentration has the next highest luminance and so on. However, at the detector
angle of 40 degrees, the sample with 0.47% polymer has the largest luminance value.
And at angles far from the specular reflection angle of 48 degrees, the samples with
the largest polymer concentrations have the highest luminance values.
As mentioned, at the specular reflection detector angle, the lower the polymer
concentration, the higher the reflected luminance. At low polymer concentrations,
there is little misorientation of the helical axes (i.e., most of the axes are oriented
perpendicular to the sample surface). So, almost all domains of the sample will reflect
only at the specular reflected angle. However, for samples with higher polymer
concentrations, some of the domains will have axes misoriented from the sample
normal, thus decreasing the total number that are oriented perpendicular to the
surface. As a consequence, the higher polymer concentration samples will reflect less
light in the specular direction.
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69
"d
03OPicdPi
• r* H
0p)
% p o ly m e r
. 0 .2510
0 .47
0.720)13aCO
1.4<30o
0 .7 2
0 .4 710
0 .25
10 0 1020 20 30 40 50 60
azim uthal angle (deg)
Fig. 3.13. Log plot of luminance versus azimuthal angle for four samples
with different polymer concentrations. Vertical dashed lines refer
to replot of data in Fig. 3.14. Solid lines drawn as an aid to the eye.
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70
As the polymer concentration increases, the reflected intensity at wide angles
increases (i.e., an improved viewing angle) because o f the greater misorientation in the
helical axes. To clearly emphasize this point, the data in Fig. 3.13 is replotted along
the dashed vertical lines at the detector angles o f 40, 35 and 30 degrees, respectively,
and shown in Fig. 3.14 as plots of reflected luminance versus polymer concentration
for the three different detector angles.
As shown in the left hand plot of Fig. 3.14, at the detector angle of 40 degrees (i.e.,
8 degrees from the specular reflection angle), the sample with 0.47% polymer now has
the highest reflected luminance. As shown in the remaining two plots of Fig. 3.14, at
even wider angles, the samples with higher polymer concentrations have the largest
reflected luminance values.
3.4.3 Model of Reflected Intensity versus Polymer Concentration and Detection
Angle
A simple model is developed to describe the measured data as being the
result of two effects: the increased viewing angle resulting from the increase in
distribution o f helical axis orientation with increasing polymer concentration; and the
decrease in volume fraction of Bragg scatterers with increasing polymer concentration
because the polymer network creates defect areas which do not Bragg reflect light.
The volume fraction of non-Bragg scatterers is the ratio of the volume of non-Bragg
scatterers, V ^, to the total volume, V, which is then V^/V. The volume fraction of
Bragg scatterers is then VB=1-VNB/V.
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71
2000{0=30 degrees{0=40 degrees ^=35 degrees
1500cvi
oj 1 000
A A
0.0 0.5 1.0 0.0 0.5 1.0 0.0 0.5 1.0
p o l y m e r c o n c e n t r a t i o n % (x)
Fig. 3.14. Plot o f luminance versus polymer concentration for the three detector
angles 40, 35 and 30 degrees, respectively, which are indicated
by the dashed lines in Fig. 3.13.
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72
As the polymer concentration is increased, increases resulting in a decrease of
the overall reflected intensity. This effect is apparent in the data shown in Fig. 3.13 for
the reflected luminance values at wide angles for the higher polymer concentration
samples. If the reflected luminance were only the result of helical axis misorientation,
then the sample with 1.4% polymer should have the highest reflected luminance. But
as shown in the data, the reflected luminance is comparable to the sample with 0.72%
polymer concentration. The decrease in the Bragg reflected intensity as the result of a
decrease in volume fraction of Bragg scatterers accounts for this result.
The model is described more quantitatively in terms of the total reflected intensity,
I(x,y) of the detected light at <|>, as being directly proportional to the product of the
two effects previously discussed
I(x,y) a v(x)f(x,y) (62)
where
r ( H ) / 2 (63)
and where x is the polymer concentration, <|> is the detector angle, p the incident light
angle and y the helical axis orientation angle, all with respect to the sample normal.
Also, v(x) is the volume fraction of Bragg scatterers and f(x,y) is the fractional number
of helical axes oriented at y for a given polymer concentration x.
The mathematical description o f the decrease in Bragg reflected intensity due to a
polymer concentration increase can be developed by several approaches. In one
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73
approach, physical arguments about the form of the function can be used to develop
v(x), and in another approach, geometrical arguments can be used.
The first approach begins by investigating the form of v(x) for a sample with no
polymer. For this situation, there are few defects so the entire volume is essentially
composed of Bragg scatterers and thus v(0)=l. As the polymer concentration
increases, then v(x) decreases. Using a Taylor series expansion and retaining only the
lowest order term because the polymer concentrations used are small results in
v(x)=l-Bx (64)
where B is a parameter fit to the data.
Equation (64) can also be developed by modelling the domains as cylinders as
illustrated in Fig. 3.15. From the geometry, the volume of a given domain, labelled i,
is
Vi =jcr2t (65)
where r = d/2 and d is the domain diameter and t is the thickness of the sample. Then
the number of domains per unit volume is nv = 1/V; . Thus the total defect (or
non-Bragg scattering) volume for the sample is
Vnb = V(l/7rr2t)(27crht + jrfft) = V(2h/r + hVr2) (66)
where h is defined in Fig. 3.15. Using the experimental result from section 3.1.1 that
domain size is inversely proportional to the concentration, (0.12/x)-5, gives
= V(4hx/H + 4hV/H2) (67)
where H=0.12-5x, Because x is a small number, to first order then,
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74
defecti£giQ12_planartexture
defect
planartexture
defect area accounted for with fill factor
Fig. 3.15. Schematic representation of the geometry of the domains created
by the polymer used in the experiments.
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75
Vne = V(4hx/H) (68)
and the volume fraction of non-Bragg scatterers is then
Vnb/V = V(4hx/H)/V = 4hx/H. (69)
Using this cylindrical geometry description does not encompass the entire defect
area. Considering the maximum packing fraction, the fill factor is given by
So, accounting for the fill factor by multilplying the expression in Eq. (69) by the
inverse o f Eq. (70) and setting (l/f)(4h/H)=B, then the volume fraction of Bragg
scatterers is
which is the same result as derived in the first approach. In this second approach,
numbers from experimental data can be used to actually determine what the
coefficient, B, in Eq. (71) should be. Substituting the measured values for h
determined from the optical microscope examination (h=0.5|j.m) and the coefficient, H,
from Fig. 3.2, results in a value of approximately 40 for B. An exact determination of
B requires development of more sophisticated models.
A simple description for the distribution in orientation of helical axes, f(x,Y), can
also be derived. With no polymer, almost all helical axes are oriented perpendicular to
the sample surface. As the polymer concentration is increased from zero, domains are
created with helical axes slightly misoriented from the normal, and a few domains with
helical axes oriented at wide angles. At the high polymer concentrations, there is a
f=(7trh+7rh2/2)/(3 ,/2(r+h)2-7tr72) (70)
Vb = 1 - V nbA^=1-Bx (71)
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76
large number of helical axes that are slightly misoriented, and a decreasing number out
to wider and wider angles. Due to the physical symmetry, there are equal numbers
oriented on both sides of the normal to the surface.
One mathematical function that describes this situation is a Gaussian distribution
(Other functions also similarly describe this situation such as a Lorentz function;
however, the Gaussian distribution gives the best results when comparing data to the
model.),
™ = <72>
Figure 3.16 shows the Gaussian distribution as a function o f the variable y for
different standard deviation (a) values. As shown in Fig. 3.16, an increase in the
standard deviation mimics the physical effect of the increasing misorientation in helical
axes with increasing polymer concentration. Consequently, the Gaussian distribution
can be a reasonable representation of the helical axis orientation, where the effect of
the polymer is contained in the standard deviation.
For no polymer, the standard deviation should be zero (<J=0), which makes the
Gaussian function a delta function (i.e., all helical axes are oriented perpendicular to
the surface). As the polymer concentration increases, the standard deviation increases.
One approximation to describe this situation is to write a series in powers of the
polymer concentration asoo
o (x ) = Z c ,x = c 0 + C i X + C 2 X 2 + .... (73)
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f(y)
(a v
)
77
2 .5
2.0
<7 = 5
5
0
cr=
0.5
0 . 0 l— - 6 0 - 4 0 - 2 0 0 20 40 60
7 (a .v .)
Fig. 3.16. Gaussian distribution as a function of the variable y
for different standard deviations.
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78
Because the polymer concentration is a small number, then higher order terms can be
neglected and
c (jc) =c0 + cix (74)
At x=0, then c(x)=0, so c0 =0 and the equation for the standard deviation becomes
c (jc) = cix = Gc (75)
where C is a parameter found by fitting the model to the data.
Taking the above into account, the equation f(x,y) that describes the fraction of
helical axes oriented at an angle y as a function of polymer concentration for a given
incident light angle (i,which will Bragg reflect light into the detector angle <{> is,
-Y2M i ) = £;e*c* (76)
Now, the complete equation to describe the reflected intensity as a function of
polymer concentration, incident light angle and detector angle can be written
I ( x , y ) = A ^ - e ^ (77)
where the terms A, B, and C are fitting parameters.
3.4.4 Comparison of the Model to the Data
Figure 3.17 shows the data from Fig. 3.14 where the solid line is the fit of the
model to the data. The fitting parameters for a particular measurement are included on
the respective plot. The estimated error in the measurements and fitting parameters is
15%. As shown in Fig. 3.17, there is a reasonably good fit of the model to the
measurements.
The average values for the fitting parameters determined from the three sets of
measurements are A=135, B=43.3 and C=11.3. The two important parameters are B
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79
2000A= 160
B =501500C= 12
1000
500
CM a 8ooC= 11
400
600 B=40
C= 11400
200
0 1 2p o ly m e r c o n c e n t r a t i o n (%)
Fig. 3.17. Comparison of measured data (points) to the model (solid line).
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80
and C where B determines the amount of light lost due to scattering and C the
standard deviation o f the domain orientation distribution. Also, it is found that the fit
is somewhat less sensitive to changes in the fitting parameter B than C.
The average value for B (43.3) found in fitting the model to the data indicates there
is approximately a 50% decrease in reflected light due to scattering by defects at the
higher polymer concentrations. Furthermore, this average B value is comparable to
the value of 40 determined from geometrical considerations.
The standard deviation values as a function of polymer concentration are shown in
Table IV. The values range from zero with no polymer, to 3.0 degrees for 0.47%
polymer, to 9.1 degrees for 1.4% polymer.
3.5 Measurement and Model of Reflection Spectra versus Polymer Concentration and
Detection Angle
3.5.1 Measurement of Reflection Spectra
The measurement geometry is similar to that shown in Fig. 3.12. In addition,
a polarizer was placed after the light source to produce a polarized light. Another
polarizer was placed in front of the PR704 camera to select the n polarized component
of the reflected light. The crossed polarizers reduced the effect of reflections from the
glass surface of the sample. An iris was placed between the sample and the camera
and stopped down to produce a collection angle of less than one degree.
The solid lines in Figs. 3.18 and 3.19 show the results of measurements on selected
samples with different polymer concentrations. For samples with low polymer
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81
Table IV. The table shows standard deviations as a function of polymer
concentration from the fit of the model to the data.
polymerconcentration
(%)
standard deviation (a)
(degrees)0.00 0.00.25 1.6
0.47 3.0
0.72 4.70.90 5.8
1.12 7.2
1.40 9.1
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82
d e t e c t o r a n g le
1.12p o ly m e r c o n c e n t r a t i o n (%)
0 .7 20.00.4
0.030.04 -
0.2 0.02
0.020.01
0.0
0.015
Sj 0.05 0.02 0.010IDK
0.005
0.00
0.0150.008
250.05 0.0100.005
0.0050.003
0.00400 600 800 400 600 800 400 600 800
■ w avelength (n m )
Fig. 3.18. Measured (solid line) and calculated (dashed line) reflection spectra
for the incident light angle of 5 degrees and the detector angles indicated, a polarization incident and it polarization detected
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83
detector anglepolym er concentration (%)0.0 1.120 .7 2
0.4
0.080.30.02
220.2
0.04
0.0
0.02
0.02 32
0.01
- V i__0.00
0.05 0.0 0.01 4 2
0.00400 600 800 400 600 800 400 600 800
wavelength (nm)
Fig. 3.19. Measured (solid line) and calculated (dashed line) reflection spectra
for the incident light angle of 22 degrees and the detector angles indicated,
a polarization incident and it polarization detected
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84
concentrations, there is little reflected intensity at wide detector angles. Also, these
samples show peak and valley details around the center Bragg wavelength, which are
more emphasized for the 22 than 5 degree incident light angle. There is a washing out
of the fringes and a smoothing of peak and valleys for samples with higher polymer
concentrations.
3.5.2 Model of Reflection Spectra Utilizing 4x4 Berreman Method
The following utilizes the general procedure discussed in chapter two and the
results from the preceding sections of chapter three to calculate the reflection spectra
from the samples listed in Table II as a function of polymer concentration.
Because the domains appear to extend entirely from top to bottom, only one layer
need be considered in Eq. (45) from chapter two. This effectively eliminates the
matrix for multiple reflections between domains along the vertical direction. The
possibility o f light entering one domain at oblique incidence and propagating into
another layer is unlikely if the cell thickness is considered to be small compared to the
lateral dimensions of the domain. Assume light is incident at the edge of a domain.
For light incident on the display at 22 degrees, then light is incident on the liquid
crystal material at 14 degrees after taking into account the refraction at the glass-air
interface. The lateral distance the light travels is 5 p.m/tan(76°) which equals 1.25 (xm.
Optical microscope analysis indicates the domains are separated by defects with a
distance of around 1.25 pm. Consequently, any light that propagates out of a domain
will not enter another domain and can be neglected.
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85
Because the domains have a planar geometry, the 4x4 Berreman method to
calculate the r, and t, matrices o f Eqs. (48) and (49) from chapter two can be used.
The computer program utilized here for the 4x4 Berreman method was developed in
part by Dr. Doyle St. John31.
As before, a model is assumed in which there is a distribution in the orientation of
domains. Also, there is a possible distribution in pitch37-38. Variations in pitch due to
surface undulations can be neglected because the variations occur on the order of
1.0mm, which is larger than the area from which reflection spectra are measured.
Variations in pitch due to the polymer network can occur as will be shown.
Consequently, an appropriate averaging over pitch variations is required.
The domains are considered as an uncorrelated ensemble of Bragg scatterers
because there is no explicit relation in orientation and pitch between domains. Thus
averaging is only required over the various configurations a domain can have and
adding the resulting intensities weighted by the appropriate distribution function.
For a given incident light and detector angle, the reflection spectra is calculated for
various pitches, with the resultant reflectivity value for each pitch calculation
multilplied by the appropriate pitch weighting function. The resultant reflectivity value
from these calculations is then multiplied by the appropriate orientation weighting
function, where the orientation angle of the helical axis is determined by the incident
light and detector angle. This calculation can be written as
R{x,y) =jR(y,P)Ax,y)q(x,P)dP (78)
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86
where R(y,P) is the reflection spectra calculated by the 4x4 Berreman method, f(x,y) is
the fraction of helical axes oriented at a given angle y, q(x,P) is the pitch weighting
function, x the polymer concentration and P is the pitch.
Reflection spectra are calculated for light with a polarization incident at angles of 5
and 22 degrees with respect to the sample normal and detection of the n polarization
component of the reflected signal at the specular angles of 5 and 22 degrees and angles
of the specular angle plus 10 and 20 degrees, respectively for each incident light angle.
The Gaussian distribution from section 3.4.3, f(x,y), and appropriate standard
deviation determined in section 3.4.4 is used for the distribution in orientation of
helical axes as a function of polymer concentration. Another Gaussian distribution is
used for the variation in pitch-V-Pq)2
q M = ̂ e (79)
Standard deviation (op) values of 0.0 are used for the low polymer concentration
samples, 0.8%P0 are used for the medium polymer concentration samples and a
standard deviation of 6%P0 for the higher polymer concentration samples, where P0 is
the natural pitch of the material.
The dashed lines in Figs. 3.18 and 3.19 show the results of the calculations for
three different (low, 0.0%, medium, 0.72%, and high, 1.12%) polymer concentrations.
The calculations show greater reflected intensity at the wider detection angles for the
higher polymer concentration samples, as expected.
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87
The reflection spectra for no pitch variations have distinctive peaks and valleys
around the center Bragg wavelength in addition to large fringes at the wings of the
Bragg reflected wavelength range. As the pitch variation is increased, the fringes are
washed out and there is a smoothing o f the reflection spectra at all wavelengths. This
smoothing of the reflection spectra for a given pitch variation is slightly greater for the
5 degree incident light angle calculations as opposed to those at 22.
3.5.3 Comparison of Calculated to Measured Reflection Spectra
As shown in Figs. 3.18 and 3.19, there is excellent agreement between the
measured and calculated reflection spectra. In particular, the pronounced peaks and
valleys around the center Bragg wavelength for the incident light angle of 22 degrees
calculated from theoretical considerations are found to occur experimentally in almost
a one-to-one correspondence. Based on this agreement, it is concluded the theoretical
development of the physical phenomena investigated in this research represents a good
description of the reflection properties from polymer modified imperfect cholesteric
liquid crystals.
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Chapter 4
Illumination and View Angle of Reflective Cholesteric Displays
This chapter discusses the effect different illumination and observation conditions
have on the display properties o f chiral nematic liquid crystal material stabilized with a
polymer network. Display properties investigated are reflected luminance, contrast
ratio, hue, color quality and viewing angle. The model developed in chapter 3 is
expanded to describe the measured display properties and analysis of the data
determines optimal illumination/detection conditions.
4.1 Introduction
As shown in chapter three, the introduction o f a polymer network into a chiral
nematic liquid crystal creates a multi-domain CLC. The structure of the domains
created by the preparation method discussed in section 3.2.1 results in an improved
viewing angle as discussed in section 3.4.2. The inclusion of a polymer network also
results in the improvement of many other display properties40,41. These properties, and
their dependence on illumination/detection conditions are examined in this chapter.
Reflective cholesteric displays are prepared in the same fashion as the samples
discussed in section 3.2.1., however, with a polymer concentration that results in
optimal color and spatial uniformity across the display in the planar state, in addition to
88
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89
creating a weakly scattering, stable focal conic state. Samples with too low a polymer
concentration lack spatial uniformity and have an unstable focal conic state. Samples
with too large a polymer concentration lack good color quality and are no longer
bistable.
Two samples with suitable polymer concentrations for good color and functional
bistable switching are selected for detailed measurements on their display properties as
a function of illumination/detection angles. One sample had the chiral concentration
adjusted to reflect green, the other yellow with polymer concentrations o f 0.9 and
0.78%, respectively. The back of the samples are treated to provide a black
background so that in the focal conic state the display appears black. Depending on
how the electic field is applied and removed, the material can be stabily placed in either
the planar or focal conic states by a high or low field pulse, respectively.
4.1.1 Measurement Conditions
Reflected luminance is measured from a sample when the material is in the
imperfect planar texture. Luminance is the integrated reflected intensity times the
photopic response weighting function. Luminance measures the light actually
perceived by the eye. For example, two intensity units of red light do not appear as
bright as two intensity units o f yellow light because o f the photopic response of the
eye. The luminance measurement takes this into account. The photopic response
function is approximately Gaussian in shape and peaks at around 550 nm.
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90
The contrast ratio is defined here as the luminance measured in the reflecting state
divided by the luminance in the scattering state. The higher the number, the better the
contrast. Typical contrast ratios are 7 to 1 for newspapers and 20 to 1 for high quality
print. Viewing angle is measured and reported here as the angular width over which
the contrast ratio falls to half its maximum value.
Color is determined by measuring the chromaticity coordinates. These numbers
indicate the hue and saturation (i.e., color quality) of the reflected color. The numbers
are displayed on a chromaticity diagram.
The display properties are measured using the geometry shown in Fig. 4.1a. The
samples are illuminated at four different incident light angles of P = 10, 29, 48, and 65
degrees, respectively, with a 50W tungsten-halogen light source confined to the x-y
plane. Due to refraction of the light by the air-glass interface, the angle between the
incident light angles and the sample normal as seen by the liquid crystal material are 6,
18, 30 and 37 degrees, respectively (Fig. 4.1b) as calculated using the standard Fresnel
equations.
For a given incident light angle, the display properties such as reflected luminance
are measured with a Spectrascan PR704 camera rotated in both azimuthal, <|), and
polar, 0, angles. The azimuthal angle range is from -30 to 85 degrees and the polar
angle range is from -10 to 30 degrees.
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91
detector
C 3 .sample
lightsource
(a)
incident light
y y
n
(b)
Fig. 4.1. Measurement geometry (a) and the effect of refraction on the
incident light as a result of the air-glass interface (b).
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92
4.2 Reflected Luminance Measurements
4.2.1 Reflected Luminance Measurements
Figure 4.2 shows the results of the measurements with the camera fixed in the
zero degree (8=0) polar plane and rotated through a range of azimuthal angles from
-30 to 85 degrees. The upper set of curves is reflected luminance from the yellow
sample and the lower set o f curves from the green sample.
As shown in this data, there is a near symmetry in reflected luminance about the 10
degree azimuthal angle for the samples illuminated with a 10 degree incident light
angle.
However, there is an increasing asymmetry in reflected luminance about the
specular reflected azimuthal angle for increasingly higher angles of incidence. In
particular, at the larger angles of incidence of 48 and 65 degrees, the reflected
luminance broadens towards azimuthal angles less than the specular reflected angle
and there is a relatively sharp drop in reflected luminance at azimuthal angles beyond
the specular reflected angle. As an example, for the reflected luminance from the
yellow sample at an incident light angle of 65 degrees, the luminance at the azimuthal
angle of 65 degrees (i.e., the specular angle) is around 800 cd/m2, at 50 degrees, 800
cd/m2 and 80 degrees, 500 cd/m2, respectively.
For both samples, the highest reflected luminance value (selected either from the
individual azimuthal angle measurements for a given incident light angle or from the
area under a given curve) is obtained for an incident light angle of 10 degrees. There
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93
incident light angle(deg)
6000 yellow-sam ple 29
<u 4000
48
3 2000
65.»
- • • '0 L_ - 4 0 - 2 0 0 20 40 60 80 100
azim uthal angle (deg)4000
incident light angle
29 (de§)
greensample
3000
oj 2000
48
65
0- 4 0 - 2 0 0 20 40 60 80 100
azim uthal angle (deg)
Fig. 4.2. Reflected luminance measurements as a function of azimuthal detector
angle for the incident light angles shown from the yellow sample (upper)
and the green sample (lower). Solid lines drawn as aid to eye.
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94
is a decrease in the maximum reflected luminance between samples illuminated at 29
degrees as compared to 10 degrees. This trend continues to the largest incident light
angle o f 65 degrees.
The luminance for the yellow sample is greater than that for the green sample
because of the broader range of wavelengths reflected by the yellow sample
(8?i=X8n/n) and the photopic response of the eye.
4.2.2 Reflected Luminance about the Zero Degree Polar Plane
For these measurements, the sample is illuminated at incident light angles of
10, 29, 48, and 65 degrees, respectively. For each incident light angle, the camera is
set at a polar angle of -10, 0, 10, 20 or 30 degrees, respectively. Having fixed the
incident light and the polar detection angle, the camera is then swept in azimuthal
angle. Figure 4.3 shows the results for the case where the incident light angle is fixed
at 29 degrees to illuminate the sample that reflected green.
As shown in Fig. 4.3, there is a symmetry in reflection about the zero degree polar
plane as indicated by the similarity in reflected luminance for the -10 degree and 10
degree polar angle measurements. Similar results are found in other measurements at
different incident light angles for both samples.
4.2.3 Physical Model for Measured Reflected Luminance Results
A physical model is developed to describe the measured reflected luminance
from the two samples as being the result of two effects. First, there is a decrease in
reflected intensity as the angle between the incident light and helical axis orientation
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lum
inan
ce
(cd
/m
95
3500
polar angle3000
2500w-1
2000
1500
20
30500
- 2 0 0 20 40 60 80
a z i m u t h a l a n g le (deg)
Fig. 4.3. Reflected luminance measured as a function of azimuthal and polar
angle for an incident light angle of 29 degrees. Solid line drawn
as an aid to the eye.
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96
increases. The physical cause for this decrease is that only the projected fields on the
x-y plane contribute to Bragg reflection1. Second, there is a decrease in reflected
luminance at wide detection angles with respect to the specular angle due to the
gaussian distribution of helical axes about the sample normal.
Based on the sample preparation conditions and the results o f chapter 3, it is
expected that the helical axis orientation distribution about a given plane should be
symmetric. So, the plane of incidence defined by the illuminating source is a mirror
plane o f symmetry. For every helical axis oriented upward at some angle with respect
to the plane of incidence (e.g., helical axes 1 and 2 in Fig. 4.4a), there is a
corresponding helical axis oriented downward (e.g., helical axes 1' and 2').
Consequently, irrespective of the incident light angle, there is expected a symmetry in
reflection about the plane of incidence for a given azimuthal angle. This symmetry is
observed as discussed in section 4.2.2.
The overall measured reflected luminance is greater for light incident at 10 degrees
than larger incident light angles as shown in the data of Fig. 4.2. This result is
explained in the following. The distribution in orientation o f axes is shown to be
largest at the sample normal and thus the greatest fraction of light due to helical axis
orientation will be reflected from these domains. The reflected intensity is also an
increasing function of decreasing angle. Thus there is a greater reflected luminance
for light incident at 10 degrees than larger incident light angles from domains with axes
oriented along the sample normal because the angle between the incident light and the
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97
helical axis 1 helical axis 2
incident light
helical axis 1' (a) helical axis 2'
helical axis 1 helical axis 2
reflected light from axis 1
incident light
reflected light from axis 2
^ specular reflected light^ ^decreasing
(b) azimuthal angle
helical axis 1
reflected light from axis 1
helical axis 2
reflected light from axis 2
incident light
(c)
specular M reflected light
decreasing azimuthal angle
Fig. 4.4. Schematic representation of helical axis orientation and incident light angle.
The helical axis orientation is the same for diagrams (b) and (c) while the
incident light angle differs between (b) and (c).
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98
helical axes is smaller for smaller incident angles. While the angle will decrease
between the incident light for large incident light angles and domains with large axis
misorientation, the number of these domains is small and thus generally, the reflected
luminance from these domains will be less than light reflected from domains with axes
oriented normal to the sample surface.
For light incident at or near the sample normal, there is a symmetry in the angle
between helical axes about the specular reflected angle (Fig. 4.4b). As a result, a
symmetry is expected in the reflected luminance for this case and is observed in the 10
degree, and to some extent in the 29 degree, incident light angle measurements
discussed in section 4.2.1.
When the incident light angle is far from the sample normal, the angle between the
light source and the helical axis orientation varies from a larger value to a smaller
value when moving towards the direction of incidence through the specular reflected
angle (Fig. 4.4c). As shown in Fig. 4.4c, the angle between the incident light and
helical axis 2 ( |) is greater than that for 1 (Q. As mentioned, the reflected intensity is
an increasing function o f decreasing angle between the incident light and a given
helical axis. So, for light incident at large angles with respect to the sample normal,
moving from azimuthal detection angles near the specular angle in to smaller angles,
the angle between the incident light and a given helical axis will decrease and the
reflected luminance would increase. However, because there is a gaussian distribution
in orientation, there are a decreasing number of domains with increasing axis
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99
misorientation. Thus, moving from azimuthal detection angles near the specular angle
in to smaller azimuthal angles, the number of domains that can Bragg reflect light into
the smaller angles would decrease and thus the reflected luminance would decrease.
These two competing effects cause the asymmetry and broadening in reflected
luminance from samples illuminated at the wider angles as observed in the measured
data for the incident light angles of 48 and 65 degrees (Fig. 4.2).
A model is developed to calculate the reflected luminance as the product of the
two effects just discussed: one, the change in reflected intensity as the angle between
the incident light and helical axis orientation change; and second, the fractional amount
of helical axes oriented at a given angle to Bragg reflect light into the detector at some
angle <f>.
Reflected intensity, I(P,<|>), from a CLC in the plane of incidence where P is the
incident angle and <|> the detector angle is quantitatively determined by using the 4x4
Berreman method, r(p,<j>,A.), to calculate the reflection spectra for a given P and <}> and
integrating over wavelength as
I(p,<|>)~Jr(P,<|>,A.)<ft (80)
From chapter 3, the distribution in helical axis orientation is a function of 7 where
the incident angle (P) and detection angle (<|>) as shown in Fig. 4.1 and after
appropriate corrections for the air-glass interface define y = (P - <p)/2. The
distribution is also a function of polymer concentration, x. The fraction of light Bragg
reflected at some angle <)> for a given incident light angle p and including the decrease
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100
in reflected intensity due to defects is described in chapter 3 as Eq. (77) which can be
rewritten because the polymer concentration for these measurements is a fixed value as
M = A e £ (81)
where A is a constant.
The expression for the reflected luminance as a function o f incident and detector
angle is then,
Z ( M ) = M ( M ) e ^ (82)
In addition, cosine corrections for the detector and the photopic response function are
included in the model43,44. The fitting parameters in this model are the normalization
factor N and the standard deviation a. For the green sample, the standard deviation is
determined in chapter 3 by holding the angle y fixed and varying the polymer
concentration, as opposed to the approach discussed here, where the polymer
concentration is held fixed and the angle y varied. In chapter 3, a standard deviation
value of 5.8° was found for the green sample with 0.9% polymer as shown in Table
IV.
A comparison between the data for the yellow (green) sample shown in Fig. 4.2
and calculations using Eq. (82) is shown in Fig. 4.5 (4.6). There is excellent
agreement between the measurements and calculations for both samples. The plots in
these figures show the standard deviation values used to fit the model to the data.
Table V lists the standard deviation values for the green sample. The average value of
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yellow s a m p le_________ in c id e n t l ig h t an g le
6000
4000
2000
29
4000
2000
482000
1000
65800 <7=7.4
400
- 4 0 - 2 0 0 20 40 60 80 100azim uthal angle (deg)
Fig. 4.5. Comparison of calculated (solid line) and measured (points) luminance.
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102
g r e e n s a m p lein c id e n t l ig h t a n g le4000
(7=5.9
2000
03000 29(7=6.5
2000
S 1 000
048cr=5.5
1500
500
065(7 = 5
600
400
200
0 ---------- I—— 40 - 2 0 800 20 40 60 100
a z im u t h a l a n g le (deg)
Fig. 4.6. Comparison of calculated (solid line) and measured (points) luminance.
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103
Table V. Table showing a from fitting the model to the
measurements for the green sample and
comparison to a of chapter 3 (5.8°) as
% difference |(ach3-a)/ach3|-
incident light (deg)
a(deg)
% difference
10 5.9 229 6.5 1249 5.5 565 5.0 14
a (average) 5.7 2
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104
a for the green sample found from this fitting is 5.7°. Thus only a difference of 2% is
found between the o found here and the value found in chapter 3.
Calculation of reflected luminance out of the plane of incidence requires a
3-dimensional model because there is no simple approximation for the reflected
intensity as a function of solid angle (i.e., for 0 not equal to zero).
4.2.4 Luminance Polar Plots
Using similar data as discussed in section 4.2.2, 2-dimensional polar plots of
the reflected luminance for all incident light angles are determined. Figure 4.7 (4.8)
shows the plots for the yellow (green) sample at the incident light angles of 10, 29, 48
and 65 degrees, respectively. The solid lines are drawn through the data as an aid to
the eye. Projection of the lines is based on the data and physical models. As the
incident light angle increases, the plots generally become more asymmetric in
azimuthal angle. However, all plots show the expected symmetry in polar angle and
that the symmetry is independent of illumination angle.
4.3 Contrast Ratio Measurements
4.3.1 Contrast Ratio Measurements
These measurements utilize the reflected luminance values discussed in
sections 4.2.1 and 4.2.2. The luminance from the samples in the focal conic state is
measured in a similar fashion. The contrast ratio as a function of incident light angle
and azimuthal angle is then determined by dividing the reflected luminance by the
luminance in the focal conic state.
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105
incident incident lightyellow sample
Luminanceh«8b
(x 10 c d /m 2)
8 0 - 6 0 - 4 0 - 2 0 - 2 0
80incident light incident light
8 0 -6 0 -4 0 -2 0 (D - 2 0
8 0 -6 0 -4 0 -2 0 - 2 0
M 0) tO - i 60W)<d O G-tf d—-
L 8 0 -6 0 -4 0 -^ 2 ^ (p 20 40 60 80
- 4 0
- 6 0
- 8 0 L
azim uthalangle(d eg )
Fig. 4.7. Two-dimensional polar plots of reflected luminance for the yellow sample, (solid line drawn as an aid to the eye)
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106
incidentlightangle
- 8 0 - 6 0 - 4 0 -
in c id e n t
a n g le
- 8 0 - 6 0 - 4 0 - 2 0 - 2 0
g r e e n s a m p le 30 L u m in a n ce
(x IQ2 c d / m 2)
in c id e n tl ig h t
J L'0 60 ^ 8 O _ 3 0 _ g 0 _ 4 o _ 2 O
- 2 0
- 4 0 -
- 6 0
in c id e n tl ig h ta n g le
60 -
- 80 - 6 0 - 40 -
b <u
§ I?! _4°J L
20 40 602 ^ 0 -
- a z im u th a l a n g le
L (d eg )
Fig. 4.8. Two-dimensional polar plots of reflected luminance for the green sample, (solid line drawn as an aid to the eye)
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107
Figure 4.9 shows the results of the measurements. The individual curves within
each group are for incident light angles of 10, 29, 48, and 65 degrees, respectively.
As shown in the data, the largest contrast ratio values are found in the zero to
twenty degree azimuthal angle range and are about the same value, regardless of the
incident light angle. For the yellow sample this value is about 9 to 1 and for the green
sample this value is about 7 to 1. These values are on the order of what is required for
newspaper text. It should be noted that these are not optimized cells (e.g., no
anti-reflection (ar) coating, no black absorbing layer coated on inside glass, etc.) and
the contrast ratio is largely determined by scattering in the focal conic state. The
contrast ratio can be improved significantly with suitable techniques to reduce the
scattering.
While the contrast ratios in the zero to twenty degree azimuthal angle range are
relatively independent of the incident light angle, there is a decrease in contrast ratio as
the azimuthal angle approaches the specular angle for large angles of incidence.
4.3.2 Physical Model for Measured Contrast Ratio Results
At the incident light angle of 10 degrees, the reflected and scattered luminance are
nearly symmetric about the specular angle of 10 degrees as shown in the top plot of
Fig. 4.10. Furthermore, they both decrease similarly with azimuthal angle. Thus the
contrast ratio, which is determined by dividing the luminance in the reflecting state by
the luminance from the scattering state, will be nearly constant over a wide range of
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cont
rast
ra
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incident light angle . (deg)
2 _________1________ 1_________1________ L- 4 0
8 r -
- 2 0 • i 4,° (a i 60azim uthal angle (deg)80 100
incident light angle
(deg)7
6
5
65 484
3 29
2 green sam ple
0- 4 0 - 2 0 0 20 40 60 80 100
azim uthal angle (deg)
Fig. 4.9. Contrast ratio measurements as a function of incident and detector angle (solid lines drawn as an aid to the eye)
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109
incident light
angle6000
4000
g 2000 reflected
rdo scattered
(Uas 00
• rH
Gj 800
reflectedincident light
angle
65
400
scattered
- 4 0 - 2 0 0 20 40 60 80 100
a z im u th a l a n g le (deg)
Fig. 4.10. Measured luminance from the yellow sample in both the imperfect planar
and focal conic states for 10° (upper plot) and 65° (lower plot) incident light angles,
(solid lines are drawn as an aid to the eye)
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110
angles as observed in the data shown in Fig. 4.9 for the 10 degree incident light angle
measurements.
There is an asymmetry in luminance from the reflecting state at large incident light
angles about the specular angle while there is near symmetry in scattered luminance
from the focal conic state as shown in the bottom plot o f Fig. 4.10. Thus for large
incident light angles, dividing the asymmetric reflected luminance by the symmetric
scattered luminance produces an asymmetry in contrast ratio.
As the incident light angle increases, there is a greater decrease in the reflected
luminance at the specular angle from the planar texture than in the focal conic state as
illustrated in Fig. 4.10. Consequently, the contrast ratio is expected to be significantly
smaller at the specular reflected angle for larger incident light angles. This is observed
in the measured results shown in Fig. 4.9. However, at large incident light angles
there is a broadening in the reflected luminance to azimuthal angles smaller than the
specular angle while the scattered luminance decreases symmetrically about the
specular angle. As a result, the contrast ratio is expected to increase from the specular
azimuthal angle to smaller azimuthal angles for the larger angles of incidence. This is
observed in the measured results (Fig. 4.9), where the contrast ratio increases from the
specular angle to around the twenty degree azimuthal angle for the incident light
angles o f 48 and 65 degrees.
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Ill
4.3.3 Contrast Ratio Polar Plots
Using measurements as discussed in section 4.2.2 for luminance in the reflecting
state and similar luminance measurements for the focal conic state, 2-dimensional
polar plots o f contrast ratio are obtained. Figure 4.11 (4.12) shows the isocontrast
curves for the yellow (green) sample at incident light angles of 10, 29, 48 and 65
degrees, respectively. The solid lines are drawn through the data as an aid to the eye.
Projection of the lines is based on the data and the physical models. The curves show
a symmetry in polar angle irrespective o f the incident light angle and show an
increasing asymmetry in azimuthal angle as the incident light angle is increased.
4.4 Chromaticity as a Function of Incident Light and Detection Angle
4.4.1 Chromaticity
Before discussing the chromaticity measurements, a background on color and
chromaticity is presented. Color is the term commonly used to describe the sensation
produced by electromagnetic radiation (in the range 380 nm to 780 nm) incident on
the eye. Color can be characterized by three attributes; hue, saturation and
brightness45. These characteristics are best described by using the color circle shown
in Fig. 4.13a.
Different hues are encountered by moving around the circle. The hues are
perceived as red, yellow,etc. Hue can be related to wavelength (although this is not
always strictly true and will be discussed in detail in Chapter 6).
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112
in c id e n t y e l low s a m p le
C o n tr a st R atio
incidentlightangle
J I I L
8 0 - 8 0 - 6 0 - 4 0 - 2- 2
in c id e n tl ig h t 60
an g le o
65
L
- 8 0 - 6 0 - 4 0 - 2 0- 2 0
in c id e n tl ig h ta n g le
48°
J L _L
Q ( £ p - 8 0 - 6 0 - 4 0 - 2
60 40
S-i <D /—v~ <10 h M oj
O d T3f t (0 ^-1 ' — 60 -
- 8 0 L
0 80
8 0 - 6 0 - 4 0 ^ 0 20 40 60
a z im u th a l - a n g le
(d eg)
Fig. 4.11. Two-dimensional contrast ratio polar plots for the yellow sample (solid line drawn as an aid to the eye)
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113
80in c id e n t
l ig h t 60 a n g le
o 40
8 0 - 6 0 - 4 0 ^ 2 0 ^ 20
g r e e n sa m p le
C o n tr a st R atio
.5
incidentlightangle
29°
J L
- 6 0
in c id e n t l ig h t 60 a n g le
65°
80 - 8 0 - 6 0 - 4 0 - 2 0 ' - 2 0 '
- 4 0
- 6 0
in c id e n tl ig h t 60
8 0 - 6 0 - 4 0
-8 0 -6 0 -4 0 ^ (1
0 - 8 0 - 6 0 - 4
a ~ ' tjon ?? 02 ^ x)h&( (0 O-
20 40 60 8 0 - 6 0 a z im u th a l
an g le
(deg)
- 8 0
60 80
Fig. 4.12. Two-dimensional contrast ratio polar plots for the green sample (solid line drawn as an aid to the eye)
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114
Saturation characterizes the quality of the color. The more saturated a color, the
better the quality (i.e., appears more pure). Saturation can be related to the spectral
bandwidth. A fully saturated color (most pure color) is light o f a single wavelength.
The broader the bandwidth, the less saturated the color. If the spectral bandwidth is
wide enough, the color appears white. Saturation is represented on the color circle by
moving radially out from the center. White is at the center, and a decreasing spectral
bandwidth (i.e., increasing saturated color) is indicated by moving radially out to the
edge of the circle. Thus, a fully saturated color (i.e., light of a single wavelength) is on
the edge of the circle.
For a given color (a given point on the color circle), as the brightness is increased,
the color tends toward white. Conversely, as the brightness is decreased, the color
tends toward black.
A more sophisticated (and quantitative) representation of color is achieved by using
the 1976 CIE Color Chromaticity Diagram shown in Fig. 4.13b. The CIE diagram is
qualitatively similar to the color circle. Movement around the CIE diagram indicates
different hues and moving radially out from the center indicates a more saturated
color. However, the CIE diagram is a quantitative representation of color. Using a
measured spectrum and taking into account the photopic response of the eye, the
subjective nature of color to different observers and other color properties (e.g.,
primary colors), two chromaticity coordinates, u' and v', are determined. The location
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115
white
brightness
o r a n g e _ r e d
whitesaturation
hue ;reen blue
black
0.6
yellow0.5 orange
redgreen
0.4
0.3
blue0.2
vio let
0.00.0 0.1 0.2 0.3 u’ 0.4 0.5 0.6 0.7
(b)
Fig. 4.13. Color circle (a) and 1976 CIE color chromaticity diagram (b).
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116
of these coordinates on the CEE Chromaticity Diagram quantitatively characterizes the
hue and saturation of a given color.
4.4.2 Physical Model to Describe Angular Hue Dependence
For a given incident light angle, P, on a perfect CLC sample, the peak reflected
wavelength is X=nPcosP10. As the angle changes, the reflected wavelength
significantly changes and thus the reflected color changes. For a polymer modified
reflective cholesteric display, there is a range of angles between the incident light and
the helical axes due to the misorientation caused by the polymer network. As a result,
there is a slightly broader range of wavelengths reflected and hence a slight
desaturation in color, but the hue change is now less sensitive to angle. This situation
is illustrated in Fig. 4.14. As shown in Fig. 4.14a, the angle between normally incident
light and the sample normal is zero, and there is some angle £ between the incident
light and the helical axis labelled 1. For light incident at a different angle (say the angle
helical axis 1 makes with the sample normal) as shown in Fig. 4.14b, then the angle
between the incident light and helical axis 1 is now zero and the angle between the
sample normal (helical axis 2) and the incident light is now £.. Because the angle
between the incident light and the respective helical axis of the two different situations
is the same, there is no net change in reflected wavelengths regarding these two axes'
orientation, although the direction of reflection is different.
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117
helical axis 1
incident light
(a)
incident light
(b)
helical axis 2
Fig. 4.14. Schematic representation o f helical axis orientation and incident
light angle with the helical axis orientation and incident light angle
in (a) reversed from that in (b).
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118
However, there will still be some hue change for the following reason. The total
light reflected at some angle is proportional to the fractional number of helical axes
oriented to Bragg reflect at that angle. There are more axes oriented normal to the
sample than at angle £. Thus, for the wider incident light angle, the reflected light will
have slightly more short wavelength components. By this same reasoning, for light
incident normal to the sample, the reflected light will have slightly more long
wavelength components.
The previous discussion considers the case of fixed observation at two positions for
a given incident light angle and shows a reversal in incident angle causes only a small
change in hue. The following discusses the change in hue for a fixed incident light
angle and a range of azimuthal detection angles.
As shown in Fig. 4.15a, for light incident normal to the sample, the magnitude of
the angle between the incident light and helical axis 1 and between the incident light
and helical axis 2 is the same and for the sake o f this illustration say -40 degrees for
helical axis 1 and 40 degrees for helical axis 2. The observed wavelength would be
npcos(-40) from helical axis 1 (e.g., say this color is green), then increase to npcos(O)
(e.g., yellow), and finally decrease back to npcos(40) (the same value as that from
helical axis 1 and would be the color green) from helical axis 2 as the detector is swept
through this range of azimuthal angles.
However, for light incident at wide angles as shown in Fig. 4.15b, there is a
different angle between the incident light and helical axis 1 (say Q and the incident
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119
helical axis 1 helical axis 2
reflected light fromaxis 1(e.g., green)
reflected light from axis 2
(e.g., green)
I (e.g., yellow) incident light w specular reflected light
decreasing (a) azimuthal angle
helical axis 1 helical axis 2
reflected light fromaxis 1 f / \(e.g.,yellow) f ^ Cv
incident light
reflected light from axis 2 (e.g., blue)
M specular reflecteed light
(b)decreasing
azimuthal angle
Fig. 4.15. Schematic diagram of helical axis orientation and incident light.
While the helical axis orientation is the same in both (a) and (b),
the incident light angle is different.
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120
light and helical axis 2 (say £). Thus, the observed wavelength would be npcos(Q
from helical axis 1 (e.g., say this color is yellow) and continually decrease to a
wavelength of npcos(^) (e.g., blue) from helical axis 2 as the detector is swept through
the same number of azimuthal angles as for the previously discussed case of normally
incident light. Because none o f the reflected wavelengths are the same, and there is a
monotonic increase in wavelength with decreasing azimuthal detector angle, the hue
change will be larger for light incident at large angles as opposed to normally incident
light for the same range of detector angles.
4.4.3 Chromaticity Measurements
For these measurements, the light source is fixed at one of two incident light angles
(10 or 48 degrees). The Spectrascan PR704 camera is used to measure the
chromaticity coordinates of the reflected color from the yellow sample and the green
sample. For a given incident light angle, the camera is rotated to various azimuthal
angles and the chromaticity coordinates measured.
Figure 4.16 shows the results of the measurements. The left column is for the
yellow sample and the right column for the green sample. The top row are
measurements at the incident light angle of 10 degrees, the second row for the incident
light angle of 48 degrees, and the last row shows the general area on the entire
chromaticity diagram where the specific values are located.
As shown in the data, there is little change in the chromaticity coordinates for all
azimuthal angles for light incident at 10 degrees. There is a slightly greater change in
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121
y e l lo w s a m p le g r e e n s a m p le0.60 0.60incident light angle 10incident light angle 10
azimuthalangle(deg)azimuthal
angle(deg) - 1 50.55 0.5530o -1 5
50- 3 0
-3 070 10
0.500.500.20,0.2 0.30.6 0.6
incident light angle 48incident light angle 48
azimuthalangle(deg)azimuthal
angle(deg) 20 - 2 020
0.540
40
60- 2 060 70<70o0.5 —I 0.4 L—
0.3 0.100.1 0.15 0.20 0.250.2
0.7 0.7
0.6 0.6
0.5 0.5
V 0 -40.3
0.4
V 0.3
0.2 0.2
0.00.00.0 0.1 0.2 0.3 0 .4 0.5 0.6 0.70.0 0.1 0.2 0.3 0.4
Fig. 4.16. Chromaticity coordinates as a function of incident light and azimuthal angle.
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122
the chromaticity coordinates as a function of azimuthal angle for light incident at 48
degrees.
Visually, the change in hue for light incident at 10 degrees for the yellow sample is
from orangish yellow to greenish yellow and for the green sample from yellowish
green to bluish green. The change in hue for light incident at 48 degrees for the
yellow sample is from yellowish orange to yellowish green and for the green sample
from greenish yellow to greenish blue. In both cases, the basic hue, be it yellow or
green does not change with incident light or detector angle, although the hue change is
slightly greater for illumination at 48 degrees as opposed to 10 degrees. However, the
hue change from these samples with polymer is still less than that from a perfect CLC.
As an example, for a perfect CLC illuminated at 10 degrees, then 48 degrees, the
change in hue for a normally incident yellow sample would be from yellow to blue.
4.5 Optimal Illumination Conditions
An analysis of the data is conducted to determine the illumination conditions that
result in the largest reflected luminance, contrast ratio, and viewing angle with the
smallest angular change in hue.
The data in Figures 4.2 and 4.9 which show reflected luminance and contrast ratio
are examined for each incident light angle. The maximum luminance or contrast ratio
a sample had from the range of azimuthal angle measurements is selected for each
incident light angle and replotted as the upper two curves shown in Fig. 4.17. The
maximum values for reflected luminance occurred at or near the specular angle. The
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7000
y e l lo w s a m p leye l low s a m p le6000
5000
4000
3000g r e e n s a m p le
'V' - - .-green s a m p le
1000V
60 70 0 10 20 30 40 50 60 70in c id e n t l ig h t a n g le (d eg ) in c id e n t l ig h t a n g le (deg)
140
20 y e l lo w s a m p le
g r e e n s a m p leS’ 60
£ 40
200 10 20 30 40 50 60 70
in c id e n t l ig h t a n g le (d eg )
Fig. 4.17. Upper two plots are maximum luminance (left) and maximum CR (right)
and lower plot is viewing angle, all versus incident light angle.
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124
maximum values for contrast ratio occurred in an azimuthal angle range from zero
(i.e., the sample normal) to twenty degrees.
Analysis of this data shows the maximum reflected luminance is obtained for the
incident light angle of 10 degrees. There is a slight decrease out to 29 degrees, and a
significant decrease from 29 degrees to 65 degrees. Analysis o f the maximum contrast
ratio versus incident light angle shows there is little change in contrast ratio,
irrespective of the incident light angle.
The data from Fig. 4.9 is analyzed to determine the viewing angle (reported here as
the angular width over which the contrast ratio falls to half its maximum value) as a
function of incident light angle and is shown in the bottom half of Fig. 4.17. As
shown, the maximum viewing angle occurs for an incident light angle of 10 degrees
and there is a monotonic decrease in viewing angle with increasing incident light angle.
As shown in Fig. 4.16, the smallest hue change as a function o f detector angle
occurs for an incident light angle of 10 degrees (i.e., near normal incidence). The hue
change with detector angle increases with increasing incident light angle.
These results indicate that the optimal illumination condition is illumination directly
from the front. However, the results indicate there is little change in display properties
for illumination angles out to 30 degrees, particularly when viewed directly from the
front. Also, the reflection symmetry in polar angle allows for equivalent off-axis
illumination.
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Chapter 5
Study on Color Quality of Chiral Nematic Liquid Crystals
As a result of the inherent broadening in the reflected wavelength band from CLCs
as the pitch increases, there is an increasing desaturation in the reflected color. This
chapter discusses the use of dichroic dyes to improve the reflected color quality (i.e.,
produce more saturated color). Using the dynamic theory of reflection, it is shown
that the incorporation of a dichrioc dye in a chiral nematic liquid crystal can
significantly alter the reflection spectrum. In effect, the altered reflection spectrum can
have a reduced bandwidth and thus produce a more saturated color. The appropriate
absorption spectra to produce a more saturated yellow is then discussed and measured
absorption spectra from three different dichroic dyes that meet this criteria is
presented. Next, the measured reflection spectra from several CLCs (prepared with a
pitch to reflect yellow) with the incorporation of a suitable dichroic dye at different
concentrations is shown and compared to samples without dichroic dyes. The
chromaticity coordinates are measured for samples with different dyes to determine
color quality. Then, using the dynamic theory of reflection and the measured
absorption curves from the three dyes studied, reflection spectra from a CLC with a
pitch to reflect yellow are calculated and compared to the measurements.
125
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126
5.1 Color
5.1.1 Reflected Color from a Chiral Nematic Liquid Crystal
The bandwidth of reflected wavelengths from a CLC is 8X=A.Sn/n where X=nP
so 8A,=nP8n/n. As the pitch increases, the bandwidth increases and consequently, the
reflected color becomes desaturated. Optical examination o f CLC material with a
pitch adjusted to reflect violet, blue or green shows color o f acceptable quality, while
optical examination of CLC material with a pitch adjusted to reflect yellow, orange or
red does not. For example, the reflected yellow has a slightly whitish yellow
appearance as opposed to a "sharp" yellow color.
To improve the color quality of the CLC material with longer pitch, a decrease in
the reflected bandwidth is necessary to increase the saturation of the reflected color.
One way to modify the reflected spectrum is to reduce the birefringence and another is
to attenuate the reflected amplitude. There has been some research on the effect of
absorption on the optical properties of CLCs46,47; however, there has been little
research on the use o f absorption in modifying the reflected bandwidth to improve
color quality.
Dichroic dyes absorb in the visible light region and are compatible with
incorporation in liquid crystal material. Consequently, the use of dichroic dyes
provides an approach to modify the reflected bandwidth and thus improve the reflected
color quality for the longer wavelength colors (yellow, orange and red).
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127
5.2 Effect o f Absorption on the Reflection Spectrum from Cholesteric Liquid Crystals
A complex index of refraction is utilized in calculations to quantitatively describe
the propagation of an electromagnetic wave in an absorbing material. Absorption is
contained in the imaginary component. The complex index of refraction is then
written as
nc = n - z'k (83)
where n is the real part and k the imaginary component.
A substitution of Eq. (83) into the expression for an electromagnetic plane wave
results ine-mwczfk _ e~ z e-m, (84)
where a = 4rckA. and <|> = 27tnz IX. The phase, <(>, is influenced by the real part of the
complex index o f refraction and the amplitude is attenuated as exp(-az/2) where a is
the absorption coefficient o f the material.
The effect of absorption on the reflection spectrum of a CLC is examined. An
absorbing material is modeled as similar to a dichroic dye but with constant imaginary
components in the complex index of refraction. Several values for the complex
coefficients are used. The imaginary component along the extroardinaiy axis is set
equal to 0.2, 0.1, 0.05, 0.02, 0.01 (ke = 0.2, etc.), respectively, and along the ordinary
axis set equal to one-tenth the value o f the extraordinary axis, 0.02, etc., (k0 = 0.02,
etc.).
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128
Using the relation discussed in Eq. (84), a = 4jtk / A, where k is the imaginary
component o f the refractive index, the absorption coefficient (a) for the material can
be determined. Figure S.l is a plot of the extraordinary component o f the absorption
coefficient for the two constant k,. values of 0.2 and 0.1. In the figure, the two
absorption curves are referred to the y-axis on the left. As shown in the figure, the
absorption coefficient falls off as 1/A,.
Also shown in Fig. 5.1 (and referred to the y-axis on the right), is the calculated
reflection spectrum for a non-absorbing CLC with pitch equal to 0.35 nm, n = 1.63,
8n = 0.228, and A0 = nP = 0.57 nm (yellow).
The upper curves in Fig. 5.2 show the results of including absorption in the
calculation o f the reflection spectrum from a CLC using the dynamic theory of
reflection with the constant k values discussed10. The lower set of curves in Fig. 5.2
show the results obtained by a different calculational approach (two-wave
approximation)48. There is good agreement between the two sets of calculations.
The significant difference between individual curves from large absorption to no
absorption shows that the inclusion of an absorbing material in a CLC can significantly
alter the reflection spectrum. As shown in Fig. 5.2, material with large absorption
coefficients cause an overall large reduction in the total reflected intensity at all
wavelengths in the Bragg reflection band, with slightly less reduction at the shorter
wavelengths and a gradual rolling decrease in the reflected intensity out to longer
wavelengths. There is an overall slight decrease in the total Bragg reflected band.
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129
0.6 0.6
0.50.5
0.40.4
0.3k = 0 . 1
0.20.2
0.0 0.0300 400 500 600 700 800 900
w a v e le n g t h (nm )
Fig. 5.1. Plot of absorption coefficient (y-axis left) for constant k values 0.2, 0.1
and Bragg reflection band (y-axis right) of a CLC with pitch to reflect yellow.
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refl
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0 .6 r -
0.5 -
0.4 -
0.3 -
0.2 -
0.1 -
0.0 -
0.3
Fig. 5.2.
130
k -0 .0 2
k =0.1
k -0.2
0.5 0.70.4 0.6 0.8
0.5
0 4
\ '
w a v e le n g t h (/xm) (a)
I 1
INi( \ i
\ \
0.9
1.0 1.5 2 .0 2.5
Calculated reflection spectra using the dynamic theory of reflection
from a CLC with the k values shown (a) and using the two-wave
approximation for the k values 0.0, 0.02 and 0.2, respectively (b).
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131
Similar results are found for material with smaller absorption coefficients but with
much less o f an overall reduction in reflected intensity.
5.3 Reflection Spectrum and Color Quality of CLCs with Dichroic Dyes
The optimal absorption condition would be to attenuate only over some subset of
the total Bragg reflection range, thus narrowing the reflection spectrum enough to
improve color quality, but not so much as to render the total reflected intensity too
low. The following presents the results on the reflection spectra and color quality of
samples using dichroic dyes that meet this absorption condition.
5.3.1 Dichroic Dyes
The goal of this research is to improve the reflected yellow color. Because the
yellow reflection spectrum from a CLC is between 530 nm to 610 nm, the study
concentrates on dyes that have an absorption spectrum that decrease significantly
around 570 nm which then provides an overlap region of 40 nm. Also, the dyes are
required to have a fairly high absorption coefficient within the overlap region between
the dye absorption spectrum and the reflection spectrum.
Three dyes are identified that meet these criteria to some extent. All three are red
dyes; one from Aldrich, DR-13, one from Hoffman-LaRoche, R4, and one from the
University of Oklahoma, C6.
To determine the exact absorption spectrum of these dyes, 5 micron thick cells with
rubbed polymide surfaces are vacuum filled with a known concentration of the dye in
the nematic liquid crystal E48. Transmission measurements are conducted with both
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132
sigma and pi polarizations to determine the absorption coefficients for both principle
axes using an Oriel 77250 l/8m monochrometer to select specific wavelengths from
the incident light source and a Si photodiode to detect the transmitted light.
Absorption values are then calculated using the relation
a = -log (I/I0 )/j£d (85)
where I is the measured transmitted intensity through the cell with the nematic/dye
mixture, Iq is the measured transmitted intensity through a cell with nematic liquid
crystal only, % is the concentration of the dye and d is the thickness of the cell.
Figure 5.3 shows the absorption spectrum along both principle axes for the three
dyes. The top curve in the figure shows the absorption curves for the dye DR-13.
The spectrum is Gaussian-like with a peak absorption of approximately 375,000 cm'1
at 510 nm for the extraordinary axis and approximately 100,000 cm'1 at 510 nm for the
ordinary axis. The absorption full width half maximum (FWHM) for the extraordinary
axis is 135 nm and 110 nm for the ordinary axis.
The middle curve of Fig. 5.3 shows the absorption spectrum along both principle
axes for the dye R4. As shown in the figure, the spectrum is Gaussian-like with a peak
absorption of approximately 350,000 cm'1 at 480 nm for the extraordinary axis and
approximately 40000 cm'1 at 480 nm for the ordinary axis. The absorption FWHM for
the extraordinary axis is 125 nm and 100 nm for the ordinary axis.
The bottom curve of Fig. 5.3 shows the absorption spectrum along both principle
axes for the dye C6. As shown in the figure, the spectrum is Gaussian-like with a peak
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133
400000
300000 D R -13
200000
100000
0
R4300000
200000
o 100000
0
C6300000
200000
100000
0400 500 600 700
w a v e le n g t h (nm)
Fig. 5.3. Measured absorption curves along the extraordinary (e)
and ordinary (o) axes for the dyes DR-13, R4, and C6.
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134
absorption of approximately 350,000 cm'1 at 465 nm for the extraordinary axis and
approximately 55000 cm'1 for the ordinary axis. The absorption FWHM for the
extraordinary axis is 120 nm and 95 nm for the ordinary axis.
The relevant parameters from the measured absorption curves (e.g., FWHM, etc.)
are listed in Table Via. Analysis of the data shows all dyes have approximately the
same peak absorption values. However, as shown in the upper plot of Fig. 5.4, the
peak absorption for the dye DR-13 occurs at a longer wavelength than R4. And R4
has a peak absorption that occurs at a longer wavelength than C6. Furthermore, the
dye DR-13 has a larger FWHM than R4. And R4 has a larger FWHM than C6.
A reasonable fit is made by modelling the absorption curves as Gaussian curves,
a ( K ) = % e (86)
where a 0 is the peak absorption value at X0 and c is the standard deviation10. The
bottom curves in Fig. 5.4 compare the modelled absorption curves for the
extraordinary axis to the measured curves for the dyes DR-13, R4 and C6,
respectively. Table VIb lists the relevant parameters (e.g., <r,etc.) for the modelled
absorption curves.
Figure 5.5 shows both the absorption curves (rescaled for the plot) for each dye
and the reflection spectrum for a non-absorbing CLC with pitch to reflect yellow. As
shown in this figure, all absorption curves overlap only a portion of the Bragg
reflection range and thus fulfill the previously discussed criteria for optimal absorption
to produce the desired results. Also, the respective dyes overlap increasingly larger
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135
Table Via. Relevant parameters for the dyes from measurements
type of peak a e (X) peak a 0 (X) 5Xe 8X0
dye cm'1 (nm) cm'1 (nm) nm nmDR-13 3.7xl05 (510) 1.0x10s (510) 135 110
R4 3.5x10s (480) 4.0xl04 (480) 125 100C6 3.5x10s (465) 5.5xl04 (465) 120 95
Table VIb. Relevant parameters for the dyes from the curve fit.
type of peak a e (X) peak a o (X) 5Xe 8X0
dye cm'1 (nm) cm'1 (nm) nm nmDR-13 3.7x10s (510) 0.9x10s (510) 125 108
R4 3.5x10s (480) 3.9xl04 (480) 118 95C6 3.4x10s (465) 5.4xl04 (465) 110 90
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136
400 0 0 0\ e x t r a o r d i n a r y a x i s
. R4 \\ \ D R - 1 3
3 0 0 0 0 0
o 200000C6
•2 100000
400 500 600 700w a v e le n g t h (nm )
400000"ft D R - 13 R4 C6
300000
•2 200000
00000
— I 1------l .vV J.. J l l — u J — l-------- 1-----400 500 600 700 400 500 600 700 400 500 600 700
w a v e le n g t h (nm )Fig. 5.4. Upper plot is measured absorption spectra for the three dyes along
the extraordinary axis while the bottom plots show both the calculated
(solid line) and measured (points) absorption spectra.
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137
ch ir a l c o n c e n t r a t i o n 26.5%0.5 0.5
D R -1 30.4 0.4
0.3 0.3
0.2 0.2
- 0.0 a° 0.4)o* 0.3
CD
0.2ao
0.0
R40.4
0.3
0.2
Ou
I 0.0 (0
0.0
0.4 0.4
0.3 0.3
0.2 0.2
0.0 0.0400 500 600 700
w a v e le n g th (n m )
Fig. 5.5. Plots for the different dyes showing the absorption spectra (y-axis left)
and Bragg reflection spectra from a CLC (y-axis right) with pitch to reflect yellow.
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regions o f the Bragg reflection range (with C6 being the smallest and DR-13 the
largest), thus slightly different results are expected between the reflection curves from
samples with the different dyes.
5.3.2 Measured Reflection Spectrum from Absorbing CLCs with Different Dyes
Samples are prepared by vacuum filling rubbed polymide surface ITO coated
glass cells separated with 5 micron spacers. The liquid crystal mixture used is the
nematic E48 and the chiral compounds CB15, R1011 and CE1. The chiral compounds
are 27.2% of the total mixture. Varying concentrations of the different dyes are added
to the chiral liquid crystal mixture as shown in Table VII. Three samples are made
with the dye DR-13 at concentrations of 0.536, 1.42 and 2.23%, respectively. Three
samples are made with the dye R4 at concentrations of 0.63, 1.29 and 2.14%,
respectively. Three samples are made with the dye C6 at concentrations of 0.55, 1.39
and 2.4%, respectively.
The reflection spectra are measured at near normal incidence with a measurement
geometry similar to that shown in Fig. 3.12 (where in these measurements; (5=2.5°,
<j>=2.50 , and 0=0°). As before, a 50W tungsten-halogen lamp is used as the light
source and a Spectrascan PR704 camera is used to measure reflection spectra and
chromaticity coordinates.
The initial chiral concentration of 27.2% results in a reflected greenish yellow
color. However, addition o f the dye concentrations used here (around 1%) results in a
shift to slightly longer Bragg reflected wavelengths (the range of wavelengths that
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139
produce yellow). The reflected spectrum shift is equivalent to the reflected spectum
from a CLC without dye at a chiral concentration o f around 26.5%. Figure 5.6 shows
the reflection spectrum for the sample with a chiral concentration o f 27.2% and one
with a chiral concentration of 26.5%. It is suspected that since the dye is
mesogen-like, adding dye to the nematic/chiral mixture is like adding more nematic to
the mixture thereby decreasing the relative chiral concentration and thus increasing the
pitch (i.e., increasing the Bragg reflected wavelengths).
The following shows the reflection spectrum from the samples with the largest dye
concentrations because the effect of absorption will be greater and thus produce the
most easily observed effects.
The upper curves in Fig. 5.7 show the reflection spectra from samples with no dye,
2.23% DR-13, 2.14% R4 and 2.4% C6, respectively. The bottom curves are the
individual plots of the curves shown at the top of Fig. 5.7. As shown in these curves,
the inclusion of a dye at these concentrations does significantly alter the reflection
spectrum as expected. All reflection spectra show a decreased intensity at the shorter
wavelengths and a gradual, rolling increase in reflected intensity at the longer Bragg
reflected wavelengths. There is also an overall decrease in the reflected full width half
maximum intensity.
The specific results of the measurements are also as expected. Where the dyes
have a higher absorption coefficient (the shorter wavelengths), there is a greater
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140
Table VII. Listing o f the concentrations of the three dyes used in the experiments.
type of dye
dye concentration
(%)DR-13 0.53 1.42 2.23
R4 0.63 1.29 2.14C6 0.55 1.39 2.40
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141
0 .6
c h ir a l c o n c e n t r a t i o n %0.5
26 .527.20.4
• i-H >
• rH
oCD
(U
0.2
0.0400 500 600 700
w a v e le n g t h (n m )
Fig. 5.6. Reflection spectra from a CLC with a chiral concentration of 27.2%
and one with 26.5%
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142
0 .5C6no dye
R40.4
D R - 13
0.0400 700500 600
wavelength (nm)0.5
2.4% C62.23% D R - 1 3 2.14% R4
0.4
0.0400 500 600 700 400 500 600 700 400 500 600 700
wavelength (nm)
Fig. 5.7. Upper plot shows collectively the measured reflection spectra from
samples with the various dyes while lower plots show the individual
spectra for samples with the dyes DR-13, R4, C6, respectively.
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143
decrease in reflected intensity as opposed to where the absorption coefficient is smaller
(the longer wavelengths), where there is a larger reflected intensity.
The sample with the C6 dye has slightly larger reflected amplitudes at the shorter
wavelengths and slightly larger FWHM than the sample with the dye R4. The sample
with the R4 dye has slightly larger reflected amplitudes at the shorter wavelengths and
slightly larger FWHM than the sample with the DR-13 dye. These results are
consistent with the absorption spectrum measurements previously shown where the
penetration into the Bragg reflection band is greatest for DR-13 and least for C6.
5.3.3 Chromaticity Measurements
The measured reflection spectra from samples with dyes have an effective
reduced spectral bandwidth as compared to a CLC sample without a dye, and thus
should produce a more saturated color. The best measurement of this for a display
application is optical observation. And optical observation of the samples clearly
showed an improved reflected yellow color. Instead of the whitish yellow for a sample
without a dye, the samples had varying degrees of a sharper yellow depending on the
dye and dye concentration.
To quantify the color quality (degree of saturation), the chromaticity coordinates of
all the samples are measured. The area of the 1976 CIE Chromaticity Diagram
examined is shown at the bottom of Fig. 5.8. The top plot in Fig. 5.8 is the measured
chromaticity coordinates for samples with DR-13, the middle plot for samples with R4
and the third plot for samples with C6. Also shown on each chromaticity diagram are
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144
0 .6 0DR-13
0.59 1.4227.2 • ♦ ♦
26.5• % chiral concentration (no dye)♦ % dye (27.2% chiral concentration)
0.55 2.2326.0
0.50R4
1.290.630.55 27.2 2.1426.026.5
0.50C6
1.39 2.40.55 27.20.55 26.5 26.0
0.50 l— 0.20 0.25 0.30u
0.6
0.4
0.2
0.00.0 0.2 u ’ 0.4 0.6
Fig. 5.8. Upper three plots show measured chromaticity coordinates from samples
with the three dyes at the various concentrations. Lower plot shows
general area on the CIE diagram where measured data is located.
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145
the chromaticity coordinates for three samples made with chiral concentrations of
27.2, 26.5, and 26%, respectively, but with no dye.
As shown in the data of Fig. 5.8, the chromaticity coordinates for all samples
regardless of the dye are closer to the diagram edge than the samples without dye.
This quantitatively shows that the inclusion of these dyes improves color quality for
reasons previously discussed. Furthermore, for all samples regardless o f the specific
dye, the chromaticity coordinates increase radially outward as the dye concentration
increases. This is consistent with the fact that as the dye concentration increases, the
absorption increases. Thus, there is a greater decrease in the effective reflected full
width half maximum resulting in a more saturated color.
The sample with the C6 dye has the chromaticity coordinates closest to the diagram
edge in the region of yellow reflection. Yellow is the area around the chromaticity
coordinates of the 26.5% and 26% chiral concentration samples without dye. (The
sample with 2.14% R4 has chromaticity coordinates close to the diagram edge, but
this is in the reflected orange color region.) Optical examination of the samples also
shows that the C6 samples have the best yellow color. This could be due in part to the
fact that the C6 dye attenuates enough of the light to improve the color quality but not
so much as to significantly reduce the overall reflected intensity. The absorption
spectrum of the R4 and DR-13 dyes overlap a larger region of the Bragg reflection
range and while this improves color quality it also reduces more of the total reflected
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146
intensity. Thus, the net effect is a reflected yellow not quite as good as that from the
C6 samples.
5.4 Calculation of the Reflection Spectrum from CLCs with Dichroic Dyes
The dynamic theory o f reflection is used to calculate the reflection spectrum for the
absorbing CLCs investigated experimentally in the previous section (5.3.2). This
approach can be used because the equations for the theory in Chapter 2 are still valid
except that the index of refraction is now replaced with the complex index of
refraction. The dynamic theory of reflection considers normally incident light so the
calculated results can be compared to the experimental results because the
measurements are made at near normal incidence.
The samples investigated experimentally are of enough thickness (5 microns) such
that almost all light is reflected within the 5 micron distance31. Consequently, this
simplifies the calculation because it allows the use of the reflection equation, Eq. (17),
for a semi-infinite thick sample which was developed in Chapter 2. This equation is
still valid for the absorbing case except that the index of refraction must be replaced by
the corresponding complex quantities. So the quantities become (where here a bold
text indicates a complex quantity); Q = Jr8n/n and e = 2rc(nP-X.)A,. The complex
quantities can be written as,
(87)(88)
ne = ne - i k e andn0 =n0- i k 0 (89)
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147
where ke and k0 are the principle absorption coefficients.
The values for the principle absorption coefficients are obtained from the modelled
absorption curves for a given dye (either DR-13, R4 or C6). Substitution of these
values into Eq. (17) and some algebraic work to handle the complex numbers is
conducted to calculate the reflection spectra for the samples with the respective dyes.
As before, reflection spectra are calculated for samples with the largest dye
concentrations because these samples had the largest absorption values and thus
produce the most easily observed effects.
The curves in Fig. 5.9 are a plot of the calculated reflection spectra for samples
with no dye, 2.23% DR-13, 2.14% R4, and 2.4% C6, respectively. The reflection
spectra for all samples show a decreased amplitude vis a vis the sample with no dye at
short wavelengths and a gradual rolling increase out to the longer wavelengths. The
sample with the higher absorbing material, DR-13, had a greater decrease in amplitude
than the sample with R4. The sample with R4 had a slightly greater decrease in
amplitude than the sample with C6. All samples had a slightly decreased FWHM as
compared to the sample with no dye. The calculated results are consistent with what
is expected.
5.5 Comparison of Calculated Reflection Spectra to Measured Results
Figure 5.10 compares the measured and calculated reflection spectra for the
samples with 2.23% DR-13, 2.14% R4 and 2.4% C6. As shown in the figure, there is
good agreement between the calculated and observed results. The calculated
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148
0.6
no dye0.5C6
0.4 R4
| 0.3 D R - 1 3CJQJCU^ 0.2
0.0400 500 600 700
w a v e l e n g t h ( n m )
Fig. 5.9. Plot shows collectively the calculated reflection spectra with
the various dyes.
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0 .5
2.23% D R -1 30.4
0.3
0.2
0.0
0.4 2.14% R4
0.3
0.2
0.0
2.4% C60.4
0.3
0.2
0.0400 500 600 700
w a v e le n g t h (n m )
Fig. 5.10. Comparison of the measured (solid line) to the calculated
(dashed line) reflection spectra for samples with the three dyes.
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150
reflection spectra show a similar increase in amplitude from short to long wavelength
as observed in the measured results. The overall amplitudes between the calculated
and measured results are about the same. The calculated results show a slightly
greater FWHM than the measurements. The good agreement between the calculations
and measurements provides further support to the physical model developed to explain
the change in reflection spectra by the inclusion of a dichroic dye with an overlapping
absorption spectrum into the Bragg reflection band.
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Chapter 6
Multi-color Displays
This chapter discusses the use of chiral nematic liquid crystals to make a
multi-color display. Chiral nematic liquid crystals have several inherent advantages in
making a color display49,50: CLCs selectively reflect light and thus produce color
without the use of color filters. Furthermore, a given reflected color is easily produced
by merely using the appropriate concentration of chiral compounds. The chapter
begins with a discussion on additive color mixing whereby a large gamut of colors can
be produced by using only three primary colors. Next, techniques to pixelate a display
by using a mechanical rib/channel separation approach is presented51. Then, an
approach to pixelate a display using a photochemical technique is discussed52. Finally,
a hybrid approach using elements from the mechanical separation technique and the
photochemical approach to pixelate a display is presented.
6.1 Introduction
The previous chapters have established the optimum conditions to fabricate,
illuminate and obtain high color quality for a reflective CLC display. However, the
type of display discussed in these chapters reflected only one color in the planar state.
It is highly desirable to develop a display that can reflect many colors in the planar
151
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152
state and have control over the exact color reflected. The following discusses several
approaches towards developing a multi-color display.
6.1.1 Additive Color Mixing
Specifically, the attribute of color being discussed is hue. As mentioned
previously, different hues are perceived as green, yellow, red, etc. One way to
produce these different hues is to change the wavelength of the light. For example,
light with a wavelength o f 590 nm appears orange, light with a wavelength of 580 nm
appears yellow, and light with a wavelength o f 610 nm appears red. While light of
these hues can be associated with a specific wavelength, there is another technique that
can be used to produce these hues (or any hue in general) that does not contain the
specific wavelengths listed as examples. Two (or more) colors can be combined to
generate a hue that is not a hue of either of the component colors. This phenomena is
called additive color mixing.
For example, red and yellow can be mixed together and the eye perceives this hue
as orange. The incident light would have wavelengths of 580 nm and 620 nm. So
while there is no wavelength around 590 nm, the eye combines these colors to
perceive the hue as orange.
A quantitative illustration of additive color mixing is facilitated by the use of the
chromaticity diagram. Specific red and yellow colors are represented by the circles as
shown in Fig. 6. la. If equal amounts of these two colors are added then the perceived
color (orange) would be the color (denoted by a square on the chromaticity diagram)
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153
0 .6yellow
0.5 yellowisnorange orange ^
0.4
0.3
0.2
0.0green
0.5 red
0.4
0.3
0.2
blue
0.0
0.5 red
0.4 pink
'reddishpurple/0.3
0.2
blue
0.00.0 0.1 0.2 0.3 u* 0.4 0.5 0.6 0.7
Fig. 6.1. Several examples of additive color mixing.
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154
shown on a line half way between the two colors. If the amount of yellow was twice
as much as red, then the perceived color would be on a line between the two given
colors of red and yellow, but one third the distance from the yellow color chromaticity
point, or equivalently stated, two thirds the distance from the red color chromaticity
point. This color would be perceived as yellowish orange and is denoted by a triangle
on the chromaticity diagram of Fig. 6.1a.
By using a set of three primary colors, virtually all colors can be produced by
additive color mixing. This is the principle that makes a multi-color display feasible,
because it is only necessary to produce three primary colors to generate a range of
literally millions o f different colors.
There are different sets o f primary colors that can be used. The definition o f a
primary color is that it cannot be produced by the additive combination of the other
two colors and that the addition of all three colors in some combination can produce
white. The typical primary colors used in a display are the colors red, green and blue.
The chromaticity diagram can be used to show the entire color gamut produced by
a set of three primary colors. As an example, a given set of three primary colors (in
this case red, green, blue) are shown as circles on Fig. 6. lb. Lines are drawn between
the three primary colors. All colors within the triangle formed by the lines can be
produced by additive color mixing. As indicated in the diagram, this is a large range of
colors.
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The following is an example of color mixing using the three primary colors. If
equal amounts of blue and red are added together, the resulting color is reddish purple
(denoted by the square on the diagram in Fig. 6.1c). Note that the color chromaticity
coordinate lies on a line half-way between the two chromaticty coordinates of the
primary colors red and blue. Now, if a small amount of green is added, the resulting
chromaticity coordinate (denoted by a triangle in the chromaticity diagram) lies on a
line between the coordinate labelled by the square in the diagram and the primary
green color chromaticity coordinate. Because only a small amount of green was
added, the final resulting chromaticity coordinate from the addition of all three colors
lies a little to the left of the chromaticity coordinate labelled with the square in the
diagram. This resulting color would be perceived as pink.
6.1.2 Pixelation
The previous section has shown that only three primary colors are needed to
generate a gamut of colors through additive color mixing. Thus, in a reflective
multi-color CLC display, a mechanism is required to spatially separate (to regions as
small as 100 microns in width) regions of chiral liquid ciystal with three different
pitches, where one pitch reflects red, one green and one blue. This three pitch section
can then be repeated to form the entire multi-color display.
Separation o f regions with different pitch requires some work. Furthermore,
spatial separation o f regions of different pitch for any length of time is difficult because
as the name liquid crystal implies, the material is a liquid and thus easily diffuses. The
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156
following presents three approaches towards pixelation o f a reflective CLC display to
achieve multi-color.
6.2 Mechanical Approach
In the general mechanical approach, some method is used to form thin ribs that
extend from the top to the bottom of the cell51. The regions between the ribs are
individual channels that are now mechanically separated from each other. Various
materials can be used to form the substrate and ribs. The key requirements are that the
ribs effectively isolate the material between the ribs (e.g., no leakage) and that the rib
layout enables a means to fill the individual channels with the appropriate material.
Various schemes can be devised to fill the channels with material of the appropriate
pitch.
6.2.1 Lithographic/Etch Technique for Rib/Channel Formation
The goal of this effort is to develop a cell that has two colors. The
motivation is to verify that the mechanical approach can work at least on a large scale
with the materials utilized in this effort.
For rib formation, an investigation is conducted on various easily accessible
materials that can be deposited relatively uniformly on a glass substrate to a thickness
of around 5 microns without excessive cracking in the material. Also, the material is
required to have the ability to be lithographically defined and easily etched. Of the
materials investigated, the best results are obtained with a black polymide made by
Brewer (dare 100). By increasing the viscosity (mixing the polymide in a 1:1 as
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157
opposed to a 2:1 ratio with a solvent) and reducing the spin speed (from 2000 rpm to
500 rpm), it is possible to deposit a layer of the polymide 5 microns thick. This
material is deposited on glass pieces with dimensions of 2" by 2".
Figure 6.2a shows a diagram of the mask used to define the areas to be etched.
The rib area is about a 0.4 mm in width and the channel area about 2 mm in width. At
one end o f the cell, there are alternating areas where material is removed unblocking
one channel end. At the opposite end, the channel is blocked. This design allows for
filling material of one pitch into alternating channels as shown in Fig. 6.2b. And then
by removing the display from the fill station and rotating it 180 degrees, the other
channels can be filled with a material of a different pitch.
After the dare 100 polymide is deposited across the entire surface of one piece of
glass, standard photoresist is deposited across the entire surface. Using the mask
shown in Fig. 6.2a, the channel areas are defined by developing the photoresist.
Finally, the remaining photoresist is removed with a suitable solvent. Now, the bottom
glass piece of the cell has 0.4 mm width ribs that are 5 microns in height with
alternating block layers at each channel edge. The glass piece is then baked at 200 C
for 1 hour to cure the polyimide.
The top glass piece o f the cell has a 300 nm layer of the same Brewer dare 100
polyimide deposited across the entire surface. In the uncured state, the polyimide is
slightly soft and malleable. Consequently, when the top glass piece is brought into
contact with the bottom piece and slight pressure is applied, the ribs push into the top
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158
n
^ 7channel ^
blocking layer
(a)
step 1
rotate 180 deg. ■
filling trough
pitch 1 (e.g., blue)
step 2
already filled with pitch 1 from step 1
pitch 2 (e.g., yellow)
t11(b)
filling trough
Fig 6.2. View of rib/channel layout (a) and method to fill alternating channels with
different pitch material (b).
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159
polyimide layer. This provides a seal to prevent diffusion of liquid crystal material
between adjacent channels through the top o f the rib and top glass piece contact area.
Of course, as long as there is no cracking or other rib defect, the polyimide ribs
prevent diffusion of the CLC material between channels.
The cell has one set of channels filled with CLC material with a pitch adjusted to
reflect blue. The cell is removed from the fill station, rotated 180 degrees, and has the
other set of channels filled with CLC material with a pitch adjusted to reflect yellow.
Figure 6.3 shows the completed cell. There are several areas where there is
leakage and incomplete filling. But as shown in the figure, there is an area that has
well defined pixels of yellow and blue. This photograph was taken three months after
filling and there is still no interdifiiision of material between these channels. This result
indicates that it is possible to fabricate a multi-color reflective display using the
mechanical separation technique discussed. Continued work is required to identify the
optimum rib material to prevent leakage. Also, the material has to be definable to
linewidths on the order of 10 microns.
6.3 Photochemical Approach
Another method to pixelate a cell to make a multi-color display is to use
compounds that are sensitive to light or temperature53. By using some technique to
control (e.g., mask) the application o f either heat or light, pixelated areas can be
defined. The following discusses the use of chiral compounds that have an ultra-violet
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160
Fig. 6.3. Sample using ribs for two color display
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161
(UV) light sensitive chiral element. Upon illumination with UV light the chirality can
be removed.
An investigation o f UV cleavable chiral compounds showed they could be placed
into one o f two categories. Those compounds that after UV illumination have the
chirality chemically removed so that there are two new compounds, neither one which
is chiral. Or, compounds that are converted to a racemic mixture. In other words,
starting with a compound that is say right-handed, after illumination, a percentage of
the material becomes left-handed. Thus, the fraction that is left-handed compensates
the same fraction of right-handed material to make that fraction of the mixture
racemic, and thus nonchiral.
The approach to pixelate a cell is to start with a material with a given pitch to
produce some color, say yellow. Then the UV cleavable chiral mixture with the
correct handedness is added to the mixture to decrease (or increase) the pitch until the
desired reflected wavelengths (color) is achieved, say blue. By placing a mask over
the cell, selected areas can be illuminated with UV light. Those areas that are
illuminated will have the chiral concentration decrease, thus the pitch will increase
resulting in a different reflected color. If the area is illuminated long enough, all UV
sensitive chiral material will be made nonchiral and the original color restored. Per the
example then, selected areas of blue and yellow could be created, where masked areas
remain blue, and unmasked areas return to yellow after UV illumination.
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162
One requirement on the UV cleavable chiral material is that it have a large helical
twisting power (HTP). The larger the HTP, then the less material that must be added
to a mixture to achieve a given pitch. Furthermore, it is desirable to start with red and
be able to add the UV cleavable material in sufficient quantity to reach violet so the
entire color spectrum can be reached with a single mixture. The best material
identified to date is the binapthalene compounds. It has the largest HTP and has
chirality o f both left and right handedness. Using the right handed binapthol material,
a mixture can be taken from red to blue. However, the solubility limit is just about
reached at concentrations (about 8%) to produce blue.
A standard chiral (the chirals are right-handed) mixture (E48, CB15, R1011, CEl)
is prepared with a chiral concentration adjusted for a pitch to reflect red. The
right-handed binapthol material is added (about 4%) to decrease the pitch until a
reflected yellow color is produced. Half of the cell is then masked and the sample is
illuminated at a high UV intensity of 17 mw/cm2 for 1 hour. The cell on the left
shown in Fig. 6.4a is the result. The half of the cell that is masked remains yellow and
the portion that is illuminated returns to the original red color. Another cell has a
standard chiral concentration adjusted for a pitch to reflect green. The left-handed
binapthol material is added (about 3%) to increase the pitch so the reflected yellow
color is produced. Half of the cell is then masked and the sample is illuminated at a
high UV intensity of 17mw/cm2 for 1 hour. The cell shown on the right of Fig. 6.4a is
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163
Fig. 6.4. Color change as the result of UV illumination on samples with (lower)
and without (upper) polymer.
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164
the result. The half of the cell that is masked remains yellow and the portion that is
illuminated returns to the original green color.
The photographs shown in Fig. 6.4a were taken one day after their preparation. A
careful examination of both cells shows small undulations where the two colors meet.
This is due to diffusion. Within three weeks all cells prepared in this fashion show
significant interdiffusion rendering them unusable for display purposes.
To reduce interdiffusion o f samples prepared with photo-cleavable chiral
compounds, the BAB monomer (0.9%) is added to the mixture and polymerized along
with the formation of the pixelated areas. The polymer significantly increases the
effective viscosity of the material. Two cells prepared in this fashion are shown in Fig.
6.4b. These photographs were taken six months after the samples were prepared. As
shown in the figure, there is now little interdiffusion between the different pitch areas.
However, for practical display purposes, interdiffusion between pixels probably should
be less than 5% of the pixel area. This translates into an interdiffusion length of less
than 10 microns. Further studies are required to establish the exact interdiffusion
lengths and interdiffiision times for samples using polymers and pixelated with
cleavable chiral compounds.
6.4 Hybrid Approach
The two previous approaches have particular advantages and disadvantages. The
mechanical separation techniques prevent interdiffiision of different pitch material, but
it is difficult to devise approaches to separately fill three channels with the three
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165
primary colors. The photochemical approach makes separation o f different pitch
areas relatively easy, but there is no simple way to use this approach to prevent
interdiffiision. A combination o f both approaches incorporates the advantages of both
but removes the disadvantages.
A cell can be made with the ribs without any detailed layout design (such as
alternating blocking layers). The only requirement in the hybrid approach is that the
ribs do not allow leakage between adjacent channels. The cell is filled with a standard
chiral mixture that originally has a pitch to reflect red, but has enough of a
right-handed photo-cleavable chiral compound to decrease the pitch so the material
reflects the color blue. The entire cell is filled with the blue mixture. Then by using a
mask, the individual channels are illuminated with UV light to produce the desired
color. Typically, this will be a series o f reds, greens, and blues.
To determine the feasibility of this approach, an early prototype cell with 15 lines
per inch is used. The standard chiral mixture with a pitch adjusted to reflect red is
prepared. The right-handed binapthol compound is added to the mixture to decrease
the pitch until the material reflects green. The entire cell is vacuum filled with this
mixture. By using a mask, a repeated three channel sequence is used to produce three
colors. In the sequence, two channels are opened and one masked and the cell is
exposed to high intensity (17 mw/cm2) UV light until the reflected color becomes
yellow. Then one o f the two exposed channels is masked in addition to continuing to
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166
mask the previously covered channel while the cell is exposed to UV irradiation until
the remainng channel becomes red.
Figure 6.5 shows the resulting cell several days after fabrication. The cell has a
sharply defined three color sequence of red, yellow and green. There is no
interdiffiision between the colors. This result indicates the hybrid approach is a viable
technique to produce a multi-color display.
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167
Fig. 6.5. A three color hybrid display
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Chapter 7
Conclusions
This is believed to be the first detailed experimental investigation of the reflective
properties from the imperfect planar texture o f cholesteric liquid crystals. The results
from this research identified optimal illumination and viewing conditions for
commercially produced reflective cholesteric displays. In addition, improved color for
monochrome and multiple color displays are discussed.
The planar texture is fractured into domains by using a dispersed polymer network
and the physical properties o f the material studied by various procedures. A method to
calculate the reflective properties from a distribution of differently oriented domains is
developed. The results show that the reflective properties of imperfect CLCs are a
function of domain parameters which include size, shape, helical axis orientation, and
pitch.
The preparation of CLC samples with a polymer network is discussed and it is
shown that as the polymer concentration is increased, the domain size decreases and
there are significant changes in the reflection spectrum. Optical microscope and SEM
examinations indicate that the domains are generally the thickness of the cell gap
spacing but that the cross-sectional areas are of larger dimensions and depend on the
polymer concentration.
168
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169
A model is developed to describe the reflected intensity as a function o f polymer
concentration, incident light and detector angle. The model describes the inclusion of
a polymer network in a CLC as having two effects on the reflected intensity. First,
increasing polymer concentration increases the distribution in orientation o f the helical
axes. The increased misorientation of the helical axes causes a larger angular
distribution of the Bragg reflected light for a given incident light angle and thus
improves the viewing angle. Second, an increasing polymer concentration creates
larger defect volumes that cause an overall total reduction in Bragg reflected intensity
at all angles. The reduction is found to be on the order of 50 % for the higher polymer
concentration samples.
Measurements are conducted to experimentally determine the Bragg reflected
intensity as a function o f detector angle for a given incident light angle. A reasonably
good fit is made between the experimentally measured results and the model. From
the fit of the model to the data, the distribution in orientation o f helical axes as a
function o f polymer concentration is determined. The distribution is Gaussian with a
standard deviation around two degrees for low polymer concentrations and around
seven degrees for the higher polymer concentrations.
Having determined the size, shape and orientation distribution of the domains as a
function of polymer concentration, the generalized procedure to determine the
reflective properties of imperfect CLCs is used to calculate the reflection spectra.
Because the domains have planar boundaries, the 4x4 Berreman method is used in the
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170
general approach. A good fit of the calculations to the measured reflection spectra is
obtained when a distribution in pitch as a function o f polymer concentration is
included. The pitch distribution could be modeled with a Gaussian function with a
standard deviation of 0.8% of P0 for medium polymer concentrations and 6% of P0 for
the higher polymer concentrations, where P0. is the natural pitch for the chiral
concentrations used.
The physical analysis, angular reflection measurements, reflection spectra
measurements and fit o f the models to the data provide a reasonable understanding of
the basic physical characteristics and optical properties of polymer modified
cholesteric liquid crystals. Furthermore, this approach can be used to calculate the
reflective properties from different imperfect cholesteric liquid crystal systems.
Samples that have pitches to reflect yellow or green and optimal polymer
concentrations are selected for a detailed study on illumination/detection conditions.
The samples are illuminated at incident angles of 10, 29, 48 and 65 degrees,
respectively. Reflected luminance, contrast ratio and chromaticity coordinates are
measured in both the azimuthal and polar planes for each incident light angle. The
results show a symmetry in reflection about the zero degree polar plane which allows
for equivalent off-axis illumination of this type o f display. There is a slight decrease in
reflected luminance and a decrease in reflection symmetry in the azimuthal plane for
incident light angles from normal out to 30 degrees and a significant decrease for
incident light angles from 30 degrees out to 65 degrees. The contrast ratio is relatively
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171
independent of incident light angle near the zero-degree detection angle. The viewing
angle as reported here is largest for near-normal incident light angles and decreases
monotonically with increasing incident light angle. The smallest change in hue with
detector angle is for near normal incident light angles. Two-dimensional polar plots of
luminance and contrast ratio are presented. A model is developed to explain the
observed results. Optimal illumination conditions are determined from the measured
results and the model and for a polymer modified reflective cholesteric display is
illumination directly from the front. However, there is only a slight decrease in display
properties for incident light angles out to 30 degrees, particularly when viewed from
the front.
It is shown that color quality is degraded as the pitch is increased to reflect longer
wavelengths (yellow, orange, red) because of the inherent increase in reflected spectral
bandwidth. Theoretical calculations show that the inclusion of an absorbing dye in the
material can significantly affect the reflection spectrum. With the choice of a dye that
overlaps only a portion of the Bragg reflection band, the reflected spectral bandwidth
can be reduced. Three dichroic dyes are identified that have absorption spectra with
differing degrees of penetration into the Bragg reflection band for a CLC that reflects
the color yellow. Reflection spectra are measured from samples that have vaiying
concentrations of the three dyes. There is a decrease in reflected amplitude where the
dye absorption spectrum overlaps the Bragg reflection band. There is a greater
decrease in reflection amplitudes for the dyes with an absorption spectrum that
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172
penetrates further into the Bragg reflection band. The modified reflection spectra for
each dye also have a reduced spectral bandwidth. The chromaticity coordinates are
measured for the samples and the results show there is a quantitative improvement in
the reflected yellow color quality (the color is more saturated). Visual observation
shows the samples with the C6 dye produce the best yellow color to the eye. The
approach of using dichroic dyes to improve color quality is currently being used in the
commercial production of reflective color displays.
Several approaches are developed to produce a multi-color display. In one
approach, standard photo-lithigraphic/etching techniques are used to form mechanical
ribs made with a black polyimide (dare 100) from Brewer. Alternate channels are
filled with either a blue or yellow reflecting CLC to form a two-color display. This
development shows the mechanical approach to forming a multi-color display is
feasible, but some effort is required to devise a scheme to fill the channels with
different pitch material. Another possible approach is the use of photo-cleavable chiral
compounds. In this approach, the binapthalene compounds are found to have the
highest twisting power. The addition of these compounds to the standard chiral
mixture changes the pitch. After adding the photo-cleavable compound to the
standard chiral mixture, the cell pixels are formed by using a mask to define areas
where the chirality can be changed through UV illumination of the exposed material.
Using this approach on several samples shows that different color areas can be
created. However, there is significant interdiffiision between pixelated areas.
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173
Including a polymer with the material significantly reduces the interdiffiision. More
research is required to determine if the interdiffiision has been reduced enough for
display use. Finally, a hybrid approach is pursued to utilize the advantages inherent in
both the mechanical and photochemical approaches. A cell is fabricated with
mechanical ribs and filled with a mixture containing the photo-cleavable compounds.
Using masks, different color areas are now easily formed by exposing different
channels to differing amounts of UV irradiation. The mechanical ribs prevent the
interdiffiision of material. The hybrid approach appears to be another promising
technique to produce a multi-color display.
This research developed a good understanding of the reflective properties of
imperfect CLCs formed by the introduction of a polymer network. Future work needs
to be conducted on the reflective properties of imperfect CLCs produced by other
techniques such as cell wall surface treatments. In addition, a detailed study should be
conducted on the formation and scattering properties of these materials in the focal
conic state. Besides providing a fundamental understanding of the scattering
properties, this study could determine how to reduce scattering in the focal conic state,
which would result in better contrast ratios. While the present research improved the
reflected yellow color quality, further work should be conducted on the use of
different dyes to improve the color quality of orange and red. Development of hybrid
multi-color cells should continue so that a high resolution (at least 300 lines per inch)
display can be produced in the near future.
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