Development of a Novel Visualization and Measurement Apparatus for the PVT Behaviours of
Transcript of Development of a Novel Visualization and Measurement Apparatus for the PVT Behaviours of
Development of a Novel Visualization and Measurement Apparatus for the PVT Behaviours of Polymer/Gas Solutions
by
Yao Gai Gary Li
A thesis submitted in conformity with the requirements for the degree of Doctor of Philosophy
Department of Mechanical and Industrial Engineering University of Toronto
© Copyright by Yao Gai Gary Li 2008
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Development of a Novel Visualization and Measurement Apparatus for the
PVT Behaviours of Polymer/Gas Solutions
Yao Gai Gary Li
Degree of Doctor of Philosophy 2008 Graduate Department of Mechanical and Industrial Engineering
University of Toronto
ABSTRACT
The Pressure-Volume-Temperature (PVT) for polymer/gas solutions is an important
fundamental property of which accurate data measurement has not been reported until recently.
The diffusivity, solubility, and surface tension are critical physical properties of polymer/gas
solutions in understanding and controlling polymer processing such as, foaming, blending, and
extracting reaction. However, the determination of these properties relies on accurate PVT data
as a prerequisite. Due to the difficulties involved in measuring the specific volume while
maintaining a sufficiently high pressure and temperature to achieve a single-phase polymer/gas
solution, accurate PVT data or volume swelling measurement of polymer/gas solutions is not yet
available. In this research, a new methodology was proposed and developed for direct
measuring the PVT properties of polymer melts saturated with high-pressure gas at elevated
temperatures. The ultimate goal is to develop and construct an apparatus that would provide
more accurate fundamental properties through PVT measurement to the foaming industry,
which is heavily involved with polymer/gas mixtures.
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In memory of my grandfather Liang who passed away during my Ph.D. program
your love, support and encouragement will always be
in my heart and my soul
To those who are affected
in the catastrophic earthquake in my home province
at the extremely difficult time our hearts unite
May God Bless Us and Our Nation
To my great parents
give me the chance to live for their endless love and support
during good and bad times I owe it with all of me
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Acknowledgements
I would like to express my sincere gratitude to my supervisor Professor Chul B. Park for
providing guidance and encouragement throughout my research. I would like also to thank my
Ph. D. thesis committee: Prof. Yu Sun, Prof. Hani Naguib Prof. Craig Simmons and the external
examiner Prof. Musa Kamal.
My gratitude is extended to the Department of Mechanical and Industrial Engineering at
the University of Toronto for providing the University of Toronto Open Fellowships. Especially
I like to thank Brenda Fung from the Graduate Office for her help during my graduate study
years. I also like to thank Sheila Baker from the purchasing office for making all the purchasing
an easy job. Also my thanks go to Teresa Wang and Geoffrey Chow. I like to also thank Oscar
Del Rio for his support in dealing with computer problems.
I also wish to acknowledge the professional technical support from Jeff Sansome, Dave
Eisdaile, Mike Smith, Len Rooseman, and Thai Do in the Machine Tool Laboratory.
I would like to thank my colleagues in the Microcellular Plastics Manufacturing
Laboratory for their support and friendship. With their help and encouragement, the Ph.D.
became more enjoyable. So my special thanks go to Dr. Jin Wang, Dr. Donglai Xu, Dr.
Gangjian Guo, Dr. Guangming Li, Dr. Hongbo Li, Dr. Patrick Lee, Dr. Qingping Guo, Dr.
Zhenjing Zhu, Dr. Takashi Kuboki, Dr. Kyungmin Lee, Dr. Balasubramanian Maridass, Dr.
Bhuwnesh Kumar, Dr. Kelvin Lee, Dr. Xia Liao, Dr. Wenli Zhu, Lilac Cuiling Wang, Sue
Chang, Kelly Jinjin Zhang, Nan Chen, Wang Jing, Sunny Leung, Anson Wong, Raymond Chu,
Jeff Qingfeng Wu, Richard Lee, John Lee, Peter Jung, Ryan Kim, Mohammed Hassan,
Mohammed Serry, Johnny Park, Kanghong Lee, Esther Lee. Their support is so valuable in
helping me to finish the thesis.
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My students Fedir Gul, Satbinder Dhesy and Yu Shuang Zhu also contributed a lot to
this research project.
I also want to thank Dr. Dean Peachy, Melissa Miller and their son Daniel of my home
stay family. They have become my Canadian family while I am far away from home. They did
not just provide me a place to live, but also give me the parental care, support and help at the
crucial first year when I tried to get acquainted to this new environment.
A Chinese proverb says “At home one relies on one’s parents, and outside on one’s
friends”. I had felt this tremendously from the understanding, support, and encouragement I
have received from my friends over those years. Although we may be far apart from some of
you at this moment, but the friendship would last forever. Could not really name each every of
them here, but just a few, they are Uncle David Xue, Auntie Huang, Uncle Hao’s family, Auntie
Kong’s family, Emmanuel Chen’s family, Dr. Hongbo Li’s family, Ross and Nancy Hayes,
Jeannette Zhang, Yvonne Feng, Audrey Lin, Alfred Sum, Jean Hsu, Xuan Yang, Tara Wu.
A special tribute needs to be paid to April Binnie for proof reading my thesis.
Finally I like to take this chance to express my deepest gratitude to my family, my
relatives and friends in China. Their endless love, continuing support, tremendous amount of
encouragement and patience made it all possible for me to completed school journey today.
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Table of Contents
Abstract …………………………………………………………………………………………ii
Dedication ………………………………………………………………………………………iii
Acknowledgements …………………………………………………………………………….iv
Table of Contents ……………………………………………………………………………....vi
List of Figures ………………………………………………………………………………….xi
Nomenclature ……………………………………………………………………………….....xv
Chapter 1. Introduction ................................................................................................................ 1
1.1 Preamble ........................................................................................................................... 1 1.2 Thermoplastic Foams ....................................................................................................... 2 1.3 Plastic Foaming Process ................................................................................................... 4
1.3.1 Introduction ..................................................................................................... 4 1.3.2 Batch Process ................................................................................................... 5 1.3.3 Continuous Process .......................................................................................... 6
1.4 PVT Measurement ............................................................................................................ 9 1.5 Role of PVT in Solubility and Surface Tension ............................................................. 10 1.6 Motivation and Scope/ Objective ................................................................................... 13 1.7 Thesis Contribution ........................................................................................................ 15 1.8 Thesis Organization ........................................................................................................ 16
Chapter 2. Literature Review ..................................................................................................... 19
2.1 Background on PVT Property Measurement .................................................................. 19 2.1.1 PVT Measurement for Pure Polymer ............................................................ 19 2.1.2 PVT Measurement for Polymer/Gas Solutions ............................................. 21
2.2 Background on Polymer/Gas Solutions Property ........................................................... 27 2.2.1 Solubility and Diffusivity .............................................................................. 27 2.2.2 Nucleation ...................................................................................................... 35 2.2.3 Surface Tension ............................................................................................. 37
2.2.3.1 Spinning Drop Method ...............................................................41 2.2.3.2 Drop Shape Techniques .............................................................42
2.3 Background on 3-D Object Reconstruction from 2-D Images ....................................... 45 2.3.1 Introduction ................................................................................................... 45 2.3.2 Active 3-D Reconstruction Method ............................................................... 45
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2.3.3 Passive 3-D Reconstruction Method ............................................................. 46 2.3.3.1 Multi-view Stereo Method .........................................................47 2.3.3.2 Model-based Multi-view Stereo Method ...................................48 2.3.3.3 Volumetric Modeling Method ...................................................49 2.3.3.3.1 Shape from Silhouettes ...........................................................50 2.3.3.3.2 Shape from Photoconsistency .................................................55
2.4 Summary ......................................................................................................................... 56 Chapter 3. Theoretical Background .......................................................................................... 58
3.1 Theoretical Background on Equation of State ................................................................ 58 3.1.1 Introduction ................................................................................................... 58 3.1.2 Equation of State (EOS) ................................................................................ 59 3.1.3 Equations of State for Polymers and Polymer/Gas Solutions ....................... 60
3.1.3.1 Introduction ................................................................................60 3.1.3.2 Sanchez-Lacombe (SL) EOS .....................................................61 3.1.3.3 Simha-Somcynsky (SS) EOS .....................................................62 3.1.3.4 Statistical Associating Fluid Theory (SAFT) .............................63
3.2 Models of PVT Measurement ......................................................................................... 64 3.3 Solubility Measurement Using MSB .............................................................................. 66 3.4 Viscoelastic Models of Polymers ................................................................................... 68
3.4.1 Maxwell Equation .......................................................................................... 69 3.4.2 Boltzmann’s Superposition Principle ............................................................ 70 3.4.3 Doi-Edwards Model and Entanglement ........................................................ 70
3.5 Surface Tension Measurement ....................................................................................... 71 3.6 Summary ......................................................................................................................... 74
Chapter 4. Design and Construction of Novel Apparatus for PVT measurement ................ 75
4.1 Conceptual Design of PVT Measurement Apparatus ..................................................... 75 4.1.1 Introduction ................................................................................................... 75 4.1.2 Analysis of the PVT Apparatus for Polymer/Gas Solutions ......................... 77 4.1.3 Detailed Analysis and Decomposition of FRs and DPs ................................ 78
4.1.3.1 Hardware Attribute ....................................................................78 4.1.3.2 Future Decomposition of FR1 and DP1 (Second Level) ...........83 4.1.3.3 Software Attribute ......................................................................86
4.2 Detailed Design and Construction of the PVT Apparatus .............................................. 89 4.2.1 Overview of the Apparatus ............................................................................ 89 4.2.2 High Pressure and Temperature Visualization Chamber .............................. 90 4.2.3 Charged Couple Device (CCD) Camera and Optical Lens ........................... 93
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4.2.4 XY Stage and Precision Control .................................................................... 94 4.2.5 Rotational Device .......................................................................................... 94 4.2.6 Image Processing Terminal ........................................................................... 97 4.2.7 Light Source, Noise and Vibration Control ................................................... 97
4.3 Theory Background and Algorithms Construction ........................................................ 99 4.3.1 Edge Detection and Volume Integration for Axisymmetric Drop Shape .... 101 4.3.2 Algorithms for 3D Volumetric Calculation of Asymmetric Drop Shape .... 104
4.3.3.1 Rotation Device and Degree of Asymmetry ............................105 4.3.3.2 Modeling of Degree of Asymmetry: Radial Asymmetry .........106 4.3.3.3 Determination of the Reference Radius ...................................107 4.3.3.4 Definition of Degree of Asymmetry (DOA) ............................109 4.3.3.5 Volume Integration of Asymmetry Drop Shape ......................110
4.4 Integration of Hardware and Software GUI Interface .................................................. 113 4.4.1 XY Stage Control Software ......................................................................... 113 4.4.2 GUI Construction for Image Capture and Rotation ..................................... 114
4.5 Summary ....................................................................................................................... 115 Chapter 5. Validation of the Proposed Design ........................................................................ 117
5.1 Introduction .................................................................................................................. 117 5.2 Empirical Verification of Error Reduction from Image Reconstruction ...................... 117 5.3 Empirical Verification Using Tait Equation for Pure Polymer PVT ............................ 119
5.3.1 Experimental Procedure and Materials ........................................................ 119 5.3.2 Density Measurement for Pure Axisymmetric Linear and Branched PP .... 120 5.3.3 Density Measurement for Pure PS685D with Asymmetry .......................... 123
5.4 Summary ....................................................................................................................... 128 Chapter 6. Measurement of the PVT Data for Polymer/Gas Solutions ................................ 130
6.1 Introduction .................................................................................................................. 130 6.2 PVT Measurement with Axisymmetry for Linear/Branched PP/CO2 Solutions .......... 130
6.2.1 Experimental Procedure .............................................................................. 130 6.2.2 Experimental Setup ...................................................................................... 132 6.2.3 Experimental Materials ................................................................................ 132 6.2.4 Volume Swelling of Linear/Branched PP/CO2 ........................................... 132 6.2.5 Effect of Temperature and Pressure on PVT of PP/CO2 Solutions ............. 136
6.2.5.1 Effect of Temperature on Volume Swelling ............................136 6.2.5.2 Effect of Pressure on Volume Swelling ...................................136
6.2.6 Effect of Branch Structure on PVT of PP/CO2 Solutions ........................... 137 6.3 Measurement of PVT Data for PS and PS/Gas Solutions ............................................ 141
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6.3.1 Measurement of PVT Data with Asymmetry for PS and PS/CO2 ............... 141 6.3.1.1 Introduction ..............................................................................141 6.3.1.2 Experiment Procedure ..............................................................142 6.3.1.3 Experimental Material ..............................................................143
6.3.2 The Temperature Effect on the Degree of Asymmetry ............................... 143 6.3.3 Temperature and Pressure Effect of PVT of PS/CO2 .................................. 145 6.3.4 Measurement of PVT for PS/HFC-152a Solution ....................................... 146
6.3.4.1 Introduction ..............................................................................146 6.3.4.2 Experimental Procedure and Material ......................................148 6.3.4.3 Temperature and Pressure Effect of PVT for PS/HFC-152a ...149
6.4 Validity of Equation of States Using Experimental Results ......................................... 150 6.4.1 Volume Swelling From EOS Predictions .................................................... 150 6.4.2 Polymer Chain Entanglement Hypothesis ................................................... 154
6.4.2.1 Introduction ..............................................................................154 6.4.2.2 Small Amplitude Oscillatory Shear Method ............................156
6.4.3 Experimental Procedure and Materials ........................................................ 157 6.4.3.1 Sample Preparation ..................................................................158 6.4.3.2 Gap Zeroing .............................................................................159
6.4.4 Chain Entanglement of Linear and Branched PP ........................................ 160 6.4.4.1 Strain Sweep and Frequency Test ............................................160 6.4.4.2 Chain Entanglement of Linear and Branched PP .....................166
6.5 Determination of Accurate Solubility Based on the PVT Data .................................... 167 6.5.1 Corrected PP/CO2 Solubility from PVT Measurement ............................... 167 6.5.2 Specific Volume of Linear/Branched PP/CO2 ............................................. 174
6.6 Summary ....................................................................................................................... 178 Chapter 7. Measurement of Surface Tension for Polymer/Gas Solutions ........................... 181
7.1 Introduction .................................................................................................................. 181 7.2 Experimental Materials ................................................................................................. 184 7.3 Measurement of Surface Tension for Linear/Branch PP/Gas Solutions ...................... 184
7.3.1 Surface Tension for Linear/Branched PP/CO2 Solutions ............................ 184 7.3.2 Temperature and Pressure Effect on Surface Tension ................................. 188 7.3.3 Branch Effect on Surface Tension between Linear and Branched PP......... 192
7.4 Summary ....................................................................................................................... 195 Chapter 8. Conclusions and Future Work .............................................................................. 197
8.1 Conclusions .................................................................................................................. 197 8.2 Future work ................................................................................................................... 201
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REFERENCES…..………………………………………………………………………….. 203 Appendix 1…………………………………………………………………………………… 233
Appendix 2...…………………………………………………………………………………. 243
Appendix 3...…………………………………………………………………………………. 256
Appendix 4...…………………………………………………………………………………. 259
Appendix 5...…………………………………………………………………………………. 260
Appendix 6...…………………………………………………………………………………. 261
Appendix 7...…………………………………………………………………………………. 262
Appendix 8...…………………………………………………………………………………. 264
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List of Figures
Figure 1-1 Overview of Microcellular Foaming Process ................................................................ 5
Figure 1-2 Overview of a Batch Foaming Process .......................................................................... 5
Figure 1-3 Schematic of a Single Foaming Extruder ...................................................................... 6
Figure 1-4 MSB Solubility Apparatus Schematic and Working Principle .................................... 11
Figure 1-5 Building Blocks of Foaming Research and Industry ................................................... 14
Figure 2-1 Schematic of Bellow Type Dilatometer ....................................................................... 20
Figure 2-2 Schematic of LVDT Dilatometer ................................................................................. 24
Figure 2-3 Schematic of Modified MSB for Polymer/Gas PVT Measurement ............................ 26
Figure 2-4 Schematic of Critical Nucleation Radius and Activation Energy ................................ 36
Figure 2-5 Surface Tension and Gravity of Small Particle at Liquid/Particle Interface* ............. 38
Figure 2-6 3-D Object Reconstruction Scheme ............................................................................. 51
Figure 2-7 Visual Hull Construction from Volume Intersection ................................................... 52
Figure 3-1 Generalized Maxwell Model Represented by Spring-Damper Systems...................... 69
Figure 3-2 Sessile Drop Coordinate System Definition ................................................................ 73
Figure 4-1 Axiomatic Design Mapping Process from FRs to DPs ................................................ 76
Figure 4-2 PVT System Schematic ............................................................................................... 78
Figure 4-3 CAD Model of Chamber Body with Rotational Device .............................................. 92
Figure 4-4 CAD Model of the High T and P Visualization Chamber ........................................... 92
Figure 4-5 Location of Rotational Device and High T and P Rotary Seal .................................... 96
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Figure 4-6 Actual PVT Apparatus Setup ....................................................................................... 99
Figure 4-7 Methodology Flowchart for Axisymmetry Drop ....................................................... 100
Figure 4-8 Image Reconstruction Schematic ............................................................................... 101
Figure 4-9 Detected Sessile Drop Edge and Volume Integration over Vertical Span................. 102
Figure 4-10 Axisymmetric Drop Side and Top View Schematic ................................................ 103
Figure 4-11 Volume Determination at ith Level of Axisymmetric Drop Shape .......................... 103
Figure 4-12 Methodology Flowchart for Asymmetry Drop ........................................................ 106
Figure 4-13 Schematic of Reference Radius Definition .............................................................. 108
Figure 4-14 Radius Asymmetry at ith Level of Asymmetric Drop Shape ................................... 110
Figure 4-15 Asymmetric Circular Area after Nθ Rotations at ith Level ....................................... 111
Figure 4-16 Area Determination of the Circular Section within Angle θ ................................... 111
Figure 4-17 Volume Determination at ith Level of Asymmetric Drop Shape ............................. 112
Figure 4-18 XY Stage Software Control GUI ............................................................................. 113
Figure 4-19 GUI Interface of the Image Capture and Rotation ................................................... 114
Figure 5-1 Accuracy Improvement from Sphere Image Reconstruction ..................................... 118
Figure 5-2 Pure Linear PP Measured and Tait Calculated Densities .......................................... 122
Figure 5-3 Pure Branched PP Measured and Tait Calculated Densities ..................................... 123
Figure 5-4 Actual Sessile Drop Profile and Level Selection at 150oC ........................................ 124
Figure 5-5 Profile Top View at 150oC ......................................................................................... 124
Figure 5-6 Profile Top View at 200oC ......................................................................................... 125
Figure 5-7 Profile Top View at 250oC ......................................................................................... 125
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Figure 5-8 Profile Top View at 200oC from Cooling .................................................................. 126
Figure 5-9 Profile Top View at 150oC from Cooling .................................................................. 126
Figure 5-10 Density Measurement from Asymmetry Drop Shape and Tait Equation ................ 127
Figure 6-1 Linear PP/CO2 Swelling vs. a) Temperatures and b) Pressures................................. 134
Figure 6-2 Branched PP/CO2 Swelling vs. a) Temperatures and b) Pressures ............................ 135
Figure 6-3 Linear and Branched PP/CO2 Swelling at 180oC ...................................................... 138
Figure 6-4 Linear and Branched PP/CO2 Swelling at 200oC ...................................................... 139
Figure 6-5 Linear and Branched PP/CO2 Swelling at 220oC ...................................................... 139
Figure 6-6 Schematic of Semicrystalline Polymer Structure* .................................................... 141
Figure 6-7 Degree of Asymmetry of Pure PS at Temperature Rising and Cooling Process ....... 144
Figure 6-8 PS/CO2 Volume Swelling vs. a) Temperatures and b) Pressures .............................. 146
Figure 6-9 PS/HFC-152a Volume Swelling at 150oC and 190oC ............................................... 150
Figure 6-10 Linear PP/CO2 and EOS Swelling at 180oC ............................................................ 151
Figure 6-11 Linear PP/CO2 and EOS Swelling at 200oC ............................................................ 151
Figure 6-12 Linear PP/CO2 and EOS Swelling at 220oC ............................................................ 152
Figure 6-13 Branched PP/CO2 and EOS Swelling at 180oC ....................................................... 152
Figure 6-14 Branched PP/CO2 and EOS Swelling at 200oC ....................................................... 153
Figure 6-15 Branched PP/CO2 and EOS Swelling at 220oC ....................................................... 153
Figure 6-16 Schematic of SAOS Experiment Wave ................................................................... 157
Figure 6-17 ARES Rheometer ..................................................................................................... 158
Figure 6-18 Linear PP Strain Sweep Test.................................................................................... 161
Figure 6-19 Branched PP Strain Sweep Test ............................................................................... 161
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Figure 6-20 Linear PP 180oC Frequency Sweep Test ................................................................. 162
Figure 6-21 Linear PP 200oC Frequency Sweep Test ................................................................. 163
Figure 6-22 Linear PP 220oC Frequency Sweep Test ................................................................. 163
Figure 6-23 Branched 180oC Frequency Sweep Test .................................................................. 164
Figure 6-24 Branched PP 200oC Frequency Sweep Test ............................................................ 165
Figure 6-25 Branched PP 220oC Frequency Sweep Test ............................................................ 165
Figure 6-26 Linear and Branched PP Chain Entanglement Density at T above Tm .................... 166
Figure 6-27 Corrected Linear PP/CO2 Solubility at 180oC ......................................................... 170
Figure 6-28 Corrected Linear PP/CO2 Solubility at 200oC ......................................................... 171
Figure 6-29 Corrected Linear PP/CO2 Solubility at 220oC ......................................................... 171
Figure 6-30 Corrected Solubility of Branched PP/CO2 at 180oC ................................................ 172
Figure 6-31 Corrected Solubility of Branched PP/CO2 at 200oC ................................................ 172
Figure 6-32 Corrected Solubility of Branched PP/CO2 at 220oC ................................................ 173
Figure 6-33 Specific Volume of LPP/CO2 and BPP/CO2 at 180oC ............................................ 176
Figure 6-34 Specific Volume of LPP/CO2 and BPP/CO2 at 200oC ............................................ 177
Figure 6-35 Specific Volume of LPP/CO2 and BPP/CO2 at 220oC ............................................ 177
Figure 7-1 Surface Tension of Linear PP/CO2 at Various Temperatures and Pressures ............. 188
Figure 7-2 Equilibrium Surface Tension of PS/CO2 Solution ..................................................... 189
Figure 7-3 Surface Tension of Branched PP/CO2 at Various Temperatures and Pressures ........ 191
Figure 7-4 Surface Tension of Linear and Branched PP/CO2 at 180oC ...................................... 192
Figure 7-5 Surface Tension of Linear and Branched PP/CO2 at 200oC ...................................... 193
Figure 7-6 Surface Tension of Linear and Branched PP/CO2 at 220oC ...................................... 193
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Nomenclature
A = Helmholtz free energy (J) Ai = asymmetric circular shape area at ith layer of the drop profile (cm2) Aθi = area of each section on the circular shape within angle θi (cm2) [A] = design matrix
resA = residual Helmholtz free energy (J/mol) segmentA = segment Helmholtz energy per mole of molecules (J/mol)
chainA = Helmholtz energy increment due to bonding per mole of molecules (J/mol)
nassociatioA = Helmholtz energy due to associating per mole of molecules (J/mol)
2α = cross section of the penetrate molecule area (m2) 0B = constant 0β = strain amplitude
c = capillary constant C = solution concentration (mol/cm3) c = the number of external degrees of freedom per chain
sC = solubility of gas in the polymer (g-gas/g-polymer) D = diffusion coefficient (m2/s)
DPs = design parameters DE = cohesive energy density (J/mol*m3)
asymmetryE = radial degree of asymmetry (m2) FRs = function requirements
mFΔ = free energy of mixing (J) g = gravity (m/s2)
iG = relaxation modulus (Pa)
NG = plateau modulus (Pa) ( )ω'G 'G = storage modulus (Pa)
''G = loss modulus (Pa) ∗Δ homG = Gibbs free energy (J) h = thickness of the sample sheet (cm)
sHΔ = molar heat of sorption (J) H = enthalpy (J) H0 = Henry’s law constant
homJ = homogenous nucleation rate (per unit volume of polymer) (#/m3.s)
hetJ = heterogeneous nucleation rate (per unit area of nucleating agent)( #/m2.s)
K = Boltzmann’s constant ≈1.380658x10-23 (J/K)
12k = binary interaction parameter dimensionless L = final sample length (cm)
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0L = initial sample length (cm) M = Molecular weight
tM = mass uptake at time t (g)
∞M = equilibrium mass uptake after an infinite time (g) eM = entanglement molecular weight (g) masssamplem = initial sample mass (g)
spherem = sphere ball mass (g) mixturem = polymer/gas solution mass (g)
Mrotation = Number of rotation integer number N = number of points integer number
Nlayer = number of layer along drop profile integer number AN = Avogadro’s constant ≈6.0221367x1023 molecules/mol
Nφ = number of small circular section within angle φ P* = characteristic pressure (MPa) P~ = reduced pressure dimensionless
bubbleP = bubble pressure (Pa) sysP = solution system pressure (Pa)
PΔ = pressure difference across the gas and polymer/gas interface (Pa)
sP = saturation pressure (Pa) platep = perimeter of the plate (m) R = gas constant (J/K*mol) R1 = first principle radii of curvature (m) R2 = second principle radii of curvature (m) R0 = radius of curvature at the origin (m)
crR = critical nuclei radius (m) 0,θjr = drop radius at any angle (m)
tippedestalr = radius of sessile pedestal tip (mm) S = entropy (J) s = number of segments per chain dimensionless wS = volume swelling ratio dimensionless
T = Temperature (K or oC) T~ = reduced temperature dimensionless T* = characteristic temperature (K or oC) teq = equilibrium time (s) U = system internal energy (J)
fυ = total specific free-volume accessible for diffusion (cm3/g)
pυ = specific volume of the polymer (cm3/g)
0υ = specific occupied volume of the polymer chains (cm3/g) v = velocity of propagation (m/s)
V* = characteristic volume (cm3/g) 0v = constant
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1v = constant VΔ = change of sample volume (cm3) 0V = initial sample volume (cm3) BV = total volume of sample holder (cm3) PV = polymer sample volume (cm3) sV = swellon volume (cm3)
V(T,P teq) = equilibrium polymer/gas solution volume (cm3) V(T,P,tini) = initial volume of pure polymer (cm3)
volumesampleinitalV = initial sample volume (cm3) taitV = Tait calculated volume (cm3) θ,jV = volume at any angle (cm3)
sphereV = sphere ball volume (cm3) PPbranchedυ = specific volume of branched PP (cm3/g)
PPlinearυ = specific volume of linear PP (cm3/g) W = free barrier energy for nucleation (J) ( )TPW , = balance readout at P and T (g)
gW = gas dissolution in polymer (g) ( )TW ,0 = balance readout at vacuum and T (g) ω = rotational velocities (radian/s) ψ = phase angle (degree) x = interaction parameter dimensionless
apparentX = gas apparent solubility (g-gas/g-polymer) correctedX = corrected solubility (g-gas/g-polymer)
segZ = compressibility factor from segment chainZ = compressibility factor from chain
nassociatioZ = compressibility factor from association gφ = volume fraction of gas dimensionless
pφ = volume fraction of polymer dimensionless
gn = molar fraction of gas
pn = molar fraction of polymer lgγ = surface tension between gas and polymer/gas interface (mJ/m2)λ = jump length (m) θ = contact angle (degree) λ = wavelength (m) Ω = number of states accessible to the system dimensionless ∗ρ = characteristic density (g/cm3)
ρ~ = reduced density dimensionless sphereρ = sphere ball density (g/cm3)
gasρ = gas density (g/cm3)
iτ = relaxation time (s)
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iσ = stress (Pa)
iη = viscosity (Pa.s) •
λ = shear deformation rate (1/s) ( 0,1θ+− jNx , 0,θjx ) = coordinate on the profile at any angle
σ = stress amplitude (Pascal) ( )ωη∗ = complex viscosity (Pa.s)
mixturep,ρ = polymer/gas solution density (g/cm3)
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Chapter 1. Introduction
1.1 Preamble
The consumption of foam products in today’s technology continues to grow at
exponential rates worldwide. A simple and most general definition of foam can be described as
a substance that is formed by trapping many gas bubbles in a liquid or solid. Foamed polymers
are used in a variety of applications in the modern world because of their unique properties
compared with unfoamed products. Some of those properties include weight reduction, superior
insulating abilities, buoyancy, and energy dissipation, convenience and comfort features.
Polymeric foams have a wide range of applications from furniture, bedding, insulation,
packaging, appliances, sports applications, shock and sound absorbers, to the transportation and
automotive industry. Some specific examples of using polymeric foams include food trays,
insulation boards used for building construction, automobile seat, bumpers fascia, headliners
and sports helmets, etc.
There are two major classes of polymeric foams: thermoplastic and thermoset foams. The
thermoplastic foams can be recycled and reprocessed, but the thermoset foams are not
recyclable and are intractable due to their heavily cross-linked chain structure and their non
thermo-reversibility[1]. Polymeric foams can also be further classified as flexible, semi-flexible,
rigid or semi-rigid depending on the composition, cell morphology and other physical and
thermal properties[2]. Polymeric foams are produced by a variety of processes, depending on the
applications. Several known foam processing techniques include extrusion, injection molding,
compression molding, blow molding, rotational molding and thermoforming. With the
increasing demand of the foam market in the past decades, a vast amount of effort has also been
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invested on the fundamental study of polymeric foams. Furthermore, studies were conducted
related to the foaming process in order to be able to improve and optimize the current
technology for developing innovative materials which could achieve better performance and
regulatory compliance.
1.2 Thermoplastic Foams
Plastic foams or cellular plastics are normally referred to as cellular, expanded or sponge
plastics. They generally consist of two phases, a solid polymer matrix and gaseous phase [2].The
gas phase typically exists in the polymer matrix as dispersed voids or cells throughout the
material. This cellular structure is formed by introducing either physical blowing agents (PBAs)
such as volatile liquids, inert gases that can be quickly released upon thermodynamic instability
or chemical blowing agents (CBAs) that can generate gases during the plastic foam process.
The cellular structure of foams or cellular materials offers many advantages over traditional
materials and non-cellular polymers. As previously mentioned, there are two types of foams:
thermoplastics and thermoset. Due to their thermo-reversible nature, thermoplastics are the
preferred class of material for processing purposes. The production of thermoplastic and
thermosetting materials has contributed appreciably to the development of the polymeric foam
industry, which itself dates back to the first half of 20th century. The production of the first
synthetic plastic foam dates back a few decades. In 1931, Swedish inventors C. G. Munters and
J. G. Tandberg invented the extrusion process for foaming polystyrene (PS) and their patent was
filed in 1935 in United States[3,4].
Commercial production of Styrofoam®, developed by Dow Chemical Co. using a
continuous extrusion process, began in 1943. The process of utilizing expandable polystyrene
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granules containing a solvent blowing agent for the production of polystyrene foam was
developed by Badische Anilin and Soda Fabrik (BASF) of Germany in the 1950’s [5]. In the
1930s both cellular polyvinyl chloride (PVC) and urethane foams were reported to be in
production in Germany [6]. Polyethylene foams were first introduced in a DuPont patent, U.S.
Pat. 2,256,483, in 1942. In 1958, Dow first commercialized a highly expanded polyethylene
foam product prepared by the extrusion process [7]. Polypropylene (PP) foams were introduced
only a couple of decades ago. In the years following their discovery, PP became one of today’s
most widely used polymeric materials because of their relatively high service temperature and
good abrasion resistance. For instance, polypropylene foams are widely used in the automobile
industry in areas such as, instrument panels, door trims, and quarter panels. In particular, the use
of molded PP foam beads as energy absorbers in car bumpers was one of the greatest
innovations in foam use [2]. High melt strength polypropylene (HMS PP), first presented by
Himont [8], with branched long chains, demonstrated a wider processing window and a much
better foaming structure over the linear conventional PP [9,10]. The world market of PP has
grown from approximately 1.5 million tons in the 1970’s, to over 25 million tons in the year
2000 [11].
There are many other types of foams besides those aforementioned. These include foams
based on butadiene-styrene, neoprene, Poly (Acrylonitrile, Butadiene, Styrene) (ABS), cellulose
and many others. However, during the last decade, efforts have been made to achieve
thermoplastic foams with finer cell sizes and more uniform cell distribution because of their
better mechanical and thermal properties[12-18]. All in all, the steady growth of polymeric foam
consumption in the last several decades is strong evidence of the important role foams play in
our society.
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1.3 Plastic Foaming Process
1.3.1 Introduction
Foaming is a unique technology and, as stated previously, almost every single type of
polymer material or resin could be used to make foam products. Having the right foaming
technique is crucial for foam product manufacturing. Thermoplastic foams are produced by the
creation of a dispersed gaseous phase through a polymer melt and gas expansion process. The
gaseous phase can be generated by the separation of a dissolved gas, vaporization of a volatile
liquid, or through the release of gas from a chemical reaction by adding chemical blowing
agents.
The added compound in the polymer melt to release gas is called a blowing agent (BA).
There are two types of blowing agents depending on their roles in gas generation: 1) physical
blowing agents (PBAs), and 2) chemical blowing agents (CBAs). PBAs are mostly liquids or
supercritical fluids, such as CO2, and N2. They do not undergo chemical transformation and will
be released in a gaseous phase upon thermodynamic instability, i.e. reduction in pressure or
increase in temperature. CBAs, on the other hand, are the compounds or mixtures that are added
into a polymer melt to release gas as result of chemical reactions. CBAs were not used in any of
the experiments involved in this research study. The PBA used in the experiments is CO2. There
exist two distinctive foaming processes, namely, batch foaming and continuous foaming. For
both batch and continuous foaming processes, there are three important stages involved: 1)
polymer/gas solution formation, 2) cell nucleation, and 3) cell growth. Figure 1-1 is an
illustration of the 3 stages of the microcelluar foaming process.
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+gas
polymer
Two Systems Two Phase
Polymer/Gas Mixture Single Phase
Polymer/Gas Solution Thermodynamic
Instability Micocellular Structure
gas injection mixing & diffusion diffusion nucleation cell growth
Figure 1-1 Overview of Microcellular Foaming Process 1.3.2 Batch Process
Batch foaming process is the simplest foaming method. It consists of a single stage or
multi-stages. The following figure shows a simple schematic of a batch foaming process.
pressurized cavity
pressure vessel o-ringsample
inert gas
control
glycerin bath
sample
FOAMINGSATURATION
Figure 1-2 Overview of a Batch Foaming Process
Batch foaming confines the polymer resins or pellets in an enclosed pressure vessel
when the vessel is heated and pressurized. Sometimes this is described as the polymer pellets
being impregnated with a blowing agent in an autoclave. In batch foaming, time is required for
the blowing agents to saturate the polymer pellets. Typically it takes several hours to several
days for a polymer sheet to become saturated. The amount of time required depends on the
polymer dimension, the diffusivity and the saturation temperature. The impregnated polymer
pellets are expanded or foamed upon an abrupt discharge of the pellets into the atmospheric
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pressure or by heating up the unexpanded parts using a steam or oil bath, as shown on the right
of Figure 1-2. The batch process is primitive, but it comprises the three important characteristics
of the foaming process: 1) polymer/gas solution forms upon saturation of the polymer pellets; 2)
cell nucleation and 3) cell growth. The cell nucleation and cell growth happen together
following the dramatic change in thermodynamic instability brought by the abrupt change in
pressure or temperature.
1.3.3 Continuous Process
The continuous process is the expanded version of the batch foaming process that
realizes each of those three characteristics at each individual stage of the foaming in
chronological order. The aforementioned extrusion and injection moldings are typical
continuous foaming processes. During the foaming process, different mechanisms and
parameters such as, temperature, pressure and shear, etc. can occur and sometimes overlap in
different stages. The whole foaming process is a very complicated kinetic procedure in which a
large amount of research has been dedicated to explore and study its mechanisms, the effect of
each parameter, as well as their combined effects. Using a very simple schematic of a typical
single extruder shown in Figure 1-3, the continuous process can be clearly and better illustrated.
polymer/gas solution formation
plastication of polymer nucleation
hopper
plasticating screw nucleation device
diffusion enhancing device
high pressure gas
cell growth
cooling unit
Figure 1-3 Schematic of a Single Foaming Extruder
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The first stage is the polymer/gas solution formation stage or the stage of gas dissolution.
In this stage, the blowing agents such as, CO2 or N2 are injected under high pressure into the
mixing section of the extruder. The blowing agents are well mixed with the molten polymer at
relatively high temperatures, usually above the polymer melting point Tm for semi-crystalline
polymers or glass transition temperature Tg for amorphous polymers. The solution formation is
governed by gas diffusion into the polymer. The diffusion processes are relatively slow and the
cycle time is relatively long. Few techniques have been used to increase the diffusion process,
such as temperature increase or pressure increase. Increasing the temperature could expedite the
diffusivity and also increasing the gas pressure could also boost the diffusion rate by increasing
the local gas concentration. Since the diffusion governs how much gas could dissolve into the
polymer matrix, the solubility limit is the overriding parameter in this stage. The amount of gas
dissolved into the polymer is a controllable processing parameter that affects melt solution
homogenization, foaming dynamics, and stability. The Flory-Huggins equation (1-1) is a
mathematical mean to determine how much gas can be dissolved in the polymer [19].
( )pgppggm xnnnKTF φφφ ++=Δ lnln (1-1)
Where mFΔ is free energy of mixing, K is the Boltzmann’s constant, T is the absolute
temperature in Kelvin, gφ is the volume fraction of gas, pφ is the volume fraction of polymer.
gn and pn are molar fraction of gas and polymer, x is the interaction parameter to take into
account the energy of the interdispersing polymer and gas molecules.
The second stage is the cell nucleation. This stage subjects the polymer/gas solution
from stage one, which forms the polymer/gas single solution, to a thermodynamic instability in
order to nucleate bubbles. This thermodynamic instability is achieved by rapidly lowering the
gas solubility in the polymer via either a temperature increase and/or a pressure drop. Upon the
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introduction of thermodynamic instability, the single phase solution system then looks for a state
of lower free energy by clustering gas molecules in the form of cell nuclei. The formation of cell
nuclei provides a relatively small mean free distance for the gas molecules in solution to diffuse
through. This cell nucleation process happens when the polymer/gas melt is decompressed at the
nucleation device shown in Figure 1-4.
There are two types of cell nucleation: homogenous and heterogeneous nucleation.
Homogenous nucleation happens throughout the material and the heterogeneous nucleation
happens at high-energy regions such as phase boundaries. From thermodynamic law, the critical
bubble radius is expressed in equation (1-2) as follows:
( )PPRbcr −
∗= γ2 (1-2)
Where crR is the critical nuclei radius, γ is the surface tension between the gas and polymer/gas
interface, Pb is the bubble pressure and P is the surrounding or polymer/gas solution pressure.
According to the homogeneous nucleation theory [20], the Gibbs free energy for the
formation of a nucleus with critical size is given by
32hom
3
16γ
π
PG
Δ=Δ ∗ (1-3)
The PΔ is the pressure difference across the gas and polymer/gas interface, γ is again the
surface tension. The bubble nucleation process is a critical stage in plastic foam production
since it governs the cell morphology and in return determines the properties of plastic foams.
The nucleation process will be described in detail in Chapter 2.
The last stage of the continuous foaming process is the cell growth. Once the cell nuclei
are formed, they tend to grow if the size is bigger than the critical bubble radius crR . The cell
continues to grow and the polymer density is reduced as the gas that is initially dissolved in the
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polymer matrix which surrounds the nuclei, diffuse into the nucleated cells. Cell growth is also
important in that it determines the final foam density as well as cell morphology. The growth of
cells is limited by the diffusion rate, the stiffness of the viscoelastic polymer/gas solution, the
availability of gas inside the solution, and the time allowed for cells to grow.
After the cell growth stage, the temperatures of polymer melt decreases as it leaves the
nucleation device or die exit.
1.4 PVT Measurement
Thermoplastic foamed products have become very popular in recent years.
Thermoplastic foams exhibit unique mechanical and thermal properties including cushioning,
impact resistance, insulation and buoyancy. They are distinguishable from their unfoamed
counterparts by virtue of their cellular structure. The unique cellular or microcellular structure is
achieved through the expansion of a blowing agent dissolved in a molten thermoplastic resin by
a batch or continuous foam process.
When gas dissolves into a molten polymer during the polymer/gas formation stage, the
polymer swells (dilates) due to gas sorption. Upon the introduction of thermodynamic instability
such as, temperature increase or dramatic pressure decrease in the polymer/gas single solution,
the cell will nucleate homogenously or heterogeneously and grow from the dissolved gas to
eventually form the cellular foam. Therefore, the pressure-volume-temperature (PVT)
relationship for polymeric materials is a subject of great importance and interest to polymer
scientists and engineers, particularly from a process design standpoint. The PVT
(pressure-volume-temperature) properties of a polymer/gas solution can be established by
measuring the amount of polymer swelling as a function of the concentration of dissolved gas at
certain temperatures and pressure levels. . Information on the PVT properties is crucial for the
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successful processing of plastic foams because both the cell nucleation and cell growth
behaviors are strongly dependent on these properties. The importance of the PVT property,
especially the PVT of polymer/gas solutions towards solubility and surface tensions, will be
described more clearly in the next section when the role of PVT in the solubility and surface
tension is depicted.
The PVT for pure polymer has been extensively studied in the past decade through
empirical and theoretical methods. A comprehensive PVT database for a variety of pure
polymers has already been established[21-24]. The study of PVT on polymer/gas solutions
(mixtures or binary system) has been the focus for many researchers in the past decade as well.
Using the gravimetric method seems to have been the most popular method for conducting the
study, but most of the experimental conditions were not at elevated temperatures and the results
were not extensive. Hence, the conclusion here is that the PVT properties of polymer/gas
solutions at high temperatures and pressures have not been extensively investigated in the
molten state, due to the difficulties of maintaining the high pressure and high temperature
required in the measurement.
1.5 Role of PVT in Solubility and Surface Tension
In continuous foaming, supercritical fluids used as blowing agents such as CO2 or N2 are
always the most important aspects of the study because how they react with the polymer matrix
determines the quality of the final foam products. Mentioned earlier, the formation of the
polymer/gas solution is part of the foaming process. How much blowing agents are indeed
needed to be able to form a homogenous polymer/gas single solution depends on information
provided on gas solubility. The most popular methods used to determine solubility is the
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gravimetric method using the magnetic suspension balance (MSB) system and theoretical EOS
calculations. The following figure shows a schematic of a MSB and its working principle.
High pressure gasVacuum
F(0,T)microbalance microbalance
F(P,T)
Polymer Sample
Solubility
Uncompensated Solubility
Volume Swelling Compensation
Buoyancy Effect
( ) ( ) ( )sPBgasg
VVVTWTPWW +++−= ρ,0,
High pressure gasVacuum
F(0,T)microbalance microbalance
F(P,T)
Polymer Sample
Solubility
Uncompensated Solubility
Volume Swelling Compensation
Buoyancy Effect
( ) ( ) ( )sPBgasg
VVVTWTPWW +++−= ρ,0,
Figure 1-4 MSB Solubility Apparatus Schematic and Working Principle
As seen from the above figure, the volume VB (volume of the coupling device plus the
volume sample container), volume of polymer sample Vp, and the swelling volume Vs of the
polymer account for the buoyancy effect and need to be considered in order to obtain reliable
solubility data. The first two volumes could be determined relatively easily, but the bottleneck
issue is how to determine the real volume dilation Vs of polymer due to gas dissolution. MSB
could monitor the weight change accurately but not the volumetric changes. Therefore, due to
the lack of the volume swelling information because of the difficulties in measuring direct
volume swelling, the MSB solubility study has to rely on theoretical equations of state (EOS) in
order to make the volume swelling predictions. Although the EOS have been proven to be
reliable when they are used to analyze the property of pure substances and mixtures, it has not
been thoroughly verified when they are used for swelling prediction in solubility calculations.
One of the reasons is that due to the complexity of the molecular reactions among polymer/gas
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matrices under various high temperature and pressure conditions, the EOS that is based on pure
thermodynamic theories could not properly model those molecular reactions and behaviours
even with proposed assumptions. Therefore, the role of obtaining accurate volume swelling
information, i.e. the PVT data when forming the polymer/gas single solution is important not
just to facilitate better solubility measurement but also to enable a good polymer/gas single
solution formation. Naturally, the question is how PVT plays an important role in surface
tension measurement application.
During the second stage of the foaming process, the critical nucleation radius, the free
energy barrier, and the nucleation rate are physical factors that would definitely influence the
outcome of the nucleation stage macroscopically. When examining the equations (1-2, 1-3, 2-9,
2-10, 2-11, 2-12) that used to quantify those factors, it is found that one of the most crucial
parameters is the surface tension, or interfacial tension (γ ) between the gas bubble and the
surrounding polymer/gas mixture. A simple definition from a molecular point of view is that the
surface tension is the intermolecular force that contracts the surface. As is self-explanatory from
those equations, the surface tension parameters do play a significant role in determining the free
energy barrier, critical cell radius, cell nucleation rate, which would all eventually determine the
cell nucleation density and the cell morphology.
There have been intensive studies and literature conducted on the surface tension.
Among them, the sessile drop method based on the Axial-symmetric Drop Shape Analysis
(ADSA) was used, which is one of the most popular and efficient methods to obtain the surface
tension data. The ADSA method has been used by many researchers to study surface tension
of not only polymer materials, but also other substances. Since supercritical CO2 is a promising
solvent for application in polymer blending and foaming, intensive surface tension studies of
polymer/CO2 solutions have also been carried out from various literatures.[25-27] In the next two
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chapters, when the detailed mathematical formulas are unveiled, we will discover not
surprisingly, that the density information of the polymer/gas mixture is one of the key input
parameters for surface tension determination. As for polymer/gas mixtures studies, the current
method of determining the density is either using the solubility from MSB combining with the
EOS volume swelling prediction or using the EOS calculation alone. This suggests that accurate
surface tension information also relies on accurate PVT information due to the requirement for
accurate polymer/gas densities information.
In conclusion, in the two most critical stages of the foaming process, it is a strong
demonstration that the solubility of gas in polymer and surface tension (or the interfacial tension)
between the gas and polymer/gas interface have dominating effects on the solution formation
and cell nucleation stages. More importantly, without the accurate PVT information of
polymer/gas solution, both solubility and surface tension would not be obtained accurately.
Therefore the method of how to obtain the accurate PVT data is the most crucial
behind-the-scenes factor in facilitating more reliable solubility and surface tension
measurements. Additionally, properties such as diffusivity of the gas in the melt, the shear and
extensional viscosities of polymer/gas solutions are also strongly influenced by the PVT data of
the respective polymer/gas solution.
1.6 Motivation and Scope/ Objective
The polymer foaming industry is divided into three major building blocks in Figure 1-6:
1) fundamental study, 2) simulation research, and 3) polymer foaming processing. The
fundamental and simulation studies serve as the sources of new and innovative knowledge for
supporting and improving the know-how and technology in real foaming process. These
fundamental properties could also be directly utilized in the foaming process without going
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through the simulation stage. Any improvement in fundamental and simulation would lead to
potential success to the polymer foaming industry overall. As shown in the following diagram,
the PVT properties, solubility and surface tension of polymer and polymer /gas mixtures along
with others belong to the fundamental section.
Fundamental
MaterialsRheologySolubility/DiffusivityPVTSurface TensionCrystallization
Simulation
Experimental SimulationComputer Simulation
Processing
ExtrusionInjection moldingRotomoldingCompression Molding
Figure 1-5 Building Blocks of Foaming Research and Industry
Precise solubility measurement using the Magnetic Suspension Balance (MSB) method
requires the true volume swelling (PVT) data of the molten polymer to account for the buoyancy
effect. The validity of the Sanchez and Lacombe (SL) and Simha and Somcynsky (SS) EOS
used to theoretically predict the volume dilation would also be important and necessary from the
accurately measured PVT information. In order to improve the design of the nucleation device
to achieve the best cell morphology and to have better foam properties, the surface tension is
influential on the nucleation stages of the foaming process. Precise surface tension measurement
using the ADSA method also requires accurate measured PVT data for determining the density
of the polymer/gas solution. Therefore, developing a new experimental apparatus that would
measure PVT information is a significant contribution. It will assist not only in obtaining more
accurate solubility and surface tension data, etc. but in providing more accurate fundamental
data for improvement in simulation studies. Thereby it will improve the foaming
experimentation which would eventually bring more innovative improvement to the foaming
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industry. In addition, having accurately measured PVT information will help to verify the EOS
predictions on volume swelling. Those serve as the biggest motivation of this thesis.
The ultimate objective is to develop and construct a novel apparatus for the first time to
accurately measure the PVT properties of various polymer/gas solutions over a wide range of
elevated temperatures and pressures. Consequently, a database for the PVT properties of various
polymer/gas solutions, such as PP/CO2, PS/CO2, PP/N2 will be built upon the measurement
results for the first time.
1.7 Thesis Contribution
For the first time in academic study of polymers and the polymer foaming industry, the
design and construction of a novel apparatus that can measure the PVT property of polymer/gas
solutions at elevated temperatures and pressures is proposed and realized in this research. The
major contributions of this research are broken down as follows:
1. Successfully designed and constructed a novel apparatus to experimentally measure the
PVT property of polymer/gas under elevated temperatures and pressure for the first time
2. Conducted experiments on the measurement of PVT for pure polymer (PP and PS)
3. Conducted experiments on the measurement of PVT for polymer/gas solutions (PP/CO2,
PS/CO2)
4. Obtained accurate CO2 solubility data in PP measured from MSB based on the measured
PVT data for PP/CO2 solution
5. Obtained accurate CO2 and PP/CO2 solution surface tension data based on the measured
PVT data for PP/CO2 solution
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6. Successfully designed and constructed a rotational device to study the degree of
asymmetry of polymer with high viscosity and melt strength
7. Studied the degree of asymmetry of PS drop through PS density measurement
8. Hypothesized the effects of the polymer chain entanglement density on polymer swelling
9. Measured polymer chain entanglement to support the hypothesis
10. Obtained the best comparison between the measured PVT data and the EOS predicted
values
1.8 Thesis Organization
In order to detail each of the above contributions, the thesis is divided into eight chapters.
The following paragraphs walk through each individual chapter briefly.
Chapter 2 presents a literature review related to the study of this thesis, namely, the PVT
measurement, solubility, diffusivity, nucleation and surface tension studies. Since the
methodology proposed is closely associated with image processing, it is important and
necessary to present the current works that has been done in computer vision and image
processing on 3-D object reconstruction from 2-D images as part of the literature survey. The
literature gathered in this chapter on the study of PVT measurement for pure polymer and
polymer/gas solutions reviews the methodology used in the research and shows the current
progress and status. The law of thermodynamic, thermodynamic equilibrium and the equation of
states (EOS) are elaborated on because they are heavily utilized in the solubility measurement.
Chapter 3 focuses on the theoretical background study. The three most important aspects
that closely relate in with this research are: 1) solubility and equations of state (EOS) from
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thermodynamic phase-equilibrium, 2) theories on PVT study and measurement, and 3) study of
surface tension in polymer processing.
Chapter 4 first describes the conceptual design of the PVT system. The axiomatic design
approach is used and provides a scientific and systematic basis for analyzing the design problem.
The details of the analysis are depicted in this chapter. Meanwhile, the design of every
component from both the hardware and software aspects of the system is also described in detail.
The last section of this chapter focuses on the algorithm development, including image
reconstruction, edge detection and volume integration. The definition of degree of asymmetry is
defined mathematically as well.
Chapter 5 emphasizes the validity of the PVT system using both theoretical and
empirical approaches. The volume measurement of precision stainless sphere demonstrates the
error reduction using the PVT system. Comparison between the measured pure polymer density
and the Tait equation calculated density is the main focus of this chapter A couple of different
polymer materials, such as PP and PS were used as the case study.
Chapter 6 turns the focus of the study to the PVT property of polymer/gas solutions. The
first section of this chapter shows the PVT study for polymer/gas system based on axisymmetry
assumption of the polymer/gas sample under high temperatures and pressures. The polymer
resins used for this study are linear polypropylene (PP) and branched polypropylene. The
blowing agent used is CO2. The experimental procedures are described for conducting the
measurement. The results of the volume swelling for linear and branched PP/CO2 solutions are
summarized. The calculation of the specific volume of PP/CO2 solution is also illustrated. The
effects of the temperature and pressure as well as the branching structure on the PVT properties
are explained in depth.
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The second focus of Chapter 6 is to address the issue of asymmetry if the polymer has
high melt strength and viscosity at relatively high temperature and does not easily form a
axisymmetric profile. The polymer resin used in this study is polystyrene (PS) and the blowing
agent is CO2. The rotational device is employed to capture the asymmetry and also to
compensate the asymmetry effect on PVT measurement by rotating the sample at a given angle
for one revolution. The effects of temperature and pressure as well as the asymmetry on the final
PVT for pure PS and PS/CO2 are illustrated. The comparison between the measured PVT data
with those predicted from EOS is also examined in details. The conclusion and comments are
made based on the direct comparison between the predicted and measured volume swelling. The
last section of this chapter shows the steps for determining more accurate solubility using the
measured PVT data.
Chapter 7 addresses the issue of the importance of accurate PVT measurement in the
surface tension study. Experimental procedures are reviewed for the surface tension method.
The materials used for the surface tension study are the same as described in Chapter 6. The
surface tension results are calculated based on the density information from PVT experiments.
The effects of temperature and pressure on the surface tension of PP/CO2 solution are depicted
in detail.
Chapter 8 provides a summary and suggested future work for this research.
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Chapter 2. Literature Review
2.1 Background on PVT Property Measurement
2.1.1 PVT Measurement for Pure Polymer
The relationship between pressure, volume and temperature ( PVT ) for polymeric
materials is a subject of importance to polymer scientists and engineers, particularly from a
process design standpoint. Pressure-volume-temperature (PVT) information for a variety of pure
polymers at temperatures above the melting point Tm of crystalline polymers or the glass
transition temperature Tg for amorphous polymers has been established through both empirical
and theoretical studies. Zoller et al. [21,22,24], Rodgers[28] and Sato et al.[29] have used the
bellow-type dilatometer to measure the density of a pure polymer, in which the polymer sample
and liquid mercury were confined inside the dilator. Figure 2-1 shows the simple schematic of
the bellow type dilatometer. Zollar et al. have described the detailed measurement procedures
and used this method to build up a PVT database for various pure polymers. This type of
dilatometer, however, is not capable of measuring the PVT properties of polymer/gas solutions.
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Electric Heaters
LVDT CoreLVDT Coil
Bellows
Pressure Fluid Inlet
Plastic Sample
Mercury
Electric Heaters
LVDT CoreLVDT Coil
Bellows
Pressure Fluid Inlet
Plastic Sample
Mercury
Figure 2-1 Schematic of Bellow Type Dilatometer
Numerous theoretical equations of state for polymer liquids have been developed[30-45]
over the past couple of decades. The equations derived from thermodynamic principles can be
used to predict the properties of polymer blends and solutions. It seems that nearly all equations
of state for polymer liquids provide a reasonably good fit to PVT data, especially at low
pressures. However, there is a major difference between the various equations in their abilities
to fit PVT data over a wide range of pressure and to predict thermodynamic properties of
polymer blends and solutions, particularly phase separation behavior. Most equations require an
empirical interaction parameter, determined from at least one experimental data point, in order
to describe accurately the phase behavior.
The modified cell model of Dee and Walsh[31,32], the Simha-Somcynsky (SS) hole
theory[43,44], the Prigogine cell model[39,40], and the semiempirical model of Hartmann and
Haque[34], were all found to provide good fits of polymer liquid PVT data over the full range of
experimental pressures. The Flory-Orwoll-Vrij[33] and the Sanchez-Lacombe (SL) lattice-fluid
equations of states [41,42]are both significantly less accurate over the wider pressure range.
Perhaps the most common empirical representation of polymeric PVT data is that of the Tait
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equation[28,46]. It is, in fact, not a true equation of state, but rather an isothermal compressibility
model. For different polymer resins, the format of the Tait equation is in similar format but the
coefficients of the equation are different depending on the specific material grade. The apparatus
to measure the PVT of pure polymer and fit with Tait eqauion is commercially available and the
most popular one is the Gnomix PVT apparatus developed and upgraded based on the
bellow-type dilatometer principle.
It has been reported that the pendent drop or sessile drop method based on axisymmetric
drop shape analysis (ADSA)[26,27,47-57]commonly used for performing surface tension
measurements, was used for measuring the density of pure polymer melts under ambient
pressure. Wulf et al.[57]used the ADSA method to determine the surface tension and the
density of pure polystyrene (PS) at ambient pressure and temperature up to 236oC. The major
limitation of this method is associated with the inaccuracy of boundary determination and the
strict axisymmetric drops.
2.1.2 PVT Measurement for Polymer/Gas Solutions In polymeric foaming process, for example, supercritial CO2 (scCO2) is being utilized as
an environmentally friendly foaming agent replacing the conventional chlorofluorocarbons
(CHFC), hydrofluorocarbon, and hydrocarbon foaming agents. When polymer and CO2 form
single phase solution system, CO2 gas dissolves into a molten polymer, and the polymer swells
(or dilates) due to gas sorption. The amount of polymer swelling or dilation is characterized by
its PVT properties, which can be obtained by measuring the equilibrium state volume of a
polymer/gas solution at any specific temperature and pressure. In polymer foaming applications,
cell nucleation and growth are governed by physical properties such as solubility[58,59],
diffusivity[60],and surface tension[26,27,61]. However, the determination of these properties relies
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on the PVT data, i.e., the polymer swelling caused by gas dissolution. For example, currently,
the most commonly used technique for gas solubility measurement in polymer melts is the use
of a magnetic suspension balance system[62-65] in which the accurate determination of gas
solubility depends on the buoyancy correction of the equilibrium polymer/gas solution volume,
i.e., the swelling of the polymer due to the dissolved gas. Therefore, knowing their PVT
properties (the polymer swelling by dissolved gas) is critical for understanding and controlling
foam processing. Unfortunately, due to the high pressures and high temperatures involved in the
measurement, there have been very limited studies on the PVT properties of polymer/gas
solutions.
Attempts have been made to measure polymer swelling under high pressure gas
conditions[66-85]. Visual observation and induction gauges are the most popular scheme among
those studies in which the length change in one or more dimensions is measured in the presence
of high pressure CO2 gas.
Bonavoglia et al.[66] measured the swelling of poly(methyl methacrylate) (PMMA),
poly(tetrafluoroethylene), and poly(vinylidenefluoride) in CO2 (5–23 MPa) at temperatures in
the range of 313–353 K. Ender [68] used the coil of a linear variable differential transformer
(LVDT) to measure the volume swelling of various elastomers under high pressures in CO2 at
relatively low temperatures. Shenoy et al.[83] also used a LVDT to evaluate CO2 polymer
plasticization. Their results show that at 22oC under CO2 pressure,
polystyrene-block-polybutadiene-block-polystyrene (SBS) elastomer undergoes compression
due to hydrostatic pressure. However, sample expansion occurs upon depressurization. At 45oC,
SBS undergoes swelling of 0.7% due to CO2 plasticization, while no post-pressurization
expansion is observed. The contrasting result is explained by change in PS domain mobility and
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discontinuity in the density-pressure relationship. The general concept of using the LVDT to
detect the dimension change to measure the volumetric change is illustrated in Figure 2-2.
Ender[68] has used the coil of a linear variable differential transformer (LVDT) to
measure the volume swelling of various elastomers under high pressures in CO2 at relatively
low temperatures. Foster et al.[69]used a cylinder-piston-type method in a compressibility
chamber to acquire PVT data by multiplying the cross-sectional area of the piston with the
linear displacement of the piston. Nikitin et al.[70] used a visual observation cell to study the
swelling of PS/ CO2 solutions at 335 K. They observed the diffusion front of CO2 in PS and
calculated a diffusion coefficient. Rajendran et al.[73] and Bonavoglia et al.[66] also employed a
direct visual observation method to measure polymer swelling in CO2. Royer et al.[74]observed
CO2 induced swellings of three poly (dimethylsiloxane) (PDMS) samples with different
molecular weights in a view cell and found that the molecular weight did not affect the
magnitude of swelling at 303, 323, and 343 K under pressures ranging from 0 to 27.6 MPa.
Wissinger et al.[75] measured the swelling of poly(methyl methacrylate) (PMMA),
polycarbonate (PC), and polystyrene (PS) in contact with CO2 at temperature from 306 to 338 K
and pressure up to 10 MPa. They used a cathetometer shown in Figure 2-2 for measuring the
length of the thin polymer films in a high-pressure view cell and identified two distinct types of
swelling and sorption isotherms. One is characterized by swelling and sorption that began to
level off at elevated pressures. The other is swelling and sorption that continued to increase with
CO2 pressure.
Zhang et al. [76] measured CO2 sorption and swelling of PMMA, poly(vinylpyridine),
polyisoprene, and three block copolymers in the presence of CO2 at 308 K and at a pressure up
to 10 MPa. They also used a cathetometer to directly measure the dimension of polymer samples
in a high-pressure view cell.
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Some researchers proposed non-direct measurement schemes, which combine both
gravimetric and volumetric methods. Using so-called combined gravimetric-dynamic method,
Keller et al.[77] studied the swelling of PC at temperature, 293 K, under pressures ranging from 0
to 6 MPa. They combined the gravimetric method with a dynamic method where the inertia of
the polymer sample was determined by slow oscillations of a rotational pendulum or by the
relaxation motion of a floating rotator.
The dynamic method showed the same order of magnitude of polymer swelling as
Wissinger and Paulatitis [75]showed for the PC/ CO2 system. Using a pressure decay apparatus
with a vibrating-wire force sensor, Hilic et al.[78] conducted simultaneous measurement of the
solubility of nitrogen (N2) at pressures up to 70 MPa and CO2 at pressures up to 45 MPa in PS
and the associated polymer swelling. The vibrating wire sensor acted as a balance to weigh the
polymer sample. They measured the swelling of PS with a precision of 0.5% at three isotherms
from 313 to 353 K, which were below the glass transition temperature of PS and observed a
significant change in both solubility and swelling at temperatures between 363 and 383 K.
Gotthardt et al.[81] studied the volume changes caused by the sorption of H2O, Ar, N2,
CO2, CH4 and Acetone in Bisphenol-A polycarbonate and of CO2 in different substituted
polycarbonates using a dilatometer at room temperature.
gas vacuum
pressure transducer
Δl
high pressure window
polymer sample
gas vacuum
pressure transducer
Δl
high pressure window
polymer sample
Figure 2-2 Schematic of LVDT Dilatometer
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Holck et al. [85]used a gravimetric sorption balance and a dilatometer based on capacitance
sensor to measure the CO2 sorption induced dilation in polysulfone and compared it with
experimental and molecular modeling results at 308 K and pressures up to 50 bar.
The most proposed methods of measuring polymer swelling require a specific shape or
state of the polymeric material. There are few papers which report swelling measurements of
molten polymers or polymeric solutions at temperatures higher than the glass transition
temperature.
Unfortunately, most of approaches are only valid for isotropic swelling and the polymer
have been pre-treated carefully to release internal stresses and ensure the isotropic behaviour.
Furthermore, the warpage of the samples limits its application and results in an inaccurate length
measurement. In general, most of the methods described above operate at fairly low
temperatures, ranging from 25°C to 100°C which are below glass transition temperature of
polymer in order to keep an appropriate shape of the sample.
Park et al. [71,79] measured the PVT properties of polymer/CO2 solutions using a foaming
extruder and a positive-displacement gear pump mounted on the extruder. The major drawback
of this method is the required (and limited) extrusion processing conditions for measuring the
PVT data.
Funami et al.[86] developed a new method of directly measuring the densities of two
polymer melt-CO2 single-phase solutions, poly(ethylene glycol) (PEG)-CO2 and polyethylene
(PE)-CO2 at high pressure and temperature using magnetic suspension balance (MSB) seen in
the following Figure 2-3.
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Figure 2-3 Schematic of Modified MSB for Polymer/Gas PVT Measurement
A thin disc-shaped platinum plate was submerged in the polymer-CO2 single-phase
solution in the MSB high-pressure cell. The weight of the plate was measured while keeping
temperature and CO2 pressure in the sorption cell at a specified level. Since the buoyancy
force exerted on the plate by the polymer/CO2 solution reduced the apparent weight of the plate,
the density of the polymer/CO2 mixture could be calculated by subtracting the true weight of the
plate from its measured weight. However, this density measuring method has some limitations
on applicable polymers. When the plate is moving up and down in the polymer melt during the
position changeover operation, a dragging force is generated. Therefore, the readout could not
be guaranteed when the viscosity of polymer melt is high.
An recent attempt to calculate the surface tension and density simultaneously using
surface tension ADSA-P method[87,88] to study the PS/N2 solution at pressure up to 500 psi and
200oC. The limitation is the ADSA method cannot handle asymmetry PS drop shape due to its
high viscosity and elasticity even at low temperature. The results is not accurate at low
temperature range and plus the operating pressure is low.
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2.2 Background on Polymer/Gas Solutions Property
2.2.1 Solubility and Diffusivity As was explained in the continuous foaming process, the solution formation of the
polymer and blowing agents is the first very critical stage, which would determine the ultimate
properties of the foam products. When a blowing agent such as CO2 is dissolved into polymer,
several physical properties of polymer such as glass transition temperature, melting temperature,
surface tension, and viscosity are changed depending on solubility of CO2 into the polymer.
Knowing the precise solubility of the blowing agent would be crucial to determine the solubility
pressure or exactly how much gas are required for achieving the polymer/gas single phase
solution formation. Therefore a thorough understanding about the interaction between the
physical blowing agents and polymer melts would be useful not only in the selection and
development of suitable blowing agents but also for optimization of the plastics foam
production process.
The solubility of gas in polymer melts is defined as the maximum amount of gas that can
dissolve into the polymer melts at a specific temperature and pressure. When a gas permeates
through a polymer membrane, several processes are involved: 1) the gas is absorbed at the
entering interface, 2) the gas dissolves at the interface to establish a quick equilibrium and 3) the
dissolved penetrate molecules diffuse through the membrane. The mechanism of permeation
involves both solution and diffusion. Microscopic and macroscopic diffusion are the two
approaches to study the diffusion.
Microscopic diffusion includes two most important models: the Meares’ Molecular
model and the Free-volume model. In the molecular model, the molecules penetrate through a
polymer matrix and it is usually assumed that microcavities of different sizes are formed and
destroyed continuously in the polymer. Small, dissolved molecules trapped in these locations are
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able to move into the direction of a driving force by the cooperative motion of adjacent polymer
chains[89]. Meares’s Molecular model is expressed in equation (2-1) as follows:
AD NE λα
π24
= (2-1)
where DE is the cohesive energy density that requires disrupting neighbouring polymer chains,
λ is the jump length, 2α is the cross section of the penetrate molecule, and AN is the
Avogadro’s constant. Meares’s model deals with prediction of the energy required for a
diffusion jump and it does not predict beforehand the value of diffusion coefficient. More
complex models[90-92] theoretically describe the overcoming of attractive forces between the
chains and the energy required for bending of polymer chains.
Another molecular model is the free-volume model proposed by Cohen and Turnbull[93]
and developed by Fujita[94]. The free-volume model describes the absolute velocity of the
penetrating molecule in the polymer matrix and it relates the diffusion coefficient to the free
volume available in the system. The equation is:
⎟⎟⎠
⎞⎜⎜⎝
⎛ −∗=
f
BADυ
exp (2-2)
0υυυ −= pf (2-3)
The D in the equation is diffusion coefficient, fυ is the total specific free-volume accessible
for diffusion, pυ is the specific volume of the polymer and 0υ is the specific occupied volume
of the polymer chains. Other forms of the free-volume model[95] are also available.
The diffusion coefficient D is a macroscopic property of a polymer-penetrate system that
does not give detailed or particular information about molecular motions of polymer chains
during the diffusion process. The concentration of penetrate within the gas/polymer interface is
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not known unless the solubility of the gas in the polymer has been determined. In simple cases,
it is customary to assume that the gas/polymer system follows Henry’s law[96] which gives the
general relationship between the concentrationsof penetrate and the pressure on polymer:
ss
s PRTHHC ⎟
⎠⎞
⎜⎝⎛ Δ−= exp0 (2-4)
where sC is solubility of gas in the polymer, H0 is the constant of Henry’s law, R is the gas
constant, T is the temperature in Kelvin, sHΔ is the molar heat of sorption in Joule and sP is
the saturation pressure in Pascal. The molar heat of sorption can be a negative or positive value
depending on the polymer-gas system.
The fundamental equation of macroscopic diffusion was derived by Fick in 1855. These
are Fick’s first and second law. The mathematical theory is based on the hypothesis that the rate
of transfer of diffusing substance through unit area of a section is proportional to the
concentration gradient measured normal to the section. Fick’s first law relates the diffusion flux
to the concentration difference and the diffusion coefficient is assumed to be constant across the
membrane.
adxdCDj =−= (2-5)
where a is a constant, and if the flux and concentration gradient can be accurately determined,
then the diffusion coefficient can be evaluated directly.
Fick’s second law considers the mass balance:
2
2
dx
CdDdxdj
dtdc
−=−= (2-6)
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Equation (2-6) assumes one-direction diffusion. In many polymer systems, however, the
diffusion coefficient D depends markedly on the concentration and D varies from point to point,
in which case equation (2-6) becomes:
⎟⎠⎞
⎜⎝⎛
∂∂
∂∂
==xCD
xdxdj
dtdc
(2-7)
Diffusion and sorption are the direct causes of the volume swelling when gas is dissolved into
the polymer matrix. There are a few models available to study the sorption behaviour of rubbery
and glassy polymers.
Crank and Park and other researchers used the kinetic study of the sorption and
desorption of gases and vapours in polymers as a means for determining the diffusion
coefficient. In the batch process, a sheet of polymer sample is saturated with the blowing agent
by placing it in a high-pressure chamber connected to the blowing agent reservoir. At this high
pressure, the blowing agent will continuously diffuse into the polymer matrix until the solubility
limit is reached. Although the solubility limit theoretically occurs at time infinity, the
instantaneous concentration of the blowing agent in the polymer can still be obtained using the
following equation[97]:
( )
( )∑∞
=∞ ⎥⎥⎦
⎤
⎢⎢⎣
⎡ +−
+−=
02
22
2212exp
12
181m
th
tmD
mMM π
π (2-8)
where D is diffusivity, tM is the mass uptake at time t and similarly ∞M is the equilibrium
mass uptake after an infinite time at which the equilibrium of the system is reached; t is the
elapsed time and h is the thickness of the sample sheet.
The amount of mass uptake eventually levels off at ∞M in the absorption process, and
the solubility limit can be calculated by dividing the mass uptake ( ∞M ) by the mass of the
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polymer sample. On the other hand, the solubility limit of gas dissolved into the polymer
depends on the system pressure and temperature and can be estimated by Henry's law[96].
At the processing pressure and temperature, the estimation of the solubility of CO2 in
some polymers has been given in the literature[17,98]. There are many methods and techniques
available to determine the solubility. These methods include: 1) pressure decay method[99-102], 2)
piezoelectric sorption method[103-106], 3) Gas-liquid chromatography method[107-109], and 4)
Gravimetric method[104,110-115]. The following paragraphs briefly describe each of these
measurement methods.
The pressure decay method was first proposed by Newitt and Weale [102] in 1948 for the
experimental measurement of gas solubility in polystyrene melt. The principle used is that in a
confined sorption chamber at constant temperature with known volume, when the gas is
absorbed into the polymer matrix, the pressure of the chamber will decrease accordingly.
Therefore, by measuring the pressure drop due to gas sorption, the solubility can be determined.
The apparatus built based on the pressure decay method is called the Durrill’s apparatus
[99] With the pressure decay experimental approach, Lundberg et al. measured the solubility of
nitrogen and methane in polyethylene[101], solubility of methane in polystyrene[116], and
solubilities of methane in polyisobutylene[100]. Newitt et al. investigated the solubility of
hydrogen and nitrogen in polystyrene[102]; Durrill et al. systematically determined the solubility
of nitrogen (N2), helium(He), carbon dioxide (CO2), and argon(Ar) in polyethylene,
polyisobutylene, polypropylene, polystyrene and polymethylmethacrylate [99]. Sato et al. used
the pressure decay method to study the solubility of carbon dioxide and nitrogen in molten
polypropylene (PP) and high-density polyethylene (HDPE). The solubilities were measured at
temperatures 433.2, 453.2, and 473.2 K and pressures up to 17 MPa. The solubility increased
almost linearly with pressure. While the solubility of carbon dioxide decreased with increasing
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temperature, that of nitrogen increased in the temperature range examined. The solubility of
nitrogen in glassy polystyrene (PS) was measured at 313.2, 333.2, and 353.2 K and pressures up
to 17 MPa.
In 1975, Bonner et al. creatively devised a novel piezoelectric sorption technique to
determine gas solubility in polymers at high temperature and high pressure conditions [103-105].
The principle of the piezoelectric sorption method is based on the fact that the relevant
frequency of piezoelectric crystal increases with increase in mass loaded on the surface of the
crystal. Therefore the relevant frequency of piezoelectric crystal can be applied to determine
solubility of gas dissolved in a polymer coating layer on the surface of the crystal[104]. With the
piezoelectric sorption method, Bonner et al. measured the solubility of nitrogen and ethylene in
low-density polyethylene[104,105]. The drawback of the piezoelectric sorption method is that it
can not be used to measure the solubility at high temperature due to the polymer sample’s
viscosity change at high temperature.
Gas-liquid chromatography was first applied by Prausnitz et al. to determine the gas
solubility in polymer at high temperature in 1976[107,108]. Based on the gas-liquid
chromatography, the solubility of ethylene, n-butane, vinylacetate, n-hexane, benzene, toluene,
and n-octane in low-density polyethylene were successfully measured[108]. In addition, the
solubility of methyl ethyl ketone, acetone, isopropyl alcohol, vinyl acetate, sulfur dioxide,
methyl chloride, ethane, ethylene, and carbon dioxide in polyethylene and in ethylene-vinyl
acetate copolymer were studied[107]. Gas-liquid chromatography is a simple and rapid method
for measuring solubility of volatile compounds in polymer melts. But the main problem of this
method is that the pressure is limited to ambient pressure range.
The volumetric and gravimetric methods have been widely used to measure not only the
diffusivity but also the solubility of CO2 in polymer[65,66,70,73-76,99,117,118]. The gravimetric method
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was applied to study the sorption of gas in polymer melt. Based on the gravimetric method,
Bonner etc. studied the sorption of benzene in polyisoprene and polyisobutylene at 80°C; the
sorption of cyclohexane in polyisobutylene at 100°C; and the sorption of cyclohexane in
ethylenevinyl acetate copolymer (EVA), isooctane in EVA, isooctane in poly(vinyl acetate) at
110°C [119].
Baird investigated the kinetics sorption of n-pentane in polystyrene at 30°C[109]. The
solubility of vinyl chloride monomer (VCM) in PVC powders has been studied by Berens etc. at
temperatures from 30 to 110 °C[111]. Berens et al. also investigated the solubility of nitrogen,
carbon dioxide, vinylchloride, methanol, acetone, n-butane, and benzene in PVC at temperatures
below Tg[112]. Kamiya et al. precisely determined the solubility of gases in polymers at high
pressure. The solubilities of N2 and CO2 in LDPE, CO2 in polycarbonate (PC); and N2, CH4,
C2H6, and CO2 in polysulfone and PS were measured as a function of pressure up to 50 atm[114].
They carefully measured the polymer swelling and exactly determined the solubility of N2, Ar,
CO2 in poly(vinyl benzoate) at 25-65 oC and up to 5Mpa[115].
Typically a quartz spring or a microbalance with precision was employed to measure the
in situ weight gain of a polymer sample as gas dissolved into it. Recently, a new apparatus based
on the gravimetric concept called magnetic suspension balance (MSB) became widely used in
measuring gas solubility in a variety of polymers at relatively high temperature and pressure. In
this research, the gravimetric method called magnetic suspension balance (MSB) will be the
apparatus utilized for the solubility measurement. Figure 1-4 from Chapter 1 shows a schematic
and a picture of the MSB apparatus. Sato et al. [62,64,120,121], Oshima et al.[86,117,122,123] and Li et
al.[58,60,124-126] have carried out intensive studies on blowing agents, such as CO2, N2 and butane
solubility in a variety of polymers or polymer blends, such as PP, PS, and PVC using the MSB
apparatus. The MSB and equation of state will be discussed in greater detail in the theoretical
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background section in Chapter 3. Although the gravimetric method is accurate in measuring the
solubility at moderate high temperature and pressure, a correction for buoyancy is necessary due
to the volume swelling or dilation of the polymer sample from the gas dissolution. In general,
the method needs correction of the volume swelling predicted using the equation of state (EOS)
for polymer. Detailed theoretical background regarding EOS will be discussed in Chapter 3 as
well since EOS is intensively used to predict the volume swelling of polymer/gas solutions in
order to help account for the buoyancy effect in the solubility measurement using the MSB
method.
There have been several studies on CO2 solubility and diffusivity in polymer and
associated change in polymer property[123,127-132]. Recently, Tomasko et al. made a
comprehensive review on CO2 solubility and diffusivity in polymer, the effects of CO2
dissolution on the polymer property, and their applications.
As seen from the equations, diffusivity determines how fast the gas can diffuse into the
polymer melts and it is a dynamic process while, on the other hand, solubility determines how
much gas can be dissolved into polymer melts at a saturated equilibrium state. In this research,
since our focus is on the PVT property of the polymer/gas solution at equilibrium states, which
means the polymer is completely saturated with blowing agents, solubility information is the
most important aspect that will be dealt with. As mentioned previously, one of the contributions
of this thesis is to obtain more accurate volume swelling from PVT measurement so that the
buoyancy effect caused by the polymer volume dilation due to gas dissolution could be more
precisely accounted for. Therefore, more accurate solubility can be determined from the MSB
method.
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2.2.2 Nucleation
As discussed previously in the section on foam processing, cell nucleation is the second
critical stage of the foaming fabrication process. Over the last few decades, vast number of
studies already been devoted to the study of cell nucleation. From the classical thermodynamic
law[133], when a thermodynamically equilibrium system is subject to any degree of instability,
there exists a critical size in the saturated system for bubbles to be nucleated. The following
equation determines the critical nuclei size:
systembubble
critical PPR
−=
γ2 (2-9)
This is known as the Laplace equation, and it represents the mechanical equilibrium between the
critical nucleus and its surroundings. γ is the surface tension at the phase interface.
For a metastable system, if the size of the nuclei is bigger than the critical size, the
bubble will start to grow, then the equilibrium would be interrupted and the system becomes
unstable. The relationship between the free energy barrier and the critical radius resulting from
thermodynamic instability is shown in the figure 2-4. The X axis represents the radius of the
nuclei and the Y axis represents the free energy barrier or the activation energy. The activation
energy is the energy needed to enable the bubbles to be nucleated at the critical radius so that the
nucleated bubble can keep growing once its radius is at or over this critical bubble radius,
otherwise the bubble will collapse. The activation energy or the energy barrier is at the
maximum when the bubble reaches the critical radius. When the bubble is growing beyond this
critical radius, the energy required is dramatically decreased.
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criticalhetR criticalRhom
Heterogeneous Nucleation Homogeneous Nucleation
Nucleus Radius R
actW
Figure 2-4 Schematic of Critical Nucleation Radius and Activation Energy
Nucleation of bubbles in the polymer can be described using the classical nucleation
theory[134-136], that was originally developed for a single-component system where the second
phase is created by evaporation of the liquid when superheated. The theory was then extended
by Blander and Katz[134] to a diffusion system where one component is volatile and forms
bubbles. There are two types of nucleation: homogenous nucleation and heterogeneous
nucleation.
The rate can also be determined through the classic nucleation theory. For homogenous
nucleation, the nucleation rate is articulated using the following equation:
( ) ⎟⎟⎟
⎠
⎞
⎜⎜⎜
⎝
⎛
−−=
2
3
hom3
16exp2
systembubble PPkTmNJ πγ
πγ
(2-10)
Bubble nucleation is heterogeneous when it is initiated at some preferred sites by mixing
the polymer with an additive, or the nucleation sites could have impurities inside the polymer
matrix. In general, nucleation tends to occur at the boundary of the matrix and additive rather
than inside the polymer matrix as with homogenous nucleation.
For heterogeneous nucleation, the nucleation rate is determined as:
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( ) ⎟⎟⎟
⎠
⎞
⎜⎜⎜
⎝
⎛
−−=
2
33/2
316exp2
systembubblehet
PPkTmQNJ πγ
πγ
(2-11)
Combined with the second law of thermodynamics and Gibbs’ free energy theory, the
initial energy needs to be overcame or the so-called free barrier energy for nucleation is derived
for both homogenous and heterogeneous systems as follows:
( )23
316
systembubble PPW
−=
πγ (2-12)
The above equations are a strong demonstration that surface tension serves as one of the
important parameters in determining every aspect of the nucleation process, from the critical
bubble radius, free energy barrier to nucleation rate. The surface tension between the gaseous
phase and the polymer/gas solution do play a significant role during the polymer process where
the cell size and cell density are important issues in controlling the final morphology of the
foamed products.
This would then lead to the next section of our discussion, which will reveal another
strong reason why this research is important and viable not only for academia but also for the
foaming industry.
2.2.3 Surface Tension
Surface tension is an intermolecular force caused by attraction and propulsion of
molecules at the interface between two mediums. Figure2-5 vividly illustrated the force balance
between gravity (fw) and surface tension (fs) of a small particle on a liquid surface. The unit for
Surface Tension used to be “dyne/cm”, but has been standardized to “mN/m” as a SI unit.
Numerous techniques have been developed for the measurement of interfacial properties. Wu[137]
gives a complete review on different techniques to measure the surface tension of polymer melts.
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Some of the major methods including the Wilhelmy plate technique[138-143]the drop weight
method[139-142], the oscillating jet method [139,142] the capillary wave method[139,142], the spinning
drop method[139-142,144-146], and drop shape techniques [139-143,147-160] are discussed briefly in this
section. Among those methods, the spinning drop method, drop shape techniques, i.e. the
pendant drop and sessile which are based on the analysis of the equilibrium shape of a drop in a
forced field, are often applied in the surface tension measure for polymer melts and polymer/gas
solutions.
Figure 2-5 Surface Tension and Gravity of Small Particle at Liquid/Particle Interface* *Source: http://en.wikipedia.org/wiki/Surface_tension
As the name implies, the Wilhelmy plate technique uses a detection plate for surface
tension measurement. The plate used is usually made of platinum or glass. When the bottom of a
vertically-oriented detection plate makes contact with a liquid surface, the liquid wets the plate
surface upward and a meniscus is created. At this moment, the surface area of the liquid is
expanded and surface tension tends to contract the surface area as a counteraction, and immerse
the plate downward. This method determines surface tension by measuring the force bringing
the plate downward via a counter balance. The measured downward force F directed to the plate
is related directly to the liquid surface tension [161]. The relation between the force and the
surface tension is expressed as follows:
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θργ
cosplatelv p
gVF Δ+= (2-13)
where platep is the perimeter of the plate, V is the volume of the displaced liquid, ρΔ is the
density difference between the liquid and air, and g is gravity. In general, if only the
measurement of surface tension is desired, then the plate is roughened to produce a zero contact
angle (complete wetting). This approach has a relatively simple and a high degree of accuracy
(results are typically given with an error of approximately 0.2%), but a major disadvantage of
the Wilhelmy plate technique is the requirement of a relatively large amount of liquid. The use
of a large reservoir can also make it difficult to maintain a high degree of purity, which is of
critical importance to all surface tension measurements since the introduction of impurities,
even small quantities, can dramatically affect the interfacial properties[162]. Moreover, this
method is rarely applied for surface tension of polymer melts or polymer/gas solution because of
their high viscosity.
Another similar method to the Wilhelmy plate method is the Du Nouy ring method
[139,140,143]. In this method, a circular loop of wire is used in place of a platinum plate. However,
while the Wilhelmy Plate method keeps the plate bottom immersed in the liquid surface, this
method requires lowering the liquid surface to detect the peak force upon removal of the ring
from the liquid surface. The disadvantages are: 1) the shape of the thin wire ring material
changes, which affects the measurement results, 2) the ring is less accurate when dealing with
higher viscosity materials, and 3) variations in surface tension over time cannot be measured
due to the mechanics of removing the ring from the surface[143].
The drop weight method was proposed in the 1900s. Since the weight of the drop falling
off the capillary correlates with the interfacial tension, the surface tension is then determined
through the following equation [163-165]:
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frgV
πργ
2Δ
= (2-14)
where V is the drop volume, r is the radius of the capillary and f is an empirical factor tabulated
as a function of cRr / ( cR , is a characteristic dimension defined as 3/1V )[163,164,166]. There are
some drawbacks to this method. First, although the technique itself is simple, the measurement
of the drop weight is very sensitive to vibration. Second, the vibrations of the apparatus can
cause premature separation of the drop from the end of the capillary before the drop reaches the
critical size. Last, since adsorption may occur when conducting the surface tension
measurements of multi-component solutions, the results may not reflect equilibrium saturation
of the solutes at the interface.
The oscillating jet method uses the oscillating jet generated by forcing the liquid through
an elliptical orifice with properties of standing waves[139,142,167]. In the absence of viscosity and
compressibility, the surface tension is related to measurable physical properties including the
wavelength of the oscillations, liquid density, mean radius of the orifice (i.e., average of the
minimum and maximum radii), and flow rate. In this method, the wavelengths are measured by
passing parallel light waves perpendicular to the jet stream[142]. Bohr[168] applied the method to a
real liquid by taking into account the influence of the velocity profile of the jet on surface
tension. The oscillating jet method has been used to study the surface tension of surfactant
solutions[139]. This method also gives reasonably accurate values of surface tension even if the
jet velocity profile is not included in the calculations [142]. A major problem associated with this
method is the cost of equipment because of the high degree of accuracy required in measuring
wavelengths.
If a deep body of liquid is perturbed by a vibrator, the surface of the liquid will oscillate
where the wavelength of the surface waves depends on the liquid surface tension and gravity[139].
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Such waves are called capillary-gravitational waves, as theoretically formulated by Kelvin[169].
The proper equation is as follows:
ρλπγ
πλ 2
22 +=
gv (2-15)
where v is the velocity of propagation, λ is the wavelength, g is acceleration due to gravity, γ
is surface tension, and ρ is the liquid density. It is clear that the propagation velocity is
determined by gravity for long waves and by surface tension for short waves (i.e., called
capillary waves) [142].
The theory of capillary waves is more complicated for viscous liquids, especially for
surfactant solutions with viscoelastic surface properties[142]. Similar to the oscillating jet method,
the theory of oscillations at a flat interface is based on the analysis of the Navier-Stokes
hydrodynamic equations and the boundary conditions at an interface. The details can be found
in References[170-173]. Again, similar to the oscillating jet method, the major problem associated
with the capillary method is the cost of equipment. In general, this method is more complex
from both theoretical and experimental aspects. Another disadvantage of this method is the large
amount of liquid required for each experiment.
Only a handful of methods are developed that could be used to measure the interfacial
tension of polymer melts or polymer/gas solutions, due to difficulties of the high temperature
involved and high viscosities of polymer melts. Those measurement methods are elaborated in
the following sections.
2.2.3.1 Spinning Drop Method
In this technique, a drop of liquid (or a bubble) is suspended in a denser liquid, and both
the drop and the surrounding liquid are contained in a horizontal tube spun about its longitudinal
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axis[142]. As a result of spinning, gravity has little effect on the shape of the drop. At low
rotational velocities (ω ), the drop (bubble) has an ellipsoidal shape, but when ω is sufficiently
large, it becomes cylindrical. Under the latter condition, the interfacial tension is calculated from
the following equation[174]:
23
41 ρωγ Δ= r (2-16)
where r is the radius of the cylindrical drop, and ρΔ is the density difference between the drop
and the surrounding liquid. One of the advantages of the spinning drop method is its
applicability to determine surface tension of highly viscous liquids when many traditional
methods are unsuitable. For instance, this method is appropriate for polymer melts with a
viscosity of 300-500 Pa*s [142]. In these experiments, a solid polymer is initially placed in the
tube that is heated to the melting temperature of the polymer while spinning in an oven with a
control window.
2.2.3.2 Drop Shape Techniques
Drop shape methods have been developed to determine the liquid-vapor or liquid-liquid
interfacial tensions and the contact angle from the shape of a pendant drop, sessile drop, or
captive bubble. In essence, the shape of a drop is determined by a combination of surface
tension and gravity effects. Surface tension tends to make a drop spherical whereas gravity tends
to elongate a pendant drop or flatten a sessile drop. When gravitational and surface tensional
effects are comparable, then, in principle, one can determine the surface tension from an
analysis of the shape of the drop. There are several advantages using the drop shape method: 1)
it only requires small amounts of the liquid, 2) it is easy to handle, and 3) it can be used in many
difficult experimental conditions such as studies of temperature or pressure dependence of
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liquid-fluid interfacial tensions. Drop shape methods have been applied to materials ranging
from organic liquids to molten metals and from pure solvents to concentrated solutions.
Also, since the profile of the drop may be recorded as digital images, it is possible to
study interfacial tensions in dynamic systems, where the properties are time dependent.
In the drop shape method the balance between surface tension and external forces, such as
gravity, is reflected mathematically in the so-called Laplace equation of capillarity.
Currently, the pendant drop or sessile drop is the most commonly used drop shape
method to measure the interfacial tension for polymer melts and is also most promising for the
challenging cases such as high pressure and high temperature application. Harrison et al.
measured interfacial tensions for PS oligomer (Mw=1850)/CO2[175] at 45 °C up to 310 bar where
γ decreases from 37.4 dyn/cm at 1bar to 1.5dyn/cm at 310 bar. Recently the sessile drop method
based on the Axisymmetric Drop Shape Analysis (ADSA) has been used intensively to study the
interfacial tension of polymer/gas solutions and has become one of the most popular and
efficient methods to obtain the surface tension data.
Rotenberg [54,176] developed the powerful technique, Axisyrnmetric Drop Shape Analysis
(ADSA), which fits the measured profile to a Laplacian curve using a nonlinear procedure. The
simplicity and accuracy of the ADSA method was further improved as Cheng [56,177]
implemented image processing techniques to detect the edge of the drop automatically. He
incorporated an automated edge detection technique into the ADSA program that improved
considerably the accuracy of the results and the efficiency of the "first generation" of the ADSA
technique (i.e. Rotenberg ADSA). del Rio [178,179] developed a second generation of ADSA to
overcome the deficiencies of the numerical schemes of the first generation using more efficient
algorithms. He used the curvature at the apex rather than the radius of curvature and the angle of
vertical alignment as optimization parameters.
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The latest third generation of ADSA developed by Mina et al.[180] would overcome some
inconsistent results from the previous two generations of ADSA. The detailed development of
this third generation ADSA can be found in Mina’s Ph.d. thesis[180].
Since supercritical CO2 is a promising solvent for application in polymer blending and
foaming, intensive surface tension studies of polymer/CO2 solutions have also been carried out
as documented in various literature. Huyk et al.[26,27,181] studied the surface tension of polymer
melts in supercritical carbon dioxide using Axisymmetric Drop Shape Analysis-Profile
(ADSA-P) method. Huyk et al.[26] investigated the surface tension of polystyrene (PS) melts in
supercritical carbon dioxide using the ADSA-P method at temperature ranges from 180oC to
210oC with pressure up to 4000 psi. The relationship between surface tension and density is
described by the empirical Macleod equation. They also studied the effects of molecular weight
distribution on surface tension using PS/CO2 [181] .
Again when closely examined, the equations for determining surface tension have been
closely associated with the density information of both phases. To be specific, the density
difference of the two interacting phases is one of the key variables of those formulas. This will
be seen implicitly in Chapter 3, when the theoretical background is illustrated. When the
formula is used to calculate the surface tension of polymer/gas solutions, the determination of
polymer/gas solution density once again becomes dependent on either pure equation of state
(EOS) calculations based on laws of thermodynamics or the corrected MSB solubility
measurement with the EOS predicted volume swelling. Although a more detailed theoretical
background will be described in Chapter 3, it is clear now that there is the need for obtaining
accurate density information for surface tension measurement. This is another one of the
contributions mentioned in the first Chapter. As for now, a more complete picture is painted for
the motives behind this research.
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2.3 Background on 3-D Object Reconstruction from 2-D Images
2.3.1 Introduction Reconstruction of a complex three-dimensional (3-D) rigid object from its two-dimensional
(2-D) images is a challenging computer vision problem under general imaging conditions. This
problem has sparked recent interest in the computer vision community[182-186] as a result of new
applications in telepresence, virtual reality and other graphics-oriented problems that require
realistic textured object models. Without prior information about the imaging environment such
as camera geometry, lighting conditions, object and background surface properties, etc., it
becomes very difficult to gain knowledge on the 3-D structures of captured rigid objects. There
are mainly two approaches for capturing the 3D shape of a real object: active and passive
methods. The active method can be grouped into two categories: contact and non-contact
scanners.
2.3.2 Active 3-D Reconstruction Method Contact 3D scanners probe the subject through physical touch. A coordinate measuring
machine (CMM) is an example of a contact 3D scanner. It is mostly used in manufacturing and
can be very precise. The disadvantage of CMM is that it requires contact with the object to
perform the scanning. The other disadvantage of CMM is that they are relatively slow compared
to the other scanning methods. Physically moving the arm on which the probe is mounted can be
very slow and the fastest CMM can only operate on a few hundred hertz. Laser range scanners
and encoded light projecting systems are non-contact systems that use active triangulation to
acquire precise 3D data[187]. 3D laser range scanners use laser light to probe the environment.
This technique is called triangulation because the laser dot, camera and laser emitter form a
triangle.
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Structured light 3D scanners project a pattern of light on the subject and look at the
deformation of the pattern on the subject. The pattern may be one dimensional or two
dimensional. The advantage of structured light 3D scanners is speed. Instead of scanning one
point at a time, structured light scanners can scan multiple points or the entire field of view at
once. This reduces or eliminates the problem of distortion from motion. Some existing systems
are capable of scanning moving objects in real-time.
Recently, Song Zhang and Peisen Huang[188] developed a real-time scanner using the
digital fringe projection and phase-shifting technique (a varied structured light method). The
system is able to capture, reconstruct, and render the high-density details of the dynamically
deformable objects (such as facial expressions) at 40 frames per second.
2.3.3 Passive 3-D Reconstruction Method
Compared to active scanners, passive methods work in an ordinary environment with
simple devices and the mathematics of differential geometry. A digital RGB camera from
different viewpoints captures the images of the target object while the target sits and rotates on a
turntable or as it uses multiple cameras to capture the images of the target at different
viewpoints. The 3D information is then extracted from the sequence of 2D (color) images by
using the following major techniques: 1) multi-view-stereo method 2) model based multi-view
stereo method and 3) volumetric modeling method. The volumetric modeling methods were
then later divided into two different methods and they are Shape from Silhouettes and Shape
from photoconsistency.
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2.3.3.1 Multi-view Stereo Method Early passive 3-D object model reconstruction attempts have been based on image matching.
This class of methods includes multi-view stereos which recovers 3-D geometry by using
correspondences across images, and by applying surface fitting and triangulation over the
estimated 3-D clouds of points[189-191]. The pairwise disparity estimation allows computing
image to image correspondences between adjacent rectified image pairs, and independent depth
estimates for each camera viewpoint. Takeo Kanade et al.[192] used a 4-camera system capable of
video rate image acquisition. The four cameras were used in a converging configuration for
more effective use of the camera view spaces. In addition, to recover dense stereo range data
from each set of images, they projected a varying sinusoidal pattern onto the scene to enhance
local intensity discriminability at each pixel and facilitate matches. This resulted in a
multi-baseline stereo system with active illumination. They also described in detail the
implementation of the depth recovery algorithm which involved the preprocessing stage of
image rectification.
In stereo processing, a short baseline means that the estimated distance will be less
precise due to narrow triangulation. For more precise distance estimation, a longer baseline is
desired. But with a longer baseline, however, a larger disparity range must be searched in order
to find a match. As a result, matching is more difficult, and there is a greater possibility of a
false match. Therefore, there is a tradeoff between precision and accuracy in the matching
process. T. Nakahara et al. [190] presents a stereo matching method that uses multiple stereo pairs
with various baselines generated by a lateral displacement of a camera to obtain precise distance
estimates without suffering from ambiguity. Matching is performed simply by computing the
sum of squared-difference (SSD) values. An advantage of this method is that it can eliminate
false matches and increase precision without any search or sequential filtering.
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Francis Schmitt and Carlos Hernández Esteban[193] presented another method which
combines both the shape from the silhouette technique with the multi-stereo carving technique
for the reconstruction of a 3D real object from a sequence of high-definition images. Their
method is fast and accurate for the estimation of the carving depth at each vertex of the 3D mesh.
The quality of the final textured 3D reconstruction models given in their study validated the
method.
There are disadvantages of using the multi-view stereo method. In order to find effective
correspondences, views must be close together and correspondences must be found in the
images. Resultant partial 3-D clouds of points for different views must be triangulated and fused
into a single consistent model. In case of sparse correspondence, a parameterized surface model
has to be fit to represent the sparse 3-D points for surface modeling. The explicit handling of
occlusion between views is not addressed.
2.3.3.2 Model-based Multi-view Stereo Method
In order to avoid multi-view stereo drawbacks, the model-based multi-view stereo
approach is proposed by J. Malik et al.[194]. Model-based techniques differ from traditional
stereos in that they measure how the actual scene of the images deviates from an initially given
approximate 3-D model. Model-based approaches reduce the correspondence problem for views,
which are relatively apart. Occlusion problems are also addressed by the use of an initial model
and when the fusion of view-based partial surfaces are eliminated. J. Malik et al.[194] presented
an approach for creating realistic synthetic views of existing architectural scenes from a sparse
set of still photographs using the model-based multi-view stereo techniques. The approach
combines both geometry-based and image-based modeling, plus rendering techniques and
consists of two components. The first component is an easy-to-use photogrammetric modeling
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system which facilitates the recovery of a basic geometric model of the photographed scene.
The modeling system is effective and robust because it exploits the constraints that are
characteristic of architectural scenes.
The second component is a model-based stereo algorithm, which recovers how the real
scene deviates from the basic model. By making use of the model, the stereo approach can
robustly recover accurate depth from image pairs with large baselines. Consequently, this
approach can model large architectural environments with far fewer photographs than current
image-based modeling approaches.
The view-dependent texture mapping method is also presented to better simulate
geometric detail on basic models. This approach can recover models for use in either
geometry-based or image-based rendering systems. The results were demonstrated when it was
used to create realistic renderings of architectural scenes from viewpoints far from the original
photographs.
However, model-based multi-view stereo approaches need an initial 3-D geometric
model which brings additional user interaction.
2.3.3.3 Volumetric Modeling Method
In order to avoid the disadvantages of multi-view stereos and model-based stereos, the
3-D scene space solution or the volumetric modeling method has been proposed[195-197] . This
method represents the volume of the object by making occupancy decisions about whether a
volume element i.e. voxel, contains object volume in 3-D scenes. The volumetric modeling
method allows views to be captured apart from each other, which may cause problems in other
methods. More importantly, this method eliminates correspondence problems. On the other hand,
the final model evolves from an initial volumetric scene representation in which the object of
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interest lies. In this context, there is no need to fuse an initial model and resultant 3-D object
data which is the case in multi-view and model-based stereo systems. The occlusion problem is
also addressed by using regular tessellation of the initial bounding volume as voxels. However,
volumetric modeling of object spaces depends on the calibration of the cameras for each image,
and on an initial bounding volume of the object space.
As mentioned in the introduction, the volumetric scene modeling approaches can be
further grouped into two separate approaches: 1) shape from silhouettes and 2) shape from
photoconsistency.
2.3.3.3.1 Shape from Silhouettes
Shape from silhouettes technique deals with the reconstruction of 3-D solid models by
volume intersections from a set of silhouette images. Silhouette-based 3-D reconstructions have
been well known in literature and in practice. It constructs the approximated visual hull of the
object from a finite image sequence. One of the first complete 3-D modeling systems based on
silhouette images is the so-called Hannover system by Niem et al.[198-200] Many concepts and
techniques of the current systems are based on the ones explained and implemented in this
system. Matsumoto et al.[201] improved the silhouette technique by introducing the new concept
of voting in the implementation of the volume intersection.
For practical 3-D reconstruction solutions, the problem can be simplified by using
controlled imaging environments. In such an environment, the camera makes a controlled
motion around the object, and the background surface and lighting are selected to reduce the
specularities on the acquired image. The camera has to be calibrated in such a setup to obtain the
internal and external parameters defining the physical properties of the camera and also the
camera imaging positions with respect to the rotary table turn angles. Niem et al.[198-200] and
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Matsumoto et al.[201] used a setup consisting of a rotary table (turn-table) with a fixed camera to
obtain a controlled camera motion around the object. Altalay et al.[202] has described a complete,
end-to-end system that explains the steps of using the silhouette method. The flowchart of the
silhouette-based method for 3-D reconstruction is shown in the following Figure.
Silhouette Extraction
Silhouette based Volume Intersection
3‐D Model Fine Tuning using
Photoconstistency
Appearance Reconstruction
Image Acquisition
Camera CalibrationBounding Cube Estimation
Figure 2-6 3-D Object Reconstruction Scheme There are basically six major steps of using shapes from silhouettes after image acquisition: 1)
calibration of a turn-table and extraction of the rotation axis based on vision geometry 2)
silhouette extraction 3) visual hull generation 4) voxelization 5) 3-D model fine tuning using
photoconsistency 6) appearance reconstruction
The first step is the calibration of the turn-table and the extraction of the rotation axis.
This is essential in achieving a high quality of 3-D reconstruction. One major source of
calibration error is the inaccuracy in the 3-D to 2-D mappings of the n known points. A
multi-image camera calibration approach proposed by Lavest et al.[203] is used to estimate the
precise 3-D coordinates of the geometrical calibration target when the intrinsic and extrinsic
camera parameters were represented by the unknown vector.
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The second step is to extract the silhouette of the real object from the camera images. In
controlled environments, this segmentation of the real object against the background can be
facilitated by using a background of uniform colour.
In the third step, a bounding pyramid volume is constructed using the focal point of the
camera and the silhouette. The convex hull of this bounding volume is formed by the lines of
sight from the camera focal point through different contour points of the object silhouette shown
in the following schematic. The coarse object volume or the convex hull of the object can be
computed to obtain the bounding box of the object when the camera parameters and the object
silhouettes on the images are known.
Figure 2-7 Visual Hull Construction from Volume Intersection
The fourth step is voxelization. The bounding box of the object is then discretized into
small cubes or voxels. Assuming that each side of the box is divided into n voxels, a voxel space
V containing n3 voxels is generated. Subsequently, each cube in the voxel space is projected
onto the images by using the related camera parameters. If the projected cube region on any
selected image is totally not contained by the silhouette region, it is removed from the voxel
space. Otherwise, it is kept in the object voxel space.
The next step is to augment the silhouette-based reconstruction with photometric information
existing in the images to minimize the problem of excess voxels from the visual hull
approximation due to the concavities on the object and the insufficient camera viewing points.
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In the approximated visual hull of the object obtained from finite sets of images, each
surface voxel has a set of images from which the voxel can be seen. If it is assumed that a
surface voxel is placed in the correct depth, meaning that it is on the real object surface, then the
stereo theory states that its projections on the images from which it can be seen, must be the
corresponding regions. In other words voxels having correct depth placement in the
approximated visual hull have photoconsistent projections on the images from which voxels are
seen without occlusion. The idea, theory and algorithm of using photoconsistency and carving in
volumetric voxel spaces is first introduced by Seitz et al. [195] and have recently been improved
by several researchers.[195,197,204-206] The approaches using photoconsistency to generate 3-D
models is generally called voxel coloring. Starting from an initial set of opaque voxels, voxel
coloring algorithm carves the voxels that are not photoconsistent as it goes through the opaque
voxels. The algorithm stops when all the opaque voxels are color consistent.
Furthermore, carving the voxels of the model resulting from silhouette and the use of
multiple view-based stereo has also been described. but the details and the experimental results
are not given. The system described by Gibson et al.[207] requires no pre-calibration of the
camera and uses full perspective geometry. The authors claim that self-calibration is used.
However, there is no detailed information given in the paper related to this subject. Fitzgibbon
et al. [208] describes the projective geometry of single axis rotation (rotation similar to that
discussed in our work) and gives its automatic and optimal estimation from an image sequence.
However, it is shown that 3-D structures and cameras can be calibrated up to an overall
two-parameter ambiguity. The two-parameter reconstruction ambiguity is removed by
specifying the camera aspect ratio and parallel scene lines. Apart from the use of uncalibrated
multiple views, the system is very similar to that of Hannover. In addition, the work does not
indicate any further refinement to remove the disadvantages of volume intersection method.
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A study by Mendonça et al.[209] described a method for motion estimation of an object
rotating around a fixed axis. Based on this information, 3-D positions of the points on the
contours of the objects were found by the triangulation and epipolar parameterization. The
method is relatively simple particularly compared to that proposed by Fitzgibbon et al.[208] in the
sense that it only needs a few number of correspondences. One point which is not very clear in
the study of Mendonça et al.[209] is that for the reconstruction of an object model, some means of
interpolation would be required since only contour information is used.
The last step is the texture mapping and visualization of the reconstructed object in 3-D.
Volumetric voxel representation should be transformed to a representation by triangular patches.
A simple and practical technique, called the Marching Cubes Algorithm[210,211] is generally used
in computer graphics to do such a conversion. Marching Cubes Algorithm uses the isolevel
information of the vertices of the voxel in order to interpolate an isosurface passing through the
voxel. Having constructed the geometry of the object, it is needed to recover the appearance, in
other words, the texture of the surface should be determined. Texture mapping is a well-known
technique that is used to achieve a high degree of realism in virtual reality applications. In
image-based 3-D model reconstructions, the texture of the model is extracted from the images of
the object. This increases the realism of the reconstructed model considerably[212].
As mentioned previously, the main drawback of the silhouette-based volume intersection
approach is the additional excess volume coming from an insufficient number of viewing
positions and from the concavities on the object to be modeled. It is impossible to engrave the
additional volume filling the concavities, even if the infinite number of images is used in the
process. In order to carve excess voxels from the inferred visual hull, which is approximated by
silhouette based volume intersection, an algorithm based on photoconsistency is developed.
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2.3.3.3.2 Shape from Photoconsistency
Rather than using binary silhouette images, shapes from the photoconsistency technique
employs additional colored photometric information.[195] This improves reconstruction results at
the excess voxels existing in the approximated visual hull. Shapes from photoconsistency
methods use the color consistency constraints to distinguish object surface voxels from other
voxels. Color constraints for a voxel states that a surface voxel has color consistent projection
regions on the images from which it is seen. Use of shape from the photoconsistency approach
avoids point correspondence difficulties. 3-D reconstructions based on photoconsistency require
camera parameters for each used view and a model for the object surface reflectance.
Furthermore, a very important issue in these methods is the criterion for consistency
checks. Most of the consistency criteria require a threshold or input from the user. In addition,
voxel visibility problems have to be well addressed since the color consistency checks for a
voxel requires the set of images from which the voxel is visible. Efficiency in the visibility test
for every voxel is essential. In order to easily maintain visibility information for voxels, voxel
coloring algorithm proposed by Seitz and Dyer [195] restricts the position of cameras so that no
object point is contained within the convex hull of the camera centers. However, there are
several extensions to the initial voxel coloring algorithm for the visibility problem[196,197,213-215].
Instead of using these extensions and alternatives requiring additional space and complex
updates as carving progress, or using multi sweeps along the coordinate axes, traversing a ray
from the voxel center through the camera center is proposed to check visibility. It is also
possible to find the maximum photoconsistent voxels on the ray and this eliminates threshold
checks while carving the voxel from the initial set. This algorithm is mostly inspired from the
work of Matsumoto et al.[205]
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In recent years, there has been a significant interest in 3-D reconstruction from
uncalibrated views. These auto-calibration techniques have been the object of a tremendous
amount of work[216-220] and as such effective methods to derive the epipolar geometry and the
trifocal tensor from point correspondences, have been devised[208,221]. However, most of these
methods assume that it is possible to run an interest operator such as a corner detector [208,220]to
extract from one of the images a sufficiently large number of points that can then be reliably
matched in the other images. When using images exhibiting too little texture, such interest
points are not reliable. It has been shown that projective, affine and Euclidean reconstructions
can be obtained from uncalibrated views[216,222-225]. However, these methods are sensitive to
noise and initialization and generally, the reconstruction results are valid up to a scale factor.
2.4 Summary
This chapter helps to walk through most of the literature reviews associated with the
most relevant topics of this research. The methods for pure polymer PVT measurement are
described. The methods and apparatus used to measure the PVT of polymer/gas systems are also
explained and the difficulties associated with them in measuring polymer/gas solutions PVT at
high temperature and pressure are addressed. The topic of solubility and diffusivity is also
touched upon since solubility is very important processing parameter in the polymer foaming
industry. Knowing how to accurately measure gas solubility inside a polymer melt would help
not only in achieving better products, but also in process and equipment design in terms of
knowing the right amount gas required at any specific temperature and pressure. Nucleation is
also an important issue in polymer process. The rate of nucleation would determine the cell size
and cell density that could ultimately affect cell morphology. To a large extent, the cell
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morphology is the key determining factor of the foam properties, such as mechanical, acoustic,
and insulation properties. The development of surface tension and methods of measuring it are
also addressed in detail. Since surface tension is one of the important factors in cell nucleation
and the determination of surface tension requires density information of the polymer/gas
solution as an input, the importance of getting accurate density information through PVT
measure for surface tension is also self-explanatory. The up-to-date works on 3-D object
reconstruction based on 2-D images in the content of computer vision and image processing are
also investigated. The setup of our proposed methodology is similar in the way that 2-D images
are used for obtaining 3-D information, i.e. volumetric value. Due to the nature of our
experiment the approach proposed in this research is unique and the simplest design. Details
regarding the design of the system would be elaborated in Chapter 4. In summary this chapter
not only serves as a background survey, but also gives the reasons and the motives behind this
research.
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Chapter 3. Theoretical Background
3.1 Theoretical Background on Equation of State
3.1.1 Introduction
The behaviours of any natural system can be described using thermodynamic law, which
includes postulates and equations. According to the classical thermodynamics, the following
three basic terms need to be introduced into a system: 1) Enthalpy (H), 2) Helmholtz free energy
(A), and 3) Gibbs free energy (G). Their relationships[226,227] are described as follows:
pVUH += (3-1)
TSUA −= (3-2)
TSHG −= (3-3) Where U is the system internal energy; S is the entropy; p is system pressure; and T is the
temperature of system. According to the Boltzmann equation (3-4) the entropy ( S ) of the
system could be determined as long as the Ω (the number of states accessible to the system) is
known, where K is Boltzmann's constant.
( )Ω= lnKS (3-4)
If a thermodynamic model is available and can be applied to calculate all the above state
properties (H, S, A, G) of a system, we can easily get the following equation to describe the
pressure-volume-temperature (PVT) relation of the system, which is the so-called equation of
state (EOS):
TVAP ⎟⎠⎞
⎜⎝⎛∂∂
−= (3-5)
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The ultimate target of thermodynamics is to describe the macroscopic properties of
systems at equilibrium condition. For example, thermodynamic models are used for calculations
of the enthalpies, heat capacities, and phase equilibria. Regarding equilibrium systems,
statistical thermodynamics provides a link between the microscopic world of atoms/molecules
and the macroscopic world of bulk properties. Statistical thermodynamics provides means to
calculate fundamental thermodynamic quantities or macroscopic properties from knowledge of
the quantum states available to a system comprising of particles, molecules or components. The
challenge of statistical thermodynamic is how to properly describe the small particle in a
molecular or sub-molecular level [226].
3.1.2 Equation of State (EOS)
Equation of state (EOS) is a mathematical relation between volume, pressure,
temperature, and composition[228,229]. Originally, equations of state were developed and used
mainly for pure components. They were first applied to non-polar mixtures in 1970s[230,231].
Subsequently, EOS was developed rapidly for the calculation of phase equilibrium in non-polar
and polar mixtures. The Van der Waals EOS was the first equation to predict vapour-liquid
coexistence. Many equations of state have been proposed, but most of them are categorized into
two classes: empirical (or semi-empirical) and theoretical.
Equations of state can be used over a wide range of temperature and pressure and they
can be applied to mixtures of diverse components, ranging from light gases to heavy liquids.
They can be used to calculate vapour-liquid, liquid-liquid and supercritical fluid-phase
equilibrium. The calculation of phase equilibrium has been discussed intensively in the literature
recently and this literature is reviewed in detail[232]. For the polymer system, a variety of EOSs
were also proposed for the correlation of polymer PVT behavior. The Flory EOS[33,233,234], the
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Simha-Somcynsky EOS[43,44,235-237], and the Sanchez-Lacombe EOS[41,42,238-240] are the most
widely used EOS for polymer system. In this research, SL and SS are the two equations of state
which would be used to assist in solubility studies and will be explained more in the following
sections.
3.1.3 Equations of State for Polymers and Polymer/Gas Solutions
3.1.3.1 Introduction
The details of the derivation of SL, SS and SAFT EOS are not repeated here since those
works have already been well established in the literature by many others. The basic
thermodynamic guidelines upon which those EOS are built are stated briefly. The need to
interpret and correlate the properties of polymer liquids and their solutions or polymer/solvent
solution is the initiation of many thermodynamic models.
The majority of thermodynamic theories for polymer liquids are roughly based on four
models or theories: 1) cell models, 2) lattice-fluid models, 3) hole models, and 4) perturbation
theories. Those inlcude the cell model of Prigogine[40], the modified cell theory of Dee and
Walsh[31,32], lattice theory of Flory[233] and Huggins [241], the lattic fluid model of Sanchez and
Lacombe[41,42,239,240] and Panayiotou and Vera [37,242], the non-equilibrium lattic fluid (NEFL)
model of Doghieri and Sarti[243], the group-contribution lattice fluid model of parekh and
Danner[244], and the lattice hole theory of Simha and Somcynsky[44,235].
More recently, the statistical associating fluid thoery (SAFT) modified based on
Wertheim’s thermodynamic perturbation theory (TPT)[245-248] was developed by Chapman et
al.[249,250] Later Huang and Radosz[251,252] modified the SAFT model. The criteria for the first
three models are the mathematical formalism used in accounting for the compressibility and
thermal expansion of the system. Cell models restrict volumetric changes in the system to
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changes in cell volume, that is, the space surrounding a polymer segment placed on a lattice
framework. In contrast, lattice-fluid models allow empty sites or lattice vacancies while the cell
volume is assumed constant. Hole models make allowances for both cell expansion and lattice
vacancies[28]. The main assumption of perturbation theories is that the residual (difference to
ideal-gas state) part of the Helmholtz energy of a system Ares can be written as the sum of
different terms whereas the main contribution is described by the Helmholtz energy of a chosen
reference system[253]. Most of the theoretical models use mixing rules to describe the mixtures
without changing the structure of the model and also use the reduced variables scaled by
characteristic parameters. Zoller[254] and Rodgers[28] have worked on the PVT behavor of
polymers and compared the predictions using various models. The details of those EOS, except
for SL and SS EOS, are omitted in this research because they are not used in solubility
measurement. SL and SS are the EOS used with solubility measurement in this study and is
explained more mathematically in the following sections.
3.1.3.2 Sanchez-Lacombe (SL) EOS
The Sanchez-Lacombe (SL) EOS is the most widely used thermodynamic model to
describe the PVT property of polymer/gas solutions. As previously mentioned, SL EOS is
derived based on lattice fluid theory which allows for vacancies in the lattice and assumes the
polymer has a flexible liquid structure. The reduced form of SL EOS is through equation
(3-6):
( ) ⎥⎦
⎤⎢⎣
⎡⎟⎠⎞
⎜⎝⎛ −+−−−= ρρρ ~11~1ln~~~ 2
rTP (3-6)
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In the above relations, ρ~,~,~ PT and V~ are reduced parameters. They are calculated from the
characteristic reducing parameters P*, T*, V* and ∗ρ as follows:
∗∗∗∗ ==== VVVPPPTTTVV /~;/~;/~;/~/1 ρ ;∗∗
∗=
ρTR
PMr (3-7)
r is the fraction of occupied lattice sites by a molecule composed of r segments or “mers” and M
is the molecular weight. Each molecule in this theory is characterized by P*, T*, ∗ρ that are
used as the normalization constants for the reduced parameters. These characteristic parameters
are typically fit to vapour pressure or liquid density data and are tabulated for other polymers.
Typical gas and polymer characteristic parameters could be found in the literature [91-93].
Mixtures are handled using volume fraction based mixing rules with an adjustable binary
interaction parameter 12k .
3.1.3.3 Simha-Somcynsky (SS) EOS
Hole theory was proposed by Simha and his co-workers[43,44,235,236] in order to improve
on the cell model for the liquid state. Hole theory considers that each lattice of a site can
accommodate either a small molecule or a chain segment. Also as in lattice fluid theory, hole
theory adopts an improvement of the cell model for the liquid state by the introduction of
vacancies in the lattice [44], which describes the major part of the thermal expansion. Changes in
cell volume itself, which have a non-negligible influence on the thermodynamic properties, are
also allowed. In the Simha-Somcynsky hole mode, the “square well” approximation to the cell
potential is used and non-nearest neighbour contributions to the lattice energy are included. The
resulting coupled equations of state must be solved simultaneously with an expression that
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minimizes the partition function with respect to the fraction of occupied sites. The reduced
equation for SS EOS is:
TQyQTVp ~
)2045.1011.1(2)1(~/~~22
1 −+−= −η (3-8)
( )22 033.3409.2~613/1)1ln(1
3QQ
Ty
yy
ss
cs
−+−−
=⎥⎦
⎤⎢⎣
⎡ −+
−⎟⎠⎞
⎜⎝⎛
ηη
(3-9)
Again ρ~,~,~ PT and V~ are reduced parameters in the above relations. They are calculated from
the characteristic reducing parameters P*, T*, V* and ∗ρ . Small s is the number of segments
per chain, c is the number of external degrees of freedom per chain, and
1/ 6 1/ 31/( ) , 2Q yV and yQη −= =% are dimensionless quantities.
3.1.3.4 Statistical Associating Fluid Theory (SAFT)
Although the statistical associating fluid theory (SAFT) model is not the focus of this
research, due to its rising popularity, there is a need to explain this equation of state model in
greater detail. The equation of state based on Statistical Associating Fluid Theory (SAFT)
describes the molecules which move freely in continuous space. SAFT EOS was extended based
on Wertherim’s Thermodynamic Perturbation theory[245-248] from Chapman et al.[249,250] Huang
and Radosz developed the modified SAFT equation of state. The SAFT EOS accounts for
hard-sphere repulsive forces, dispersion forces, chain formation and association. It could be
represented as a sum of four Helmholtz function terms:
nassociatiochainsegmentres AAAA ++= (3-10) or it could be also in the form of the compressibility factor:
nassociatiochainsegment ZZZZ +++=1 (3-11)
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The SAFT model describes liquid molecules as equal-sized spherical segments interacting
according to a square-well potential. The detail derivation of the above equations can be found
from studies of Huang and Radosz.
3.2 Models of PVT Measurement
Several models or equations of state (EOS) have been proposed to describe the PVT
behavior of polymeric liquids based on thermodynamic law. Those equations of state for
polymer are either empirical or theoretical. The most widely used empirical equation is the Tait
equation[46].
The Tait equation is an isothermal compressibility fitting model rather than a true
equation of state. It reliably calculates the specific volume of pure polymer at different
temperatures and pressures using PVT data measured from a bellow type dilatometer.
Tait proposed an empirical model of average isothermal compressibility for fresh and sea water
as follows:
( ) ( ) ( ) ( )( ) ⎥
⎦
⎤⎢⎣
⎡+−+
=PTB
TPCPTBTPvTPv ,, 0 (3-12)
Where 0P is the initial pressure and ( )TPv ,0 , ( )TB and ( )TC are functions of temperature
only. Wohl [255] took the similar concept and rewrote the compressibility definition to derive the
following equation:
( )( ) ( )
( ) ⎥⎦
⎤⎢⎣
⎡+
=⎥⎦⎤
⎢⎣⎡
∂∂
−PTB
TCP
TPvTPv T
,,
1
0
(3-13)
After performing integration on the above equation, the following can be derived:
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( ) ( ) ( ) ( ) ⎭⎬⎫
⎩⎨⎧
⎥⎦
⎤⎢⎣
⎡+
−+−=
0
00 1ln1,,
PTBPP
TCTPvTPv (3-14)
By letting 00 =P the equation becomes:
( ) ( ) ( ) ( ) ⎭⎬⎫
⎩⎨⎧
⎥⎦
⎤⎢⎣
⎡+−=
TBPTCTvTPv 1ln1,0, (3-15)
Where the zero-pressure isotherm is:
( ) TvvTv 10,0 += (3-16)
And the ( )TB is also known as:
( ) TBeBTB 10
−= (3-17)
where 010 , Bandvv are constants. They are determined based on the empirical fitted data for
each different material grade. The ( )TC is a universal constant and is independent of
temperature. The value is 0.0894. Therefore the following equation is the finalized general Tait
equation form:
( ) ( ) ( ) ⎭⎬⎫
⎩⎨⎧
⎥⎦
⎤⎢⎣
⎡+−=
TBPTvTPv 1ln0894.01,0, (3-18)
The equation has various forms and coefficients depending on the grade of the polymer sample
used.
Empirical studies have been carried out to examine the PVT relationship for polymer/gas
solution empirically besides using EOS to calculate the PVT relation. Most of the background
for polymer/gas PVT measurement were already explained in previous literature section.
Foster et al.[69] used a cylinder-piston-type method in a compressibility chamber to
acquire PVT data by multiplying the cross-sectional area of the piston with the linear
displacement of the piston. Ender[68] has used the coil of a linear variable differential
transformer (LVDT) to measure the volume swelling of various elastomers under high pressures
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in CO2 at relatively low temperatures. Wissinger et al.[75] presented a method of measuring
polymer swelling by determining the changes in length of a thin polymer film. And the change
in volume is related to its changes in length using the following relation:
13
00−⎟⎟
⎠
⎞⎜⎜⎝
⎛=
ΔLL
VV (3-19)
Unfortunately, their approach is only valid for isotropic swelling. Furthermore, the
warpage of the samples limits its application and results in an inaccurate length measurement. In
general, most of the methods described above operate at fairly low temperatures, ranging from
25°C to 100°C. Park et al. [71] measured the PVT properties of polymer/CO2 solutions using a
foaming extruder and a positive-displacement gear pump mounted on the extruder. The major
drawback of this method is the required (and limited) extrusion processing conditions for
measuring the PVT data.
3.3 Solubility Measurement Using MSB
Having talked in Chapter 2 about what has been done in measuring the solubility data of
gas in the polymer matrix, the focus now is on how solubility is measured and calculated using
magnetic suspension balance (MSB), since one of the motives of this research is to facilitate a
better MSB solubility measurement by using PVT apparatus. Seen from the previous MSB
schematic, the polymer sample was placed in a container inside the sorption chamber before the
experiment. The chamber was then sealed, evacuated, and preheated to the experimental
temperature. The read-out from the balance at the vacuum condition (P=0) and this specific
temperature (T) was denoted as ( )TW ,0 . The chosen blowing agents, such as CO2, N2 or butane
were compressed and introduced into the sorption chamber. The pressure was maintained by a
syringe pump. A Jalabo TD-6 heating circulator was utilized to control the temperature of the
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sorption chamber with precision. The mass of the sample will increase during the sorption
period untill the equilibrium state is reached or in other words, the sample will be saturated with
the surrounding gas reservoir at that pressure. When the equilibrium state is reached, the sample
mass will not change unless a high pressure is introduced by having more compressed gas enter
the sorption chamber. At that particular pressure (P) and temperature (T), the weight read-out of
the balance is denoted as ( )TPW , . Therefore the amount of gas that dissolved into the polymer
at each pressure and temperature condition is denotes as gW and is calculated through the
following equation:
( ) ( ) ( )sPBgasg VVVTWTPWW +++−= ρ,0, (3-20)
Where gasρ is the density of the gas and can be measured in situ by the function of MSB; BV
is the total volume of the sample holder and measuring load coupling devices shown in Figure
1-5. This BV volume is determined using the buoyancy method with the high-pressure gas; and
PV is the volume of the pure polymer sample at pressure P and temperature T. This volume can
be determined from the Tait equation of pure polymer with the weight of the polymer sample.
sV is the swellon volume of the polymer/gas mixture due to the gas dissolution. If this swellon
volume term is being ignored, then the reading of the balance will be the so-called “apparent”
solubility of the polymer/gas solution.
In order to get accurate solubility data, volume swelling has to be taken into account. But
with the lack of direct measurement data, the only method is to utilize those equations of state
(EOS) to predict the swelling information. This is one of the reasons why EOS is important and
has been detailed in the beginning of this chapter. Among the various EOS, the most popular
ones are the SL, SS and SAFT EOS. The SL and SS EOS are also going to be the focus of this
research in the latter chapter when the swellings from direct measurement from the newly
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developed PVT apparatus are compared with those predictions. By taking into account the true
volume swelling sV from the direct measurement, the equation can then be used to determine
the true solubility directly without relying on the predicted values from EOS.
3.4 Viscoelastic Models of Polymers
Since the hypothesis made in the later section from the research results is strongly
related with the viscoelasticity property of polymer material, it is necessary to elaborate on the
study of polymer’s viscoelastic characteristic. The polymer materials are non-Newtonian fluid in
nature. Newtonian fluid is a fluid that does not pose elastic properties and has no memory of
past deformations. The study that needs to be done with Newtonian fluid is the measurement of
its deformation rate, rather than its strain. Since the polymer material is non-Newtonian fluid
and is both elastic and viscous in nature the so-called viscoelasticity is one of the most important
rheological properties of polymer melt. This uniqueness of the elastic and viscous nature of
polymer determines many of the properties of polymer melt in experiments and industrial
processing. The following example describes the distinctive difference between elasticity and
viscoelasticity. Rubber is different from polymer material in that the chains in the former are
cross-linked by chemical means. A rubber material can be regarded as macroscopic
three-dimensional network formed of strands of polymer chain with both ends as cross-links.
Because the cross-links in rubber keep the chain strands from moving away from their relative
positions over a distance larger than the strand size itself, the chains do not flow with the
deformation and are able to recover their conformations once the deformation is released. In
contrast to this behaviour, an un-cross-linked polymer exhibits the elastic response only at its
linear region for momentary deformations. But under a prolonged deformation, it cannot recover
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its original shape because the molecular chain has flowed. Therefore, for a polymeric melt, the
elasticity and viscosity are both considered. The slow flow property of the polymer is
characterized by its viscosity. There are two different approaches to model the viscoelasticity of
polymeric fluids[256]: 1) models based on the polymer chain dynamics within the linear region,
such as Maxwell equation and Boltzmann’s superposition principle, and 2) models based on the
molecular theory such as Elastic Dumbbell Model, the Rouse Model and the Doi-Edwards
Model.
3.4.1 Maxwell Equation
An easy way to describe the Maxwell equation is to use a simple spring and damper to
represent the elastic and viscous natures of the viscoelasticity of polymeric fluids.
F
……
.
damper spring
F
……
.
damper spring
Figure 3-1 Generalized Maxwell Model Represented by Spring-Damper Systems
Figure 3-1 shows a simplified and generalized Maxwell model represented by spring and
damper combinations. The general Maxwell equation is as follows:
( ) ( )∑=i
i tt σσ (3-21)
with
( ) ( )•
−=+ λτη
στ
σi
ii
ii tt
dtd 1
(3-22)
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and
i
ii G
ητ −= (3-23)
Where iτ is the relaxation time of the viscoelastic system, iσ is the stress, iη is the viscosity,
•
λ is the shear deformation rate and iG is the relaxation modulus.
3.4.2 Boltzmann’s Superposition Principle
Boltzmann’s superposition principle assumes that if the stress at the present time t is
caused by a step strain at an earlier time t’, the stress is linearly proportional to the strain, and
the proportionality or the modulus decreases with the separation of the time, t-t’. The modulus, a
decaying function of t-t’, is denoted by G(t-t’). Boltzmann’s superposition principle says that
when a system has been applied with small step strains at different times, t1, t2, ..etc…before the
present time t, then all those stresses caused by the individual step strains are independent of
each other, and the total stress at t could be simply expressed as the summation of all those
stresses:
( ) ( ) ( )∑ Δ−−=i
ii tttGt λσ (3-24)
3.4.3 Doi-Edwards Model and Entanglement
The theories developed based on molecular interaction are the most complicated area in
polymer rheology. Since it is not the main focus of this research, mathematical rigour is not
attempted in this introductory treatment for the Elastic Dumbbell Model and the Rouse Model.
Since the effect of the polymer chain entanglement density on the volume swelling hypothesis is
postulated in a later section based on research findings, the Doi-Edwards Model developed from
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polymer chain entanglement is worth taking a brief look at. Chain entanglement is a kind of
intermolecular interaction that occurs in a concentrated long-chain region of polymer melt.
Unlike other types of intermolecular interactions, it does not involve any energetic change and
does not give rise to a change in the electron density, hence chain entanglement cannot be
observed by microscopes or static scattering or absorption spectroscopies. The Doi-Edwards
Model could be represented in a simple form as follows:
N
e GRTM ρ
= (3-25)
eM is the entanglement molecular weight and NG is the plateau modulus[257-259].
Chain entanglement mainly affects chain motions. Another strong effect of chain
entanglement is the observation of a clear plateau in the linear relaxation modulus
( )tG [257,259,260] and storage modulus spectrum ( )ω'G [260]. Those terms could become clear in
the later sections when the rotational rheometer is used to study the polymer chain entanglement
density.
3.5 Surface Tension Measurement
As described in the earlier background and literature review, many different techniques
and apparatus have been developed to study and measure surface tension. Out of all those
methods, the drop shape method becomes the most used because of numerous advantages. For
instance, drop shape method only requires a small amount of sample to conduct an experiments
in comparison with the Wilhelmy plate technique. Also the drop shape method is easy to handle
and can be used in difficult experimental conditions such as in studies of high temperature and
pressure effects on surface tension. In addition, this method can be applied to a variety of
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materials, ranging from organic liquids to molten metals and from pure solvents to concentrated
solutions. In our case, this method is utilized for polymer/gas solutions. Also, as pointed out by
Hoofar et al. [180], the drop shape method could be used to study surface tension in a dynamic
system by recording digital images where the properties are time dependent. So in this section, a
brief theoretical background based on what has been introduced previously will be expanded on
to illustrate the mathematics behind the drop shape method.
Traditionally, the Young-Laplace capillary equation, as shown in equation (3-26) is the
basis of the surface tension measurement. The equation actually shows a balance between
surface tension and external forces, such as gravity, in mathematical form. It also shows the
relationship between the radii curvature and the pressure difference across a curved interface.
⎛ ⎞⎜ ⎟⎝ ⎠
lg1 2
1 1Δ P = γ +R R
(3-26)
where γlg is the surface tension, R1 and R2 represent the two principle radii of curvature, and ΔP
is the pressure difference across the interface. In the absence of any other external forces
except gravity, it can be expressed as a linear function of elevation:
gzPP ρΔ+Δ=Δ 0 (3-27)
Where 0PΔ is the pressure difference at a reference plane and z is the vertical coordinate of the
drop measured from the reference plane. From the above two equations, it is evident that, if the
shape information of the drop is given, then surface tension determination would be possible.
On the other hand, if the surface tension is known, the shape of the drop could also be
determined. From Figure 3-2, the Young-Laplace equation can be expressed as a set of the
following first-order differential equations:
dx = cosφds
(3-28)
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dz = sinφds
(3-29)
dφ sinφ= 2 + z -ds x
χ (3-30)
χ, the shape parameter is defined as:
20 lg= ΔρgR /γχ (3-31)
where R0 is the radius of curvature at the origin of the (x, z) coordinate system and Δρ is the
density difference between the polymer-gas solution and gas phases. The overall method to
determine γlg is outlined as follows: 1) Obtain the (x, z) coordinates of the boundary profile of a
sessile drop in equilibrium with the blowing agent using the captured images from the PVT
visualization system; 2) Starting from an initial estimate of the γlg and the empirically derived
parameters, a sessile drop profile is also calculated from Equations (3-28) to (3-31) [261]; 3) This
theoretically determined sessile drop profile will be compared with the ones measured from the
images taken by the PVT visualization system. The former will be updated in an iterative
process until the best fit between the two is obtained; 4) From the updated sessile drop profile,
the surface tension value will be determined using the Young-Laplace equation. The detailed
numerical method can be found in Ref. [261]
Figure 3-2 Sessile Drop Coordinate System Definition
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3.6 Summary
The main purpose of this chapter is to build a strong and in-depth background on the
theories of the issues that will be used or addressed in this research. Starting from the
thermodynamic laws to describe single component or mixture systems, the postulates and
relations are briefly introduced to lay the ground work for deriving the thermodynamic
equations of state (EOS). Equations of state (EOS) are intensively used to describe and
determine the property of pure substances as well as mixtures. SS EOS and SL EOS are the ones
used in conjunction with MSB solubility measurement through providing predicted volume
swelling to compensate the buoyancy effect. Therefore, much more attention is paid to closely
looking at their mathematical formulations.
Following the EOS, the literature of PVT measurement for pure polymer and
polymer/gas mixtures is briefly iterated. The brief derivation of the Tait equation shows that the
Tait equation has a general format for different types of polymer materials and that it is the
coefficients that distinguish among polymers. The pros and cons of the methodologies used for
polymer/gas PVT measurement are depicted. The major drawback of those methods is their low
operating temperature where there is not polymer/gas single solution formation. In this research
the experimental temperature is usually above the melting point (Tm) of crystalline polymer,
such as PP or glassy transition temperature (Tg) of amorphous polymer, such as PS. A brief
introduction on the modeling of this unique viscoelasticity nature of polymer or polymer/gas
solution provides a foundation for the later study on the polymer chain entanglement effect on
the volume swelling. Lastly, usage of the drop shape method to measure the surface tension is
addressed mathematically so that it is easier to physically see the determining factor in surface
tension measurement.
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Chapter 4. Design and Construction of Novel Apparatus for PVT measurement
4.1 Conceptual Design of PVT Measurement Apparatus
4.1.1 Introduction
The familiar phrase, “problem solving is what engineers do” is quite true and
non-deniable, in that the essence of it explains that engineers need to use the right technique for
problem solving. Therefore, for our design problem, the well-known Axiomatic design method
is applied and used to generate feasible design solutions.
The Axiomatic design method was developed by Suh[262] at the Massachusetts Institute
of Technology (MIT) as a systematic framework for guiding engineering designs based on two
axioms. The design process itself is actually a mapping process from functional domain to
physical domain. The things that need to be achieved in the design are defined as function
requirements (FRs) and the corresponding parameters that could meet the function requirement
are defined as design parameters (DPs). Under the context of the FRs and DPs, design is also
defined as the creation of a synthesized solution to satisfy perceived needs through the mapping
process between the FRs and DPs. Figure 4-1 shows the general mapping relationship.
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…....
FRs
……
1
2
3
4
5
FRs
……
1
2
3
4
5
Mapping
Functional Space Physical Space
…....
FRs
……
1
2
3
4
5
FRs
……
1
2
3
4
5
Mapping
Functional Space Physical Space
Figure 4-1 Axiomatic Design Mapping Process from FRs to DPs
Many researchers have been using this method to successfully achieve their ultimate objectives
in their research.There are two axioms that govern a good design. The following lists the two
axioms
Axiom 1 The Independence Axiom
Maintain the independence of functional requirement Axiom 2 The Information Axiom
Minimize the information content Axiom 1 deals with the relationship between functions and physical variables, and
Axiom 2 deals with the complexity of the design. Once those FRs are defined and the DPs are
identified, the mapping process between the functional domain and the physical domain can be
represented by a design equation as
[ ] DPsAFRs = (4-1)
where FRs and DPs are vectors and [A] is the so-called design matrix. The elements of
the matrix represent the degree of coupling between iFR and jDP . If the coefficient of the
design matrix A is small or near zero, then the function requirement of FRs correspond to a
weak or independent magnitude relationship with DPs, which implies that the changes of that
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particular DP could not alter that FR or vice versa. If there is strong relationship between FRs
and DPs, the coefficient A is denoted by some non-zero value, mostly 1 or just a symbol. In
order to satisfy the independent axiom A, the design matrix A has to be a diagonal or triangular
matrix. A design with a diagonal matrix is an uncoupled design and with a triangular matrix it is
a decoupled design. Uncoupled or decoupled designs have a set of DPs that meet the specific
FRs and their relationship also meets the independence axiom. On the other hand, coupled
designs are not satisfactory because they fail to meet the requirement of Axiom 1 and needs to
be reconsidered in picking the right DPs.
In this research, the primary goal is to develop a new system that could measure the PVT
information for polymer/gas solutions at high temperatures and pressures; hence the axiomatic
design method was chosen to help create a conceptual design of the PVT measurement system.
4.1.2 Analysis of the PVT Apparatus for Polymer/Gas Solutions
Our proposed new method adopts the pendent/sessile drop technique and combines it
with a visualization system that allows for the tracking of the swelling of a polymer melt due to
gas dissolution over a wide range of elevated temperatures and pressures.
The overall design of the system consists of two major functional attributes: the software
attribute and the hardware attribute. The software attribute is the implementation of the function
modules that perform individual tasks as well as the integration of these modules. The
individual tasks are as follows: image capture, image reconstruction, and volume integration.
The hardware attribute is the actual physical components that are either delicately machined
components or are standard parts purchased off the shelf, to be able to realize the functions
required from the software attribute when integrated together. Such components comprise of a
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camera system, high temperature and pressure visualization chamber, light source, and image
processing terminal, etc. Figure 1 shows a schematic of the overall PVT system.
Image Processor
Temperature Controller
CCD Camera
Rotational Droplet Rod
High T and P Cell
High Pressure Supply
Gas Source
Backlighting
Vibration Free Table (VFT)
XY Precision Stage Motor
Figure 4-2 PVT System Schematic Those two major functional attributes are then integrated to construct the complete
apparatus. The software algorithm, such as the camera movement and image capture, etc. that
are the next level FRs within the software attribute, were developed and implemented in the
actual system to facilitate the functions such as stage movement and camera triggering for image
capturing, etc. through the apparatus.
4.1.3 Detailed Analysis and Decomposition of FRs and DPs
4.1.3.1 Hardware Attribute
As mentioned, hardware attributes are those experimental components that work only
when integrated with software functional modules. The process of defining the major functional
requirements (FRs) is explained in the following paragraphs.
Since the design adopts the concept of the pendent/sessile drop technique with
visualization, the apparatus must consist of a customized high-temperature and pressure
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visualization chamber, a charged couple device (CCD) camera, and a computer terminal
installed with the image grab card for the CCD camera. In order to be able to provide a high
temperature and pressure environment, the chamber system itself also needs to have electrical
heater(s), temperature control system, pressure supply system, as well as a light source with a
diffuser for the illumination of the CCD camera. In order to improve the accuracy of the
calculation of the image processing, an XY lead ballscrew stage with a nanometer resolution is
needed so that the camera can move to capture multiple images for the purpose of getting higher
resolution through image reconstruction. Also in order to eliminate most of the unexpected
external noise (vibration mainly), the whole system setup would need a vibration free table as a
base so that the system could enjoy a vibration free environment as much as possible during the
experiment. One additional defined function requirement is to have the system capable of
rotating the pendent/sessile droplet in any desired angle to study the effect of asymmetry drop
shape, as well as to obtain reliable results when the drop shape is not axisymmetric. This
rotation would allow a 360 revolution view of the polymer sample so that a complete profile can
be captured on camera to obtain more accurate volume information for some polymers, i.e.
polystreyene (PS) with higher melt strength and viscosity which can not form axisymetric
shapes as easily compared with others. As such, the solution to this requirement is to have a step
motor as one of the hardware components to provide the rotation.
Therefore, from the above description, the specific functional requirements (FRs) for
developing a comprehensive PVT measurement system that is able to achieve the ultimate
objectives can be summarized as follows:
FR1 = Visualization
FR2 = Image capture
FR3 = Multiple image capture
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FR4 = Sample rotation
FR5 = Vibration noise reduction
FR6 = Data storage/processing
Also with the brief descriptions from each FRs, in order to fulfill the above FRs, the
following design parameters (DPs) are proposed and summarized respectively:
DP1 = Steel chamber with sapphire window
DP2 = Charged Couple Device (CCD) camera
DP3 = Precision XY stage
DP4 = Step motor
DP5 = Vibration free table
DP6 = Computer terminal
With all FRs and DPs identified, the design equation for the hardware of the system can be
written in the following matrix:
⎥⎥⎥⎥⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢⎢⎢⎢⎢
⎣
⎡
⎥⎥⎥⎥⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢⎢⎢⎢⎢
⎣
⎡
=
⎥⎥⎥⎥⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢⎢⎢⎢⎢
⎣
⎡
6
5
4
3
2
1
666564636261
565554535251
464544434241
363534333231
262524232221
161514131211
6
5
4
3
2
1
DPDPDPDPDPDP
AAAAAA
AAAAAA
AAAAAA
AAAAAA
AAAAAA
AAAAAA
FRFRFRFRFRFR
(4-2)
The diagonal elements Aii of the design matrix can be noted using symbol "x", simply
because each jDP is chosen directly to accomplish the corresponding iFR . An examination of
all the non-diagonal elements of the matrix is required in order to determine the effects of each
jDP on the other iFR .
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The steel chamber with sapphire window only provides the visualization capability to the
system and will not affect other functional requirements, such as image capture, image rotation,
etc. Therefore the steel chamber with sapphire window has no relationship with other FRs and
the remaining coefficients other than A11 on that row are denoted as “0” based on the coefficient
definition of the design matrix. Similarly, the CCD camera would not affect other FRs except
the image capture; therefore all the coefficients, such as A21, A23, A24 and A25 in that row, except
A22, are all zeros.
The purpose of multiple image capture is to increase the resolution of the reconstructed
image from those captured ones. By increasing the resolution, the number of pixels would
increase and the pixel size would reduce which is beneficial for volume integration. This image
reconstruction concept will be elaborated more in a later section. In order to accomplish this task,
the camera needs to be mounted on a stage that has precision movement. Therefore this XY
stage with micrometer movement and nanometer error resolution would fulfill the requirement.
In addition, the capture of multiple images is also strongly associated with the CCD camera. If
the camera is not working, then this multiple image capture functional requirement would not be
realized even with a functional precision stage. Therefore the A32 and A33 should be non-zero.
Other than A32 and A33, all other coefficients terms should be zero since the XY stage does not
have a strong relationship with other FRs.
The sample rotation mechanism is used to capture the asymmetry of some highly viscous
polymers, such as PS, that cannot easily form nice axisymmetric dorm drop shapes at desired
temperatures. An ideal axisymmetric dorm drop shape would be the best for image analysis to
achieve the best accurate volume integration results. The step motor is used to couple with the
sample droplet so that the sample can rotate inside the chamber. It is clear to see that the use of a
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rotational motor is pretty much independent of other FRs. As a result, the coefficients other than
A33, should all be zeros.
Noise reduction and control is another key aspect of the system design, which helps to
eliminate any external factor that can affect the accuracy of experimental results. The
installation of a vibration free table would certainly help to damp out any external noise that
could propagate to the chamber system as well as keep the whole apparatus setup level. So the
coefficient A55 is definitely a non-zero and denoted as big X. The installation of the vibration
control device would not affect image storage and processing but does have some relationship
with other FRs. For instance, if the vibration is so severe and without the vibration free device,
those FRs, such as image capture, sample rotation, etc, could not be carried out properly. On the
other hand, the chance of having detrimental vibration noise is not likely, so the relationship of
the vibration free table with other FRs is there, but not strong and it is being recognized and
denoted using small x.
The last major function requirement is data storage and processing. This functional
requirement could be easily met by using a computer with sufficient storage space. For data
processing, the relevant tools or software required will be properly installed on the computer
terminal. It may appear as though the computer terminal will only serve as the storage and
processing station that has nothing to do with other FRs, but it indeed will affect the image
capture. Without the storage and processing ability, the captured images would have nowhere to
go and would not be able to be processed. In this case, the coefficients of A62, A66 should not be
zeros. Other coefficients on this row are then zeros. From the above detail analysis, the matrix
(4-2) can be reformatted as:
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⎥⎥⎥⎥⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢⎢⎢⎢⎢
⎣
⎡
⎥⎥⎥⎥⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢⎢⎢⎢⎢
⎣
⎡
=
⎥⎥⎥⎥⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢⎢⎢⎢⎢
⎣
⎡
6
5
4
3
2
1
6
5
4
3
2
1
0000000000000000000
DPDPDPDPDPDP
XXXXXXxxxx
XXXX
XXX
FRFRFRFRFRFR
(4-3)
Equation 4-3 is a lower triangular matrix, which implies that the functional requirements
can be achieved if the design parameters are implemented in the proper sequence. . Furthermore,
the design in this parental level is an uncoupled design. The first Axiom is satisfied by having a
decoupled or uncoupled design.
In order to meet the requirement of Axiom 2, it is necessary to decompose these FRs and
DPs to lower level hierarchies to try to minimize the design information.
4.1.3.2 Future Decomposition of FR1 and DP1 (Second Level)
As stated in the previous section, in order to minimize the design information of the
parent level, it is sometimes good practice to future decompose some FRs and DPs into sub
levels. In this case, one more level of decomposition of FR1 and DP2 would need to be added
because there are more functional requirements identified on the visualization chamber system.
In another words, there are more design details that need to be added onto the visualization
chamber to achieve other types of functional requirements. In addition, the corresponding DPs
are also required in response to those second-level FRs from the chamber system. The following
sections depict the detailed analysis of the decomposition and formulation of the second level
design matrix.
Firstly, the chamber body needs to be maintained at a high temperature and pressure
reservoir. Therefore, a heating device and pressure supply equipment need to be attached to the
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chamber. Secondly, due to the introduction of high pressure gas inside the chamber, a proper
sealing solution is required at the visualization window, as well as at the connecting surface of
the chamber with other component(s) while maintaining a high pressure level. In summary,
those additional functional requirements for the chamber would be identified as:
FR11 = High temperature
FR12 = High pressure
FR13 = Sealing at high temperature and pressure
In response to the second-level FR11, the electric heaters and temperature controller
system are needed. The heaters are inserted into the grooves that are machined out of the
chamber body. Those heaters are connected to a temperature controller, which can actively
control and maintain the set temperature of the chamber system using PID control. In response
to the high pressure functional requirement FR12, the gas injection and release port are needed
so that the chamber can be pressurized by allowing high pressure gases to be injected. Last,
since the pressurized chamber could have leakage at some of the openings, such as the place the
sapphire windows are housed, proper high temperature and pressure seals and seal groove are
required to be used. In summary, those additional design parameters DPs are listed as below:
DP11 = Electric heater and temperature control system
DP12 = High pressure supply unit
DP13 = High temperature and pressure seal
The design equation then can be represented as:
⎥⎥⎥
⎦
⎤
⎢⎢⎢
⎣
⎡
⎥⎥⎥
⎦
⎤
⎢⎢⎢
⎣
⎡
=⎥⎥⎥
⎦
⎤
⎢⎢⎢
⎣
⎡
13
12
11
333231
232221
131211
13
12
11
DPDPDP
AAA
AAA
AAA
FRFRFR
(4-4)
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Together with the temperature controller, the electric heaters that are inserted into the
groves into the chamber body would provide the heat capacity to ensure the chamber
temperature is maintained at desired levels. The pressure supply unit through the gas injection
port into the chamber would provide pressurized gas into the chamber cavity. Those two
functional requirements are independent of each other; in that neither one could have an affect
on each other. Therefore, A12, A13 and A21 are zeros. The rest of the coefficients of the first two
rows are non-zeros. If the seal happens to be defected or worn out after being used for many
experiments, then the high pressure gas supply alone would not have the chamber maintained at
high pressure. Hence A23 is not zero. On the other hand, the choice of high temperature and
pressure seal would always be providing proper seal and heat resistance no matter if the heat or
the gas supply is working or not. Therefore A31 and A32 are zeros and A33 is non-zero.
The equation (4-4) could then be rewritten as:
⎥⎥⎥
⎦
⎤
⎢⎢⎢
⎣
⎡
⎥⎥⎥
⎦
⎤
⎢⎢⎢
⎣
⎡=
⎥⎥⎥
⎦
⎤
⎢⎢⎢
⎣
⎡
13
12
11
13
12
11
000
00
DPDPDP
XXX
X
FRFRFR
(4-5)
The newly rewritten matrix equation (4-5) proves to be an upper triangular matrix. It
implies that the second level design is also a decoupled design with all the design elements
added onto the body chamber. Each of the functional requirements could be achieved without
interfering with the others. In conclusion, this is a sound design solution.
With those proposed decoupled designs, the big picture for constructing the hardware
part of the apparatus is now becoming clear. The CCD camera, with its optical lens that is
synchronized with the computer image-processing terminal, is mounted on a high-resolution XY
stage driven by a precision step motor providing precise x and y directional movements. The
visualization chamber, where the pendent/sessile droplet sample is housed, is located between
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the light source and the CCD optical lens. The chamber is maintained at user-defined
temperatures and pressures through precision PID temperature controls and syringe pump
pressure controls. Another step motor (stepper) coupled with the pendent or sessile droplet
would rotate the sample if required to capture the asymmetry drop shape of high viscous
polymer/gas solution and to obtain more accurate results. The diffuser attached to the light
removes the noise from the light, making it more uniform when it shines on the pendent or
sessile drop, and the vibration free table damps out the external vibration noise so that the
system that sits on it and would not be affected. A similar approach is taken to finish the
design process for the software part of the PVT apparatus in the following sections.
4.1.3.3 Software Attribute
Having chosen the Axiomatic design technique to successfully finish the hardware
component design, the same design concepts and logic could be used in the design of the
software of the system. The design of software is easier compared with hardware design and it is
mostly involved with algorithm designs in order to achieve certain functionality. The
implementation of the algorithm is going to be addressed in a later section.
In the PVT measurement system, the image of the pendent or sessile drops is first
captured and saved. The most important step during the image analysis is the acquisition and
determination of the drop boundary based on the pixel intensity values of the greyscale image.
Normally, the image contains the image data in the form of digital picture element or pixels. The
value of each pixel is called the intensity or grey level (in the black-and-white case). There are
256 grey levels to represent an image, with 0 representing black and 255 representing white.
The intensities of pixels at the boundary layers gradually vary and fade out into the
neighbouring black or white background (in our case, the sessile drop is a black or white
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background (in our case, the sessile drop is black object and the background is white). The
errors in image processing are mostly involved in the assessment of the exact boundary
determination. Either using the high precision/resolution CCD camera or enlarging the drop by
an optical system will reduce the pixel size and increase the number of pixel points, which in
turn reduces the relative errors involved in the boundary determination.
Thus, instead of acquiring a small, single image, it is proposed to take multiple images
for PVT measurements. This is the FR3 in the hardware attribute section. The detaied procedure
is: the sessile or pendant droplet sample is first magnified at the maximum magnification of the
CCD camera; then, sequential images are taken locally along the drop boundary to cover the
whole drop. Therefore, these captured individual images need to be reconstructed into one
single image during post-image analysis. The drop profile of the reconstructed images is
required to be identified as boundary coordinates of the pixel unit. Then, based on those pixel
coordinates, numerical integration algorithm is needed to compute the volume based on the drop
profile. Lastly, the calibration for converting the pixel unit into metric length is required so that
the pixel volume information can be represented in terms of the metric dimension. Hence, the
functional requirements FRs for the software development are:
FR1 = Image reconstruction
FR2 = Image profile recognition
FR3 = Volume integration
FR4 = Volume conversion
In response to the first FR1, an image stitching software or a simple algorithm could be
utilized for reconstructing those individual images into one image. For image profile recognition,
the precise subpixel edge detection algorithm is then employed to identify the edge boundary
coordinates in terms of the pixel unit. The Canny edge detector is used and it is proven to be the
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best subpixel edge detector.[56,263-267] Polynomial curve fitting and Simpson’s integration
techniques are used to develop the algorithms to compute the polymer-gas drop volume. Finally
a calibration procedure performed before the experiment would be able to obtain the conversion
factor between the pixel and metric unit. Therefore, the design parameters (DPs) to satisfy the
FRs can be chosen as follows:
DP1 = Image stitching algorithm
DP2 = Edge detection algorithm
DP3 = Numerical integration algorithm
DP4 = Calibration technique
The design equation can be represented in the following matrix:
⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢
⎣
⎡
⎥⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢⎢
⎣
⎡
=
⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢
⎣
⎡
4
3
2
1
44434241
34333231
24232221
14131211
4
3
2
1
DPDPDPDP
AAAA
AAAA
AAAA
AAAA
FRFRFRFR
(4-6)
Since the calibration process is commenced usually before the experiment, it is desired
to switch their FR4 and DP4 to the front to be FR1 and DP1. The sequence of other FRs and
DPs remained. After the swap, the calibration DP1 is then independent of all other FRs. Hence
the coefficient of the first row should be all zeros, except A11. The edge detection algorithm
(DP3) can not be finished unless the image reconstruction (DP2) is carried out successfully. The
edge detection and image reconstruction has no relationship with the calibration (DP1),
therefore the coefficients in the middle two rows are all zeros except A22, A32 and A33. For the last
DP4, the numerical integration for volume would not be possible until all of the above are
realized. Hence, it strongly depends on the successful completion of all the others functional
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requirements and that its coefficients are all non-zeros. A perfect lower triangular matrix is
generated from the software design and it is written as below:
⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢
⎣
⎡
⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢
⎣
⎡
=
⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢
⎣
⎡
4
3
2
1
4
3
2
1
000000
DPDPDPDP
XXXXXXX
XXX
FRFRFRFR
(4-7)
This low triangular matrix again illustrates that the proposed design for the software
construction is a perfect design with the right sequence of order as shown in 4-6 and 4-7. The
sequence of the design parameter is the actual experimental sequence or step in post-image
processing, so it makes more sense now to explain why it is a perfect design with triangular
matrix. For instance, the image profile detection can not be done until the images are captured
and reconstructed. Similarly, only after the profile of the images is detected and being
represented in terms of pixel coordinates, can the use of the integration technique that calculates
the drop volume that is based on the pixel boundary profile, actually proceed.
4.2 Detailed Design and Construction of the PVT Apparatus
4.2.1 Overview of the Apparatus
Based on the conceptual design of the PVT measurement apparatus, the design of the
detailed system components is carried out in this section. The overall system consists of four
major components: 1) high temperature and pressure visualization chamber, 2) CCD camera, 3)
precision XY stage, 4) rotational device and 5) light source.
The high temperature and pressure chamber is the actual housing where the sample is
placed. Since there is no off-the-shelf equipment available, the high temperature and pressure
chamber has to be designed from scratch and each of its components are machined from the
departmental machine shop with precision.
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The high-pressurized gas (blowing agent) is injected into the chamber to maintain the
desired pressure level. This requires the use of high pressure syringe pump that could pump the
gas into high pressure levels before delivering into the high temperature and pressure chamber.
The electrical cartridge heaters and temperature controller are chosen for the chamber to elevate
and maintain the desired chamber temperature.
The CCD camera provides high-resolution image capturing capability for taking the
sessile drop of polymer/gas solution pictures at high temperatures and pressures. From those
captured images, we are able to use image-processing tools to track the volume changing
information at the equilibrium state of the polymer/gas solution.
The precision XY stage is to facilitate the move of the camera to take multiple images
for reconstruction. The camera is carefully mounted on the stage and the stage is controlled
through the control software via sending the pulse signal to the step motors to control and
implement the X and Y direction movement. The rotation device gives the system the ability to
accommodate some polymer/gas with an asymmetrical drop shape.
The light source provides the necessary illumination into the chamber cell so that the
camera could capture the image. The light source needs to be uniform and stable to get rid of
any possible noise, therefore, a lighting system with uniformity and stability control is chosen
for the system construction.
4.2.2 High Pressure and Temperature Visualization Chamber
The high pressure and temperature visualisation chamber is the major component of the
PVT apparatus. It is the place where the sessile drop sample is housed. The design of the
chamber system is complex and delicate. Many functions need to be realized in this small
chamber while maintaining a high degree of freedom for easy operation. The detail functional
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requirement and corresponding design parameters have already been depicted in the previous
section. Firstly, the chamber needs to have a visualization window so that the light can go
through and at the same time the camera can take images. Secondly, the chamber needs to be
designed so that there is gas injection and an exit channel so that the high pressure gas can be
injected to maintain high chamber pressure, as well as for releasing the high pressure gas upon
completion of the experiment.
In addition to the gas injection and release, the thickness of the chamber would also be
considered as a key factor as the safety concerns when handling with high pressure gas, the
safety factor of 6 is chosen to make sure the chamber material itself, plus its fasten bolts, would
be able to bear such high pressures of up to 6000psi pressure load. Thirdly, the chamber should
have a place to insert the cartridge electrical heaters so that the system can be heated up to the
desired temperature. How to have proper seal when dealing with high pressure gas is always the
important issue when designing and making the system. Any leakage (bigger than 0.001ml)
from the system while running experiment is unacceptable. Therefore it is critical to choose the
proper seal for the chamber. The place needs to be sealed are the visualization window opening,
the place where the rotational motor shaft goes through as well as at the junction place where
the chamber meets other parts. Costume made rotary seal is used for the rotational motor shaft.
Moreover, there should be a house for locating the rotational motor right underneath the
chamber so that the motor shaft can be perfectly aligned and coupled with the sessile droplet.
Lastly, there need to have a cooling system using either water or air that can be attached
to the system to cool the sections where the rotary seal and two bearings are located as shown in
Figure 4-3. This is to prevent the build up of the local heat conducted from the chamber body so
that the durability and performance of the seal and bearing can be maintained over a long
duration of time. Figure 4-3 shows the CAD assembled chamber on the left, and on the right is
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the cross-sectional view of the whole chamber system to give a big picture of where all the
added detail designs are located in the chamber.
Visualization Chamber
Rotary Seal
Shaft Bearing Cushion
Base Support
Rotating Motor
Shaft Bearing House
Visualization Chamber
Rotary Seal
Shaft Bearing Cushion
Base Support
Rotating Motor
Shaft Bearing House
Figure 4-3 CAD Model of Chamber Body with Rotational Device
Figure 4-4 shows more features of the chamber parts with the sapphire window, such as the
window seal groove, cartridge heater holes, cap screw holes, etc. The four evenly distributed
heaters would ensure the thermal uniformity of the chamber body so to keep stable drop profile.
34 5
6
1: Cap screw holes 2: Cartridge heater holes 3: Sapphire window
4: Thread fitting 5: Chamber Space 6: Static Seal
1
2
34 5
6
34 5
6
1: Cap screw holes 2: Cartridge heater holes 3: Sapphire window
4: Thread fitting 5: Chamber Space 6: Static Seal
1
2
Figure 4-4 CAD Model of the High T and P Visualization Chamber
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4.2.3 Charged Couple Device (CCD) Camera and Optical Lens
The camera is a vital component of the PVT apparatus. There would not be any
information captured for the purpose of image processing if the camera were not available.
Picking a high resolution camera would ensure the good quality of the images captured. The
Pulnix TM-4100CL monochrome progressive scan CCD camera with dual-tap output and a
frame rate of 15 fps at full 2048x2048 resolution is used for the purpose of image acquisition.
The TM-4100CL camera features the latest Kodak KAI-4021 CCD imager for the best image
quality and sensitivity. This camera is used in many different applications, ranging from
machine vision, intelligent transportation systems to high-definition graphics, etc.
The CCD camera provides an analog video signal that is digitized by a frame grabber
installed in a host computer. The digitized image contains the image data in the form of digital
picture elements or pixels. The value of each pixel is called the intensity or grey level (in the
black-and-white case). The most commonly used equipment utilizes 640 x 480 pixels and 256
grey levels to represent an image where 0 and 255 represent black and white, respectively. Thus,
a digitized image is mathematically represented by an array of real numbers from 0 to 255.
In order to receive a magnified image, a set of lenses is chosen to be assembled with the
CCD camera to form the complete imaging acquisition system. This set of macro lens system
from Schneider comprises of an Apo-Componon 8/40 optical lens, a Unifoc 12 helical mount, a
50 mm extension tube and a C-Mount camera adaptor. When the aperture of the lens and the
focal length are adjusted each time, the magnification of the image is changed as well. Having
the biggest magnification is theoretically sound for our purpose, but the image quality is also
very important. Therefore, before the experiment, the aperture of the lens and the light intensity
are adjusted so that the best quality of image and at the same time, the maximum magnification,
can be attained.
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4.2.4 XY Stage and Precision Control
An XYRB™ crossed roller table from the Danaher Motion Company is used as the
precision XY stage to facilitate the CCD camera movement. The crossed roller stage is a low
profile stage designed for a wide range of applications. Common uses include factory
automation, microelectronics assembly, and laser machining. The stage uses 3mm crossed roller
ways and provides high stiffness. Precision ground preloaded ball screws allow for a higher
speed than a lead-screw driven stage. A specialized monolithic center couples the upper and
lower axes, making them stage stiff and compact. Both motors are mounted at the center section,
so that they move with the lower axis. The two precision step motors provide two axial
freedoms, X and Y, respectively. The total linear travel span of the motor stage in X and Y
direction is 2 inches. The step motor has 400 steps per revolution with 8 micrometer position
accuracy for its encoder. The total load capacity is 75 Kg, which is rigid enough to carry the
weight of the CCD camera without significantly affecting its performance. The stage supports 3
axes controls and high accuracy of positioning control. The controller and amplifier are
provided from the manufacturer. The amplifier provides the power to the motor stage. The
controller could control three axes: X, Y and Z. The first two are used for the XY stage stepper
and the last one, the Z, is used for controlling the step motor coupled with the sessile droplet for
rotational purposes. PID control is utilized to achieve accurate motor positioning control with
minimal amount of error due to repetitive movements.
4.2.5 Rotational Device It has been assumed that the shape for some polymer/gas sessile drops is axisymmetrical or
has axisymmetry, which means the profile of the drop is axisymmetrical in one revolution. In
other words, it is assumed that the PP/gas sessile drop would form a near-perfect parabolic or
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dorm shape that would give us the best drop profile for performing the volume integration. This
assumption holds since PP has low melt strength and viscosity when it is at a temperature well
above its melting point. In addition, the plasticization effect of dissolved gas at high
temperatures would future reduce its melt viscosity and help the polymer melt to flow easier.
But this assumption does not hold for all polymers. For amorphous polymers like polystyrene
(PS), it has high melt strength and viscosity and it does not have melting point Tm, instead, it has
the so-called glassy transition temperature Tg. The PS polymer matrix behaves like rubber and
the melt strength remains relatively high at higher temperatures. The processing temperature for
PS is usually around 200oC, which posts the problem for PVT experimental studies of the
PS/gas melt at relatively low temperature with its non-symmetric drop shape using the same
technique for PP material. Therefore, the motive for creating the rotational device is to be able
to capture and study the degree of asymmetry and its effect on the PVT measurement with
respect to the temperature and pressure.
The purpose of the rotation device is to capture the asymmetry of the sessile drop shape
for polymers with higher melt strength, such as PS used in this study. In addition, the rotational
device would also help to compensate the effect of asymmetric drop shape on the PVT
measurement via capturing the drop profiles at different angels. The rotational device comprises
of a step motor, an amplifier, a power supply, two ball bearings, and a coupling device. The
coupling device is used to connect the motor shaft with the sessile droplet so that when the
motor rotates, the sessile droplet could also rotate simultaneously at the same pace as the motor.
Therefore, through carefully programmed motor move steps, the precise rotational angle could
be realized on the sample droplet. The ball bearing is housed as shown in figure 4-6 at the two
far ends of the motor shaft to keep it aligned while rotating. The stepper has 500 steps per
revolution, which means that 500 pulses are sent to the motor to trigger the 1 revolution (360o)
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rotation of the motor shaft. The motor is connected to the XY stage controller as its third axis.
The desired rotational angle is set in the GUI program when the rotation is needed. The rotation
angle is usually as an integer number, such as 5 or 18 degrees.
Another key feature involved with the rotation device is the rotary seal. As seen from the
following figure, the motor shaft is coupled with the sessile droplet inside the chamber and
without a proper seal the gas could leak through the shaft and the pressure would not be
maintained inside the chamber. The solution to this problem is the use of the high temperature
and pressure rotary seal custom designed and produced for this particular application from
Trelleborg Seal Inc. The rotary seal is made out of special Teflon Perfluoro Rubber (FFKM)
material that can handle temperatures of up to 260oC and 5000psi pressure. The rotational
device including the motor and the location of the rotary seal is shown in the section view of the
following Figure 4-5. The sessile droplet where the polymer sample pellet sits on top is also
shown in this figure. This figure also provides a clear picture of where the sessile drop locates in
the chamber during the real experimental environment.
Rotational Device
High T and P Rotary Seal
High T and P Rotary Seal
Rotational Device
High T and P Rotary Seal
Ball Bearings
Coupling Device
Sessile Droplet
Rotational Device
High T and P Rotary Seal
High T and P Rotary Seal
Rotational Device
High T and P Rotary Seal
Ball Bearings
Coupling Device
Sessile Droplet
Figure 4-5 Location of Rotational Device and High T and P Rotary Seal
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4.2.6 Image Processing Terminal
Computers have become one of the most important parts of people’s daily lives and even
more so for those in academia. Computers are used to serve as image storage and processing
terminals in our PVT system. The images captured from the experimental are stored in the
computer memory. The image processing software, such as the edge detector and image
stitching tool are installed. The developed volume integration algorithm and some other
necessity that was needed in the post image processing are all installed on the computer terminal.
Without this powerful computer device, the time-consuming calculations of dealing with large
amounts of images and pixel points would not even be possible.
4.2.7 Light Source, Noise and Vibration Control
Light source is used to provide illumination to the CCD camera so that the image can be
captured. A white light source composed of a wide range of wavelengths, white light forms
chromatic effects such as rainbow and chromatic aberration that can cause blurring and loss of
clearness of the image of the drop at the edge[268,269]. These chromatic effects can be reduced
using light with a narrow range of wavelengths. Therefore, a band-pass filter (i.e., a filter that
transmits wavelengths between the two cut-off wavelengths of the filter) can be used to pass
only a narrow band of the visible wavelengths. The choice of an optical filter involves a trade
off between the intensity and the bandwidth of light. In other words, the wider the bandwidth,
the higher the light intensity. An appropriate filter is expected to reduce the effects of both
chromatic aberration and the rainbow effect, while maintaining sufficient intensity for the
illumination.
The results from surface tension measurements[180] show that the use of any optical filter
(red, green, or blue) reduces the discrepancy between the surface tension values obtained for
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large and small drops. This may be explained by the fact that filters reduce the chromatic effects
caused by white light, so they improve the quality of the image. In other words, chromatic
effects make the image of the drop blurry at the interface (i.e. the edge). Thus, the edge of the
image deviates from the real physical edge; hence, the error increases. The results indicate that
the use of the blue filter (with a wavelength range of 400-500 nm) reduces the discrepancy
between the surface tension values obtained for large and small drops more than the other filters
examined. Thus, the blue filter is used in this research. In addition to the blue filter, a light
source from SCHOTT with uniformity and intensity control was purchased to be used as the
system light source to achieve the best image quality. The controller of the light source could
not only vary the intensity of the light but could also to control the uniformity of the light shone
on the sample.
For the purpose of eliminating any possible external mechanical noise, a vibration free
table is used as the base for the whole experimental setup. The table is supported by air at a
constant pressure level. In other words, the table is acting as a damping system so that any
vibration noise caused by external sources reaching the table would be damped out from the
air-floating table. Therefore the effect of the vibration on the PVT system sitting on the table
would be minimized. Another important usage of this vibration free table is to keep the whole
PVT apparatus levelled through its adjustable air cushions. The following Figure 4-6 shows a
real picture of the constructed PVT apparatus based on the proposed design methodology. The
detail components mentioned before such as the CCD camera, the lens, the blue filter, the water
cooling and the vibration free table, etc. are all shown in this figure.
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8
12
3
4
5
6
7
119
10
Figure 4-6 Actual PVT Apparatus Setup
The high temperature and pressure chamber(4), water cooling system (6) and rotational
device (5) are sat on a millimetre resolution rail at the centre of the vibration free table (3). The
CCD camera (2) and the XY stage (1) are in line with the chamber to the right; The polarizer
diffuser (10), blue filter (9) and light source (8) are in line with the chamber to the left.
4.3 Theory Background and Algorithms Construction
The overall methodology and experimental procedure are elucidated in two different
flow charts. The first flow chart in Figure 4-7 shows the case of dealing with the axisymmetry
drop shape and the second flow chart in Figure 4-12 is used for the asymmetry drop shape case.
The second flow chart is illustrated in a later section. However, for the time being, it is assumed
that the polymer pendent/sessile drop is axisymmetric, which means that the droplet profile is
axisymmetric with respect to its vertical centerline. At the beginning of each experiment, the
camera parameters, such as the working distance relative to the drop sample, the image contrast
1 XY Precision stage 2 CCD camera 3 Vibration free table 4 Visualization chamber 5 Rotational motor 6 Water cooling 7 Syringe pump 8 Pressure transducer 9 Blue filter 10 Polarizer diffuser
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through optical lens, and so on, are adjusted for maximum zoom while ensuring the best image
quality at the boundary. Calibration is then carried out to determine the pixel size in x and y
orientation, with respect to the XY stage movement. The calibration determines the size of the
pixel in terms of the metric length based on the movement of the stage since the unit step length
of the stage is known. This is a crucial step since it not only helps to correct some possible
optical distortions but also provides the conversion factor between the image pixel size and the
real drop’s metric dimension for volume integration.
Axialsymmetry
Drop shape
Image Recon. &
Edge Detection
Volume Swelling &
PVT Determination
Ultimate Result
Axialsymmetry
Drop shape
Image Recon. &
Edge Detection
Volume Swelling &
PVT Determination
Ultimate Result
Figure 4-7 Methodology Flowchart for Axisymmetry Drop
The number of images to cover the whole pendant/sessile drop is calculated based on the
magnification of the optical system and the resolution of the CCD camera. For a given number,
the step-wise movements of the XY stage in both x and y directions are determined. Those x and
y increments are programmed and stored into the motion controller to guide the step motor to
move the XY stage and camera with precision. The images are captured when the camera pauses
briefly in between each new x and y movement. The series of images are then combined and
reconstructed to form a complete drop image based on the movements using the image
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processing tool. Figure 4-8 show an illustrative schematic of the image reconstruction using
pendent drop as an example. The algorithm for image reconstruction is shown in the Appendix1.
Figure 4-8 Image Reconstruction Schematic
4.3.1 Edge Detection and Volume Integration for Axisymmetric Drop Shape
After the image reconstruction is completed, the precise edge detection algorithm is used
to detect the drop boundary and generate the edge pixel coordinates. The Canny edge detector is
used to extract the boundary pixel information into coordinates. There are many other edge
detection algorithms available besides the Canny edge detector, such as the Sobel edge detection.
However, Canny’s edge detector is the best-known subpixel edge detector even for poor quality
images. The Canny edge detector defines the detection and localization criteria of a class of
edges based on the first derivative. The detected edge information is in the form of coordinates
based on the sessile drop boundary pixel information. The output of such an operator will have
high magnitudes at the pixels where the gray levels change rapidly, i.e., at the edge of the drop.
After this stage, the edge is a discrete curve in which the minimum distance between the two
adjacent points is equal to the size of a pixel. To achieve higher precision, the edge is
smoothened using a cubic spline technique to provide subpixel resolution. The boundary points
can be represented as (xi,xj) and a simple f(x) notation can be used to represent the drop profile
after spline fit through all the points.
Monitor Virtual
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21
.
.
.
.
.
.
.
NN-1N-2
Sessile Drop
Boundary
2N-1, 2N . . . . . . . . . . . . . . .0,1,2
xj
xi
)( ixf
21
.
.
.
.
.
.
.
NN-1N-2
Sessile Drop
Boundary
2N-1, 2N . . . . . . . . . . . . . . .0,1,2
xj
xi
)( ixf
Figure 4-9 Detected Sessile Drop Edge and Volume Integration over Vertical Span
Among the numerical integration methods, composite Simpson’s 1/3 method which has
superior and finer segments, is selected[270] to compute the final volume of the pure polymer or
polymer-gas solution drop. Simpson's rule is a Newton-Cotes formula for approximating the
integral of a function using quadratic polynomials (i.e., parabolic arcs instead of the straight line
segments used in the trapezoidal rule). Simpson's rule can be derived by integrating a third-order
Lagrange interpolating polynomial fit to the function at three equally spaced points. Compared
with differential geometry approach dealing with Euclidean space, working with numerical
integration in Cartesian coordinate is more straightforward and conventional in this study.
General Simpson’s 1/3 rule has the following form:
( ) ( ) ( ) ( )∫ ∑∑ ⎥⎦
⎤⎢⎣
⎡+++==
−
=
−
=
b
a n
n
jj
n
ii xfxfxfxfhdxxfI
2
6,4,2
1
5,3,10 )(*4*4**
31
(4-8)
where ( )
nxx
nabh n )( 1−
=−
=
For the volume integration of the axisymmetric drop shape, Simpson’s rule is used to
compute the volume of the drop as the volume summation of every small frustum of a cone at
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infinitesimal small height along the splined drop profile shown in Figure 4-9. Since the drop
shape is axisymmetric, the radius at any layer ii is equal respect to its centerline in side and top
views as schematically shown in Figure 4-10.
riR −liR −
riR −liR −( )iRfi
riR −liR −
riR −liR −( )iRfi
Figure 4-10 Axisymmetric Drop Side and Top View Schematic
Figure 4-11 schematically illustrate how the volume is computed at any given level i
along the drop profile.
iR
1+iRhΔ
( )iRf i
iR
1+iRhΔ
( )iRf
iR
1+iRhΔ
( )iRf i
Figure 4-11 Volume Determination at ith Level of Axisymmetric Drop Shape
The unit volume shown in the above Figure 4-10 is determined as:
( )211
2 ****31
++ ++Δ= iiiii RRRRhV π (4-9)
where ( ) ( )[ ]ii RfRfh −=Δ +1
With the summation of all the unit volume along the spline drop profile, the total volume
is expressed as:
( ) hRRRRdhhAVlayer
layer
N
iiiiiNtotal Δ++== ∑∫
=++∞→
***31lim)(
1
211
2π (4-10)
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where ( ) ( )[ ]ii RfRfh −=Δ +1
If the notations from Figure 4-9 are used, an alternative expression based on equation
4-10 can be used as follow for the total drop volume:
( )∑∑∫=
++=
∞→++Δ==
N
jjijijiji
N
iN
total RRRRhdhhAV1
21,1,,
2,
1
***31lim)( π (4-11)
where
( )( )
( ) Nxfxfh
xxR
xxR
N
jijiNji
jijiNji
/)()(
2/
2/
1
1,1,121,
,,12,
−=Δ
−=
−=
++−++
−+
The i= 1,2,……2N and j = 1, 2, ….N. 2N is the total number of the pixel points. The
algorithm is also attached in Appendix 1.
The volume swelling ratio in this study was defined by comparing the final equilibrium volume
with the initial volume as follows:
( )( )
( )PPsample
tPT
tPT
tPTw m
V
V
VS eq
ini
eq
υ*,,
,,
,,== (4-12)
where V(T,P teq) is the measured equilibrium polymer/gas solution volume at temperature T,
pressure P, and equilibrium time teq. V(T,P,tini) is the volume of the neat PP sample at temperature
T, pressure P. PPυ is the specific volume of the pure polymer sample which can be calculated
using Tait equation (5-1), (5-2) and (5-3) in Chapter 5. Unlike the generalized Tait equation
(3-18), those Tait equations are derived specifically for the polymer resins used in this research.
4.3.2 Algorithms for 3D Volumetric Calculation of Asymmetric Drop Shape
In the case of asymmetric sessile drop, the rotational device is utilized to compensate the
effect of the asymmetric drop shape on the final volume integration through rotating the sessile
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drop at small angle. The degree of asymmetry of each drop is defined and analyzed for each
experiment. The volume integration of the asymmetric drop shape is slightly different than the
aforementioned axisymmetric scenario in how to obtain the cross sectional area of the drop in
radial direction. The detail algorithm development of defining the degree of asymmetry as well
as the volume integration is elucidated in the following sections and the algorithm is included in
Appendix 1.
4.3.3.1 Rotation Device and Degree of Asymmetry
The purpose of having the rotational device as part of the PVT system has been
emphasized previously. It is one of the key design features that allows the PVT system to not
only capture the asymmetry drop shape of polymer/gas with high viscosity and melt strength,
but also to compensate the effect of the asymmetry drop shape in volume determination. The
details of establishing the definition of degree of asymmetry and the development of the
mathematical algorithm are described in the following sections. As mentioned earlier, the
methodology is slightly different in dealing with asymmetric drops. Figure 4-12 shows the
methodology flowchart for an asymmetry drop shape case.
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Asymmetry
Drop shape
Rotational Device
Determine Degree of Asymmetry
Rotation Done?
Volume Swelling &
PVT Determination
Asymmetry
Drop shape
Rotational Device
Determine Degree of Asymmetry
Rotation Done?
Volume Swelling &
PVT Determination
Figure 4-12 Methodology Flowchart for Asymmetry Drop
4.3.3.2 Modeling of Degree of Asymmetry: Radial Asymmetry
It is, then, very important to be able to define a term that could describe degree of
asymmetry or the skewness for the study. The approach for defining the degree of asymmetry is
radial asymmetry of the sessile drop with respect to a reference radius.
The concept of using the radius to define the degree of asymmetry is to directly
determine how the radius of any asymmetric drop shape differs from the reference radius. The
reference radius is assumed to be axisymmetric or near axisymmetric and it is picked where the
shape of the polymer sessile drop is approximately at near symmetry. The polymer used in
particular is the PS. The experiments to determine the effect of an asymmetry drop shape are
carried out at various temperatures in vacuum conditions. The vacuum conditions would allow
for the study of the effect of asymmetry of the drop shape on the pure polymer PVT
measurement, but would also allow for the study of the temperature effect on the asymmetry.
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During the actual experiment, the radius of the PS sessile drop at the 250oC, the 200oC
and the 150oC during the temperature cooling round are chosen to be the reference points. It is
believed that at those temperatures during the cooling the PS drop has better shape because as
the temperature reached 250oC, the PS polymer chain should have already been relaxed and the
shape should have become much more axisymmetric compared with the same temperatures
during the initial heating process. Therefore, the temperatures in the cooling process are the
temperatures that will maintain better axisymmetric shape and will be used as the reference
temperatures. This is the direct method that characterizes the differences in radius in order to
quantitatively define the degree of asymmetry. The detailed mathematical modeling is described
in the following sections.
4.3.3.3 Determination of the Reference Radius
The experimental temperatures are carefully planned and set to help conduct the
experiment. For instance, 150oC, 200oC and 250oC are the three temperatures that are needed to
be used in the experiment. At the start of the experiment, the temperature is raised (temperature
increasing ramp) from 150oC to 200oC and finally to 250oC. About 15 to 20 minutes is allocated
at each temperature to ensure equilibrium state is reached. The temperature is then decreased
(temperature decreasing ramp) in a reverse fashion from 250oC to 200oC and 150oC at the end.
The time maintained at each temperature during the cooling round is the same as the
temperature rising. Since high temperature helps get more axisymmetric drop shape, it is
believed that the drop shape at the temperature during the cooling round is much closer to the
ideal symmetry. Therefore the radii of the drop along the drop profile at the temperatures in the
increasing ramp are used as the reference radius. TGA test (Appendix 7) is carried out to make
sure the PS sample is not degraded or decomposed at 250oC
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Since the drop is also rotated at different angles, the average radius value obtained from
the radii at those different angles at the same level on the drop profile is defined and used as the
overall reference radius of the drop for that temperature.
Figure 4-12 shows a schematic of how the reference radius is picked at each angle for
asymmetry drops. The left is the side view of a drop and the right is the top view of a drop at
angle 0θ . At each rotation angle, the profile of the sessile drop is determined through a subpixel
edge detector and the edge information is stored in pixel coordinates. Along the drop profile at
angle 0θ , the radius is defined as
( ) 2/000 ,,1, θθθ jjNj xxr −= +− (4-13)
The same mathematical is repeated for the drop profile at other rotated angles, such as 1θ . Then
those radii at each of the same levels but at different angles, are summed and averaged as the
average reference radius for that drop profile at that particular level.
0,1 θ+− jNx0,θjx 0,θjr
1θ
0θ
1−Mθ0
0,1 θ+− jNx0,θjx 0,θjr
1θ
0θ
1−Mθ0
Figure 4-13 Schematic of Reference Radius Definition As shown in the above Figure 4-13, the reference average radius is determined through the
following equation:
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( ) 2/*
1,,1
11, ijijN
rotationM
i
N
jrotationij xx
MNr θθθ −= +−
==∑∑ (4-14)
where θπΔ
=rotationM
where j is integer from 1, 2, 3. ……2N, where 2N is the number of points and N is the
number of levels from the drop profile. Angle Δθ is the specified amount of rotating angle and it
is a user-defined value. Mrotation is the number of rotating of the axisymmetric drop shape based
on the value of Δθ which is always chosen based on the motor steps per revolution, It is
preferred to have an integer number for Δθ so that it can be evenly divided by 2π. In the
experiments carried out in this study, the step motor has 500 steps for each revolution. In order
to have integer number of turn at each rotation, when the rotation angle is 18oC, the steps the
motor turns is 50steps/rotation which is a reasonable setting. Therefore, the angle is chosen at
18o apart every rotation starting from 0o. With 11 rotations, the whole drop profile would be
covered completely.
4.3.3.4 Definition of Degree of Asymmetry (DOA)
Then the degree of asymmetry is calculated for all the layers by comparing the radius of
from asymmetric profile with the reference radius at corresponding layers. Figure 4-14 shows
schematically how to obtain the radius from asymmetric drop profile at ith level.
Then this is repeated for all the profiles at different rotating angles. Finally, the total
error, denoted as E, from all the layers and rotating angles are summed and averaged. This
average values is then normalized with respect to the surface area ( )2* tippedestalrπ of the stainless
steel pedestal since the pedestal surface radius tippedestalr is a constant value. Then this
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normalized Easymmetry is just a number without unit and it is then defined as the degree of
asymmetry for the sample at that particular temperature.
( )2
1,,
12 **1 ∑∑
=
−
=⎟⎟⎠
⎞⎜⎜⎝
⎛−
∗=
N
jijij
M
irotationtippedestalasymmetry rR
MNrE
rotation
θθπ (4-15)
where M rotation is the number of rotations. This newly defined error term asymmetryE could be
used to as an index or definition of the Degree of Asymmetry (DOA) of the PS sessile drop.
From the magnitude of the DOA, it could then serves as an indicator to how the shape of the PS
sessile drop is close to the ideal symmetry case.
4.3.3.5 Volume Integration of Asymmetry Drop Shape
When the sessile drop is non-symmetric, the integration used in the axisymmetry case is
not applicable. But the edge detection and spline technique are still applicable in finding out the
boundary information. As described in the asymmetry definition, since the shape is not
axisymmetric, at angle 1θ , the radius at each level along the profile is not uniform. Figure 4-14
shows the radius at ith level of a asymmetric drop profile..
1θ
i1,θriR −1,θliR −
1,θriR −
1,θliR −
( )iRf
1θ
i1,θriR −1,θliR −
1,θriR −
1,θliR −
( )iRf
Figure 4-14 Radius Asymmetry at ith Level of Asymmetric Drop Shape
After number of rotations, the radii at each angle from ith level form an asymmetry
area. Figure 4-15 shows schematically the formation of this asymmetric circular area.
θN
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1θ
i
1θ
1,θriR −1,θliR − 1,θriR −
1,θliR −
2θ3θ4θ
Nθ
2,θriR −
2,θliR −
3,θliR − 4,θliR −
NliR θ,−NriR θ,−
( )iRf
( )jR θ
1θ
i
1θ
1,θriR −1,θliR − 1,θriR −
1,θliR −
2θ3θ4θ
Nθ
2,θriR −
2,θliR −
3,θliR − 4,θliR −
NliR θ,−NriR θ,−
( )iRf
( )jR θ
Figure 4-15 Asymmetric Circular Area after Nθ Rotations at ith Level
Spline technique is then applied to the circumference of this asymmetric area and
Simpson integration is used to accurately obtain the areas of each of the small circular section
bounded within each rotation angle θ. The detail area integration mathematically of the area is
illustrated graphically in Figure 4-16 as follow:
1θ
1,θriR −
NliR θ,−Nθ
1,θriR −
NliR θ,−
iRφ
1+iRφ
φΔ
1θ
1,θriR −
NliR θ,−Nθ
1,θriR −
NliR θ,−
iRφ
1+iRφ
φΔ
Figure 4-16 Area Determination of the Circular Section within Angle θ From the spline, each of the small θ i circular section is divided into number of even smaller
sections with angle Δφ. The area within each Δφ is determined as:
21
2360 ⎟⎟⎠
⎞⎜⎜⎝
⎛ +Δ= +ii
i
RRA φφφ
φπ (4-16)
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Therefore the area of θ i section is the summation of all those Aφ i and it expressed as:
( )2
1
121 2360
lim360 ∑∫
=
+
∞→ ⎟⎟⎠
⎞⎜⎜⎝
⎛ +Δ==
φφφ
φθ
φπφφπN
i
iiN
iiRR
dRA (4-17)
After obtain the areas within each θ i angle, the total area of this ith level asymmetric circular
section is the summation of all the Aθ i areas as:
( )∑
=−−−−−− ++++++=
θ
θθθθθθ
N
ilirilrlri AAAAAAA
12211 L
(4-18)
As shown in the following Figure 4-17, the area at ith level is then integrated along the
splined profile to calculate the volume of hΔ at ith level.
iA
1+iA( )iRfhΔi
iA
1+iA( )iRfhΔi
iA
1+iA( )iRfhΔi
Figure 4-17 Volume Determination at ith Level of Asymmetric Drop Shape This unit volume is computed as:
( ) hAAAAV iiiii Δ+∗+= ++ *31
11 (4-19)
where ( ) ( )[ ]ii RfRfh −=Δ +1
Similarly, the volume of the asymmetric sessile drop is the volume summation of those
unit volume with infinitesimal small height along the splined drop profile. The total volume is
expressed as:
( )∑∫=
++∞→
++∗Δ∗==layerN
iiiii
layerNtotal AAAAhdhhAV
111 *
3lim)( π
(4-20)
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Where ( ) ( )[ ]ii RfRfh −=Δ +1 One more note here is that there may be different approaches for volume estimation for
the asymmetric drop and the algorithm used in this research takes into the consideration of the
asymmetric drop shape and rigorously analyzes the asymmetric cross sections at different levels
for area and volume integration. It yields fairly accurate results based on the pure PS density
measurement.
4.4 Integration of Hardware and Software GUI Interface
4.4.1 XY Stage Control Software The XY stage is controlled through software from Galil Motion Co. The software
provides a graphic user interface (GUI) shown in the following Figure 4-18 for basic control of
the motion system.
Figure 4-18 XY Stage Software Control GUI
The commands are listed in a manual and the control of the system can be achieved
either through entering the command into the interface or via a script written with all the basic
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commands. A simple script is written to initialize the XY stage at the beginning of each
experiment. For instance, the speed of the motor shaft rotation that determines the axis moving
speed when driven by the motor, and the maximum moving range of each axis, etc. would be
included in this script. When the script file is downloaded into the controller, the motor would
follow the setting when it drives the XY stage. During the calibration process, the interface is
used and those basic commands are entered manually to complete the calibration process.
4.4.2 GUI Construction for Image Capture and Rotation
In order to improve the efficiency and ability for easy operation during the
experimentation, the process of setting up the camera movement steps, rotation angles and the
image storage are automated through the development of the graphic user interface using Visual
Basics language. Figure 4-19 shows a screen shot of the GUI interface. The detailed
development algorithm is attached in Appendix 2 for reference.
12
3
4
5
6
Figure 4-19 GUI Interface of the Image Capture and Rotation
1 Monitor window 2 x & y movement input 3 Rotation input
4 Time duration input 5 Data storage directory input 6 Action buttons
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The GUI allows users to enter the number of images needed to be captured by providing
the step movement for the XY stage so that the camera will move by following the exact
command. It also allows the user to enter the rotational angle of the sample droplet when
dealing with asymmetry measurement. Also, the time between each capture can also be
specified via the interface. Once all of the inputs are correctly entered, pressing the start button
would then start the experimental process and the images would be automatically saved in the
computer terminal.
4.5 Summary
The first half of the chapter described the design process using Axiomatic design
technique in detail. Each of the apparatus components was also thoroughly described. Although
the design process utilized the Axiomatic design tool, the actual implementation of the
components was an iterative process. When problems were anticipated during the apparatus
constructing, the designs were then re-evaluated for modifications until the problems or issues
were resolved.
There are some criterions for designing or choosing specific components. The selection
criteria are mostly dependent on system improvement, trial and error, etc. For instance, the
original CCD camera has low resolution about 640x480. When the image reconstruction proved
to be pros to error reduction, then a higher resolution CCD camera (2048 x 2048) is acquired to
achieve better image resolution even for a single image. The light source with variable intensity
is picked so that we could have various intensities under different conditions. The optimal light
intensity is selected after trial and errors when the best image quality is achieved.
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The second half of chapter was devoted to describe the algorithm development for
volume integration of both axisymmetric and asymmetric sessile drop cases. In the case of
asymmetric sessile drop, rotational device was used to facilitate the algorithm development. The
definition of degree of asymmetry was also defined and detail mathematics to calculate the
degree of asymmetry was developed and presented.
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Chapter 5. Validation of the Proposed Design
5.1 Introduction
There are several ways to verify the validity of our proposed design as well as the accuracy
and repeatability of our constructed PVT measurement apparatus based on our design
methodology. These methods are the precision stainless sphere ball volume measurements to
verify the significance of error reduction in using image reconstructions and empirical approach
of using the PVT system to measure the densities of pure polymers and compare them with Tait
calculated densities to verify the system accuracy and repeatability in dealing with both
axisymmetric and asymmetric sessile drops.
5.2 Empirical Verification of Error Reduction from Image Reconstruction
In order to demonstrate and verify the improvement in accuracy using the concept of
multiple image reconstruction, an absolute volume determination experiment is carried out using
a known volume precision sphere. The precision sphere was placed on the tip of a custom made
needle rod through a magnetic force inside the visualization chamber with maximum camera
magnification and optimal image quality. The temperature of the chamber was at room
temperature and no gas was injected to pressurize the chamber. Three separate experimental
case studies were carried out for the reconstruction. The first case captured one image, the
second case captured 6 images, and the third case took 9 images. The mass and density of the
reference stainless spheres were measured using a density measurement device (ASTM
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D792-00) and the actual volume of the sphere was determined by using the water displacement
method (sphere
spheresphere
mV
ρ= ) as the “absolute” volume for error analysis.
The error analysis is carried out by comparing the measured volume using the proposed
approach with the “absolute” volume. It is clearly shown from Figure 5-1 the accuracy is
dramatically improved as the number of images used for reconstruction increases. For a constant
camera resolution and field of view (FOV), the image will have a smaller pixel size if the
camera’s magnification is increased. The accuracy will be improved as the pixel size decreases
continuously and the number of images increases during edge detection and image
reconstruction. The error was about 2.8% in the single sphere image experiment. However, the
error decreased dramatically to 0.776% for 6 images and to 0.361% for 9 images. This
demonstrates that our proposed methodology gives clearer edge information in terms of the
pixel size. It is believed that the accuracy will be further improved with accurate calibration,
higher resolution camera.
0 2 4 6 8 100.0
0.5
1.0
1.5
2.0
2.5
3.0
Erro
r (%
)
Number of Image
Single Image 6 Image Reconstruction 9 Image Reconstruction
Figure 5-1 Accuracy Improvement from Sphere Image Reconstruction
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But for dynamic measurement in observing the volume change overtime, a single image
may have to be used because the volume of polymer specimen is changing continuously while
the camera moves around and captures the images. The average time needed for taking 6 images
and 9 images were roughly 20 seconds and 31 seconds, respectively.
5.3 Empirical Verification Using Tait Equation for Pure Polymer PVT
Several models or equations of state (EOS) have been proposed to describe the PVT
behavior of polymeric liquids based on thermodynamic law. Those equations of state for
polymer are either empirical or theoretical. The most widely used empirical equation is the Tait
equation in describing the pure polymer properties. The Tait equation is an isothermal
compressibility fitting model rather than a true equation of state. It reliably calculates the
specific volume of pure polymer at different temperatures and pressures using PVT data
measured from a bellow type dilatometer to obtain required fitting parameters. The detailed Tait
equation derivation has been described in Chapter 2; the different forms of Tait equation were
used for different polymer materials to calculate the density of the pure polymers at different
temperatures. At the same time, the pure polymer densities were also determined through the
PVT system. The density results from Tait and from the experiment measurement will be
compared.
5.3.1 Experimental Procedure and Materials
Pure polymer materials are used to serve the purpose of verifying the accuracy and
reliability of the PVT system. The pure polymer materials are linear and branched PP, PS 685D.
For PP and PS the procedures of conducting the pure PVT experiment are almost the same. A
simplified procedure is as follows:
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1) Select polymer pellet and measure the sample weight using precision balance
2) Prepare the sessile drop sample using vacuum oven
3) Conduct the PVT experiment at specific temperature at vacuum condition
4) Calculate the density of pure polymer at each temperature using the PVT measured
volume and mass information
5) Determine the pure polymer density using Tait equation at each set temperature and
vacuum
6) Compare the densities values obtained from experiment in step 4 with the ones
calculated from Tait in step 5.
5.3.2 Density Measurement for Pure Axisymmetric Linear and Branched PP
Following the simplified procedure, the pellet is picked from the virgin resin and the
weight of the pellet is picked such that it is between 8 to 12 mg due to the diameter limitation of
the sessile pedestal. The weight of the pellet is measured using the microbalance from MSB
system. The single pellet is then carefully placed in the middle of the heated pedestal with
tweezers. The pedestal with sample pellet is then placed in the vacuum oven at the temperature
near melting point for semi-crystalline polymer or the glass transition temperature for
amorphous polymer for about an hour to get rid of possible air pocket or moisture inside the
sample upon melting. Then the sessile sample is naturally cooled in the vacuum condition to
room temperature afterwards. The sessile drop with the best shape is picked for the experiment.
In addition, the size of the sessile drop depends on the size of the sessile pedestal. The size of
the pedestal can be changed if a bigger size is necessary.
Specific care was taken to make sure to get the best axisymmetric drop profile and at the
same time to make sure the sample did not stay in the oven for too long to prevent degradation.
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Again, the TGA tests (Appendix 7) show that the neither the temperature nor the duration of the
experiment time would cause degradation of the sample.
Density measurements for neat PP were conducted in vacuum at five different
temperatures of 180°C, 190°C, 200°C, 210°C, and 220°C, which are all above their melting
points. The vacuum pump helped to achieve the vacuum reservoir inside the visualization
chamber. After approximately half an hour in the vacuum at each of these temperatures, the
images were taken. The density experiments were carried out three times at each temperature to
ensure repeatability, and the average values were reported as the final values.
On the other hand, the Tait equations for branched PP and linear PP resins used in this
research have the following forms, respectively[124]
PP
PPbranched+
++
=8
2
9
6
10*146.1
T10*1.221
10*773.5
10*485.6υ (5-1)
PP
PPlinear+
++
=7
2
9
6
10*86.9
T10*1.06
10*45.6
10*46.7υ (5-2)
The specific volume υ has units of m3/kg, pressure P is in Pascal and temperature T is in
degrees Celsius.
Figure 5-2 shows the comparison between the measured PP densities and the known data
derived from Tait equation for linear PP at those five different temperatures.
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180 190 200 210 2200.710
0.715
0.720
0.725
0.730
0.735
0.740
0.745
0.750
Dens
ity (g
/cm
3 )
Temperature (oC)
This work Tait Equation from Gnomix Measurement
Figure 5-2 Pure Linear PP Measured and Tait Calculated Densities
The results show an excellent agreement between the Tait calculated data and the
experimentally obtained values. Figure 5-3 shows the same comparison between the Tait
calculated density and the measured density of pure branched PP at those four temperatures.
Since repeated experiments were carried out, the error bars throughout this thesis show the
standard errors from those experiments. Again, the obtained results illustrate a very good
agreement between experimental results and theoretical calculations. Providing the Tait
equation for pure polymer PVT calculations has been proven to be very accurate and reliable,
these pure polymer density experiments validate our method of approach as well as the
experimental set-up for measuring the volume of a polymer /CO2 solution.
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190 200 210 2200.70
0.71
0.72
0.73
0.74
0.75
0.76
0.77
0.78
0.79
0.80
0.81
0.82
Dens
ity (g
/cm
3 )
Temperature (oC)
Experiment Measured Density Tait Calculated Density
Figure 5-3 Pure Branched PP Measured and Tait Calculated Densities 5.3.3 Density Measurement for Pure PS685D with Asymmetry
In addition to the pure PP density measurement, in the study of the shape parameter,
particularly the asymmetry shape effect of the drop on the PVT measurement, the pure PS
density is also measured at various temperatures. The main purpose of the asymmetry study is
to demonstrate that from the use of rotational device, the effect of asymmetry on the density
calculation could be compensated so that accurate volume can still be obtained despite the
asymmetric drop shape.
The PS resins are PS 685D supplied from Dow Chemical and its Tait equation has the
following form:
( ) ( )[ ] ( )( ) ⎭⎬⎫
⎩⎨⎧
⎥⎦
⎤⎢⎣
⎡−∗
∗+−−+=
37.376exp*1ln0894.0137.3769724.0,
TDBCPTATPv (5-3)
where A, B, C, D are constant coefficients and their values are A= 5.996*10-4, C= 0.0689476
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, B=1.79784*103, and D=-4.761*10-3, respectively. Temperature T is in Kelvin, and pressure is
in psi. The PS Tait equation 5-3 has more resemblance with the general Tait equation described
in Chapter 2.
The Figure 5-4 shows the asymmetry drop profile from an actual experiment sessile
drop.
0 200 400 600 800 1000 1200 1400 1600 1800 2000-2200
-2000
-1800
-1600
-1400
-1200
-1000
-800
-600
Level 1Level 2Level 3
0 200 400 600 800 1000 1200 1400 1600 1800 2000-2200
-2000
-1800
-1600
-1400
-1200
-1000
-800
-600
Level 1Level 2Level 3
Figure 5-4 Actual Sessile Drop Profile and Level Selection at 150oC
In order to show how the drop shape looks like from top view, the radii at randomly
chose three levels from the drop profile at each of the experimental temperature at all the
rotational angles are plotted from Figure 5-5 to 5-9.
‐400
‐300
‐200
‐100
0
100
200
300
400
‐400 ‐300 ‐200 ‐100 0 100 200 300 400
Top View at 150oC
Level 1
Level 2
Level 3
Figure 5-5 Profile Top View at 150oC
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‐400
‐300
‐200
‐100
0
100
200
300
400
‐400 ‐200 0 200 400
Top View at 200oC
Level 1
Level 2
Level 3
Figure 5-6 Profile Top View at 200oC
‐400
‐300
‐200
‐100
0
100
200
300
400
‐400 ‐200 0 200 400
Top View at 250oC
Level 1
Level 2
Level 3
Figure 5-7 Profile Top View at 250oC
Figure 5-5 to 5-7 showed the drop radius profile at those three layers at 150oC, 200oC
and 250oC respectively during the temperature rising round. Figure 5-8 and 5-9 showed the
radius profile from 200oC and 150oC during the temperature cooling round. The figures clearly
showed the actual circumferential profile of the asymmetry drop at three different levels of the
drop. Figure 5-4 showed the worst asymmetry shape at the temperature 150oC and Figure 5-6
showed more circular shape at 250oC. At temperatures during the cooling process, Figure 5-7
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and 5-8 showed that the drop shape still remained fairly good circular shape when temperature
dropped.
‐400
‐300
‐200
‐100
0
100
200
300
400
‐400 ‐200 0 200 400
Top View at 200oC
Level 1
Level 2
Level 3
Figure 5-8 Profile Top View at 200oC from Cooling
‐400
‐300
‐200
‐100
0
100
200
300
400
‐400 ‐200 0 200 400
Top View at 150oC
Level 1
Level 2
Level 3
Figure 5-9 Profile Top View at 150oC from Cooling
The volumes of the PS sessile drop were determined and the densities were calculated at
from all the rotated angles during the temperature rising round. Figure 5-10 showed the density
results comparison with Tait equation. The results indicated that the measured densities from
asymmetry sessile drop agreed very well with Tait equation values at all three temperatures.
Therefore the conclusion drawn here is that PS sessile drop is not axisymmetric in nature at low
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temperature, but with the help of rotational device, the effect of asymmetry drop shape is
compensated and the volume calculation is still reliable and accurate.
125 150 175 200 225 250 2750.80
0.85
0.90
0.95
1.00
1.05
1.10
1.15 Measured Density Tait Density
Den
sity
(g/c
m3 )
Temperature (0C)
Figure 5-10 Density Measurement from Asymmetry Drop Shape and Tait Equation
In other words, with the ability to rotate the sample droplet, accurate density information
can still be obtained for polymer melts or polymer/gas solutions with asymmetric drop shape
regardless the temperature effect on the asymmetry nature of the drop profile. The effect of
temperature on asymmetry is shown in Chapter 6.
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5.4 Summary
The emphasis of this chapter is on rigorous verifications of the validity of the proposed
image reconstruction method in error reduction as well as the accuracy and repeatability of
using this newly constructed system to measure the PVT information of pure polymer and
polymer/gas solutions at high temperatures and pressures.
A precision stainless sphere ball was used to demonstrate the error reduction from image
reconstruction. Three sets of images were taken for reconstruction purposes demonstrated that
the accuracy improved significantly when more images were taken for reconstruction. The
second part of the chapter focused on the pure polymer density measurement to demonstrate the
accuracy and repeatability of the system in measuring volume. Three pure polymer materials,
namely, linear PP, branched PP and PS 685D were used in the experiments at different
temperatures and in vacuum conditions. The measured densities were compared with densities
calculated from the Tait equation. It was found that the empirically measured density matched
very well with the theoretically calculated value; therefore, the accuracy, the reliability of using
this newly developed system to conduct experiments has been confirmed.
During the experiment with pressurized supercritical blowing agent (CO2), it is not
feasible to measure the initial volume at each pressure level using inert gas, such as Helium for
the same sample pellet unless different samples are used to carry out the experiment separately
at each pressure level at one temperature. This would prolong the experiment time and
complicate the experimental procedure. In addition, the inert gas molecular may still dissolve
into the polymer sample which would affect the measurement outcome. Since the verification
proves the system accuracy, using Tait equation to compute the initial sample volume would
reduce the experiment complexity but also provide a precise initial sample volume. Since the
pure PP PVT measurement at high temperature and vacuum conditions already verified the
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system reliability, it is not that significantly important to measure the specific gravity of PP at
room temperature.
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Chapter 6. Measurement of the PVT Data for Polymer/Gas Solutions
6.1 Introduction
In a polymer/gas solution systems, when gas dissolves into a molten polymer the
polymer swells (or dilates) due to gas sorption. The amount of polymer swelling or dilation is
characterized by its PVT properties, which can be obtained by measuring the equilibrium state
volume of a polymer/gas solution at any specific temperature and pressure. The ultimate goal of
this research is to develop a new method for direct PVT property measurements of polymer/gas
solutions. The method utilizes the pendent/sessile droplet technique and combines it with a high
temperature and pressure visualization chamber, where the polymer swelling caused by high
pressure gas, can be monitored. The detailed development of this PVT apparatus has been
discussed in the previous chapter. The system enables the assessment not only of the dynamic
change of the polymer/gas solution volume with respect to time, but also, more importantly, the
final volume at equilibrium state. The overall methodology is illustrated in a flow chart seen in
Figure 4-7.
6.2 PVT Measurement with Axisymmetry for Linear/Branched PP/CO2
Solutions
6.2.1 Experimental Procedure The overall methodology and experimental procedure are elucidated in a flow chart as
shown in Figure 4-7. It is assumed that the polymer pendent/sessile drop is axisymmetric to
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begin with, which means the droplet profile is axisymmetric with respect to its vertical
centerline.
At the beginning of each experiment, the camera parameters, such as the working
distance relative to the drop sample, the image contrast through optical lens, and so on, are
adjusted for maximum zoom while ensuring the best image quality at the boundary.
The calibration is then carried out to determine the pixel size in the x and y orientation,
with respect to the XY stage movement. The calibration determines the size of the pixel in terms
of the metric length, which is based on the movement of the stage, since the unit step length of
the stage is known. This is a crucial step since it not only provides the conversion factor
between the image pixel size and the real drop’s metric dimension at the image reconstruction,
but it also helps to correct some possible optical distortions. The detail calibration technique is
summarized in Appendix 3.
The number of images needed to cover the whole pendant/sessile drop is calculated
based on the magnification of the optical system and the resolution of the CCD camera. For a
given number, the step-wise movements of the XY stage in both x and y directions are
determined. Those x and y increments are programmed and stored into the motion controller to
guide the step motor to move the XY stage and camera with precision. The images are captured
when the camera pauses briefly in between each of the new x and y movements. The series of
images is then combined and reconstructed to form a complete drop image based on the
movements using an image processing tool.
After the image reconstruction is completed, the precise Canny edge detection algorithm
is used to detect the drop boundary and generate the edge pixel coordinates. The Canny edge,
which is based on the first derivative and localization criteria of a class of edges, is the most
successful subpixel edge detector. The boundary profile coordinates are identified. To improve
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the accuracy of the drop profile coordinates, repeated points, i.e., pixels with the same
grey-levels at one location, are averaged into distinctive data points (xi, xj) using the smoothing
spline technique.
Finally the Simpson’s 1/3 rule is applied for integration to compute the final volume of
the polymer-gas solution drop. Among the numerical integration methods, composite Simpson’s
1/3 method has superior and finer segments over the Trapezodial rule. A detailed mathematical
formulation is described in Chapter 4.
6.2.2 Experimental Setup
In Chapter 4, the system components are introduced one by one in detail. The PVT
apparatus is the assembly of those components together. In brief, the experimental apparatus
consists of the following components: a high-pressure chamber with a sapphire visualization
window; a 2024 x 2024 resolution JAI Pulnix TM4100 CL camera with a control software (Easy
Grab); Schneider 4/80 lens and extension tubes; a temperature controller (Omega CN132) with
thermocouple (Omega RTD); four cartridge heaters; an automatic high-precision XY stage with
Galil motion controller and control board; a manual 1” XYZ stage to adjust the position of the
light source; a syringe pump connected to the gas tank; and a backlight source with a light
equalizer/diffuser.
6.2.3 Experimental Materials
Linear polypropylene (Borealis MD 55) and Branched PP (Borealis HMS WB130) with
Tm = 162oC ~ 165°C, CO2 (99.99% purity, BOC Coleman grade) were used
6.2.4 Volume Swelling of Linear/Branched PP/CO2
First of all, the absorption test is carried out using MSB system to see how long it take
the pellet sample to be saturated and reach equilibrium at all pressure levels at the lowest
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temperature 180oC for both linear and branched PP. It is found out that approximately 15 to 20
minutes would be the time for a resin pellet to reach equilibrium under pressurized supercritical
CO2 reservoir. The results are included in the thesis in Appendix 8.
The density measurement for PP/CO2 solutions were also conducted at 180°C, 200°C,
and 220°C under high pressure CO2. At each temperature, the pressure started from 1000 psi
and went up to 4500 psi, at 500 psi increments. At each pressure level, the PP/CO2 solution was
maintained for 35 to 45 minutes to ensure the equilibrium of the system was reached.
Equilibrium was considered to have been achieved when the total volume of the polymer/gas
solution no longer changed.
When a polymer melt is exposed to a high pressure gas, two competing mechanisms will
affect the specific volume. On the one hand, the hydraulic pressure will decrease the specific
volume of compressible polymer/gas solutions. On the other hand, the dissolved gas under high
pressure would cause the polymer to swell and increase the specific volume. The latter is
typically higher than the hydraulic pressure effect. This means that the presence of gas evidently
enhances the overall activity of the polymer/gas system[271] and thus, creates more free volume
for the CO2 molecule to penetrate into after the gas fills the existing free volume. The increased
specific volume (i.e., increased free volume) causes an increase in the solubility and diffusivity
[124]. The dissolved CO2 causes a plasticization effect to reduce the viscosity of the polymer/gas
mixtures and to increase the chain mobility [132,272]. Also this increased specific volume
decreases the surface tension of polymer[273]. In summary, despite the hydraulic compression
effect, the high-pressure gas increases the specific volume and thereby affects the solubility,
diffusivity, viscosity and surface tension. All of these fundamental parameters are critical in
determining the foaming behaviours, and it should be emphasized that the swelling caused by
gas dissolution governs all of these parameters.
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180 200 2200.981.001.021.041.061.081.101.121.141.161.181.201.221.24
Swel
ling
Rat
io
Temperature (oC)
1000psi 1500psi 2000psi 2500psi 3000psi 3500psi 4000psi 4500psi
a) at Temperatures
500 1000 1500 2000 2500 3000 3500 4000 4500
1.00
1.04
1.08
1.12
1.16
1.20
1.24
Swel
ling
Rat
io
Pressure (psi)
1800C Linear PP/CO2
2000C Linear PP/CO2
2200C Linear PP/CO2
b) Pressures
Figure 6-1 Linear PP/CO2 Swelling vs. a) Temperatures and b) Pressures
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180 200 2200.981.001.021.041.061.081.101.121.141.161.181.201.221.24
Volu
me
Swel
ling
Rat
io
Temperature (oC)
1000psi 1500psi 2000psi 2500psi 3000psi 3500psi 4000psi 4500psi
a) Temperatures
500 1000 1500 2000 2500 3000 3500 4000 4500
1.00
1.04
1.08
1.12
1.16
1.20
1.24
Swel
ling
Rat
io
Pressure (psi)
1800C Branched PP/CO2
2000C Branched PP/CO2
2200C Branched PP/CO2
b) Pressures
Figure 6-2 Branched PP/CO2 Swelling vs. a) Temperatures and b) Pressures
As depicted from equation (4-12), the swelling ratio is the quotient of the total PP/CO2
mixture volume at an equilibrium state over the initial pure polymer volume. The final volume
is measured experimentally and the initial pure polymer volume is determined as the product of
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the pre-weighted mass of the pure polymer sample and its density is calculated using the Tait
equation. Figures 6-1 and 6-2 show the volume swelling of linear PP/CO2 and branched PP/CO2
solutions at all the temperatures and pressures, respectively.
6.2.5 Effect of Temperature and Pressure on PVT of PP/CO2 Solutions
6.2.5.1 Effect of Temperature on Volume Swelling
When the pressure is constant, higher temperatures result in less volume swelling in the
PP/CO2 solution. This is true for both linear PP/CO2 and branched PP/CO2 solutions. It is clearly
seen from the above Figure 6-1 a) and 6-2 a) that the volume swelling of both PP/CO2 solutions
decreases when the temperature increases. As the temperature increases, the polymer chains
become softer and more relaxed. As a result, the free volume increases and the specific volume
increases. On the other hand, the solubility of CO2 in PP is known to decrease as the
temperature increases. This means that the diffusion of CO2 out of the polymer matrix increases
more at a higher temperature compared to the increased free volume of polymer. So, despite the
increased free volume in the PP matrix, the PP/CO2 solution will lose CO2 at higher
temperatures. As the pressure climbed higher, the volume swelling was governed by the gas
content, and the sensitivity of the volume swelling with respect to the temperature became
smaller.
6.2.5.2 Effect of Pressure on Volume Swelling
As discussed, the increasing solubility of CO2 at a higher pressure caused more CO2 to
dissolve into the PP matrix, inducing more volume swelling. It is seen from the results that when
pressure increases at each individual temperature, the volume swelling ratio increases for both
linear and branched PP/CO2 mixtures. Both Figures 6-1 b) and 6-2 b) show that the measured
volume swelling ratio of the linear and branched PP/CO2 solution increased as the pressure
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increased at 180°C, 200°C, and 220°C. At a fixed temperature, when the pressure increased, the
volume of the polymer/gas mixture also increased, so did the volume swelling ratio. Since the
solubility of CO2 increases with an increase in the pressure as mentioned above [124], more CO2
dissolves into the PP matrix, which would induce more volume swelling.
However, as the pressure went higher, it was observed that the equilibrium volume and
volume swelling ratio will eventually approach a plateau region. In other words, the rate of
increase in volume swelling becomes smaller and the swelling graph starts to level off as the
pressure keeps increasing. This implies that the volume will not expand indefinitely as the
pressure goes up at a constant temperature. Wissinger et al. [75]also reported similar behaviours
of volume swelling and sorption that began to level off and reached limiting values for PC/CO2
and PMMA/CO2 systems at low temperatures of about 35oC and 32.7oC, respectively, when
pressure was in the range of 70 atm to 100 atm.
On the one hand, after passing some pressure levels, such as after 3000psi, the hydraulic
effect from the higher pressure may start to exhibit a stronger volume compression effect than it
does at relatively low pressure levels. If this is the case, then it will counteract or prevent more
volume swelling due to gas dissolution at very high pressures. On other hand, the chain
structures of both linear and branched PP would also be part of the reason in restricting itself
from expanding indefinitely through absorbing more gas at high pressures. The long chain
structure effect and the possible implications of chain entanglement on volume swelling will be
analyzed in later sections.
6.2.6 Effect of Branch Structure on PVT of PP/CO2 Solutions
As the effects of pressure and temperature on the volume swelling have been explained,
it is now appropriate to analyze the polymer itself to study how its long chain structure,
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especially the branched long chain structure in branched PP, would affect the volume swelling.
This section is going to focus more on the branching effect on the PVT rather than other aspects
of structure effect, such as chain entanglement and chain entanglement density. The latter will
be dealt with in a separate section in detail. The swelling between linear and branched PP at
each temperature were shown separately. Figure 6-3 shows the comparisons of the volume
swelling between linear and branched PP/CO2 at 180oC.
500 1000 1500 2000 2500 3000 3500 4000 45001.00
1.04
1.08
1.12
1.16
1.20
1.24
Swel
ling
Rat
io
Pressure (psi)
1800C Linear PP/CO2
1800C Branched PP/CO2
Figure 6-3 Linear and Branched PP/CO2 Swelling at 180oC
Figure 6-4 shows the comparisons of the volume swelling between linear and branched
PP/CO2 at 200oC and, lastly, Figure 6-5 shows the comparisons of the volume swelling between
linear and branched PP/CO2 at 220oC. The volume swelling data was tabulated with error in
Appendix 6.
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500 1000 1500 2000 2500 3000 3500 4000 4500
1.00
1.04
1.08
1.12
1.16
1.20
Volu
me
Swel
ling
Pressure (psi)
2000C Linear PP/CO2
2000C Branched PP/CO2
Figure 6-4 Linear and Branched PP/CO2 Swelling at 200oC
500 1000 1500 2000 2500 3000 3500 4000 4500
1.00
1.02
1.04
1.06
1.08
1.10
1.12
1.14
1.16
1.18
Volu
me
Swel
ling
Pressure (psi)
2200C Linear PP/CO2
2200C Branched PP/CO2
Figure 6-5 Linear and Branched PP/CO2 Swelling at 220oC
Of all the results, one immediate conclusion could be quickly reached is that: in general,
the linear PP/CO2 mixture has a higher volume swelling over the branched PP/CO2 mixture due
to the branched chain structure and possible high polymer chain entanglement density of
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branched PP. When long chained structures of linear PP are being branched, the movement of
the branched chain structure or chain mobility is greatly restricted. The melt viscosity, as well as
the melt strength of the branched PP is significantly enhanced over the linear PP. The
improvement of the melt strength is good in preventing the cell collapse in the foaming process
because cell walls have higher strength and rigidity and could withstand the force exerted from
cell growth. This will in turn help to maintain the cell structure and eventually the foam
morphology. Thereby, the mechanical properties of branched PP foam products are proven to be
better than those foamed from linear PP[9].
As shown in Figure 6-3, at 180˚C branched and linear PP/CO2 have similar volume
swelling at pressure levels of up to 2500psi. But when the pressure goes higher than 2500 psi,
branched PP starts to have less swelling. In other temperatures, linear PP/CO2 always has higher
swelling over branched PP/CO2 at all pressures. This implies that the branching structure would
be effective in preventing volume dilation at relatively high temperatures and pressures.
When the pressure kept increasing, the branched PP/CO2 had a much smaller volume
swelling compared to linear PP/CO2. Since the long-chain branched PP from Borealis is
produced by the Daploy process, which is characterized by an after-treatment of the native
polypropylene granules out of the polymer synthesis at temperatures well below the melt
temperature of polypropylene[274,275], mircogels were formed and found in very small amounts
of the final product (usually below 1wt% concentration). The effect of the branch would involve
the promotion of strain hardening that increases the melt strength, which could then result in
zero-shear viscosity increase and reduction in fluidity.
At higher temperatures of 200oC and 220oC, the resistances, such as increased melt
strength and strain hardening generated from branched structures, were counter-balanced to
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some extent by the increase of temperature and pressure, the linear PP still has significant higher
volume swelling than branched PP at all pressures.
6.3 Measurement of PVT Data for PS and PS/Gas Solutions
6.3.1 Measurement of PVT Data with Asymmetry for PS and PS/CO2 6.3.1.1 Introduction
Polymer has been categorized into two different types according to their matrix structure,
namely, amorphous and semi-crystalline. When ordinary small molecules pack themselves in
regular three-dimensional arrays, they can then be considered as crystalline. When polymer is
amorphous, the molecules lack position order on the molecules. Semicrystalline polymer
contains both crystalline and amorphous regions in their polymer matrix as seen in the following
two dimensional schematic.
Crystalline region
Amorphous region
Figure 6-6 Schematic of Semicrystalline Polymer Structure* *source: http://chem.chem.rochester.edu/
Semicrystalline polymers have true melting temperatures (Tm) at which the ordered
regions break up and become disordered. In contrast, the amorphous regions soften over a
relatively wide temperature range (always lower than Tm) known as the glass transition (Tg).
Fully amorphous polymers do not exhibit Tm and when polymers are all above Tg they become
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liquids. Typical semicrystalline polymers are like polyethylene (PE) and polypropylene (PP) and
conventional amorphous polymers are polystyrene (PS) and poly(methyl methacrylate)
(PMMA).
PS is used in this study to emphasize the effect of the high melt strength on the
formation of the sessile drop shape, and thereby the effect on the final results of PVT
measurement. In order to easily capture the effect of asymmetry, pure PS density experiments
are carried out. The experiments were carried out. The experiment was carefully constructed so
that the rotational device was utilized to rotate the droplet at very small angle for one revolution
to capture the drop shape. The results from those each individual angle will be compared and
analyzed.
6.3.1.2 Experiment Procedure
At each of the temperatures, enough time was allocated for the sample to reach
equilibrium and the chamber was vacuumed. The sessile droplet was rotated at every 18oC. The
reason for picking this angle was to make the number of the rotation and the motor rotation step
integer numbers with 500 steps per revolution from the step motor. A single image of the drop
was captured at every rotated angle. In the cooling round, the temperatures were cooled from
250oC to 200oC and finally to 150oC.
At each of the temperatures, there were 11 pictures taken since the 11 rotations were at
18o for each rotation. In this temperature setting, the asymmetry shape effect would be
dramatically differentiated from the two 150oC and 200oC temperatures since the they retained a
better axisymmetric shape from high temperature of 250oC during the cooling and since
presumably the shape would be closer to symmetry at high temperatures, which was shown to
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be true in the experimental results. Three sets of experiments were carried out to repeat the
measurement three times and the results from every experiment were analyzed and compared.
After conducting the pure PS density experiment to investigate how the asymmetry
could effect the experimental results, another three sets of sample were prepared at 250oC to
conduct the PS/ CO2 volume swelling experiment with CO2 as blowing agent. For the PVT
experiment, the same three temperatures, 150oC, 200oC to 250oC, were used and the pressures
started from 1000 psi to 4000 psi at 1000 psi increments.
6.3.1.3 Experimental Material
Polystyrene (PS685D) supplied from Dow Chemcial Company and CO2 (99.99% purity,
BOC Coleman grade) were used in this study.
6.3.2 The Temperature Effect on the Degree of Asymmetry
As has been defined and modeled in Chapter 3, there are two approaches to define the
degree of asymmetry: radial asymmetry and volumetric asymmetry. Figure 6-7 shows the plot of
the degree of asymmetry vs. temperatures. This degree of asymmetry is based on the radius
symmetry defined in Chapter 4. See equation 4-17. It is very obvious to observe that when the
temperature increases from 150oC to 250oC, the degree of asymmetry decreases dramatically
from the first experiment and the third experiment.
It is also observed that the degree of asymmetry is reduced in the first experiment during
the temperature rising process. For example, in the second experiment, the Easymmetry value
dropped from 1 at 150oC to 0.5 at 200oC and eventually reached almost 0 at 250oC. From the
definition of Easymmetry the bigger values implies that the radius of the drop at that temperature
deviates more from the reference radius, which is more axisymmetric In other words, the bigger
the Easymmetry value, the more the drop shape will have asymmetry. For instance, the Easymmetry
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value for the first experiment is around 2 at 150oC and 1.7 at 200oC. This means the shape of the
sessile drop from the first experiment is more skewed to start with than those in the second and
third experiment. On the contrary, since the third experiment started with a better drop shape, its
Easymmetry value is much smaller even at the low temperatures. Those results indicate that the
increase in temperature helps the high viscous PS polymer chain structure to relax more and
form more symmetry shapes, which is desired in accurate volume calculation.
On the other hand, during the temperature cooling process, the degree of asymmetry
almost remains unchanged by going from 250oC to 150oC. From Figure 6-7, the Easymmetry values
are pretty much the same (close to 0) for all three temperatures. The results illustrate that the
higher the temperature, the better the sessile drop shape is to close near the axisymmetric dorm
shape and the better the drop shape forms at high temperatures, which could be retained even as
the temperature dropped, which means the polymer chain contraction due to the temperature
drop would not significantly affect the overall shape.
140 160 180 200 220 240 260-0.5
0.0
0.5
1.0
1.5
2.0
2.5
3.0
Nor
mal
ized
Deg
ree
of A
sym
met
ry E
asym
met
ry
Temperature (oC)
Experiment 1 Experiment 2 Experiment 3
Figure 6-7 Degree of Asymmetry of Pure PS at Temperature Rising and Cooling Process
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6.3.3 Temperature and Pressure Effect of PVT of PS/CO2
Three PS sessile drop samples were prepared at 250oC to help form a more axisymmetric
drop shape. In order to prevent sample degradation due to the long exposure at high temperature,
the PS sessile droplet stayed at 250oC for only 15 minutes. The following Figure 6-8 shows the
swelling ratio of PS/CO2 solutions at all three temperatures and four pressures. The results are
very similar to the case of PP/CO2 swelling at high temperatures and pressures. When the
pressure is constant, higher temperatures also result in less volume swelling in the PS/CO2
solution. It is clearly seen from the above Figure 6-8 a), that the volume swelling decreases
when the temperature increases at all pressure levels. As the temperature increases, the polymer
chains become softer and more relaxed. As a result, the free volume increases and the specific
volume increase. On the other hand, the solubility of CO2 in PS decreases as the temperature
increases. The volume swelling significantly drops at 250oC compared to the drop from 150oC
to 200oC. This means that the diffusion of CO2 out of the polymer matrix increases more at a
higher temperature compared to the increased free volume of polymer. So the PS/CO2 solution
loses more CO2 at higher temperatures.
150 200 2501.00
1.02
1.04
1.06
1.08
1.10
1.12
1.14
1.16
1.18
1.20
1.22
Volu
me
Swel
ling
Rat
io)
Temperature(oC)
1000psi 2000psi 3000psi 4000psi
a) Temperatures
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1000 2000 3000 40001.00
1.05
1.10
1.15
1.20
1.25
Swel
ling
Rat
io
Pressure (psi)
150oC PS/CO2
200oC PS/CO2
250oC PS/CO2
b) Pressures
Figure 6-8 PS/CO2 Volume Swelling vs. a) Temperatures and b) Pressures
The increasing solubility of CO2 at a higher pressure caused more CO2 to dissolve into
the PS matrix, inducing more volume swelling. It is seen from Figure 6-8 b) that when pressure
increases at each individual temperature, the volume swelling ratio increases. But as the
pressure goes higher, we observe that the equilibrium volume and the rate of volume swelling
will eventually slow down which is also observed in the PP/CO2 case. This implies that the
volume will not expand indefinitely in PS/CO2 case as the pressure goes up at a constant
temperature. This trend is obvious at 250oC temperature.
6.3.4 Measurement of PVT for PS/HFC-152a Solution 6.3.4.1 Introduction
A variety of physical blowing agents (PBAs), such as chlorofluorocarbon (CFCs),
Hydrochlorofluorocarbons (HCFCs), Hydrofluorocarbons (HFC), butane, or pentane are
currently used in the plastic foam industry for low-density foam processing because of their low
diffusivity and high solubility [123]. The drawback for CFCs is their environmental hazards. The
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depletion of the ozone layer associated with their usage led to the Montreal Protocol in
1987[276,277]. Under this Protocol, the production of CFCs has been banned in Europe and United
States since 1995. The most commonly used HCFCs for foam blowing agents (i.e.,HCFC-141b,
HCFC-22 and HCFC-142b) will be phased out beginning January 1st 2010. In addition, there
is a significant challenge for the plastic foam manufactures those countries who have ratified the
Kyoto Protocol [276,277] and have committed to reduce their emissions of carbon dioxide and five
other greenhouse gases, i.e., water vapor, carbon dioxide, methane, nitrous oxide, and ozone..
Therefore, the issue to find the next generation of environmental substances which can
be used as a replacement for CFCs and HCFCs in foam manufacturing is becoming imminent.
Currently, extensive research has been devoted to develop new blowing agents for foam
production [132,271,278]. The potential blowing agent replacement candidates will be HFCs (134a,
152a, or experimental HFCs), hydrocarbons (HCs) and inert gases such as carbon dioxide (CO2)
and nitrogen (N2). Among these conceivable surrogated gases, HFCs, i.e., HFC 134a and HFC
152a, offer superior thermal insulation capabilities and are desirable candidates for the
replacement of CFCs and HCFCs[279-281]. Nevertheless, the low solubility and low diffusivity
associated with HFC 134a [280,282] has made the foaming processes challenging despite its
reasonably good R-value. In order to obtain low-density foams, it is necessary to employ a high
system pressure to increase the HFC 134a content that could be dissolved. Previous research has
demonstrated that the use of high HFC 134a content would lead to foams exhibiting a rather
poor morphology. Gendron et al.[283] indicated that foaming polystyrene (PS) with HFC-134a
content above 7.5 wt.% would result in large voids, which were in the order of a few millimeters,
due to the inhomogeneous dissolution of the HFC-134a. On the other hand, it is known that
HFC-152a has a higher solubility and diffusivity. However, there are serious concerns regarding
the storage and long term insulation performance of the end-product due to its flammability and
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fast diffusion coefficient at room temperature. Moreover, it is believed that the rapid diffusion of
HFC-152a will significantly decrease the amount of gas that will remain in the foam over time
and deteriorate the thermal insulation efficiency of the product over its lifetime.
6.3.4.2 Experimental Procedure and Material The volume swelling of PS685D was carried out at two separate termperatures. They
were 150oC and 190oC, respectively. The blowing agent used in this study is HFC-152a
(Formacel®
Z-2) provided by Dupont. The vacuum pump helps to achieve the vacuum reservoir
inside the chamber at the very beginning of each experiment. The initial temperature is set at
150oC. Once the temperature goes beyond the glassy transition point, the solidified sessile
drop sample starts re-melting back to the sessile drop shape and the HFC-152a gas is then
injected into the chamber to reach the first pressure level which is 200 psi. The pressure goes up
at 200 psi increaments each time until it reaches 800 psi for 150oC cases. For 190oC cases, the
same pressure levels, namely, 200 psi, 400 psi and 800 psi were studied. The camera started
taking the images. The whole camera motion repeated every 10 minutes up to 60 minutes to
ensure that the polymer melt reaches equilibrium state at the 150oC. After finished at 150oC,
the pressure was increased to 400 psi and the previous steps were repeated until the experiment
finished at 800psi. Then a new set of experiments were conducted at 1900C with similar
procedures being used at 1500C. The whole experimentation was completed when all of the
temperature levels were conducted. Image edge detection and volume integration techniques are
utilized to generate the volume information of the polymer sample at these temperatures.
The volume swelling ratios at those pressures were plotted. Also the SS and SL
predicted volume swelling for the same materials at each corresponding pressure were also
plotted on the same graph for comparison purposes. Figures 6-10 and 6-11 show that the total
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volume of the PS685D/HFC-152a solution expands as the pressure increases each time. The
density of the HFC-152a increases in the confined chamber space as the pressure increases,
hence, more HFC-152a molecular will penetrate into the PS685D polymer matrix causing more
dilation until it reaches the saturation point. In this study, instead of using EOS to predict the
volume swelling, we used our PVT apparatus to measure the volume swelling experimentally.
6.3.4.3 Temperature and Pressure Effect of PVT for PS/HFC-152a The volume of the PS/ HFC-152a increases as the pressure increases. For the fixed
temperature, as the pressure increases, the volume of the polymer/gas mixture increases, as does
the volume swelling ratio. Since the solubility of HFC-152a increases[284] as the pressure goes
up, there is more HFC-152a dissolving into the PS matrix to induce more volume swelling. It is
seen from Figure 6-9 that as the pressure goes up, the volume of the polymer/gas mixture
increases significantly. From the experiments, it was observed that the time for the mixture to
reach a stabilized state is less when the pressure is higher because of the P increased plasticizing
effect. In order not to have the hydraulic effect, the pressure would have to be the same
throughout the volume swelling calculation according to our earlier definition at each pressure
level. As previously mentioned, the Tait equation is ultilized here to compute the initial volume
of the polymer/gas mixture as the base for computing volume swelling ratio.
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0 100 200 300 400 500 600 700 8000.94
0.96
0.98
1.00
1.02
1.04
1.06
1.08
1.10
1.12
1.14
Volu
me
Swel
ling
Rat
io
Pressure
PS/HFC-152a at 150oC PS/HFC-152a at 190oC
Figure 6-9 PS/HFC-152a Volume Swelling at 150oC and 190oC
For the same pressure level, PS/ HFC-152a volume swelling decreases as the temperature
increases. This could be seen clearly from those above figures. For example, at the 800 psi
pressure level, 1500C PS/ HFC-152a has the higher volume swelling. At higher temperatures,
although the liquid-polymer is softer and more relaxed, the solubility of HFC-152a decreases as
the temperature increases[284] and the overall polymer/gas volume decreases, thereby, the
volume swelling drops.
6.4 Validity of Equation of States Using Experimental Results
6.4.1 Volume Swelling From EOS Predictions
As mentioned earlier, the volume swellings have been often predicted using EOS based
on thermodynamic principles. The materials used in the experiment were the same and the
temperature and pressure parameter settings were similar to the ones used in the EOS for the
predictions. The following figures show all of the comparisons between experimentally
measured swelling ratios with SL and SS EOS predictions at different temperatures for both
linear PP/CO2 and branched PP/CO2 solutions.
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Figure 6-10, Figure 6-11 and Figure 6-12 show the comparisons for linear PP/CO2 with
SL and SS EOS predictions at 180oC, 200oC and 220oC, respectively.
500 1000 1500 2000 2500 3000 3500 4000 4500 50001.00
1.05
1.10
1.15
1.20
1.25
1.30
1.35
1.40
1.45
1.50
1.55
1.60
Swel
ling
Rat
io
Pressure (psi)
180oC SL Swelling 180oC SS Swelling 180oC PVT Exp. Swelling
Figure 6-10 Linear PP/CO2 and EOS Swelling at 180oC
500 1000 1500 2000 2500 3000 3500 4000 4500 50000.95
1.00
1.05
1.10
1.15
1.20
1.25
1.30
1.35
1.40
1.45
1.50
1.55
Volu
me
Swel
ling
Pressure (psi)
200oC SL Swelling 200oC SL Swelling 200oC PVT Exp. Swelling
Figure 6-11 Linear PP/CO2 and EOS Swelling at 200oC
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500 1000 1500 2000 2500 3000 3500 4000 4500 50000.95
1.00
1.05
1.10
1.15
1.20
1.25
1.30
1.35
1.40
1.45
1.50
1.55
Volu
me
Swel
ling
Pressure (Psi)
220oC SL Swelling 220oC SS Swelling 220oC PVT Exp. Swelling
Figure 6-12 Linear PP/CO2 and EOS Swelling at 220oC
The following Figure 6-13, Figure 6-14 and Figure 6-15 show the comparisons for
branched PP/CO2 with SL and SS EOS predictions at 180oC, 200oC and 220oC, respectively.
500 1000 1500 2000 2500 3000 3500 4000 4500 5000
1.00
1.05
1.10
1.15
1.20
1.25
1.30
1.35
1.40
1.45
Volu
me
Swel
ling
Pressure (Psi)
180oC SL Swelling 180oC SS Swelling 180oC PVT Exp. Swelling
Figure 6-13 Branched PP/CO2 and EOS Swelling at 180oC
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500 1000 1500 2000 2500 3000 3500 4000 4500 5000
1.00
1.05
1.10
1.15
1.20
1.25
1.30
1.35
1.40
1.45
Volu
me
Swel
ling
Pressure (psi)
200oC SL Swelling 200oC SS Swelling 200oC PVT Exp. Swelling
Figure 6-14 Branched PP/CO2 and EOS Swelling at 200oC
500 1000 1500 2000 2500 3000 3500 4000 4500 50000.95
1.00
1.05
1.10
1.15
1.20
1.25
1.30
1.35
1.40
1.45
Swel
ling
Rat
io
Pressure (psi)
220oC SL Swelling 220oC SS Swelling 220oC PVT Exp. Swelling
Figure 6-15 Branched PP/CO2 and EOS Swelling at 220oC
As shown in all of the results, at all three temperatures, EOS predictions show increasing
volume swelling as the pressure increases. The SL EOS show a concave upward increasing
trend and the SS EOS show a more linear increase. The experimental volume swelling results
also show the increase of volume swelling as pressure increases. However, the rate of increase,
i.e., the slope of the volume swelling curve, decreases as the pressure increases and starts to
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level off as the pressure goes up to a certain high value at all three temperatures. Disregard the
discrepancies between the SL and SS EOS predictions, for our results show that SL and SS EOS
overestimate the swelling ratio of polymer/gas solutions. The SS EOS predictions are somewhat
close to the experimental measured results. In other words, the SS EOS predictions are better
than SL EOS predictions.
Although those EOS do provide a means to help obtain the volume swelling when a
direct experiment measurement is not available. Due to the limitation of using purely
thermodynamic laws to model and predict the real time molecular movement and interactions,
the discrepancies can not be avoided when compared with the accurately measured values.
Since these EOS have been mainly developed for neat polymers and blends, some modifications
would be required for accommodating the polymer/gas mixture behaviours. It would be to
improve their fitting parameters based on the experimental results so that they could make better
predictions. Further experiments and theoretical work need to be conducted to make these
results fit well with EOS.
6.4.2 Polymer Chain Entanglement Hypothesis
6.4.2.1 Introduction It seems that there is an upper limit for polymer/gas volume swelling, based on the
obtained volume swelling results in the previous figures. It is then hypothesized that due to the
polymer chain entanglement, the volume swelling of polymer/gas (linear PP/CO2 and branched
PP/CO2), solutions would eventually reach a plateau at some high pressure ranges even greater
than 4500psi, which is the highest pressure tested in the experiment. The chain entanglement
would have similar effects on the volume swelling regardless of the polymer chain structure.
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By comparing the experimental volume swelling to the EOS predicted values, it is seen
that the experimentally measured volume swelling would not increase indefinitely with the
increase of the pressure. The experimental volume swelling results also show the increase of
volume swelling as the pressure increases, but the rate of increase, i.e., the slope of the volume
swelling curve, decreases as the pressure increases and starts to level off as the pressure goes up
to a certain high value at all three temperatures.
The same phenomena were also observed from the branched PP/CO2 volume swelling. It
is, then, hypothesized that the polymer chain entanglement would eventually be the determining
factor as postulated previously in the study of volume swelling of linear PP/CO2 mixture.
Wissinger et al. reported similar behaviors of volume swelling and sorption that began to level
off and reached limiting values for PC/CO2 and PMMA/CO2 systems at low temperatures of
about 35oC and 32.7oC, respectively, when the pressure was in the range of 70 atm to 100 atm.
Besides the possible increased hydraulic effect at higher pressures, it is contemplated
that due to the polymer chain entanglement, the polymer matrix would not be stretched
indefinitely unless the internal force is strong enough to break the chain entanglement. In other
words, there is an upper limit for the volume of polymer to expand because of the constraint
posed by the polymer chain entanglement. An entanglement is visualized as the looping of a
portion of one polymer chain backbone about another polymer chain and the entanglement
density is the number of entanglement junctions per unit volume and is calculated through
Equation (6-9). The entanglement junctions confine the motion of chain molecules under
applied stress as transient ‘cross-link’ point. Chain entanglement is an important feature of
polymers, which is one of the factors controlling rheological, viscoelastic, solid mechanical and
adhesive properties of polymers.
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The effects of the entanglement on viscosity and elasticity[285], intrinsic brittleness and
toughness[286], and deformation mechanism[287,288] have been reported. It will be important to
investigate how the entanglement limits the swelling of polymer melts. The simple approach is
to obtain and compare the chain entanglement densities of linear and branched PP at
temperatures above their melting point. The polymer chain entanglement density could be
measured at zero-shear viscosity of the polymer melt using the dynamic rheometer analysis.
In our PVT experiment, since the gas dissolution process is fairly steady
macroscopically, there is no significant shear applied onto the polymer matrix. Therefore, it is
feasible to use a rotational rheometer to conduct the zero-shear viscosity measurement. At very
low frequencies, such as 10-4 Hz, it is assumed that there is almost no shear applied to the
polymer melt using the rotational rheometer and that the viscosity measured at this point would
be considered as the zero-shear viscosity. As the frequency increases, the polymer chain
undergoes stress release and the polymer long chain molecules then expand and relax over time
and the dense polymer chain entanglement will then be greatly released. Thus, the viscosity, and
the resistance to flow the polymer melt, would be dramatically reduced. This is the so-called
shear thinning effect.
6.4.2.2 Small Amplitude Oscillatory Shear Method
The small amplitude oscillatory shear (SAOS) is the method generally used to determine
the LVE properties of molten polymers. This type of test can be done in either strain- or
stress-controlled mode. The features of this SAOS experiment is shown in the following Figure
6-16[289].
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Figure 6-16 Schematic of SAOS Experiment Wave
For SAOS in strain-controlled mode, a sinusoidal strain is imposed on the sample:
( ) ( )tt ωββ sin0= (6-1)
where 0β is the strain amplitude, and ω is the frequency. If 0β is sufficiently small, the
resulting stress is also sinusoidal with a phase angle ψ :
( ) ( )ψωσσ += tt sin0 (6-2) whereσ is the stress amplitude. The amplitude ratio is defined as
00 / βσ≡dG (6-3)
The storage modulus 'G and loss modulus ''G are:
( )ψcos'dGG = (6-4)
( )ψsin''dGG = (6-5)
( ) ωψωη /cos/''dGG == (6-6)
( ) ωψωη /sin/''''dGG == (6-7)
The absolute value of the complex viscosity is:
( ) ( )[ ] ( )[ ]2''2' ωηωηωη +=∗ (6-8)
6.4.3 Experimental Procedure and Materials
Rotational rheometers are widely used to measure the rheological properties due to their
simplicity and easy operation. The Advanced Rheometric Expansion System (ARES) rotational
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rheometer is utilized to measure the complex viscosity (Eta’), the storage shear modulus (G’)
and the loss modulus (G”). There are two tests conducted in order to obtain that data. The first
test is the dynamic stain sweep to determine the linear regime since the maximum strain for
linear viscoelastic behaviours varies with frequency, temperature and polymer. The second test
is the dynamic frequency sweep test where the selected frequency range is applied to the sample
above the melting point. Figure 6-17 shows a picture of the rheometer used in this study.
Figure 6-17 ARES Rheometer
The material used is PS 685D from Dow Chemical. The key procedures of using the
rhometer are described in the following and the step procedure is attached in Appendix 4.
6.4.3.1 Sample Preparation
Since the parallel disk is used in the rheometer as the sample platform, the disk-shape
sample is therefore needed to be prepared prior the measurement. The most convenient method
of sample-disk preparation is compression molding. The compression molding method
minimizes the strain and thermal histories of the polymer sample under the high temperatures
above the melting point. The big round disk sample is prepared and then cut into small pieces to
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fit between those parallel disks of the rheometer. The linear and branched PP samples were
molded at 165oC using a stainless steel mold plate with a diameter of 100 mm and a 2.0 mm
thickness. The thickness of the mold is important because the sample must be slightly thicker
than the rheometer gap, but thin enough to avoid a large normal force during the sample loading.
6.4.3.2 Gap Zeroing
Variations in temperature and removal of the fixture can change the zero position of the
upper plate. Therefore, the gap must be corrected for each experiment and at each temperature.
Both the fixtures and the instrument frame will expand until they reach thermal equilibrium, and
this affects the gap. To avoid problems arising from non-equilibrium thermal behaviours, the
chamber is also preheated to the experimental temperature for several hours prior to zero the gap.
The ARES require gas flow to heat up the system, and air is used instead of nitrogen to reduce
operating costs.
Initial zeroing is carried out by setting the gap to zero after lowering the upper fixture up
until it touches the bottom plate. The upper fixture plate is first lowered manually to a position
very close to the bottom plate. Then the “zero” button in the GUI interface is pressed. The
fixture automatically moves to touch the bottom plate. Touching is confirmed by monitoring the
normal force, as well as the gap value displayed on the GUI interface. The software from ARES
will confirm when the gap between the two plates becomes zero from its online monitor
software. A sample must be loaded carefully to avoid air bubbles between the sample and the
lower plate. After placing the sample on the plate, it is pushed down in the center and a spatula
is used to sweep the bubbles from the center to the rim. Before setting the desired gap, the edge
of the sample is trimmed with the gap set slightly larger than its final value. The step-by-step
procedure for sample loading and gap zeroing is as follows:
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There were a total of 6 experiments that were carried out to do the measurements since we had
to run each material with three different temperatures, namely, 180oC, 200oC and 220oC. Those
temperature settings followed exactly with our PVT experiment so that we could really correlate
the polymer chain entanglement density with our postulated hypothesis.
6.4.4 Chain Entanglement of Linear and Branched PP 6.4.4.1 Strain Sweep and Frequency Test
There were two tests carried out to obtain the data. The first test was the dynamic stain
sweep to determine the linear regime since the maximum strain for linear viscoelastic
behaviours varies with frequency, temperature and polymer. Figures 6-18 and 6-19 show the
strain sweep test results for both linear and branched PP polymers. An important piece of
information extracted from those results was the maximum strain of those materials. The
technique for checking the values is to look for the time where the G’ and G’’ start to change. It
is easy to figure out from the graphs that at the beginning, the values of G’ and G’’ were steady
while the strain value kept increasing. At the time when the strain value passed 10, big changes
started to show for both G’ and G’’. Therefore, the value 10 was the maximum strain picked for
both of the materials as being the strain input for the frequency sweep test.
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10-2 10-1 100 101 102104
105
100
101
Strain [%]
G' (
)
[Pa]
G" (
)
[Pa]
tan_delta ()
[ ]
LPP Strainsweep
Figure 6-18 Linear PP Strain Sweep Test
10-1 100 101 102104
105
10-1
100
101
Strain [%]
G' (
)
[Pa]
G" (
)
[Pa]
tan_delta ()
[ ]
BPP Strainsweep
Figure 6-19 Branched PP Strain Sweep Test
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The second test was the dynamic frequency sweep test, where the selected frequency
range was applied to the sample above melting point. The frequency test result plots are shown
from Figure 6-20 to Figure 6-25. The first three figures are the results for linear PP.
10-4 10-3 10-2 10-1 100 101 102100
101
102
103
104
105
106
102
103
104
105
Freq [Hz]
G' (
)
[Pa]
G" (
)
[Pa] Eta* (
) [Pa-s]
LPP_180oC_frequencysweep
Figure 6-20 Linear PP 180oC Frequency Sweep Test
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10-3 10-2 10-1 100 101 102100
101
102
103
104
105
106
102
103
104
105
Freq [Hz]
G' (
)
[Pa]
G" (
)
[Pa] Eta* (
) [Pa-s]
LPP_200oC_frequencysweep
Figure 6-21 Linear PP 200oC Frequency Sweep Test
10-4 10-3 10-2 10-1 100 101 102
100
101
102
103
104
105
106
102
103
104
105
Freq [Hz]
G' (
)
[Pa]
G" (
)
[Pa] Eta* (
) [Pa-s]
LPP_220oC_requencysweep
Figure 6-22 Linear PP 220oC Frequency Sweep Test
The following three are the frequency sweep test for branched PP at all three
temperatures.
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10-4 10-3 10-2 10-1 100 101 102101
102
103
104
105
102
103
104
105
Freq [Hz]
G' (
)
[Pa]
G" (
)
[Pa] Eta* (
) [Pa-s]
BPP_180oC_frequencysweep
Figure 6-23 Branched 180oC Frequency Sweep Test
As expected, the results from those plots showed that the complex viscosity of both the
linear and branched PP had decreased as the frequency increased. Duo to the limitation of the
frequency range of the rheometer and the time required to run extremely low frequencies, the
frequencies were chosen to start from 5x10-3 instead of from 10-4. From the graphs it is easy to
see that the complex viscosity tended to have plateaus at really low frequencies. This was
especially shown in the linear PP frequency test. At those plateaus, we could extract the value
for the corresponding G’ values from the graph.
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10-4 10-3 10-2 10-1 100 101 102101
102
103
104
105
102
103
104
105
Freq [Hz]
G' (
)
[Pa]
G" (
)
[Pa] Eta* (
) [Pa-s]
BPP_200oC_frequencysweep
Figure 6-24 Branched PP 200oC Frequency Sweep Test
10-4 10-3 10-2 10-1 100 101 102
101
102
103
104
105
102
103
104
105
Freq [Hz]
G' (
)
[Pa]
G" (
)
[Pa] Eta* (
) [Pa-s]
BPP_220oC_frequencysweep
Figure 6-25 Branched PP 220oC Frequency Sweep Test
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6.4.4.2 Chain Entanglement of Linear and Branched PP
Liu et al. [288] has studied the deformation mechanism of polyphenylquinoxaline (PPQ-E)
film using theoretical prediction and microscopic observation. The entanglement density,
estimated from the plateau modulus on the dynamic mechanical property curves, was used to
predict the deformation mechanism of PPQ-E. One of the commonly used equations to calculate
the chain entanglement density is as following[290,291]:
RT
GNV
nA
e0= (6-9)
Where NA is Avogadro constant, R is the gas constant and nG0 is the plateau modulus of the
melt at temperature T. From the measurement results, the nG0 is the G’ modulus from the
rheometer results at corresponding plateau of the complex viscosity. The polymer chain
entanglement densities of both linear and branched pp are plotted in Figure 6-26.
170 180 190 200 210 220 2301E20
1E21
1E22
1E23 Linear PP Branched PP
Cha
in E
ntan
glem
ent D
ensi
ty (m
-3)
Temperature (oC)
Figure 6-26 Linear and Branched PP Chain Entanglement Density at T above Tm
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Figure 6-26 showed that both linear PP and branched PP has high chain entanglement
density although the entanglement density of linear PP is one magnitude smaller than that of
branched PP. When temperature increases, the chain entanglement density decreases for both
linear and branched PP. At each fixed temperature, since the chain entanglement density of
linear is smaller than branched PP, the volume swelling of linear PP should be higher than
branched PP which is indeed the results obtained. Due to the high chain entanglement density of
both linear and branched PP, there may be an upper limit for the ultimate expandability of the
polymer chains. In another word, the existence of such a highly entangled polymer chains in
both linear and branched PP may prevent the polymer chains being stretched or deformed
indefinitely under high shear. During the PVT experiment, the only possible shear can be
generated is from the volume swelling due to gas dissolution which is so small and can not
overcome the highly entangled chains. Therefore it is hypothesis at some high pressure ranges,
with the effect from high chain entanglement the volume swelling is going to reach plateau. It is
also predicted the swelling of branched PP will reach the plateau first compared with linear PP
because of higher chain entanglement density.
6.5 Determination of Accurate Solubility Based on the PVT Data
6.5.1 Corrected PP/CO2 Solubility from PVT Measurement
How the magnetic suspension balance (MSB) is used to measure the solubility of gas
inside the polymer and how the EOS has been used to help the measurement in providing
predicted volume swelling, have been introduced in Chapter 3. In this section, using the
experimentally measured volume swelling to help obtain more accurate solubility data is
elaborated. The corrected solubility is also going to be compared with those corrected from the
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EOS. To begin, a brief derivation is needed on how to derive the solubility correction from the
MSB apparatus.
The read-out from the balance at the vacuum condition (P=0) and this specific
temperature (T) was denoted as ( )TW ,0 . When the equilibrium state is reached inside the
sorption chamber with the presence of pressurized blowing agents, the sample mass will not
change unless a high pressure is introduced by having more compress gas go into the sorption
chamber. At that particular pressure (P) and temperature (T), the weight read-out of the balance
is noted as ( )TPW , . Therefore, the amount of gas that is dissolved into the polymer at each
pressure and temperature condition is denoted as gW and is calculated through the following
equation:
( ) ( ) ( )sPBgasg VVVTWTPWW +++−= ρ,0, (6-10)
Where gasρ is the density of the gas and can be measured in situ by the function of MSB; BV
is the volume of the sample holder, including the sample container and the measuring load
coupling devices shown in the Figure 1-5. This volume is determined using the buoyancy
method with the high-pressure gas; and PV is the volume of the pure polymer sample at
pressure P and temperature T. This volume can be determined from the PVT equation of pure
polymer plus the weight of the polymer sample. The sV is the swollen volume of the
polymer/gas mixture due to the gas dissolution. If this swollen volume term becomes ignored,
then the reading of the balance will be the so-called “apparent” solubility of the polymer/gas
solution. Next, the measured weight gain is defined as the apparent weight gain through the
following equation:
( ) ( ) ( )PBgasapparentg VVTWTPWW ++−= ρ,0,, (6-11)
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The apparent solubility, apparentX can be determined from the above equation as:
masssampleapparentgapparent mWX /,= (6-12)
In order to get an accurate solubility data, volume swelling has to be taken into account. After
obtaining more accurate and true volume swelling from the direct measurement using our PVT
apparatus, the apparent solubility can be corrected as true or accurate corrected solubility as:
masssample
sgasapparentcorrected m
VXX
∗+=
ρ (6-13)
From the definition of the volume swelling in equation (4-11), the swollen volume sV which
occurs due to gas dissolution, can be interpreted as the initial sample volume multiple the
swelling ratio:
( )1* −= wvolumesampleinitals SVV (6-14)
Combine the above equation 6-13 and 6-14, and the corrected solubility could be simplified into
the following equation:
( ) purepwgasapparentcorrected SXX ,1 υρ ∗−∗+= (6-15)
where purep,υ is the specific volume of the pure polymer sample and can be calculated
through the Tait equation. With all of the mathematics in hand, the corrected solubility is
determined from the measured volume swelling, as well as from the apparent solubility obtained
from the MSB experiment. Since the temperature and pressure settings are almost the same for
both MSB solubility and PVT measurement, the swelling ratio measured from the PVT
apparatus were directly used in the MSB measurement without major data correlation.
In each of the following figures, the apparent solubility is shown as a black square
symbol. SL and SS EOS corrected solubility are shown as purple circles and blue triangle
respectively. The experimentally corrected solubility based on equation 6-15 is represented as a
red triangle. For linear PP/CO2 solutions, the result plots are shown from Figure 6-27 to Figure
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6-29. At pressures below 3000psi, the corrected solubility using experimental swelling is very
close to the SS EOS corrected solubility. When the pressure increases higher to above 3000 psi,
the corrected solubility from the experimental swelling becomes smaller due to small volume
swelling at high pressures, which contributes to a lesser buoyancy effect. This is more clearly
illustrated at higher temperatures, such as 200oC and 220oC. Very similar to the volume swelling
comparison between the SL and SS EOS prediction, the SL correction shows a concave inward
increase of solubility as the pressure increases at each temperature and the SS correction shows
a more linear trend of the solubility when the pressure kept increasing. The experimental
corrected solubility follows the same trend as the measured volume swelling, in that it shows the
signs of levelling off at high pressures and it also indicates that the solubility would likely reach
a plateau when the pressure increases indefinitely. In other words, it implies that when the “CO2
absorbing” capacity of the polymer matrix is reached or the polymer matrix is totally saturated
with CO2 , there is no place for the polymer matrix to stretch and the solubility limit would then
be reached at some high pressure levels.
500 1000 1500 2000 2500 3000 3500 4000 4500 50000.0250.0500.0750.1000.1250.1500.1750.2000.2250.2500.2750.3000.3250.3500.3750.4000.4250.450
Solu
bilit
y (g
-gas
/g-p
olym
er)
Pressure (psi)
180oC Apparent Solubility 180oC Exp. Corrected Solubility 180oC SS Corrected Solubility 180oC SL Corrected Solubility
Figure 6-27 Corrected Linear PP/CO2 Solubility at 180oC
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500 1000 1500 2000 2500 3000 3500 4000 4500 50000.0250.0500.0750.1000.1250.1500.1750.2000.2250.2500.2750.3000.3250.3500.3750.4000.4250.450
Solu
bilit
y(g-
gas/
g-po
lym
er)
Pressure (psi)
200oC Apparent Solubility 200oC Exp. Corrected Solubility 200oC SS Corrected Solubility 200oC SL Corrected Solubility
Figure 6-28 Corrected Linear PP/CO2 Solubility at 200oC
500 1000 1500 2000 2500 3000 3500 4000 4500 50000.020.040.060.080.100.120.140.160.180.200.220.240.260.280.300.320.340.360.380.400.42
Solu
bilit
y(g-
gas/
g-po
lym
er)
Pressure (psi)
220oC Apparent Solubility 220oC Exp. Corrected Solubility 220oC SS Corrected Solubility 220oC SL Corrected Solubility
Figure 6-29 Corrected Linear PP/CO2 Solubility at 220oC
For the branched PP/CO2 solutions case, a similar conclusion can be drawn based on the
results shown in Figure 6-30, Figure 6-31 and Figure 6-32. Both SL and SS corrected solubility
showed concave inward and linear increase trends, but the experimental corrected solubility
showed the trend of reaching a plateau if the pressure kept increasing. Again, in the case of
200oC and 220oC at pressures below 3000psi, the corrected solubility using experimental
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swelling was very close to the SS EOS corrected solubility. When the pressure increased higher
to above 3000 psi, the corrected solubility from the experimental swelling became smaller due
to volume swelling limitation at high pressures.
500 1000 1500 2000 2500 3000 3500 4000 4500 50000.025
0.050
0.075
0.100
0.125
0.150
0.175
0.200
0.225
0.250
0.275
0.300
0.325
Solu
bilit
y (g
-gas
/g-p
olym
er)
Pressure (psi)
180oC Apparent Solubility 180oC Exp. Corrected Solubility 180oC SS Corrected Solubility 180oC SL Corrected Solubility
Figure 6-30 Corrected Solubility of Branched PP/CO2 at 180oC
500 1000 1500 2000 2500 3000 3500 4000 4500 50000.025
0.050
0.075
0.100
0.125
0.150
0.175
0.200
0.225
0.250
0.275
0.300
0.325
Solu
bilit
y (g
-gas
/g-p
olym
er)
Pressure (psi)
200oC Apparent Solubility 200oC Exp. Corrected Solubility 200oC SS Corrected Solubility 200oC SL Corrected Solubility
Figure 6-31 Corrected Solubility of Branched PP/CO2 at 200oC
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500 1000 1500 2000 2500 3000 3500 4000 4500 50000.025
0.050
0.075
0.100
0.125
0.150
0.175
0.200
0.225
0.250
0.275
0.300
0.325
Solu
bilit
y (g
-gas
/g-p
olym
er)
Pressure (psi)
220oC Apparent Solubility 220oC Exp. Corrected Solubility 220oC SS Corrected Solubility 220oC SL Corrected Solubility
Figure 6-32 Corrected Solubility of Branched PP/CO2 at 220oC
In summary, the SL EOS corrected solubility has a bigger discrepancy with the SS EOS
and experimentally corrected solubility. The SS EOS corrected solubility is similar to
experimental corrected solubility only at pressures below 3000psi. Due to the polymer chain
structure and chain polymer entanglement, the results have shown a limited volume swelling at
higher pressures and the hypothesis postulated previously states that there is an upper cap for the
volume to expand with the gas dissolution. Therefore, this would be reflected in the final
solubility correction. Not surprisingly, the experimentally corrected solubility indicates that
there indeed exists an upper limit for gas solubility as well. The conclusion is clearly illustrated
in all of the figures. Despite the discrepancy between the SL, SS EOS corrected solubility and
experimental corrections; the directly measured swelling data from the PVT apparatus enabled
us to not rely on the EOS prediction while obtaining accurate solubility data.
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6.5.2 Specific Volume of Linear/Branched PP/CO2
With the accurately measured volume swelling of the PP/CO2 solution that is due to the
CO2 dissolution, the buoyancy effect from the solubility measurement using MSB could be
compensated more precisely to obtain more accurate solubility information of the CO2 in the PP
matrix. This is done in the previous section using the measured swelling to get the true
corrected solubility information. This is also the reason why this section in particular is placed
right after the apparent solubility is corrected, since the determination of the mixture specific
volume required the final solubility of the polymer to be known.
With the amount of the CO2 gas dissolved in the PP matrix that were determined, the
equation used in determined the corrected solubility could be used agai to help derive the
equations to calculate the density information for the PP/CO2 solution at high temperatures and
pressures. The definition of the volume swelling ratio is again reiterated here as:
( )
( )
( )
PPsample
tPT
tPT
tPTw m
V
V
VSRatioSwellingVolume eq
ini
eq
υ*,,
,,
,,== (6-16)
Therefore, the swollen volume which occurs due to gas dissolution, can be expressed as the
difference between the initial sample volume and the final equilibrium polymer/gas solution
volume shown in the following equation (6-2):
( ) ( )inieqs tPTVtPTVV ,,,, −= (6-17) where V(T,P,teq) is the measured equilibrium polymer/gas solution volume at temperature T,
pressure P, and equilibrium time teq. The V(T,P,tini) is the volume of the neat PP sample
calculated at temperature T, pressure P using the Tait equation. The measured volume of
polymer/gas solution is:
( ) mixturepmixtureeq mtPTV ,,, υ∗= (6-18)
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The initial sample volume is calculated as the following:
( ) purepsampleini mtPTV ,,, υ∗= (6-19)
In addition, the mixture mass of the polymer/gas solution is the summation of the initial polymer
sample mass and the dissolved gas amount:
2cosamplemixture mmm += (6-20)
2com is the dissolved CO2 inside the polymer matrix and samplem is the initial polymer sample
mass. The final corrected solubility from MSB is defined as:
sample
co
mm
s 2= (6-21)
Substitute equation (6-6) into (6-3), the final measured volume is expressed as:
( ) ( ) mixturepsampleeq smtPTV ,1,, υ∗+= (6-22) The initial volume calculated from the Tait density and initial sample mass is already expressed
in equation (6-4). Therefore, equation (6-2) can be rewritten to describe swollen volume due to
gas dissolution as:
( )[ ]purepmixturepsamples smV ,,1 υυ −∗+= (6-23) And the specific volume of the mixture could be obtained by rearranging the above equation
(6-9) as:
( )sS purepw
mixturep +
∗=
1,
,
υυ (6-24)
The s in the above equations is the same term as X corrected in equation (6-15). Therefore a
simple substitution would help in getting the final formula for obtaining the equilibrium
polymer/gas mixture specific volume as:
( )[ ]purepwgasapparent
purepwmixturep SX
S
,
,, 11 υρ
υυ
∗−++
∗= (6-25)
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In equation (6-25), apparentX and gasρ are directly measured from the MSB apparatus, wS is the
volume swelling ratio obtained directly from the PVT apparatus. The purep,υ is the specific
volume of a pure polymer sample that can be calculated reliably from the Tait equation.
Therefore, currently the prediction of volume swelling from those EOS is not needed to for
solubility measurement using MSB. The only thing needed is the volume swelling information
for the PVT measurement. All other relevant information, such as the corrected solubility of gas
in the polymer, the density of the polymer/gas solution, can be obtained through equations 6-15
and 6-25 respectively.
Figure 6-33, Figure 6-34 and Figure 6-35 showed the specific volume of linear and
branched PP/CO2 solution verse CO2 gas pressure at each individual temperature.
500 1000 1500 2000 2500 3000 3500 4000 4500 50001.22
1.24
1.26
1.28
1.30
1.32
1.34
1.36
1.38
180oC Linear PP/CO2
180oC Branched PP/CO2
Spec
ific
Volu
me
(cm
3 /g)
Pressure (psi)
Figure 6-33 Specific Volume of LPP/CO2 and BPP/CO2 at 180oC
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500 1000 1500 2000 2500 3000 3500 4000 4500 50001.22
1.24
1.26
1.28
1.30
1.32
1.34
1.36
1.38 200oC Linear PP/CO2
200oC Branched PP/CO2
Spec
ific
Volu
me
(cm
3 /g)
Pressure (psi)
Figure 6-34 Specific Volume of LPP/CO2 and BPP/CO2 at 200oC
500 1000 1500 2000 2500 3000 3500 4000 4500 50001.22
1.24
1.26
1.28
1.30
1.32
1.34
1.36
1.38 220oC Linear PP/CO2
220oC Branched PP/CO2
Spec
ific
Volu
me
(cm
3 /g)
Pressure(psi)
Figure 6-35 Specific Volume of LPP/CO2 and BPP/CO2 at 220oC
All three figures show that linear PP/CO2 have a high specific volume compared with
branched PP/CO2. This is expected because of higher volume swelling ratios observed in the
former compared with the latter. For the same amount of polymer sample, even the CO2 has
higher solubility in linear PP than in branched PP, the increase of the volume outweighs the
mass increase due to the dissolution of the CO2 gas; Therefore, the specific volume is higher
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for linear PP/CO2 solutions. At 180oC and 200oC, both linear and branched PP/CO2 saw a slight
increase of specific volume at low-pressure ranges, from 1000 psi to 2000 psi. The specific
volume then decreased steadily after, from 2500 psi and onwards. This can be explained by
two factors: 1) the decrease of the volume swelling rate as the pressure increases, 2) the increase
of the CO2 density as the pressure increases
When the pressure keeps increasing above 2500psi, the increase of volume swelling is
getting smaller. The apparent solubility and the CO2 density increase as the pressure increases.
From equation 6-25, with an increase in the value of denominator and a decrease from the
numerator, the net result is the decrease mixture specific volume. In another word, the increase
in the mixture weight due to heavier CO2 dissolution is higher than the increase in the mixture
volume due to an already slowdown volume swelling, which resulted in a decrease in mixture
specific volume.
In addition, as mentioned in an earlier section, at higher pressures, the hydraulic effect
could also be one of the contributing factors.
6.6 Summary
Chapter 6 mostly focused on the study of PVT properties, such as volume swelling and
the corrected solubility of both linear and PP/CO2 solutions at high temperatures and pressures.
The temperatures were at 180oC, 200oC and 220oC and the pressure started from 1000psi to
4500psi. The results showed that the volume swelling increased as the pressure increased. On
the other hand, the increase in temperature resulted in a decrease in volume swelling for both
linear and branched PP/CO2 solutions. Some of the linear PP/CO2 swelling results and detailed
discussions are already published[292].
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Due to the long chain branching (LCB) effect, the branched PP showed significantly less
volume swelling in all temperatures and pressures. It was discovered that at each fixed
temperature, the rate of volume swelling decreased as the pressure increased and there existed a
plateau or upper limit for the volume swelling of linear PP and branched PP/CO2 solutions. This
phenomenon then lead to the hypothesis made in this study that states that due to the polymer
chain structure and chain entanglement density, there was an upper limit for polymer/gas
volume swelling at high pressures. In the rheometer test conducted for linear and branched PP at
180oC, 200oC and 220oC, the results showed that branched PP had much higher chain
entanglement density than linear PP.
The volume swellings from the measurements were also compared with SL and SS EOS
prediction values for both linear and branched PP. It showed that both SL and SS predicted
continuously increasing volume swelling as the pressure increased at constant temperatures. The
discrepancy between SS EOS predictions with measured values was the smallest.
The corrected solubility data from both experiments and EOS were also plotted. The
results also indicated that the solubility tended to reach some plateaus as the pressure increased
for both linear and branched PP cases.
Experiments were carried out to investigate the effect of shape asymmetry of amorphous
PS at three different temperatures and vacuum conditions. The results demonstrated strongly
that as the temperature increased, the drop shape becomes more asymmetric and the results were
more accurate. In addition, the results from Figure 6-8 showed that the rotational device helped
to compensate or eliminate the effect of asymmetry, which would facilitate accurate PVT
measurement of asymmetric polymer drop sample. The PS/CO2 PVT showed that as the
temperature increased, the PS/CO2 had less swelling, but the swelling increased as the pressure
increased.
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Due to the need for exploring more environmentally-friendly gas blowing agents, the
HFC-152a was used to study its PVT behaviour with PS solutions at high temperatures but with
relatively low pressures of up to only 800psi. At low pressures, the swelling of PS/HFC-152a
showed concave increasing trend as the pressure increased.
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Chapter 7. Measurement of Surface Tension for Polymer/Gas Solutions
7.1 Introduction
The surface (interfacial) tension of polymer melts is an important thermodynamic
parameter and it plays a key role in many polymer processing applications such as foaming,
blending, coating and wetting. The effort to understand and control processes involving these
applications would benefit from a better understanding of events at the molecular level.
However, the high viscosity and the limited thermal stability of polymer melts as well as the
difficulties in carrying out experimental studies due to high temperature and pressure
requirement, accurate and reliable experimental data are often not available.
Supercritical fluids are well established as a processing solvent in various polymer
applications such as foaming, blending, modification, composites formation, particle production
and polymerization. Supercritical carbon dioxide (SF-CO2) is becoming an increasingly
interesting foaming agent in the production of microcellular polymer foams.[131,293] In order to
form polymeric foam, bubbles must first nucleate and grow within the molten or plasticized
material. The initial nucleation is induced by a change in thermodynamic instability either
through temperature increase or pressure drop. During this process, a second phase is
generated from a metastable polymer/gas homogeneous mixture. According to the classical
nucleation theory[136], properties such as diffusivity (D), gas concentration (c), surface tension
(γ), temperature (T), and degree of supersaturation are the parameters controlling the nucleation
rate, N:
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⎥⎦
⎤⎢⎣
⎡Δ
−= 2
3
316exp
PkTcfN πγ
(7-1)
Particularly, relationships between surface tension and foaming are of great interest, as foaming
is strongly influenced by the surface tension of polymer. The energy barrier of the cell
nucleation can be lowered by lowering the surface tension. The free energy barrier equation is
brought back here again as follows:
( )23
316
systembuble PPW
−=
πγ (7-2)
As a polymer-gas mixture has a lower surface tension than that of the pure polymer, the
Gibbs free energy for the formation of a nucleus will be reduced in cubic power of the surface
tension, and in turn will cause the nucleation rate to increase exponentially. Therefore,
understanding and controlling the surface tension of polymer/gas solution is important for
optimizing the foaming process. However, although some data about the surface tension in pure
polymer at elevated pressures have been reported, only a little fundamental knowledge on the
surface tension of the polymer/gas solution is available because of the experimental difficulties
in performing measurements on highly viscous polymer liquids at high pressure and
temperature.
Jaeger et al.[291] investigated the interfacial properties of high viscous polystyrene (PS) in
supercritical CO2 at pressure up to 25 MPa. Dimitrov et al.[290] found the interfacial tension of
poly(ethylene glycol)nonylphenyl ether (PEG-NPE)-CO2 to be a linear function of CO2 density
up to 800 kg/m3. Enders et al.[294] used Cahn-Hilliard theory in combination with equations of
state (the original statistical associating fluid theory (SAFT), the perturbed-chain statistical
associating fluid theory (PC-SAFT) or the Sanchez-Lacombe (SL) lattice theory) to describe the
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temperature and pressure dependence of the interfacial properties between PS-gas mixture and
the pure gas phase. However, it was not possible to predict the interfacial tension in
quantitative agreement with experimental data. The theoretical framework needs further
improvement with respect to the polydispersity of the polymer.
Park et al.[25-27] and Li et al.[61] recently used Axisymmetric Drop Shape Analysis (ADSA)
to determine the surface tension of polymer melt in supercritical fluids, such as supercritical
CO2 and supercritical nitrogen (N2). The ASDA approach relies on a numerical integration of
the Laplace equation of capillarity.[295] During this procedure, the density difference between
polymer-supercritical fluids mixtures and the supercritical fluids was an input parameter.[296]
One of the most important requirements for the accurate calculation of the interfacial tension of
binary systems is the correct calculation of the densities of the coexisting phases. As
mentioned in previous chapters, Sanchez-Lacombe (SL) and Simha-Somcynsky (SS) equation
of state (EOS) were normally applied to estimate the pressure-volume-temperature (PVT) data
of the polymer-supercritical fluids mixtures, which gave the density data. Nevertheless, the
experimental data for the density of polymer-supercritical fluid systems are rather rare.
Funami et al.[86] developed a new method of directly measuring the densities of two
polymer melt-CO2 single-phase solutions, poly(ethylene glycol) (PEG)-CO2 and polyethylene
(PE)-CO2 at high pressure and temperature using a magnetic suspension balance (MSB). A
thin disc-shaped platinum plate was submerged in the polymer-CO2 single-phase solution in the
MSB high-pressure cell. The weight of the plate was measured while keeping temperature and
CO2 pressure in the sorption cell at a specified level. Since the buoyancy force exerted on the
plate by the polymer-CO2 solution reduced the apparent weight of the plate, the density of the
polymer-CO2 mixture could be calculated by subtracting the true weight of the plate from its
measured weight. However, this density measuring method has some limitations on applicable
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polymers. When the plate is moving up and down in the polymer melt during the position
changeover operation, a dragging force is generated. Therefore, the readout can not be
guaranteed when the viscosity of polymer melt is high.
To determine the density of polymer-gas, the solubility of gas in polymer and the
volume of the polymer-gas mixture are required. The volumetric and gravimetric methods
have been widely used to measure the solubility of gas in polymer and polymer blends as
described in Chapter 2 and 3. However, neither the volumetric nor the gravimetric method
alone can generate the accurate solubility data because the gas dissolution in polymer causes
volume swelling in polymer. The correction of volume swelling can be obtained either by
prediction using EOS for polymer, such as Flory EOS,[234] SL EOS, and SS EOS or direct
experimental measurement using the PVT apparatus developed in this research.
7.2 Experimental Materials
Linear PP (DM 55 Borealis, Mn=105,473), branched PP (Daploy WB130HMS Borealis,
Mn=122,395) and CO2 (Coleman grade, 99.99% purity, BOC Canada) were used in this study.
7.3 Measurement of Surface Tension for Linear/Branch PP/Gas Solutions
7.3.1 Surface Tension for Linear/Branched PP/CO2 Solutions
The technique of Axisymmetric Drop Shape Analysis Profile (ADSA-P) was used to
determine the surface tension from the image captured in PVT measurement. Surface tensions
were obtained by fitting the shape and dimensions of the axisymmetric menisci acquired to the
theoretical drop profile according to the Laplace equation of capillarity.
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⎟⎟⎠
⎞⎜⎜⎝
⎛+=Δ
21
11RR
P γ (7-3)
where ΔP is the pressure difference across the curved interface; γ is the surface (interfacial)
tension; R1 and R2 are the principal radii of curvature of the drop. The value of surface tension
was generated as a fitting parameter after a least-squares algorithm was employed to minimize
the difference between experimental drop profiles and theoretical ones.
Within the ADSA formalism, the density was originally introduced through the capillary
constant:
( )
γρ gc ⋅Δ
= (7-4)
where c is the capillary constant; Δρ is the density difference between liquid/fluid interface; g is
the acceleration due to gravity. The determination of c through ADSA would yield the surface
tension while Δρ is a readily available input parameter.
Once the mass of CO2 dissolved in polymer and the volume of the polymer-gas mixture
are known, the density of polymer-gas mixture can be calculated from its volume and mass (sum
of the initial mass of polymer and the mass of dissolved CO2). Then, Δρ is calculated by the
following equation:
gasmixturep ρρρ −=Δ , (7-5)
where ρmixture is the density of polymer-gas solution.
The temperature and pressure dependences of the specific volume for the polymer melt
can be described by the Tait equation:
( ) ( ) ( )[ ]TBPCTVTPV +−= 1ln1,0, (7-6)
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The Tait equations for the specific linear PP and branched PPused in this study were
derived based on the measured PVT behaviour using the bellow type dilatometer[22-24,254] are as
follows, respectively[124]:
10001086.91006.1
1045.61046.7
7
2
9
6
, ×⎟⎟⎠
⎞⎜⎜⎝
⎛+×××
++×
×=
PT
Ppurepυ (7-7)
100010146.110221.1
10773.510485.6
8
2
9
6
, ×⎟⎟⎠
⎞⎜⎜⎝
⎛+×××
++×
×=
PT
Ppurepυ (7-8)
where the specific volume υp,pure is in (cm3/g), the temperature T is in (oC) and pressure P is in
(Pa).
The solubility of CO2 in PP melts was measured gravimetrically using a MSB
(Rubotherm GmbH). When CO2 dissolves in polymer, it swells polymer. Because the
buoyancy caused by the swelling changes during the solubility measurement, to perform
accurate measurement, the weight of dissolved CO2 has to be measured with consideration of
the buoyancy effect:
( ) ( ) ( ) ( )( )spBCOCO VVVPTTWPTWPTW +++−= ,0,,,22
ρ (7-9)
where the balance readout at temperature, T, and pressure, P was recorded as W(T, P), and
vacuum (P ≈ 0) was recorded as W(T, 0). The ρCO2 is the density of gas and can be measured
in situ by the function of MSB. VB is the volume of the sample holder; and VP is the volume of
the pure polymer sample at pressure P and temperature T (without gas), which can be calculated
by evaluating the pure polymer’s PVT equations. VS is the swollen volume of the polymer/gas
mixture due to the gas dissolution. Without considering the swelling effect, the solubility
measured from the read-out of the MSB is denoted as apparent solubility apparentX . This apparent
solubility, apparentX can be determined from the above equation as:
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masssampleapparentgapparent mWX /,= (7-10)
In order to get an accurate solubility data, the volume swelling has to be taken into
account. After obtaining more accurate and true volume swelling from direct measurement
using our PVT apparatus, the apparent solubility can be corrected as true or accurate corrected
solubility as:
masssample
sgasapparentcorrected m
VXX
∗+=
ρ (7-11)
From the definition of the volume swelling in equation (4-15) the swellon volume sV can be
interpreted as the initial sample volume multiply by the swelling ratio:
( )1* −= wvolumesampleinitals SVV (7-12)
Combine the above equation 7-11 and 7-12, the corrected solubility could be simplified into the
following equation:
( ) purepwgasapparentcorrected SXX ,1 υρ ∗−∗+= (7-13)
where purep,υ is the specific volume of pure polymer sample and can be calculated through Tait
equation. With all the mathematics in hand, the corrected solubility is determined from the
measured volume swelling as well as the apparent solubility obtained from the MSB
experiment.
Thus, the corrected CO2 solubility in polymer (WCO2) with buoyancy effect
compensation will be obtained from equation 8. As the mass and volume of polymer-gas
mixture are known, the density of polymer-gas solution phase, ρp,mixture, can be obtained from
purepw
corrected
mixturep
mixturepmixturep S
XVW
,,
,, υ
ρ∗
== (7-14)
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7.3.2 Temperature and Pressure Effect on Surface Tension
Figure7-1 shows the equilibrium surface tension results of linear PP/CO2 system at all
three experimental temperatures and the pressures. First of all, the results show that at each
fixed temperature, the surface tension decreases when the pressure increases. When the pressure
is fixed, the surface tension decreases as the temperature increases. But this conclusion is true
only for pressures up to 2000psi. When the pressure went beyond 2000psi, the surface tension
dependence on temperature dropped dramatically. Those results are similar to what has been
reported in the study of PS/CO2 from Park et al. [25-27]. From the Figure 7-2, they observed that,
in the PS/CO2 system at temperature between 170oC and 210oC, the dependence of surface
tension on temperature becomes less with increasing pressure. When the pressure values reach
above 2000 psi, the dependence diminishes. And it was concluded that increasing temperature is
effective at reducing surface tension only when moderate pressure is applied during a polymer
process from their study. But they did not report the dependence of surface tension on
temperature at higher pressure beyond 2500 psi since their experiments were run at a maximum
pressure of 2500 psi.
180 200 2202
4
6
8
10
12
14
16
18Pressure (psi)
1000 1500 2000 2500 3000 3500 4000 4500
Surf
ace
Tens
ion
(mJ/
m2 )
Temperature (oC)
Figure 7-1 Surface Tension of Linear PP/CO2 at Various Temperatures and Pressures
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From our experimental results, at 2500 psi, the surface tensions across all three
temperatures are similar. When the pressure was increased to 4500psi, the surface tension values
slightly increased when the temperature increased.
Figure 7-2 Equilibrium Surface Tension of PS/CO2 Solution
Figure 7-3 shows the surface tension of branched PP/CO2 at all three temperatures and
pressures up to 4500psi. It further confirms our observation from the linear PP/CO2 case. It is
clearly shown that the surface tension dependence on temperature as in the branched PP/CO2
case follows the exactly same trend as it does in the linear PP/CO2 case. Before the pressure
reaches 2000 psi, the surface tension drops when the temperature increases. The dependence of
surface tension on temperatures diminishes at pressure beyond 2000 psi. On the contrary, the
surface tensions slightly increase at higher pressures when the temperature increases.
When the pressure increases, the surface tension decreases because a higher pressure
would mean that more CO2 gas dissolves into the polymer matrix and the solubility increases.
When gas is dissolved into the polymer melt, the free volume is occupied with gas molecules at
the beginning. When more gas penetrates into the polymer chain, more free volume is created
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accompanied by a plasticizing effect. This leads to an increase of molecular mobility and results
in a decrease of the melt viscosity. This increase in molecular mobility and decrease of the melt
viscosity would lower the surface tension of the polymer/gas mixture system. Moreover, this
increase of solubility due to an increasing in pressure would decrease the free energy of the
polymer/gas solution; hence the surface tension will decrease. Li et al.[61] used the density
gradients theory to model and predict the surface tension relation with pressure for PS/CO2 and
PP/CO2 solutions and it showed that the surface tension decreases dramatically as pressure
increases.
Park et al. [25-27] also modeled the temperature and pressure dependence of surface
tension using the second order linear regression model. It explained that when the pressure
increases, the largest factor causing the surface tension decrease is the internal energy. At higher
pressure, there are fewer holes present in the polymer matrix due to the high gas solubility. With
the removal of the holes, the free energy of the system is then decreased and, therefore, the
surface tension would drop as well. As for the reasons behind the surface tension’s
dependence on the temperature, it is explained that the increase in temperature would reduce the
segregation between molecular constituents; hence, the surface tension drops with temperature
at moderate pressure.
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180 200 220
4
6
8
10
12
14
16
18
Pressure (psi) 1000 1500 2000 2500 3000 3500 4000 4500
Surf
ace
Tens
ion
(mJ/
m2 )
Temperature(oC)
Figure 7-3 Surface Tension of Branched PP/CO2 at Various Temperatures and Pressures
There are two competing forces between the effect of T and the effect of gas content
dissolved in the PS. First, as the T increases, the surface tension decreases as the inter-molecular
distance increases. But as the T increases, the solubility decreases because the solubility
decreases. It is known that the surface tension decreases as the amount of gas dissolved in the
polymer increases. So this lowered gas content (with an increase in T) increases the surface
tension. So as the T increases, these two mechanisms are competing with each other. At low P,
the effect of dissolved gas is not dominant. But as the P increases, the dissolved gas content
increases. So the dissolved gas content dominates the surface tension. The break point for
PP-CO2 combination is: 20.6 MPa (3000psi). Above this point, the gas content governs the
surface tension and below this point, the T governs the surface tension.
Usually contact angle is also determined when surface tension is studied. But contact
angle is not measured in this research and the contact angle will be different when different
materials were used as the pedestal. Also the contact angle is also various when different grade
pellets are used since the sample pellets are from the manufacturing and it is possible the dirty
particle or impurity may affect the drop shape but the information is not provided precisely.
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TGA tests were carried out to see whether there were any degradation and the results shown that
the degradation is minimal. The TGA test results are going to be included in the Appendix 7 as
well.
7.3.3 Branch Effect on Surface Tension between Linear and Branched PP
It is believed that the branching of the PP molecules reduces the rate of the nucleation
process of the blowing agent because of an increase in the surface tension with branching. Since
the branched PP has larger elastic components, such as high melt elasticity and polymer chain
entanglement density, it will require a larger amount of work to create a new surface and thus a
higher surface tension. The following figures show the surface tension comparisons of linear
PP/CO2 and branched PP/CO2 at each temperature.
500 1000 1500 2000 2500 3000 3500 4000 4500 50002
4
6
8
10
12
14
16
18
20 BPP/CO2 at 180oC
LPP/CO2 at 180oC
Surf
ace
Tens
ion
(mJ/
m2 )
Pressure (psi)
Figure 7-4 Surface Tension of Linear and Branched PP/CO2 at 180oC
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500 1000 1500 2000 2500 3000 3500 4000 4500 50002
4
6
8
10
12
14
16
18
20 BPP/CO2 at 200oC)
LPP/CO2 at 200oC)
Surf
ace
tens
ion
(mJ/
m2 )
Pressure (psi)
Figure 7-5 Surface Tension of Linear and Branched PP/CO2 at 200oC
500 1000 1500 2000 2500 3000 3500 4000 4500 50002
4
6
8
10
12
14
16
18 BPP/CO2 at 220oC
LPP/CO2 at 220oC
Surf
ace
Tens
ion(
mJ/
m2 )
Pressure (psi)
Figure 7-6 Surface Tension of Linear and Branched PP/CO2 at 220oC
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From all three figures at three various temperatures, the surface tension decreases as the
pressure increases for both linear and branched PP/CO2 solutions. This is consistent with the
results seen in the previous sections as well as those in the literature aforementioned.
Those results also clearly show that the branched PP/CO2 has higher surface tension than
linear PP/CO2. Long chain branching (LCB) in branched PP polymer enhances polymer chain
entanglements and reduces polymer hydrodynamic volume. The LCB structure also greatly
improved the polymer elasticity, as evident from the increases in storage modulus, relaxation
modulus and die swell[297]. In comparison to linear polymer melts, long chain branched polymer
melts show enhanced strain-hardening due to the fact that while the backbone of the branched
macromolecule is stretched by deformation, the side chains are compressed.
In addition, the long branches of PP induce more chain entanglements in melt state,
contributing to enhancing the melt strength over linear PP[298,299]. It is also seen that the
branching structures affect the gas solubility and the swelling. Due to the increased melt
strength and viscosity of branching structure as well as the reduction of gas solubility and
volume swelling, the surface tension of branched PP is also increased over linear PP. However,
the surface tension of branched PP/CO2 and linear PP/CO2 starts to converge at higher pressure
levels from 2500 psi to 4500 psi as shown in all three figures. This means the effect of
branching on surface tension is diminished from the increase of the pressure. When the pressure
increases to higher levels, it helps to get more gas dissolved into the polymer. The plasticization
effect due to more gas dissolution into the polymer matrix would reduce the melt strength and
viscosity, which would counteract the branching effect on the surface tension. When the
pressure is high enough, its effect dominates the branching effect, therefore the surface tension
of branched PP/CO2 will decrease and the surface tension for both linear and branched PP/CO2
converges at high pressure.
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7.4 Summary
The focus of this chapter is to combine the surface tension measurement technique with
the determined density information from PVT to obtain more accurate surface tension
measurements of polymer/gas solutions. The solution systems used in the surface tension study
are the same as those used in the PVT study from Chapter 6. They were linear PP/CO2 and
branched PP/CO2 solutions.
The effects of temperature, pressure and branching structure on the surface of PP/CO2
solutions were shown in detail based on the experimental results. It was found that the surface
tension will decrease as the temperature increases. But this decreasing dependence of surface
tension on temperature only hold at pressured up to 2000 psi. This observation from the
experimental results is similar to the one reported from Park et al. [27,181] when they saw that the
dependence of surface tension of PS/CO2 solution on temperature diminishes at a pressure of
2500 psi. Pressure also affects the surface tension through solubility. The solubility of CO2
increases as the pressure increases, the free energy of the system would drop when more gas is
dissolved into the polymer matrix to occupy the holes and therefore the surface tension also
decreases as a result of the pressure increase.
The branching structure also has impact on surface tension. Branching structure would
enhance the polymer melt strength, strain-hardening and melt viscosity, which make the
polymer chains become less mobile than linear polymer. The restriction on the chain mobility
due to branching effect will cause the gas solubility in branched polymer to decrease; thereby
the surface tension of branched PP/CO2 solution is higher than linear PP/CO2. However when
the pressure increases to higher levels, the branching effect on the surface tension become
diminishing. This indicates that the higher the pressure, the more gas is dissolved into the
polymer. The plasticization effect of having more gas dissolved into the polymer matrix would
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reduce the melt strength and the viscosity; therefore, the surface tension will decrease as the
pressure increases. The decrease in surface tension due to the increase in pressure is higher than
the increase in surface tension from effect of branching at higher pressure, therefore the results
show that the surface tension of linear and branched PP/CO2 started to converge as pressure
increases beyond 2500psi.
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Chapter 8. Conclusions and Future Work
8.1 Conclusions
A novel apparatus has been designed and constructed based on the need for more
accurate determination of the PVT property of polymer/gas solutions at elevated temperatures
and pressures.
During thermoplastic foaming, the polymer/gas solution formation, cell nucleation and
cell growth, are the most important stages. It has been shown that the gas solubility in a polymer
melt would determine the proper polymer/gas formation. The surface tension at both the gas and
polymer/gas interfaces would strongly affect the behaviour of cell nucleation and cell growth
which are crucial factors in determining the properties of final foam products. However,
accurate determination of both solubility and surface tensions need reliable and precise PVT
information. SL and SS EOS have been used quite extensively in predicting the volume swelling
and in calculating the density of the polymer/gas mixtures to facilitate better measurement of the
solubility and surface tensions. However, with the limitation of using pure theories, the urgency
for developing an experimental apparatus to obtain the polymer/gas solutions’ PVT information
is imminent.
This research study, motivated by these strong needs, used the Axiomatic design
methodology to propose, verify and construct a unique experimental apparatus which could
enable the accurate measurement of polymer, polymer/gas solutions PVT at high temperatures
and pressures. The design and construction process of the system were depicted in detail.
The error reduction from image reconstruction was verified using the system to measure
the volume of a stainless sphere ball. The results showed that, when the number of images taken
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increases, the error in volume calculation drops significantly due to the pixel size reduction and
the boost in increasing pixel number. The densities of pure linear PP, branched PP and PS were
measured using the PVT apparatus at high temperatures but under vacuum conditions. Their
densities in the same condition were also calculated from the Tait equation. The density results
obtained from two different means showed excellent agreement. This proved that the PVT
system is accurate, reliable and repeatable in conducting the PVT experiments for pure polymers
as well as polymer/gas solutions.
The PVT properties of linear and branched PP/CO2 solutions were intensively studied at
high temperatures and pressures. The temperatures were at 180oC, 200oC and 220oC and the
pressure ranged from from 1000psi to 4500psi. The results showed that the volume swelling
increased as the pressure increased. On the other hand, the increase in temperature resulted in a
decrease in volume swelling for both linear and branched PP/CO2 solutions.
Due to the long chain branching (LCB) effect, the branched PP showed significantly less
volume swelling in all temperatures and pressures. The LCB helped increase the melt strength
and viscosity but restricted the chain mobility, and thereby it was less easy for the gas molecules
to penetrate into the branched structure of branched PP matrix.
It was found that, at each fixed temperature, the rate of volume swelling decreased as
pressure increased and there exists a plateau or upper limit for the volume swelling of linear PP
and branched PP/CO2 solutions. This finding indicated that due to the long chain structure and
chain entanglement, the polymer could not physically stretch or dilate indefinitely from
dissolution of the gas as pressure increased. This phenomenon then led to the hypothesis made
in this study, which dictates that due to the polymer chain structure and chain entanglement
density, there was an upper limit for polymer/gas volume swelling at high pressures. The
polymer chain entanglement density experiments were then carried out using the rotational
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rheometer to further study the chain entanglement property of linear and branched PP. It was
discovered that branched PP had a much higher chain entanglement density than linear PP. The
chain entanglement density decreased as temperature increased. For the same polymer at high
temperatures, the low entanglement density resulted in less chain agglomerations. This made it
easier for the gas molecules to diffuse out of the matrix at a high temperatures, leading to a drop
in the solubility of the gas and a decrease in volume swelling. At the same temperature, linear
PP has less chain entanglement density and therefore has less chain entanglement that would
have less restriction on the chain mobile and allowed more gas molecules to diffuse into the
polymer matrix as the pressure increased.
As mentioned in the Chapter 1, one of the motivations of this research is to help
facilitate more accurate solubility measurements as well as verify the validity of EOS prediction
volume swelling. The volume swellings from the measurements were then compared with SL
and SS EOS prediction values for both linear and branched PP. It showed that both SL and SS
predicted continuously increasing volume swelling as the pressure increased at constant
temperature. SL showed a concave upward increase and SS showed a more linear increase. SS
predictions were the closest EOS predictions to the experimental measurement values. The
discrepancy between the EOS prediction and the measurement values may be due to the
inability of predicting the real molecular dynamics and behaviours using pure thermodynamic
laws. Nonetheless, the PVT measurement provided the means to obtain the volume
measurement directly and gave room for improvement in making those two EOS model
predictions better fit with experimental data.
The corrected solubility data from both the experiments and EOS were also plotted. The
results again showed similar trends as in the swelling comparison. The SS EOS corrected
solubility was the closet to the experimental corrected solubility. The results also indicated that
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the solubility tended to reach some plateau as the pressure increased for both linear and
branched PP cases.
Another important topic regarding the shape asymmetry effect on the PVT measurement
was investigated thoroughly. The experiments were carried out using PS at three different
temperatures and in a vacuum condition. The results demonstrated strongly that, as the
temperature increased, the drop shape becomes more asymmetric. The results also demonstrated
that the rotational device helped to compensate the effect of asymmetric drop shape on PVT
measurement. Therefore, the rotational device enable the system to measure the PVT data
accurately even with asymmetric polymer drop. The PVT information for PS/CO2 was also
investigated. The study showed that as the temperature increased, the PS/CO2 had less swelling
but the swelling increased as the pressure increased.
Due to the need of exploring more environmentally friendly gas blowing agents, the
HFC-152a was used to study its PVT behaviour with PS solutions at high temperatures, but at
relatively low pressures of up to only 800 psi. At low pressures, the swelling of PS/HFC-152a
showed a concave increasing trend as the pressure increased. However, the temperature effect
on the volume swelling was the same and the volume swelling was also less at high
temperatures.
Finally, the surface tensions of both PP/CO2 solutions were investigated using the
experimental determined density data. At constant T, as P increases, the surface tension drops
for both linear and branched PP/CO2 solutions. There is clear competition between the
temperature effect and the gas content effect on surface tension. The gas content was the
dominate factor at pressure up to 2500psi. This observation agreed with what other researchers
discovered for PS/CO2 solutions. At pressures from 2500 psi to 3500 psi, the dependence of the
surface tension on the temperature was minimal. After the pressure surpassed 3500 psi, the
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surface tension saw a slight increase due to decrease in solubility caused by the temperature
increased. Due to the branching effect, the surface tensions of branched PP/CO2 solutions were
higher than linear PP/CO2 only at relatively low pressures of up to 2500 psi. When the pressure
increased beyond 2500psi, the surface tension between the linear and branched PP/CO2
solutions at each temperature became very close to each other, this indicated that the increase in
pressure helps to diminish the branching effect over those two long chain polymers.
8.2 Future work
Although this research has successfully developed a unique and sound system to measure
the PVT of polymer/gas solutions accurately for the first time, there are still improvement works
that needs to be carried out to take full advantage of this system. The system improvement
would allow for potential system components modification or upgrade. For example, if the size
of the sessile drop needs to be changed, then the pedestal needs to be machined to accommodate
the change.
The following suggestions are made for the direction of future research using this PVT
measurement apparatus.
1. Conduct intensive PVT measurements on various polymer/gas solution combinations.
2. Establish a rigorous and complete PVT database for variety of polymer/gas solutions.
3. To improve the technique of fabricating a better droplet tip with a sharp edge so that the
boundary between the sample and tip can be easily distinguished.
4. This study simply compared the volume swelling results from experimental and the EOS
prediction. Discrepancies were found but they were not fully investigated, therefore it is
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necessary and worthwhile to carry out more in-depth study on how to improve the
modelling of the EOS so that better predictions can be made.
5. Surface tension property studies were only carried out using PP/CO2 solutions. In order
to obtain more accurate surface tension values and to better understand the role of
surface tension in cell nucleation and growth, more experiments need to be carried out
using variety of polymer/gas solutions
6. The asymmetry of other polymer/gas drop shapes is worth investigating. A better index
or universal constant can be established to describe the drop shape asymmetry in general.
7. Lastly, the experiments carried out in this study were confined to the usage of only the
sessile drop. Since the design of the PVT apparatus is also capable of dealing with
pendent droplets, it would be important to conduct all the above experiments using the
pendent drops to further investigate the difference between those two techniques.
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APPENDIX 1 Image Movement Input Algorithm %-------------------------------------------------------------------------- %%%%% This program is used for the image reconstruction based on the X-Y | %%%%% stage movement and the calibration, using all the image taken | %%%%% By Hongbo Li, Gary Li | %--------------------------------------------------------------------------| %%%% define the movement distance in terms of pixel from calibration %%%% Dy=[0, 115.91, 316.59, 432.5, 432.5, 316.59, 115.91, -115.91, -316.59 -432.5, -432.5, -316.59, -115.91 ]'; Dx=-[0, 435.25, 318.603, 116.647, -116.647, -318.603, -435.25, -435.25 -318.603, -116.647, 116.647, 318.603, 435.25 ]'; %%% save the image file name based on the number sequence %%% filenames='p1.tif' 'p2.tif' 'p3.tif' 'p4.tif' 'p5.tif' 'p6.tif' 'p7.tif' ... 'p8.tif' 'p9.tif' 'p10.tif' 'p11.tif' 'p12.tif' 'p13.tif' 'p14.tif' 'p15.tif'... 'p16.tif' 'p17.tif' 'p18.tif' 'p19.tif' 'p20.tif' 'p21.tif'... 'p22.tif' 'p23.tif' 'p24.tif' 'p25.tif' 'p26.tif' 'p27.tif' 'p28.tif' 'p29.tif'... 'p30.tif' 'p31.tif' 'p32.tif' 'p33.tif' 'p34.tif' 'p35.tif' 'p36.tif' 'p37.tif'... 'p38.tif' 'p39.tif' 'p40.tif' 'p41.tif' 'p42.tif' 'p43.tif' 'p44.tif' 'p45.tif'; %%%% Important Note %%%% %%%% Vertical movement using the x directional pixel movement values %%%% Horizontal movement using the y directional pixel movement values %%%% Remember: New Program there is no sign changes;
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Image Reconstruction Algorithm %%% Edge Reconstruction %%% clear; close all; clc; B=[ ; ]; C=[ ; ; ]; %%% Load the stage step movement and all the images file %%%% %%% Movement: Dx, Dy in the unit of pixies based on calibration %%%% %%% Image Files: "bmp" format, or "Tif" format in the sequence taken %%%% Image_Movement_Input; volume_cylinder=0; DX_total=0; DY_total=0; for i=1:length(Dx) image_file = uigetfile('*.tif;*.bmp','Choose image file'); image_file=char(filenames(i)); I = imread(image_file);
figure(1); hold; imshow(I);
%%%%possible thresholding/smoothing and edge detection routine %%%%% %%%%use the canny edge detection algorithm to obtain the edge coordinates %%% %%%%threshold value and sigma can be changed%%%%
BW1 = edge(I,'canny',0.1,1); figure(2); imshow(BW1); drop_edge = bwmorph(BW1,'remove',3 );
[X Y]= find(drop_edge); X=X+Dx(i); Y=Y+Dy(i); DX_total=DX_total+Dx(i);DY_total=DY_total+Dy(i); X=X+DX_total; Y=Y+DY_total;
%%%% Put the X and Y cooridnates into a matrix %%%% A=[X,Y]; B=[B; A]; %%%% Plot the constructed image%%%%% figure(3); plot(B(:,1),B(:,2),'b.'); end ;
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Axialsymmetric Volume Integration Algorithm %--------------------------------------------------------------------------- %Combine cropping and volume calculation script this program crops droplet %image in half by finding profile maximum and spline the boundary %calculate partial volumes separately using curve fitting and integration %Script features cropping routines and edge detection and volume calculation %routines that can be used separately %For spline fit function checkxy is used for removing duplicates and noise, %checkxy MUST be in the workin directory! %--------------------------------------------------------------------------- clc; cla; clf; syms s; v_left=0; v_right=0; v_total=0; V_final=0; image_file = uigetfile('*.tif;*.bmp','Choose image file'); I = imread(image_file); %%%%possible thresholding/smoothing routine here%%%% BW1 = edge(I,'canny',0.1,1); drop_edge = bwmorph(BW1,'remove',3 ); [X,Y] = find(drop_edge); %%%% plot to check for artifacts %%%% figure(1); plot(X,Y,’b.’); %%%%Find the highest point of the drop or the apex of the drop%%%% %%%%that is the smallest value for x %%%% minX = min( X ); index = find( X==minX ); centerY = mean( Y(index) ); %%%%2048- centerY image width, modify for larger images%%%% %%%%480 - image height, modify for actual image%%%% width=2048-centerY; Image_right = imcrop(BW1, [centerY 0 width 2048]);
figure(2); imshow(Image_right);
imwrite(Image_right,'right_part.tif','tif','Compression','none','WriteMode','overwrite');
figure(3); imshow(Image_left);
imwrite(Image_left,'left_part.tif','tif','Compression','none','WriteMode','overwrite');
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Image_left = imcrop(BW1, [0 0 centerY 2048]); %%%%calculate the right part volume%%%% right_image_file = imread('right_part.tif'); drop_edgeR = bwmorph(right_image_file,'remove',3 ); [X1,Y1] = find(drop_edgeR); figure(4); plot(X1,Y1,'ro'); %removing duplicates, function checkxy MUST be in the working directory! [xx1,yy1] = checkxy(X1,Y1,'R'); xx_right=xx1'; yy_right=yy1'; ymin=min(Y1); yyy_right=yy1-ymin; %%%% Volume Integration Calculation %%%% pp=spline(xx_right,yy_right); [B,c,L,K,D]=unmkpp(pp); x_max=max(xx_right); x_min=min(xx_right); %ymin=min(yy_right); ymin=min(Y1); NT=10000; xright=linspace(x_min,x_max,NT); yright=ppval(pp,xright); figure(5); hold; plot(xright,yright,'o'); volume=0; for i=1:length(xright)-1 if xright(i)<= 996
v_right=v_right+1/3*pi*(abs((xright(i+1)-xright(i))))*((yright(i)-ymin)^2+(yright(i)-ymin)*(yright(i+1)-ymin)+(yright(i+1)-ymin)^2);
elseif xright(i)>= 996
volume=0; end; end; %%%%left part volume calculation%%%% left_image_file = imread('left_part.tif'); drop_edgeL = bwmorph(left_image_file,'remove',3 ); [X2,Y2] = find(drop_edgeL);
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figure(6); plot(X2,Y2,'bd'); % removing duplicates, function checkxy MUST be in the working directory! [xx2,yy2] = checkxy(X2,Y2,'L'); xx_left=xx2'; yy_left=yy2'; ymax=max(Y2); yyy_left=abs(yy2-ymax); figure(7); hold; plot(xx_left,yy_left,'rd'); volume = 0; %%%%Calculate volume integrals %%%% pp=spline(xx_left,yy_left); xmax=max(xx_left); xmin=min(xx_left); %ymax=max(yy_left); ymax=max(Y2); NT=10000; xleft=linspace(xmin,xmax,NT); yleft=ppval(pp,xleft); figure(8); plot(xleft,yleft,'*'); for i=1:length(xleft)-1 if xleft(i)<= 986
v_left=v_left+1/3*pi*(abs((xleft(i+1)-xleft(i))))*((yleft(i)-ymax)^2+abs((yleft(i)-ymax))*abs((yleft(i+1)-ymax))+(yleft(i+1)-ymax)^2);
elseif xleft(i)>= 986 volume=0; end; end; %%%%Total volume by combining the v_left and v_right together%%%% v_total=(v_right+v_left)/2; step_size = 0.5; % the XY stage step size is 0.5 um per step cal_factor = 0.187329365; % the calibration factor is pixel/step vol_conversion_factor = ((step_size/cal_factor)*10^-4)^3; v_final=v_total*vol_conversion_factor; format long date_time = fix(clock); V =[date_time, v_final]; %%%%%saving file and appending data to existing values%%%% fid = fopen('volume data.txt','a+','n'); fprintf(fid,'%12.0f %9.2f\r\n',V); fclose(fid);
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Function “checkxy” Algorithm function [x,y] = checkxy(x,y,Ntest) %CHECKXY check the given data x = x(:).'; y = y(:).'; NT=length(x); if any(diff(x)<0), [x,index] = sort(x); y = y(index); end if (Ntest=='R') %[b0,indx]=min(y); a0=x(indx); a0=x(NT);b0=y(NT); else if (Ntest=='L') %[b0,indx]=max(y); a0=x(indx); a0=x(NT);b0=y(NT); else error('wrong input') end end %%% Note, here we must keep the highest value of Y, since it is sensitive to %%% the final volume; %%% Depending on which part of the image, the extreme value y (at the end) %%% has to be selected mults = knt2mlt(x); if any(mults) % remove repeat sites, averaging the corresponding values for j=find(diff([mults,0])<0) y(j-mults(j)) = mean(y(j-mults(j):j)); end repeats = find(mults); x(repeats) = []; y(repeats) = []; %temp = warndlg(... %'Data has been modofied', ... % 'Repeated values found ...'); %waitfor(temp) end n0=length(x); if a0==x(n0) x(n0)=a0; y(n0)=b0; end if a0 ~=x(n0) x(n0+1)=a0; y(n0+1)=b0; end lx = length(x); if lx<2 error('There should be at least two data points.') end if lx~=length(y)
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error(['The number ',num2str(lx),' of data sites should match',... ' the number ',num2str(length(y)),' of data values.']) End
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Asymmetric Volume Calculation Algorithm (Fortran) C THIS ALOGRITHM IS DEVELOPED TO SPLINE THE PRIMETER OF EACH C LAYER OF THE DROP AND THEN USE SIMPSON’S RULE TO INTEGRATE C TO COMPUTE THE VOLUME OF ASYMMETRIC DROP SHAPE C THIS IS TO CALCULATE THE VOLUME OF SESSILE DROP PROGRAM VOLUME CALCUATION OF A SESSILE DROP PARAMETER (IMAX=560) ! TEMP=150 C PARAMETER (IMAX=570) ! TEMP=200 C PARAMETER (IMAX=506) ! TEMP=250 PARAMETER (KMAX=100) PARAMETER (PAI=3.1415926) REAL RL(0:KMAX,0:IMAX),RR(0:KMAX,0:IMAX) REAL THETAL(0:KMAX), THETAR(0:KMAX) REAL TOT(0:IMAX) REAL AREA(0:KMAX,0:IMAX) REAL TEMP C CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC C DATA INPUT TEMP=150. C TEMP=200. C TEMP=250. IF (TEMP .EQ. 150.) THEN OPEN (2, FILE='E:\3\SPLINE150L.DAT',STATUS='OLD') READ (2,*) (THETAL(K),K=1,KMAX) DO I=1,IMAX READ (2,*) (RL(K,I), K=1,KMAX) ENDDO CLOSE (2) OPEN (4, FILE='E:\3\SPLINE150R.DAT',STATUS='OLD') READ (4,*) (THETAR(K),K=1,KMAX) DO I=1,IMAX READ (4,*) (RR(K,I), K=1,KMAX) ENDDO CLOSE (4) ENDIF IF (TEMP .EQ. 200.) THEN OPEN (12, FILE='E:\3\SPLINE200L.DAT',STATUS='OLD') READ (12,*) (THETAL(K),K=1,KMAX) DO I=1,IMAX READ (12,*) (RL(K,I), K=1,KMAX) ENDDO CLOSE (12) OPEN (14, FILE='E:\3\SPLINE200R.DAT',STATUS='OLD') READ (14,*) (THETAR(K),K=1,KMAX) DO I=1,IMAX READ (14,*) (RR(K,I), K=1,KMAX) ENDDO CLOSE (14)
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ENDIF IF (TEMP .EQ. 250.) THEN OPEN (22, FILE='E:\3\SPLINE250L.DAT',STATUS='OLD') READ (22,*) (THETAL(K),K=1,KMAX) DO I=1,IMAX READ (22,*) (RL(K,I), K=1,KMAX) ENDDO CLOSE (22) OPEN (24, FILE='E:\3\SPLINE250R.DAT',STATUS='OLD') READ (24,*) (THETAR(K),K=1,KMAX) DO I=1,IMAX READ (24,*) (RR(K,I), K=1,KMAX) ENDDO CLOSE (24) ENDIF DO K=1,KMAX RL(K,0)=0. RR(K,0)=0. ENDDO C CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC C VOLUME CALCUATION VOL=0. DO I=1,IMAX TOT(I)=0. C DO K=1,KMAX-1 C AREA(K,I)= C & PAI*((RL(K,I)+RL(K+1,I)+RL(K,I-1)+RL(K+1,I-1))/4.)**2 C & *(THETAL(K+1)-THETAL(K))/360. C & +PAI*((RR(K,I)+RR(K+1,I)+RR(K,I-1)+RR(K+1,I-1))/4.)**2 C & *(THETAR(K+1)-THETAR(K))/360. C TOT(I)=TOT(I)+AREA(K,I) C ENDDO DO K=1,KMAX-1 AREA(K,I)=1./3.*PAI*( & (( RL(K,I-1)+RL(K+1,I-1) )/2.)**2 & +(( RL(K,I-1)+RL(K+1,I-1) )/2.)*(( RL(K,I)+RL(K+1,I) )/2.) & +(( RL(K,I)+RL(K+1,I) )/2.)**2 & )*(THETAL(K+1)-THETAL(K))/360. & + & 1./3.*PAI*( & (( RR(K,I-1)+RR(K+1,I-1) )/2.)**2 & +(( RR(K,I-1)+RR(K+1,I-1) )/2.)*(( RR(K,I)+RR(K+1,I) )/2.) & +(( RR(K,I)+RR(K+1,I) )/2.)**2 & )*(THETAR(K+1)-THETAR(K))/360. TOT(I)=TOT(I)+AREA(K,I) ENDDO TOT(I)=TOT(I)*(2.6953E-4)**2
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VOL=VOL+TOT(I)*1.*(2.6803E-4) ENDDO IF (TEMP .EQ. 150) THEN ERR=(VOL-0.014416)/0.014416 ! T=150 DEGREE C WRITE(*,*) 'VOL=', VOL, ' CC' WRITE(*,*) (VOL-0.014416) WRITE(*,*) 'ERR=', ERR*100, ' %' ENDIF IF (TEMP .EQ. 200) THEN ERR=(VOL-0.014848)/0.014848 ! T=200 DEGREE C WRITE(*,*) 'VOL=', VOL, ' CC' WRITE(*,*) (VOL-0.014848) WRITE(*,*) 'ERR=', ERR*100, ' %' ENDIF IF (TEMP .EQ. 250) THEN ERR=(VOL-0.01528)/0.01528 ! T=250 DEGREE C WRITE(*,*) 'VOL=', VOL, ' CC' WRITE(*,*) (VOL-0.01528) WRITE(*,*) 'ERR=', ERR*100, ' %' ENDIF OPEN (6, FILE='AREA.DAT', STATUS='UNKNOWN') DO I=1,IMAX WRITE (6,*) I,TOT(I) ENDDO CLOSE (6) END
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APPENDIX 2 Motion Stage GUI Development Algorithm Private Response As String Private hDmc As Long Private Controller As Integer Private RC As Long Private Px() As Long Private Py() As Long Dim stoploop As Boolean Private Declare Sub Sleep Lib "kernel32" (ByVal dwMilliseconds As Long) Private Declare Function timeGetTime Lib "winmm.dll" () As Long Private Sub Btn_AutoImage_Click() Dim i As Long Dim j As Long Dim k As Long Dim h As Long Dim Duration As Single ' in hour Dim Interval As Long ' in minute Dim UnitAngle As Long Dim Sleeptime As Long 'millisecond Dim totalloop As Long Dim Kt As Long 'get current time Dim Comma As Integer Dim Item As String Dim Totalitem As Integer Dim CommandString As String Dim SaveDirectory As String Dim Output As Long Dim Imagefile As String Dim Today As String Totalitem = List_Data.ListCount Output = 1 Today = Date$ + "-" If Txt_Duration.Text = "" Then Txt_Duration.SetFocus
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End If If Txt_Interval.Text = "" Then Txt_Interval.SetFocus End If UnitAngle = 0 If chk_Rotation.Value Then If txt_RotationAngle.Text = "" Then txt_RotationAngle.SetFocus Else UnitAngle = Val(txt_RotationAngle.Text) End If End If Txt_Duration.Enabled = False Txt_Interval.Enabled = False txt_RotationAngle.Enabled = False Duration = Val(Txt_Duration.Text) * 60 'convert hour to minute Interval = Val(Txt_Interval.Text) totalloop = Duration / Interval Sleeptime = Interval * 60 ' seconds stoploop = False Pbar_Waittime.Max = Sleeptime If txt_SaveDir.Text = "" Then SaveDirectory = "D:\GaryPics\" Else SaveDirectory = txt_SaveDir.Text End If If Totalitem > 0 Then Btn_AutoImage.Enabled = False j = 1 Do While (j <= totalloop And Not stoploop) DoEvents Pbar_Waittime.Value = 0 Btn_Pause.SetFocus '=========== If chk_Rotation.Value Then
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k = 0 'set the counter for rotation angle Do While ((k * UnitAngle) <= 360) 'get data points and display them in listbox For h = 0 To Totalitem - 1 List_Data.Selected(h) = False List_Data.Refresh Next '========= lbl_RotationAngle.Caption = Str(k) + ":" + Str(k * UnitAngle) If k > 0 Then CommandString = "PRZ=" + Str((UnitAngle * 500 / 360)) CommandString = CommandString + ";" + "BGZ" + ";" + "CB0;AM;SB0" RC = DMCCommand(hDmc, CommandString, Response, ResponseLength) Call RTrim(Response) If Len(Txt_Response.Text) > 32000 Then Txt_Response.Text = Txt_Command.Text + vbCrLf + Response Else Txt_Response.Text = Txt_Response.Text + Txt_Command.Text + vbCrLf + Response End If End If '============== '360 degree = 500 pulses 'time taken for rotating shaft by unitangle is unitangle*250ms/360 for sp=2000 '============== i = 0 Do While (i < Totalitem) 'scan each point and take picture at desired spots Item = Trim$(List_Data.List(i)) Lbl_CurrentPoint.Caption = Item CommandString = "PR" + Item CommandString = CommandString + ";" + "BGXY" + ";" + "CB0;AM;SB0" 'pause for 250 millisecs Kt = timeGetTime While Abs(timeGetTime - Kt) < 250 DoEvents
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Wend RC = DMCCommand(hDmc, CommandString, Response, ResponseLength) Call RTrim(Response) If Len(Txt_Response.Text) > 32000 Then Txt_Response.Text = Txt_Command.Text + vbCrLf + Response Else Txt_Response.Text = Txt_Response.Text + Txt_Command.Text + vbCrLf + Response End If DoEvents 'select the data point that has been processed If List_Data.Selected(i) = False Then List_Data.Selected(i) = True List_Data.Refresh End If 'Check if motion is completed by checking the value of generaloutput0 RC = DMCRefreshDataRecord(hDmc, ByVal 0&) RC = DMCGetDataRecordByItemId(hDmc, DRIdGeneralOutput0, DRIdAxis1, DRTypeLONG, Output) Do While (Output = 0) DoEvents RC = DMCRefreshDataRecord(hDmc, ByVal 0&) RC = DMCGetDataRecordByItemId(hDmc, DRIdGeneralOutput0, DRIdAxis1, DRTypeLONG, Output) Sleep (5) Loop 'Save image to files when desired position is reached If chk_Rotation.Value Then Imagefile = SaveDirectory + Today + Str(j) + "-" + Str(i + 1) + "-" + Str(k) + "-" + Str(k * UnitAngle) + ".tif" End If Sbar_Main.Panels(3).Text = "Image File saved to:" + Imagefile EBW8Image1.Save Imagefile, eGrayLevelTiff Sbar_Main.Panels(2).Text = "Scanned points:" + Str(j) + ":" + Str(i + 1) + ":" + Str(k) + ":" + Str(k * UnitAngle) i = i + 1 Loop ' end of the loop for taking pictures at various points
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'// end of the code for rotation k = k + 1 Loop '// end of the loop for rotation Else 'no rotation, only points along perimeter 'get data points and display them in listbox For h = 0 To Totalitem - 1 List_Data.Selected(h) = False List_Data.Refresh Next i = 0 Do While (i < Totalitem) 'scan each point and take picture at desired spots Item = Trim$(List_Data.List(i)) Lbl_CurrentPoint.Caption = Item CommandString = "PR" + Item CommandString = CommandString + ";" + "BGXY" + ";" + "CB0;AM;SB0" 'pause for 250 millisecs Kt = timeGetTime While Abs(timeGetTime - Kt) < 250 DoEvents Wend RC = DMCCommand(hDmc, CommandString, Response, ResponseLength) Call RTrim(Response) If Len(Txt_Response.Text) > 32000 Then Txt_Response.Text = Txt_Command.Text + vbCrLf + Response Else Txt_Response.Text = Txt_Response.Text + Txt_Command.Text + vbCrLf + Response End If DoEvents 'select the data point that has been processed If List_Data.Selected(i) = False Then List_Data.Selected(i) = True List_Data.Refresh End If 'Check if motion is completed by checking the value of generaloutput0
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RC = DMCRefreshDataRecord(hDmc, ByVal 0&) RC = DMCGetDataRecordByItemId(hDmc, DRIdGeneralOutput0, DRIdAxis1, DRTypeLONG, Output) Do While (Output = 0) DoEvents RC = DMCRefreshDataRecord(hDmc, ByVal 0&) RC = DMCGetDataRecordByItemId(hDmc, DRIdGeneralOutput0, DRIdAxis1, DRTypeLONG, Output) Sleep (5) Loop Imagefile = SaveDirectory + Today + Str(j) + "-" + Str(i + 1) + ".tif" Sbar_Main.Panels(3).Text = "Image File saved to:" + Imagefile EBW8Image1.Save Imagefile, eGrayLevelTiff Sbar_Main.Panels(2).Text = "Scanned points:" + Str(j) + ":" + Str(i + 1) i = i + 1 Loop ' end of the loop for taking pictures at various points End If 'condition check for rotation j = j + 1 Kt = timeGetTime While Abs(timeGetTime - Kt) < (Sleeptime * 1000) And Not stoploop Pbar_Waittime.Value = Abs(timeGetTime - Kt) / 1000 DoEvents Wend If stoploop Then Exit Do End If Loop ' end of the loop of each interval End If Btn_AutoImage.Enabled = True Btn_OpenData.Enabled = True Txt_Duration.Enabled = True Txt_Interval.Enabled = True Call MsgBox("Done Done Done!!!", vbOKOnly, "Warning") End Sub
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Private Sub Btn_CloseData_Click() List_Data.Clear Btn_OpenData.Enabled = True Btn_CloseData.Enabled = False Btn_AutoImage.Enabled = False End Sub Private Sub Btn_Initialization_Click() EBoard1.DriverIndex = 0 '+ change EBoard1.SetParamNm "BoardTopology", "MONO" '- change ' Create a channel and associate it with the first connector on the first board ECamera1.Mpf = "CHANNEL" ECamera1.SetParamNm "DriverIndex", 0 '+ change ECamera1.SetParamNm "Connector", "M" '- change ' Choose the video standard '+ change ECamera1.SetParamNm "CamFile", "TM-4000CL_P15RG" '- change ' Choose the camera expose duration ECamera1.SetParamNm "Expose_us", 66667 ' Choose the pixel color format ECamera1.SetParamNm "ColorFormat", "Y8" ' Set the acquisition mode to snapShot ECamera1.SetParamNm "AcquisitionMode", "SNAPSHOT" ' Choose the way the first acquisition is triggered ECamera1.SetParamNm "TrigMode", "IMMEDIATE" ' Choose the triggering mode for subsequent acquisitions ECamera1.SetParamNm "NextTrigMode", "SAME" ' Choose the number of images to acquire ECamera1.SetParamNm "SeqLength_Fr", -1 ' Choose the tap configruation 'ECamera1.SetParamNm "TapConfiguration", "BASE_2T8-2X_1Y" ' Choose the tap configruation 'ECamera1.SetParamNm "TapStructure", "DUAL_B" ' Choose the image flip style 'ECamera1.SetParamNm "ImagFlipX", "OFF" ' Choose the image flip style
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'ECamera1.SetParamNm "ImagFlipY", "OFF" ' Choose the image grab window 'ECamera1.SetParamNm "GrabWindow", "NOBLACK" ' Configure the receiving EImage: ' (set image size corresponding to camera capture) ImageSizeX = ECamera1.GetParamNm("ImageSizeX") ImageSizeY = ECamera1.GetParamNm("ImageSizeY") EBW8Image1.SetSize ImageSizeX, ImageSizeY EBW8Image1.EnableScrollBars = True ' Link the Camera with the EImage: ECamera1.Cluster = EBW8Image1 ' Enable the signals SurfaceFilled and AcquisitionFailure: ECamera1.SetParamNm "SignalEnable:2", "ON" ECamera1.SetParamNm "SignalEnable:7", "ON" '============================================ ECamera1.SetParamNm "ChannelState", "ACTIVE" Lbl_Status.Caption = "" '============================================ Btn_Initialization.Enabled = False End Sub Private Sub Btn_OpenData_Click() Dim InputData As String Dim fname As String Dim b As String Dim x As Long Dim y As Long Dim i As Integer Cdlg_Main.FileName = "" Cdlg_Main.ShowOpen fname = Cdlg_Main.FileName If fname <> "" Then 'File #1 will always be used for reading in the source data file Open fname For Input As #1 b = "" i = 0
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Do Until EOF(1) i = i + 1 'Input #1, InputData ReDim Px(i - 1) ReDim Py(i - 1) Input #1, Px(i - 1), Py(i - 1) b = Str(Px(i - 1)) + "," + Str(Py(i - 1)) List_Data.AddItem (b) Loop Close #1 End If If List_Data.ListCount > 0 Then Btn_CloseData.Enabled = True Btn_OpenData.Enabled = False Btn_AutoImage.Enabled = True End If End Sub Private Sub Btn_Pause_Click() Dim CommandString As String stoploop = True CommandString = "AB" RC = DMCCommand(hDmc, tempcommand, Response, ResponseLength) Call RTrim(Response) If Len(Txt_Response.Text) > 32000 Then Txt_Response.Text = Txt_Command.Text + vbCrLf + Response Else Txt_Response.Text = Txt_Response.Text + Txt_Command.Text + vbCrLf + Response End If Txt_Duration.Enabled = True Txt_Interval.Enabled = True If chk_Rotation.Value Then txt_RotationAngle.Enabled = True End If
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End Sub Private Sub Btn_Send_Click() Dim additionalresponse As String Dim SpeedNumber As Long Response = Space(256) ResponseLength = 256 If Txt_Command.Text = "" Then Txt_Command.Text = ";" End If RC = DMCCommand(hDmc, Txt_Command.Text, Response, ResponseLength) Call RTrim(Response) If Len(Txt_Response.Text) > 32000 Then Txt_Response.Text = Txt_Command.Text + vbCrLf + Response Else Txt_Response.Text = Txt_Response.Text + Txt_Command.Text + vbCrLf + Response End If If RC = DMCERROR_BUFFERFULL Then RC = DMCGetAdditionalResponseLen(hDmc, ResponseLength) If RC = 0 Then additionalresponse = Space$(ResponseLength + 1) RC = DMCGetAdditionalResponse(hDmc, additionalresponse, ResponseLength) RTrim (additionalresponse) If Len(Txt_Response.Text) > 32000 Then Txt_Response.Text = additionalresponse Else Txt_Response.Text = Txt_Response.Text + additionalresponse End If End If End If Txt_Command.Text = "" Txt_Response.SelStart = Len(Txt_Response.Text) End Sub Private Sub Btn_Stop_Click() Dim tempcommand As String Dim additionalresponse As String
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Response = Space(256) ResponseLength = 256 'Stop the stepper motor tempcommand = "ST" RC = DMCCommand(hDmc, tempcommand, Response, ResponseLength) tempcommand = "CS" RC = DMCCommand(hDmc, tempcommand, Response, ResponseLength) Call RTrim(Response) If Len(Txt_Response.Text) > 32000 Then Txt_Response.Text = Txt_Command.Text + vbCrLf + Response Else Txt_Response.Text = Txt_Response.Text + Txt_Command.Text + vbCrLf + Response End If End Sub Private Sub chk_Rotation_Click() If txt_RotationAngle.Enabled Then txt_RotationAngle.Enabled = False txt_RotationAngle.Text = "" Else txt_RotationAngle.Enabled = True End If End Sub Private Sub ECamera1_Signal(ByVal SignalType As MULTICAMLibCtl.enumMcEventType, ByVal Obj As Object, ByVal Last As Boolean) If SignalType = eMcSigAcquisitionFailure Then Lbl_Status.Caption = "Acquisition Failure" Else If SignalType = eMcSigSurfaceFilled Then Obj.Refresh ' Retrieve the frame rate and display it Value = ECamera1.GetParamNm("FrameRate_Hz") Lbl_Status.Caption = "FrameRate_Hz " + Value End If End If End Sub Private Sub Form_Load() Dim tempcommand As String
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Dim Kt As Long '============================== ' Controller card detecting Response = Space(256) ResponseLength = 256 DiagsOn = False hDmc = -1 Controller = 1 If Command$ <> "" Then Controller = Val(Command) End If If Controller < 1 Or Controller > 15 Then Controller = 1 End If RC = DMCOpen(Controller, 0, hDmc) If RC = 0 Then RC = DMCVersion(hDmc, Response, ResponseLength) Sbar_Main.Panels(1).Text = Response RC = DMCCommand(hDmc, ";", Response, ResponseLength) 'Initialize the stepper motors tempcommand = "MT 2.5,2,2;SP 2000,2000,2000;AC 100000,100000,100000;DC 50000,50000,50000" RC = DMCCommand(hDmc, tempcommand, Response, ResponseLength) Else hDmc = -1 MsgBox "Error: could not connect to controller " + Trim$(Str$(Controller)) + ". RC = " + Trim$(Str$(RC)) Unload Frm_Main End If Me.Show '====================================== 'Initialization of Evision Board 'initialize buttons Btn_OpenData.Enabled = True Btn_CloseData.Enabled = False Btn_AutoImage.Enabled = False
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txt_RotationAngle.Enabled = False 'Btn_Initialization_Click End Sub Private Sub Form_Unload(Cancel As Integer) stoploop = True End Sub Private Sub Txt_Command_GotFocus() Btn_Send.Default = True End Sub Private Sub Txt_Command_KeyDown(KeyCode As Integer, Shift As Integer) If KeyCode = vbKeyEscape Then TabStrip.SetFocus End If End Sub Private Sub Txt_Command_KeyPress(KeyAscii As Integer) If KeyAscii >= 97 And KeyAscii <= 122 Then KeyAscii = KeyAscii - 32 End If End Sub
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APPENDIX 3 Calibration is carried out in vacuum condition at the experimental temperature prior to
each experiment. The calibration is done at all the levels across the sample horizontally in X
direction and vertically in Y direction. The following graphically illustrates how the calibration
is determined in both directions. The number of levels is determined to cover the whole drop.
Calibration in X direction
x1x2x3x4
x
y
At level 1, the edge point on the X axis at pixel coordinate 1X of the drop is moved across the
lens (or the screen) to a new location at NX _1 with the stage moved N step towards right (or
left) direction as illustrated as following two pictures
1X NX _1
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During the N step movement, the number of pixel is determined as: 1_1 XX N −
Since each step of the stage is 0.5μm, the pixel size at level 1 can be determined as:
1_1
*00005.0XX
N
N −
Similarly, the pixel size at all other levels could be determined.
Calibration in Y direction
y1 y2 y3 y4
x
yy5 y6 y7
At level 1, the edge point on the Y axis at pixel coordinate 1Y of the drop is moved across the
lens (or the screen) to a new location at NY _1 with the stage moved N step in upward (or
downward) direction as illustrated as following two pictures
During the N step movement, the number of pixel is determined as: 1_1 YY N −
1Y
NY _1
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Since each step of the stage is 0.5μm, the pixel size at level 1 can be determined as:
1_1
*00005.0YY
N
N −
Similarly, the pixel size at all the levels could be determined. Since the pixel is not a perfect
square pixel, the pixel size would be averaged in both X and Y directions to be as the calibration
factor. This calibration factor is used as the conversion factor for the volume conversion from
pixel to metric unit.
The following table shows the calibration results from one of the experiments.
Experiment_Set_4 1 step = 0.5 um 0.00005
x initial x final step number step length pixel size pixel/step 1426 1892 2500 0.125 0.000268 0.1864 867 1346 2500 0.125 0.000261 0.1916 269 743 2500 0.125 0.000264 0.1896 537 1009 2500 0.125 0.000265 0.1888
1240 1719 2500 0.125 0.000261 0.1916 425 905 2500 0.125 0.00026 0.1920
avg 0.000263 0.1900
y initial y final step number step length pixel size pixel/step
762 1235 2500 0.125 0.000264 0.1892 1055 1530 2500 0.125 0.000263 0.1900 983 1456 2500 0.125 0.000264 0.1892 493 966 2500 0.125 0.000264 0.1892 158 632 2500 0.125 0.000264 0.1896 54 529 2500 0.125 0.000263 0.1900
Averageavg 0.000264 0.1895 0.189767
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APPENDIX 4
Rheometer Parallel-disks Sample Loading Procedure
The following is a very simple procedure that describes how to make a proper sample
loading onto the two fixture plates prior to the real measurement.
1. Lower the upper plate until it touches the bottom plate
2. Set the gap to zero
3. Raise the upper plate until the gap is 15 mm
4. Load the sample on the bottom plate
5. Lower the upper plate until the gap is 4mm
6. Close the cover and start sample heat at set temperature
7. Start to lower the upper plate with 0.5 mm at a time after the temperature reaches a set
point
8. Lower the upper plate at 2 mm gap from bottom plate
9. Trim the sample flush with the edge of the disks
10. Repeat steps 6 and 7
11. Lower the upper plate at 1.5mm gap from bottom plate
12. Trim the sample flush with the edge of the disks
13. Repeat steps 6
14. Start to lower the upper plate with 1.0 mm gap distance
15. Start the rheometer experiment
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APPENDIX 5 Table Molecular Weight Information of Linear, Branched PP and PS Sample Linear DM55 PP Branched HMS WB 130 PP PS 685D
Mw (g/mol) 481,750 654,039 338,800 Mn (g/mol) 105,473 122,395 196,200
Mw/ Mn 4.57 5.34 1.73 Molecular Weight Distribution of Linear and Branched PP
2 3 4 5 6 7 8-0.1
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
Wei
ght f
ract
ion,
d(w
t)/d(
log(
MW
)))
Log(MW)
Linear PP DM55
Molecular Weight Distribution for Linear PP DM55
2 3 4 5 6 7 8-0.1
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
Wei
ght f
ract
ion,
d(w
t)/d(
log(
MW
)))
Log(MW)
Branched PP HMS WB130
Molecular Weight Distribution for Branched PP HMS WB130
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APPENDIX 6
Swelling Ratio Results for Linear and Branched PP Table 1) Volume Swelling of Linear PP/CO2 at High Temperatures and Pressures Temperature(oC) 180oC
Swelling SE Error 200oC
Swelling SE Error 220oC
Swelling SE Error
Pressure (psi) 1000 1.02943 0.01555 1.01633 0.0013 1.01049 0.006271500 1.06437 0.01024 1.04834 0.0017 1.04064 0.0052 2000 1.10236 0.00772 1.0807 0.0039 1.0632 0.007322500 1.13401 0.00657 1.11105 0.00456 1.09107 0.006023000 1.16766 0.00575 1.1384 0.00227 1.11745 0.004423500 1.18741 0.0065 1.1593 5.43547E-4 1.14413 0.0059 4000 1.21233 0.00572 1.17519 0.00202 1.15738 0.002 4500 1.22621 0.0091 1.18751 0.00145 1.1668 0.00456
Table 2) Volume Swelling of Branched PP/CO2 at High Temperatures and Pressures Temperature(oC) 180oC
Swelling SE Error 200oC
Swelling SE Error 220oC
Swelling SE Error
Pressure (psi) 1000 1.02644 0.0018 1.01083 0.00244 1.00295 0.00141 1500 1.05647 0.00111 1.03413 0.0039 1.02743 0.00158 2000 1.098 0.00468 1.06597 0.00628 1.05408 0.00279 2500 1.12964 0.00228 1.09803 0.0082 1.08004 0.00217 3000 1.15805 0.00414 1.12338 0.00619 1.10723 3.98093E-43500 1.17643 0.00373 1.14829 0.00165 1.13041 0.00137 4000 1.19597 0.00749 1.16124 0.00455 1.14743 0.0014 4500 1.2124 0.01189 1.17419 0.013 1.15405 0.00201
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APPENDIX 7
TGA Test Results
220oC
250oC
1) Heat and Hold Test for a) Linear and Branched PP at 220oC for 3 Hours and b) for PS at 250oC for 1.5 Hours
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2) Temperature Ramp Test for Linear and Branched PP
3) Temperature Ramp Test for PS 685D Virgin Sample, Sample Out of Vacuum Oven
and Sample after Experiment
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APPENDIX 8
MSB Absorption Test for Saturation Time Determination 1) Linear PP/CO2 at 180oC
0 200 400 600 800 1000 1200
13.8
14.1
14.4
14.7
Wei
ght (
g)
Time (min)
1800C Linear PP/CO2 Saturation
190 200 210 220 230 240 250 260 270 280 290 300 310 320
14.11
14.12
14.13
14.14
Wei
ght (
g)
Time (min)
1800C Linear PP/CO2 Saturation
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2) Branched PP/CO2 at 180oC
0 100 200 300 40014.0
14.2
14.4
14.6
Wei
ght (
g)
Time (min)
1800C Branched PP/CO2 Saturation
90 95 100 105 110 115 120 125 130 135 140 145 150 155 160
14.40
14.42
14.44
Wei
ght (
g)
Time (min)
1800C Branched PP/CO2 Saturation