MULTILAYER CO-EXTRUSION AND TWIN-SCREW COMPOUNDING OF POLYMERIC ELASTOMER SYSTEMS by RONGZHI HUANG Submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy Thesis Advisor: Prof. Joao M. Maia Department of Macromolecular Science and Engineering CASE WESTERN RESERVE UNIVERSITY August, 2014 1 CASE WESTERN RESERVE UNIVERSITY SCHOOL OF GRADUATE STUDIES We hereby approve the thesis/dissertation of Rongzhi Huang __________ candidate for the _______Ph.D.______degree *. (signed)________Prof. Joao Maia__________________ (chair of the committee) _______Prof. Eric Baer__________________________ _______Prof. Liming Dai________________________ _______Prof. Kenneth Singer_____________________ (date) 06/19/2014_________ *We also certify that written approval has been obtained for any Proprietary material contained therein. 2 DEDICATION To my parents, Xiaolin Huang and Guihong Wang, and to my beloved wife, Yang Liu. 3 TABLE OF CONTENTS LIST OF TABLES ...............................................................................................................7 LIST OF FIGURES .............................................................................................................8 ACKNOWLEDGEMENTS ...............................................................................................16 ABSTRACT .......................................................................................................................18 PART I: Multilayer Co-extrusion of Rheologically Mismatched Polymers CHAPTER 1: Introduction to multilayer co-extrusion Introduction ...................................................................................................................21 References .....................................................................................................................28 CHAPTER 2: Co-extrusion Layer Multiplication of Rheologically Mismatched Polymers: A Novel Processing Route Abstract .........................................................................................................................38 Introduction ...................................................................................................................39 Experimental and method .............................................................................................40 Results and discussion...................................................................................................43 Conclusions ...................................................................................................................51 References .....................................................................................................................53 Tables ............................................................................................................................55 Figures ...........................................................................................................................57 4 CHAPTER 3: Continuous Co-Extrusion of Rheologically Mismatched Polymers Using Rectangular Multiplier Dies Abstract .........................................................................................................................73 Introduction ...................................................................................................................73 Experimental and method .............................................................................................75 Results and discussion...................................................................................................78 Conclusions ...................................................................................................................84 References .....................................................................................................................86 Tables ............................................................................................................................89 Figures ...........................................................................................................................93 CHAPTER 4: Micro-confinement Effect on Gas Barrier and Mechanical Properties of Multilayer Rigid/Soft Thermoplastic Polyurethane Films Abstract .......................................................................................................................125 Introduction .................................................................................................................126 Experimental and method ...........................................................................................128 Results and discussion.................................................................................................131 Conclusions .................................................................................................................137 References ...................................................................................................................138 Tables ..........................................................................................................................141 Figures .........................................................................................................................143 PART II: Twin-screw Compounding Process for Thermoplastic Elastomer 5 CHAPTER 5: Understanding the Distribution and Dispersion of Mineral Oil in Polypropylene/Styrene-Ethylene-Butadiene-Styrene Blends Upon Compounding Abstract .......................................................................................................................160 Introduction .................................................................................................................160 Experimental and method ...........................................................................................162 Results and discussion.................................................................................................165 Conclusions .................................................................................................................168 References ...................................................................................................................169 Tables ..........................................................................................................................171 Figures .........................................................................................................................173 APPENDIX Interplay Between Rheological and Structural Evolution of Benzoxazine Resins During Polymerization Introduction .................................................................................................................183 Experimental and method ...........................................................................................185 Results and discussion.................................................................................................187 Conclusions .................................................................................................................193 References ...................................................................................................................194 Figures .........................................................................................................................197 Bibliography ...................................................................................................................210 6 LIST OF TABLES CHAPTER 2 Table 2.1 Relaxation spectra of PS/PMMA ......................................................................55 Table 2.2 Parameters for POLYFLOW® simulation of PS/PMMA ................................56 CHAPTER 3 Table 3.1 Geometry parameters of the square and rectangular multiplier die .................89 Table 3.2 Extrudate dimensions from different multiplier dies .......................................90 Table 3.3 Oxygen permeability of multilayer TPU films (thickness: 300 um).................91 Table 3.4 Oxygen permeability of stretched multilayer TPU films ........................................92 CHAPTER 4 Table 4.1 Comparison of integrated endothermic peak of “hard-segments domains” in nominal 65-layer film with 75% stretching at different temperatures ............................141 Table 4.2 Mechanical properties of extruded TPU films ...............................................142 CHAPTER 5 Table 5.1 The different feeding time of PP/oil/SEBS in the internal batch mixer (unit: second) ............................................................................................................................171 Table 5.2 Twin screw configuration: the order starts from feeder to exit die; each conveying element is 2.4 cm, and each kneading element is 0.6 cm; every 4 kneading elements together have the same twisting angle in arrangement ....................................172 7 LIST OF FIGURES CHAPTER 1 Figure 1.1 Top: Layer-multiplying co-extrusion system; Bottom left: The standard multiplier die; Bottom right: Flow stacking mechanism in the die ...................................31 Figure 1.2 The AFM phase image (left) of an EAA/PEO film with nominal PEO individual layer thickness of 20 nm showing single lamellae crystals in PEO layer, and the oxygen permeability of PEO layer (right)....................................................................32 Figure 1.3 The illustration of viscous encapsulation .......................................................33 Figure 1.4 The schematics of elastic instability (left) and secondary flow (right) ...........34 Figure 1.5 The interfacial instability in the multilayer film .............................................35 Figure 1.6 The elastic recoil in a square channel from the entrance (left) to exist (right) 36 Figure 1.7 The processing window of viscosity matched system (left), and mismatched system (right) .....................................................................................................................37 CHAPTER 2 Figure 2.1 General schematics of the visualization multiplier die...................................... 57 Figure 2.2 Schematics of the cross section of the 9-layer feedblock.................................. 58 Figure 2.3 Schematics of the second-generation modular multiplier die .......................... 59 Figure 2.4 Rheological results for PS/PMMA (a), (b) and TPUs (c), (d): G’- closed symbols, G’’- open symbols ................................................................................................... 60 8 Figure 2.5 Trouton ratio as function of Hencky strain for PS 615 (a), PMMA V100 (b), and PMMA V826 (c); PTT fitting curves are in solid lines ................................................ 61 Figure 2.6 Trouton ratio as function of Hencky strain for Isoplast® 2530 (left) and TPU B (right) .......................................................................................................................................... 62 Figure 2.7 Visualization results of layered structure at the end of the 2-layer feedblock and the first generation multiplier dies (only half of the extrudate is shown due to the symmetry) .................................................................................................................................. 63 Figure 2.8 Progression of viscosity matched (a-d) and mismatched (e-h) flow along multiplier die for 32 layer films .............................................................................................. 64 Figure 2.9 Comparison between experiment and simulation results at the end of multiplier die (only half of the extrudate is shown due to the symmetry) .......................... 65 Figure 2.10 N2 in the first generation multiplier die: (a) viscosity matched PS/PMMA, (b) viscosity mismatched PS/PMMA ........................................................................................... 66 Figure 2.11 Visualization of viscosity mismatched PS/PMMA by using classical feedblock and the first generation multiplier die (a-c; 8, 32 and 128 layers, respectively), or 9-feedblock and the second-generation multiplier die, (d-g; 9, 17, 33 and 65 layers, respectively) .............................................................................................................................. 67 Figure 2.12 Visualization of viscosity mismatched TPUs by using classical feedblock and the first generation multiplier die (a-c; 5, 9 and 17 layers, respectively), or 9feedblock and the second-generation multiplier die, (d-g; 9, 17, 33 and 65 layers, respectively) .............................................................................................................................. 68 9 Figure 2.13 Simulations of the velocity profile (top) and N2 (bottom) of viscosity mismatched PS/PMMA ............................................................................................................ 69 Figure 2.14 Simulation results of viscosity mismatched PS/PMMA in the secondgeneration multiplier die with different wall-slip conditions (from top to bottom: 0%, 25%, 80%, 100%)...................................................................................................................... 70 Figure 2.15 Visualization results of viscosity mismatched PS/PMMA with external lubricant: (a) feedblock, (b)-(d) from the first multiplier die (17 layers) to the third multiplier die (65 layers) ......................................................................................................... 71 Figure 2.16 Visualization results of elasticity mismatched TPUs with external lubricant: (a) feedblock, (b) after the first multiplier die (17 layers), (c) after the second multiplier die (33 layers), (d) after the third multiplier die (65 layers) (e) film after the third multiplier and coat-hanger die (65 layers). Note the significant improvement in the layering compared to no lubricant as shown in figure 13d-g ............................................... 72 CHAPTER 3 Figure 3.1 The schematics of the square (a) and rectangular (b) multiplier die ............... 93 Figure 3.2 Rheological results for PS/PMMA (a), (b) and TPUs (c), (d): G’ is represented by closed symbol and G’’ is represented by open symbol .............................. 94 Figure 3.3 Simulations of the velocity profile (a) and N2 (b) of PS/PMMA .................... 96 Figure 3.4 Simulation results of PS/PMMA at the output of the rectangular multiplier die with different friction at the walls (from top to bottom: full, 1/2, 1/6, and no friction) ... 97 Figure 3.5 OM results of the extrudates of PS/PMMA from: (a) square dies, (b) rectangular dies ......................................................................................................................... 98 10 Figure 3.6 OM results of the extrudates of TPUs from: (a) square dies, (b) rectangular dies .............................................................................................................................................. 99 Figure 3.7 Cross-section AFM phase images of 65-layer PS/PMMA films prepared by square (a) and rectangular (b) multiplier dies ..................................................................... 100 Figure 3.8 Analytical measurements on normalized individual layer thickness of 65-layer PS/PMMA prepared by different multiplier dies................................................................. 101 Figure 3.9 Distribution of individual layer thickness of 65-layer PS/PMMA films prepared by (a) square dies, (b) rectangular dies ................................................................ 102 Figure 3.10 Cross-section AFM phase images of 65-layer TPU films prepared by square (a) and rectangular (b) multiplier dies .................................................................................. 103 Figure 3.11 Analytical measurements on normalized individual layer thickness of 65layer TPU prepared by different multiplier dies ................................................................. 104 Figure 3.12 Distribution of individual layer thickness of 65-layer TPU films prepared by (a) square dies, (b) rectangular dies ...................................................................................... 105 Figure 3.13 OM results of the extrudates of PS/PMMA with different nominal numbers of layers: (a) 129, (b) 257, (c) 513, (d) 1,025 ....................................................................... 107 Figure 3.14 Ratio of the lengths of flat interfaces to PS/PMMA extrudates as function of number of layers ..................................................................................................................... 108 Figure 3.15 OM results of the extrudates of TPUs with different nominal numbers of layers: (a) 129, (b) 257, (c) 513, (d) 1,025 ........................................................................... 110 Figure 3.16 Ratio of the lengths of flat interfaces to TPU extrudates as function of number of layers ..................................................................................................................... 111 11 Figure 3.17 Cross-section AFM phase images of PS/PMMA multilayer films with different nominal numbers of layers: (a) 65, (b) 129, (c) 257, (d) 513, (e) 1,025............ 114 Figure 3.18 Analytical measurements on normalized individual layer thickness of PS/PMMA multilayer films: (a) 65, (b) 129, (c) 257, (d) 513, and (e) 1,025 layers ...... 116 Figure 3.19 Distribution of individual layer thickness of PS/PMMA films with different numbers of layers (a) 65, (b) 129, (c) 257, (d) 513, and (e) 1,025..................................... 118 Figure 3.20 Cross-section AFM phase images of TPU multilayer films with different nominal numbers of layers: (a) 65, (b) 129, (c) 257, (d) 513, (e) 1,025 ........................... 121 Figure 3.21 Analytical measurements on normalized individual layer thickness of TPU multilayer films: (a) 65, (b) 129, (c) 257 layers .................................................................. 122 Figure 3.22 Distribution of individual layer thickness of TPU films with different numbers of layers (a) 65, (b) 129, (c) 257 ............................................................................ 123 Figure 3.23 Oxygen permeability of 65 layers TPU films with different conditions. .... 124 CHAPTER 4 Figure 4.1 Rheological results of TPUs: (a) steady shear mode and (b) oscillation shear mode; (c) extensional rheology for Isoplast® 2530, and (d) TPU B ..............................143 Figure 4.2 AFM phase images of TPU B (left), and Isoplast® 2530 (right) .................144 Figure 4.3 AFM phase images of bilayer Isoplast® 2530/TPU B: low magnification (left), high magnification (right) .....................................................................................145 12 Figure 4.4 Morphologies of nominal 65-layer Isoplast® 2530/TPU B films: (a) OM picture of film as extruded; AFM phase images of (b) extruded, (c) 75% stretched, and (d) 300% stretched films .................................................................................................146 Figure 4.5 Oxygen permeability of extruded and stretched TPU films .........................147 Figure 4.6 Oxygen permeability of 75% stretched TPU films ......................................148 Figure 4.7 DSC results of extruded and stretched TPU films (heating rate=10 oC/min-1) ..........................................................................................................................................149 Figure 4.8 DSC results of 75% stretched TPU films (heating rate=10 oC/min-1) ...........150 Figure 4.9 Schematic illustration for micro-confinement effect on forming “hardsegments domain” in Isoplast® 2530 layer, and microscopic fracture at very high deformation, in which yellow layer is Isoplast® 2530 and dark blue layer is TPU B, orange boxes are hard segments and light blue spots are chain extenders .....................151 Figure 4.10 Normal direction 2-D WAXS patterns for various TPU films: TPU B (a), Isoplast® 2530 (b), 65-layer (c), 65-layer with 75% stretch (d), nominal 65-layer with 300% stretch (e) ..............................................................................................................153 Figure 4.11 1-D WAXS profiles of various TPU films .................................................154 Figure 4.12 Oxygen permeability of 75% stretched nominal 65-layer film as function of temperatures ....................................................................................................................155 Figure 4.13 DSC results of nominal 65-layer film with 75% stretching at different temperatures ....................................................................................................................156 Figure 4.14 3-D profile on oxygen permeability of nominal 65-layer film depending on stretching ratio and temperatures ....................................................................................157 13 Figure 4.15 Stress-strain curves for various TPU films: (a) full scale, (b) initial area zoomed in ........................................................................................................................158 CHAPTER 5 Figure 5.1 Pictures of oil absorption in PP (a-c), and SEBS (d-f) phase at room temperature............................................................................................................................... 173 Figure 5.2 Optical pictures of PP/oil/SEBS with different mixing time: 15-45-15 (left), 15-30-30 (right) ...................................................................................................................... 174 Figure 5.3 DMA results of PP/oil/SEBS with different mixing time .............................. 175 Figure 5.4 DMA results for extruded PP/oil (8:1) (a), SEBS/oil (8:1) (b), and SEBS/oil (1:1) (c) blends ........................................................................................................................ 177 Figure 5.5 DMA results for the extruded TPE system after one and two compounding cycles ........................................................................................................................................ 178 Figure 5.6 BDS of the 1st and 2nd pass samples ................................................................. 179 Figure 5.7 Oscillation shear rheology of 1st and 2nd pass samples: (a) dynamic moduli as function of frequency; (b) complex viscosity as function of frequency ........................... 180 Figure 5.8 AFM phase images of TPE: (a) sample from 1st pass, (b) sample from 2nd pass ................................................................................................................................................... 181 APPENDIX Figure A.1 Ring-Opening mechanism of P-ddm ............................................................... 197 Figure A.2 1H NMR spectra of P-ddm ................................................................................ 198 14 Figure A.3 Influence of polymerization temperature on polymerization kinetics for Pddm ........................................................................................................................................... 199 Figure A.4 Polymerization kinetics of P-ddm as a function of tan δ; (a) 140oC, (b) 160oC, (c) 180oC, (d) 200oC, (e) 220oC ............................................................................................ 201 Figure A.5 Time for P-ddm to reach the final plateau in dynamic moduli ..................... 202 Figure A.6 Intermolecular hydrogen-bonding structure; (a) intermolecular H-bonding structures between monomer and opened benzoxazine, (b) opened Mannich base H-bonds to each other ............................................................................................................................ 203 Figure A.7 Polymerization kinetics of P-ddm as a function of temperature ................... 204 Figure A.8 Stress relaxation at different stages of the polymerization process of P-ddm ................................................................................................................................................... 205 Figure A.9 Non-isothermal DSC of P-ddm ......................................................................... 206 Figure A.10 Non-isothermal DSC of P-ddm after crosslinking ....................................... 207 Figure A.11 IR spectra of P-ddm with different polymerization stages at 140oC; (a) Monomer, (b) 1st tan δ peak, (c) 2nd tan δ peak, (d) cured P-ddm .................................. 208 Figure A.12 IR spectra of P-ddm at different polymerization temperatures and temperature sweep; (a) 140oC, (b) 140oC, (c) 140oC, (d) 140oC, (e) T sweep ................. 209 15 ACKNOWLEDGMENTS First, I would like to express my sincere gratitude to my thesis advisor, Prof. Joao Maia for his guidance, encouragement and support during my graduate studies. His professional approach to education and research has been invaluable to my career. I greatly appreciate to be a member of his group, learning and working in the inspirational and cutting-edge research environment. I also want to thank other members in my thesis committee, Prof. Eric Baer, Prof. Liming Dai, and Prof. Kenneth Singer for their time and useful suggestions. I would also like to appreciate the opportunity to work in the science and technology Center for Layered Polymeric System (CLiPS) funded by National Science Foundation, in which I have been trained professionally and socially. The generous financial and technical support from Goodyear Tire and Rubber Company, Lubrizol Corporation, and Saint-Gobain Company is acknowledged. Especially, I would like to thank my collaborators, Prof. Roger Bonnecaze and Benjamin Huntington from UT Austin, for their great supports and inputs throughout my graduate career. Many thanks to Maia’s research group members, past and present, Jorge Silva, Mikio Yamanoi, Alison Rodier, Arman Boromand, Chaitanya Danda, Creusa Ferreira, Jesse Gadley, Jia Liu, Parker Lee, Patrick Harris, Ricardo Andrade, Sangjin Lee, Seyedsafa Jamali, Shaghayegh Khani, Sidney Carson, Unique Luna, Xue Chen, for their support, cooperation, friendship. The Department of Macromolecular Science and Engineering has been a friendly, interactive and social environment during my graduate studies. To Kezhen Yin, William Lenart, Guojun Zhang, Cong Zhang, Hong Xu, Jia Wang, Shanzuo Ji, Yijian Lin, Chuan16 yar Lai, Shannon Armstrong, Zheng Zhou, Pengfei Cao, Matthew Herbert, Alex Jordan, Joey Mangadlao, Seyedali Monemian, Sun Hua, Mingze Sun, Saide Tang, Jung-Kai Tseng, Rocco Viggiano, Nandula Wanasekara, Amanda Way, Lianyun Yang, Tiffany Burt, Keon-Soo Jang: thank you for contribution to our harmonious “Macro family”. Finally, I extremely appreciate my parents and my wonderful wife for their great support and interest in my thesis. 17 Multilayer Co-extrusion and Twin-screw Compounding of Polymeric Elastomer Systems by RONGZHI HUANG Abstract Polymeric elastomers that possess plastic and rubber characteristics are diverse in applications and exist in many forms, such as thermoplastic elastomer (TPE) and thermoplastic polyurethane (TPU). According to different applications, the methods to process these elastomers may involve extrusion, injection molding, thermoforming, and blow molding. In this thesis, the first part mainly focuses on the co-extrusion of TPU, and the second part is about twin-screw compounding of TPE. Multilayer films prepared by co-extrusion have been extensively studied in the last two decades due to the outstanding performance in gas barrier, mechanical, optical, and dielectric properties. However, there are two limitations of the current process: first, the co-extruded materials are limited to thermoplastics; second, the polymers to be layered need to have the similar viscoelasticity. To broaden the processing window and materials selection for more applications, co-extrusion of highly elastic and rheologically mismatched polymers (e.g. TPUs) becomes necessary. In this case, there are four typical processing instabilities needed to be solved: viscous encapsulation, elastic instability, interfacial instability, and elastic recoil. Therefore, in the first part of this thesis, chapter 1 will briefly introduce the state-of-the-art in co-extrusion of rheologically mismatched polymers. Specifically, chapter 2 will discuss a new processing route involving both 18 engineering and materials solutions to address the processing instabilities. However, this approach has a limitation of producing the uniform films with more than 65 layers. Chapter 3 will address this by incorporating the rectangular multiplier dies with aspect ratio of 4:1. Then, the structure-properties relationship and micro-confinement effect of the multilayer TPU films prepared by the new approach will be discussed in chapter 4. The second part of this thesis, chapter5, will present a study on the effects of batch and continuous mixing methods of a three component thermoplastic elastomer, TPE, system of mineral oil polypropylene (PP) and Styrene-Ethylene-Butadiene-Styrene (SEBS). 19 PART I: Multilayer Co-extrusion of Rheologically Mismatched Polymers 20 CHAPTER 1 Introduction to multilayer co-extrusion 1.1 Introduction Multiphase materials with superior properties to those of one-component polymers have been extensively studied, such as polymer blends, block co-polymers, and nanocomposites [1-7]. Specific processing techniques involving self-assembly, in-situ polymerization and layer-by-layer assembly are able to tailor the multiphase materials to highly ordered structure in micro- or nano-scale, which enhance the properties and broaden the applications [8-11]. However, these methods require solvents, are expensive, not environmentally friendly, and are very difficult to scale up to commercial products in industry. Melt compounding using twin-screw extruder or batch mixer is a solvent-free process that is able to achieve co-continuous or “island-sea” morphology for polymer blends and exfoliated fillers in nanocomposites via strong shear force. This process can be easily scaled up, but it’s difficult to prepare the blends with ordered structure and nanocomposites with homogeneous distribution and dispersion. The layer-multiplying co-extrusion system that was originally developed nearly five decades ago by Tollar James works by using either two or more extruders to feed material into a feedblock followed by one or more multiplier dies as illustrated in Figure 1.1 [12]. This is a continuous melt-processing method that has throughput of 20 lbs./hour and is very easily to be scaled up. In each multiplier die the layered polymers are split vertically, compressed and expanded, and then recombined one on top of the other, which 21 doubles the number of layers [13, 14]. The process is repeated for each multiplier die. If the feedblock produces two layers, the final number of layers after n multipliers is 2n+1. This solvent-free process is not only cost-effective and environment-friendly, but is also able to tune the structure of layered polymeric system from nano- to micro- scale, which cannot be achieved by traditional polymer blends. With the current state-of-the-art, up to 4,096 layers of thicknesses as thin as 20 nm can be co-extruded [15]. When the ultrathin layers of crystalline polymers are prepared, such as polyethelyne oxide (PEO), the single and high-aspect-ratio lamellae crystals are obtained due to the nanoconfinement of the other immiscible polymer layers. The single lamellae crystals are able to change the path of the gas molecules through the film, and reduce the permeability (oxygen) by two orders of magnitude (Figure 1.2) [15]. The mechanical properties of the multilayer films can also be enhanced. Previous studies show that when a brittle polymer, PEO, is layered with a ductile polymer, poly(ethylene-co-acrylic acid) (EAA), the elongation at break of multilayer film increases to 400%, compared with 14% in single PEO layer and 340% in single EAA layer, because the stress relief based on the interaction of the microcraks in PEO with EAA layers is able to alleviate crazing [16, 17]. By tuning the hierarchical structure and layered configuration, the multilayer films possess outstanding performance in gas barrier, capacitor, Bragg reflector laser, and data storage [18-24]. However, a major limitation of the current co-extrusion process is that the different polymer melts need to have similar viscosities and elastic properties [25]. In fact, layer-multiplying co-extrusion is prone to a number of defects such as viscous 22 encapsulation, interfacial and elasticity instabilities when rheologically mismatched polymers are co-extruded, which will be discussed in details in next paragraphs [26-29]. Viscous encapsulation due to the mismatched viscosities of the co-extruded materials is the most common instability in multilayer co-extrusion. Figure 1.3 shows that along the extrusion direction the low-viscosity layer A tends to migrate to the walls with maximum stress and encapsulate the high-viscosity layer B [26]. The capsulation velocity calculated from the arc length of the high-viscosity layer is the highest at the entry of the die and decreases progressively down the channel because the low-viscosity layer is occupying a large portion of the high shear-stress region near the walls as the polymer melts flow down the channel [26]. Borzacchiello et al. used 3-D simulations to further investigate the mechanism behind the viscous encapsulation in straight die [30]. Instead of isolating the viscous encapsulation from the elastic rearrangement as presented in the previous literatures, Borzacchiello et al. conclude that the viscous encapsulation is a second-order effect of the second normal-stress difference (N2), and there are two regimes during the encapsulation [30]. In the first regime, once the two layers come into the straight die and contact each other the pressure gradient pushes the low-viscosity layer (low pressure one) until the equilibrium is achieved, the interface then shifts rapidly because the high-viscosity layer moves as a protrusion into the low-viscosity one. This phenomenon also depends on the layer composition and flow rate. In the second regime, due to the unbalanced N2, the interface having the greatest absolute N2 near the walls moves towards the midplane with the lowest N2 [30]. Secondary flow due to N2 is also a main source of the degradation in layer structure during the multiplier process [26, 31, 32]. As Dooley points out, elastic layer 23 arrangement still occurs even that the co-extruded materials have well matched viscosities. Figure 1.4 shows the two-layer polystyrene structure at the output of a square channel. Since the identical materials are layering, the distorted interface is absolutely not because of the viscous encapsulation but the result of elastic force causing the secondary flows in the square channel. Yue et al. compared the elastic rearrangement of two viscoelastic fluids in non-circular and circular channel by 2-D numerical simulation [32]. They found that this instability arises from two mechanisms: the first is due to the mismatch in N2 of the two fluids, and the second is about the geometry of the channel [32]. While a curtate cycloid interface is observed in circular channel, the less elastic layer is wrapped by more elastic layer in non-circular die [32]. Another layer deformation in co-extrusion process is the interfacial instability because of the interfacial slip between different layers, as shown in Figure 1.5. The interfacial distortion can cause inhomogeneous distribution of individual layer thickness while keeping the total thickness of the film constant [26, 33-35]. Depending on flow rates, the interfaces might have very different morphology. For example, smooth interfaces appear with low flow rate and wavy interfaces occur when high flow rate is used [26, 36]. The interfacial instability is also related to extensional viscosities of the coextruded polymers. When the layers are spread in a coat-hanger die, the stretching rate will affect the force in each layer. A wave pattern could happen when the materials with high extensional viscosities are spreading at a high rate [26]. Last but not the least, the elastic recoil is the one that should be taken into consideration for layer-multiplying co-extrusion. Figure 1.6 shows that even that two 24 identical polymers are co-extruded, the secondary flows at the corners of channel are observed [26, 37]. Overcoming these processing instabilities to broaden the processing window and materials selection range is a priority if new applications for the technology are to be developed. In current practice, the pairs of materials must fall into one of two categories in order for them to be usable in continuous multi-layering processes (Figure 1.7). The first is that of materials that have an “ideal viscosity match”, which means that at some temperature both materials must have almost equal viscosities [14]. The second category is one where the materials must have the “off-set temperature match”, which means that both materials must have almost matched viscosities at different temperatures but within a 20°C range (to minimize thermal gradients and instabilities). However, the conditions mean that up until now very high viscosity materials such as thermoplastic elastomers or rubber, and very low viscosity materials, such as liquid crystal polymers (LCPs), could not be co-extruded [38]. It is well known that LCPs have excellent gas barrier and optical properties, and elastomers have ductile mechanical properties. Multilayer co-extrusion of these two types of materials potentially might combine the advantages and enhance the properties superior to each single one. Micro- or nano-confinement can also benefit, if one can layer the rheologically mismatched polymers. For example, using a high-viscosity polymer to confine the lowviscosity polymer foam is able to control the foam size, one of the most important factors in polymer foams [39]. Nanocomposites prepared by traditional methods have difficulty to achieve good distribution and orientation, which, on the other hand, could be improved by layering a high-viscosity polymer to confine the filled-polymer layer [40, 41]. 25 Hard/soft thermoplastics that had never been layered before could be prepared as strong and ductile films/tubes through the new technique. Therefore, the first part of the thesis focuses on multilayer co-extrusion of rheologically mismatched polymers via rheology, visualization, 3-D simulation, processing additives, re-designing the feed block, multiplier die, and coat-hanger die. Then, once the technique is developed, the structure-properties relationship of the multilayer rheologically mismatched polymer films will be studied. In Chapter 2, visualization of the multilayer flows in the multiplier dies is performed to study the mechanisms of different processing instabilities. Both engineering and materials solutions then are proposed to expand the processing window that can be co-extruded and layered. Viscous encapsulation is going to be minimized by optimizing the re-designed feedblock and multiplier die to prevent crossing flows in the layers. Secondary elastic flows are reduced by promoting wall slip via the processing aids, essentially external lubricants. Experiments and finite element simulations (FEM) simulations using ANSYS POLYFLOW® are used to demonstrate the success of these approaches. In Chapter 3, the research focuses on to further improving multilayer co-extrusion of rheologically mismatched polymers, especially when thousands of layers are necessary for achieving specific properties in optical lens and food packaging films [42, 43]. The external lubricant that is immiscible with most of polymers acts as the insulating layer between polymer melts and the walls inside the dies, and is used to significantly reduce the second normal-stress difference (N2) at the wall and eliminate elasticity instabilities. However, the layer thickness of external lubricant will become thinner and thinner as the 26 number of interfaces among multilayer increases. At 65 layers, the external lubricant is too thin to exhibit the lubricating effect. Therefore, the rectangular multiplier die is designed, which incorporates the idea of “constant cross-sectional area” and has the aspect ratio of 4:1 at the output. A 9-layer feedblock, rectangular multiplier die system, and external lubricant are combined to reduce processing instabilities such as viscous encapsulation, interfacial and elastic instabilities and prepare the films with more than one thousand layers. In Chapter 4, a flexible soft TPU, TPU B, and an engineering TPU, Isoplast® 2530, are layered using the developed technique described in the last two chapters. TPU B works well in applications where the polymer is required to bend and break, but it does not have strong gas barrier properties due to its high free volume. By contrast, Isoplast® 2530 consists of 100% hard-segments and has excellent gas barrier properties, but it is too rigid for various applications. When these two materials are multilayered, the resulting material is aimed to possess both high gas barrier properties, and relatively good flexibility. The extruded multilayer TPU films then are uniaxially stretched to different amount of deformation. The structural developments in micro-scale upon stretching is investigated and related to the gas barrier and mechanical properties. 27 1.2 References 1. Shi, W., Lynd, N. A., Montarnal, D., Luo, Y., Fredrickson, G. H., Kramer, E. J., Ntaras, C., Avgeropoulos, A., Hexemer, A., Macromolecules, 47, 2037 (2014) 2. Liu, H., Chen, F., Liu, B., Estep, G., Zhang, J., Macromolecules, 43, 6058 (2010) 3. Moungthai, S., Mahadevapuram, N., Ruchhoeft, P., Stein, G. E., ACS Appl. Mater. & Interfaces, 4, 4015 (2012) 4. Alig, I., Pötschke, P., Lellinger, D., Skipa, T., Pegel, S., Kasaliwal, G. R., Villmow, T., Polymer, 53, 4 (2012) 5. Yoo, Y., Tiwari, R. R., Yoo, Y-T., Paul, D. R., Polymer, 51, 4907 (2010) 6. Andrade, R. J., Huang, R., Herbert, M. 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Res., 27, 1326 (2012) 30 Figure 1.1: Top: Layer-multiplying co-extrusion system; Bottom left: The standard multiplier die; Bottom right: Flow stacking mechanism in the die [14]. 31 Figure 1.2: The AFM phase image (left) of an EAA/PEO film with nominal PEO individual layer thickness of 20 nm showing single lamellae crystals in PEO layer, and the oxygen permeability of PEO layer (right) [15]. 32 Figure 1.3: The illustration of viscous encapsulation [26]. 33 Figure 1.4: The schematics of elastic instability (left) and secondary flow (right) [26]. 34 Figure 1.5: The interfacial instability in the multilayer film [26]. 35 Figure 1.6: The elastic recoil in a square channel from the entrance (left) to exist (right) [26]. 36 Figure 1.7: The processing window of viscosity matched system (left), and mismatched system (right) [14]. 37 CHAPTER 2 Co-Extrusion Layer Multiplication of Rheologically Mismatched Polymers: A Novel Processing Route NOTE: Parts of this work have been submitted or published in “Huang, R.; Patz, J.; Silva, J.; Andrade, R.; Harris, P.; Yin, K.; Huntington, B.; Bonnecaze, R.; Cox, M.; Maia, J. M. Int. Polym. Proc., submitted” “Maia, J., Huang, R., Cox, M., U.S. Provisional Patent Appl. No. 61/901,482 (2013)” Abstract In chapter 2, co-extruded films with up to 65 layers of two rheologically mismatched polymer systems--polystyrene/poly(methylmethacrylate)(PS/PMMA) and hard/soft thermoplastic polyurethanes (TPUs)--were successfully produced using a combination of a 9-layer feedblock, low-pressure drop multiplier dies, and external lubricants. Formation of viscoelastic instabilities was studied using a custom visualization and by finite element method (FEM) simulations of a standard multiplier. The results showed that the flow inside the standard multiplier die is highly non-uniform, with severe gradients in shear and normal stresses and viscous encapsulation occurring mainly in the initial multiplication stages where there is enough material available in the low-viscosity layers to proceed with the encapsulation. To mitigate layer degradation the standard 2- or 3-layer feedblock was replaced with a 9-layer one, thereby decreasing the thickness of each layer at the end of the feedblock. Also, subsequent layering was performed using a low flow resistance die. This new multiplier die yields a more uniform flow profile and imparts a more homogeneous thermo-mechanical history on the melt 38 which results in an improved layer stability. Simulations showed that in the standard die the second normal-stress gradients responsible for elastic instabilities at the edges of the die are very high. These can be reduced by inducing slip at the wall resulting in be much improved layer uniformity and stability. This was accomplished experimentally via the use of external lubricants, and the resulting layered structure was indeed much better than was possible to achieve with the conventional multiplier dies. 2.1 Introduction Multilayer polymeric films have drawn much attention due to their outstanding barrier, dielectric and optical properties [1-3]. As mentioned in Chapter 1, the major drawback of the current process to prepare the multilayer films is that it requires the matched viscoelasticity of the different polymer melts to be co-extruded [4-8]. There are four types of processing instabilities, especially for rheologically mismatched polymers, during multilayer co-extrusion: viscous encapsulation, elastic instability, interfacial instability, and elastic recoil [9-13]. It’s necessary to understand the mechanisms behind these instabilities and improve the process prior to new applications for the technology to be developed. Therefore, in this work, two solutions are proposed to expand the processing window and the range of materials that can be co-extruded and layered. Viscous encapsulation is minimized by optimizing the feedblock and multiplier die to prevent crossing flows in the layers. Secondary elastic flows are reduced by promoting wall slip via the processing aids, essentially external lubricants. Experiments and finite element simulations (FEM) simulations using ANSYS POLYFLOW® are used to demonstrate the success of these approaches. 39 2.2 Experimental and method 2.2.1 Materials Two commercial poly(methyl methacrylates) (PMMA), Plexiglas® VS100 and Plexiglas® V826 and one polystyrene (PS), Styron 615APR, were purchased from Arkema and Styron, respectively. PMMA and PS are incompatible polymers, however, so there is the question of whether interfacial slip plays a role in the multiplication process, so a second system made up of chemically compatible aromatic thermoplastic polyurethanes (TPUs), one “hard” made up almost exclusively of hard segments, Isoplast® 2530, and one “soft” made up of 52% hard segments, TPU B, and provided by Lubrizol Advanced Materials, Inc. were used. For some of the layering experiments, 1.5 wt% external lubricants, TR 131 or TR 251 from Struktol Company, were mixed with PS/PMMA or TPUs [14]. These lubricants are composed primarily of unsaturated primary amide. 2.2.2 Rheological Measurements Steady and oscillation shear experiments were performed on a rotational rheometer (Thermo Fisher MARS III). PS and PMMA were vacuum dried for 24 hours at 70°C, while TPUs were dried for 36 hours at 80°C prior to characterization. The rheological experiments were conducted under a nitrogen atmosphere in order to avoid oxidative degradation of the samples. The experiments were performed at 205oC for TPUs or 240oC for PS and PMMA. Time-temperature superposition was performed using the IRIS® software. The uniaxial extensional flow measurements were conducted using 40 and Sentmanat Extension Rheometer (SER) accessory [15], with sample preparation and loading following our suggested protocol [16, 17]. 2.2.3 Simulation Method The multimode Phan-Thien-Tanner (PTT) model was applied to fit the rheological behavior and simulate the flow of PS 615, PMMA VS 100 and PMMA V826, which are considered to be incompressible and isothermal throughout the multiplier dies by ANSYS POLYFLOW® [18]. Each mode of PTT model obeys the following relations: ∇ 𝝉= 1 𝜆𝑖 𝛼 exp � 𝑡𝑟𝝉� + 𝜉 (𝑫. 𝝉 + 𝝉. 𝑫) = 2𝐺𝑖 𝑫 𝐺𝑖 ∇ 𝜕𝝉 𝝉 = − ∇𝐯𝑇 . 𝝉 − 𝝉. ∇𝐯 𝜕𝑡 (1) (2) where Gi and λi are the relaxation spectra that was obtained from IRIS® calculation and relaxation time of mode i, respectively. Even though the complete relaxation spectra of the polymers were obtained, given the typical residence times of the melt in the multiplier dies and in order to save the computation time, only Gi at the longest relaxation time was used in the simulations. D is the rate of deformation tensor. The adjustable parameters (ξ and α) control the fitting in shear and extensional flows respectively, and are kept constant for all relaxation modes. The viscosity η1 , is given by η=1 (1 − ηr ) η , η = η 2 + η1, (3) (4) 41 where ηr = η2 . η 2 + η1 (5) Here the equations and parameters governing the simulation are the same as those used in our previous works [17-19]. The parameters for the three different polymers used in the simulations are summarized in Table 2.2. 2.2.4 Co-Extrusion System and Conditions The system that was used to extrude the samples was comprised of two Killion extruders, model #19782, two Zenith melt pumps, model #K46LP56, and different numbers of multiplier dies. The velocity of the melt was controlled by the speed of the melt pumps, which was set to 5 rpm, corresponding to melt velocities of 1x10-7 m3/s. The PS/PMMA systems (PS 615, PMMA VS 100 and PMMA V826) were extruded at 240°C, while the TPUs (Isoplast® 2530 and TPU B) were extruded at 205°C. A visualization multiplier die similar to the first generation multiplier die was used to collect samples, the only difference being that the former separates into four sections to facilitate sample removal. The appearance of the standard die flow channel is shown in Figure 2.1. The defining characteristic of the channel is the initial asymmetrical cross-sectional contraction of the channel, followed by a similarly asymmetrical expansion of the area in the latter half. The samples were extracted from the visualization die after cooling and were cut into five sections as shown in Figure 2.1. This allowed the flow patterns to be examined at four different locations along the flow path. After cutting, 42 the cut faces of the samples were polished using 800 and then 4000 grit sandpaper. The polished sample faces were observed under a microscope and pictures of the faces were taken. The pictures were then used for comparison and understanding of the formation of flow instabilities, as will be discussed in the results and discussion section. 2.2.5 9-layer feedblock and the second generation multiplier die In order to minimize interface deformation during the early layering stages, when the layers are thicker, a 9-layer feedblock (schematically shown in Figure 2.2) with the same output cross section area as the standard 2-layer or 3-layer feedblock was used. This was coupled to a new-generation modular multiplier die recently developed by our research group, mainly by Patrick Harris, which decreases pressure drop by more than 40% and provides a much more homogeneous thermo-mechanical history to the melt, as well as a more symmetrical flow [17]. This new die (schematically depicted in Figure 2.3) keeps the total cross-sectional area constant throughout a wedge-shaped channel that imposes the simultaneous contraction and expansion of the melt; it was shown to decrease viscous encapsulation dramatically when two rheologically mismatched polymers are layered [17]. 2.3 Results and discussion 2.3.1 Rheological results The shear viscosity, storage and loss moduli of all materials are shown in Figure 2.4. Even though PMMA V826 shows a more pronounced shear-thinning behavior, the shear viscosity of PMMA V826 is about one order of magnitude higher than that of PS 615 and PMMA VS100 at the low shear rates typical of multi-layering co-extrusion (~1-5 43 s-1). PMMA V826 also shows significantly higher storage moduli than both PS 615 and PMMA VS100. The relaxation spectra of PS 615, PMMA VS 100 and PMMA V826 are calculated by the IRIS® software and shown in Table 2.4. For the TPU systems, Isoplast® 2530 and TPU B, the viscosity ratio in the appropriate range of shear rates is over 10:1 and the elasticity ratio is higher than 100:1 in the relevant shear rate range. Due to TPU’s complicated copolymer structure, IRIS® was not capable of calculating the relaxation spectra, so no numerical simulations are performed for these systems. The Trouton ratio as function of Hencky strain of the PS and PMMA melts is depicted in Figure 2.5 PS 615 shows a relatively small strain-hardening at rates above 1 s-1, while PMMAV100 only shows strain-hardening at the highest strain rate of 10 s-1, as does PMMA V826 but to a much smaller degree. Figure 2.6 shows the extensional rheology for the TPU systems. While strain-hardening behavior of TPU B is observed at each deformation rate, it shows only at the highest strain rate of 10 s-1 for Isoplast® 2530. As shown in Figure 2.4, the PTT model fits the linear viscoelastic behavior of PS 615, PMMA VS 100 and PMMA V826 at all frequencies. For the extensional rheology, it should be noted that the PTT model (shown in Figure 2.5 as solid lines) is able to fit the extensional rheological results at low strain rates, but not at 10 s-1 because at this rate the deformation is already essentially elastic and the model is no longer valid. Considering that the strain rate and Hencky strain in the multiplier die is low, the PTT model should be able to be applied in the numerical simulations, as per our previous works [19]. Due to the symmetrical design of the multiplier die, only half of the multiplier die is simulated in this work. 2.3.2 Visualization of layered structure – the standard die 44 Images were generated from all the cut and polished samples, but due to the large resulting number of images only a select group, which shows a representative sub-group of the data, will be discussed. In particular, samples were generated for 2, 4, 8, 16, 32, 64, and 128 layers but for the sake of simplicity, in this paper only results for 2, 8, 32, and 128 layers will be shown. The left column of Figure 2.7 shows the layered structure at the end of each multiplier die for the case of viscosity matched system, and a relatively even layer formation with increasing number of layers is observed. Important discrepancies in layer formation to note are the uneven layer area exiting the feedblock. Conversely, the exiting ends of the viscosity-mismatched samples can be seen on the right in Figure 2.7, and it is clear that these are very different from the previous ones. As in the case of the viscositymatched samples, the areas of the two polymers are uneven directly after exiting the feedblock. In the 8-layer viscosity mismatched sample, the early stages of viscous encapsulation are already observable, with the PS phase starting to encapsulate the PMMA phase. Another important trait of these pictures is that a void is formed in the sample in the center, where there is a large amount of PS. This void is due to the different cooling and contraction rates of PS and PMMA, which cause the PS phase to rupture and distort the final solid sample (there is no indication that the voids are present in the melt). In the 32-layer viscosity mismatched sample, the void is still present, but there is still evidence of significant viscous encapsulation. Finally, in the 128-layer viscosity mismatched sample, the layer thicknesses throughout the sample are still visibly uneven and viscous encapsulation can still be observed. One interesting feature is that as the number of layers increases it seems to stabilize the process, which was unexpected but is 45 probably due to the progressively lower amount of low viscosity material available for encapsulation in each low-viscosity layer as they become thinner. The evolution of layer formation and thickness was also observed along the flow path from the beginning to the end of one multiplier for all cases, with representative results shown in Figure 2.8 for 32-layer viscosity matched and mismatched samples. In both cases, and since these systems begin as bilayers, there is more PS on the top of the samples and more PMMA on the bottom. Figure 2.8 (a-d) shows that for the rheologically matched system the layer thickness decreases in a relatively even fashion across all the layers and some slight elastic folding occurs, especially near the center of the die, along the entire flow path. In the flow path progression with viscositymismatched polymers, depicted in Figure 2.8 (e-h), very different results are observed. In the beginning of the multiplier, there are 16 layers but they all have different thicknesses, there existing large PS-only and PMMA-only areas. PS has congregated into a thick middle layer while the PMMA accumulates in a round section on the left side of the middle area and shows a thicker layer in the bottom half of the sample. During the compression section of the multiplier, no real changes take place in the layer formation. However, there are significant changes in the expansion section of the multiplier. PS seems to migrate more towards the right wall during the expansion phase further increasing the uneven layer formation. At the exit of the multiplier die, it can be seen that the PMMA is not as prominent in the middle of the sample and has been replaced by PS further increasing the unevenness of the layered structure. Computational simulations were performed by the UT Austin partners in order to further investigate and understand the dynamics of viscous encapsulation. As can be seen 46 in Figure 2.9, the agreement between the two is excellent, especially after the feedblock and the first multiplier die. The first layer configuration that was investigated was the two-layer system that is seen directly out of the feedblock. This is an important starting point because the PS/PMMA ratios are an even 1:1 and the interface is expected to be flat. However, both the experiments and the simulations predict an uneven distribution, with a slight bending of the interface near the wall, which results in a larger area of PS than PMMA. Concomitantly, the average velocities are also not the same (because the flow rates are), with the velocity of the PMMA layer being higher. In the viscositymismatched polymers, the same phenomenon is seen in both the experimental and simulation results. After the viscosity-matched melts pass through one multiplier, the four resulting layers show that the PS still occupies a slightly larger area than the PMMA, a feature that is also shown in the simulations. In the viscosity-mismatched pair of polymers, the interface between the two polymers has shifted and the interface is highly bent. Along the outer walls, PS has moved up to a higher position and thus is taking up more of the cross sectional area. This is the beginning of viscous encapsulation. In the comparison regarding the 8-layer viscosity matched samples, the simulation is still predicting the layer shape and thickness relatively accurately. There is not a simulation example of the eight layer system with mismatched-viscosity polymers because of software limitations upon the combination of the layer interfaces, which is nevertheless a sign that encapsulation was continuing. While looking at the progression of the layers and viscous encapsulation, the underlying cause is not readily apparent in the samples. However, it can be observed in 47 the simulations. Dooley showed that N2 is paramount to the development of elastic instabilities in co-extruded bi-layers in non-axisymmetric channels, and Figure 2.10 shows that N2 is also contributing significantly to layer distortion in our case [9]. In the viscosity-matched sample, N2 remains relatively low throughout the channel, except during the expansion section where it shows a large spike upwards. The results for the viscosity mismatched materials show a similar trend but with a much higher value of N2 overall. It is also clear from analyzing both cases that the largest inflexion of the interface occurs at the points where N2 is highest, which is in accordance with the previous findings [9]. 2.3.3 Engineering solution: 9-layer feedblock and second generation multiplier die Figure 2.11 shows the layered structures resulting from the combined use of the different feedblock and multiplier dies for the high viscosity ratio PS/PMMA system. As can be seen, the uniformity of the layered structures through 9-layer feedblock and the second-generation multiplier dies are dramatically improved when compared with those obtained from the classical feedblock and the first-generation multiplier dies. Viscous encapsulation is still very much present but progresses at a much lower rate and the elastic instabilities also seem to be present to a much lower degree. This, in turn, has made it possible to observe a third instability mechanism, folding of the rigid PMMA layers near the walls. This is most likely caused by the difference in relaxation times between the two materials. The relaxation time of PS is about one decade shorter than that of PMMA, which also has a much higher viscosity. Thus, initially the interface bends due to non-zero N2 and both phases deform, but upon relaxation the PMMA cannot relax as quickly as the PS and, due to its high viscosity, it folds and causes the observed 48 morphology. Thus, while the generated layered structure is a significant improvement upon previous state-of-the-art, is still not acceptable for practical applications. In fact, above the limit of 33 layers, even though viscous encapsulation is controlled well by the 9-layers feedblock and the new die, interfacial and elastic instabilities are still severe and compromise the layer structure. As mentioned before, PS and PMMA are incompatible polymers, so low adhesion at the interface may be increasing material mobility between layers and aiding both viscous encapsulation and elastic instabilities. Therefore, the same experiments were performed for a rheologically mismatched but chemically compatible pair of TPUs as shown in Figure 2.12 (a-c). In these, both the viscosity and the elasticity ratios are higher than those of the PS/PMMA system. Viscous encapsulation is also observed in the TPU systems, co-extruded in a low-high-low viscosity configuration, which we will term A-BA. Figure 2.12 shows that the low viscosity TPU is already fully encapsulated after the first multiplier die (5 layers) and the layered structure completely disappears after the second (9 layers). As expected, improvement of the layered structure is shown when 9layer feedblock and the second-generation dies are applied. However, since the elasticity ratio between two TPU materials is much higher than that of PS/PMMA at approximately 100:1, the elastic instabilities are even more pronounced for the TPU systems, as shown in Figure 2.12 (d-g). In this, it is clear that the “folding” edges caused by elastic instability begin inside the feedblock and destroy the layered structure at more than 33 layers. Taking advantage of symmetrical geometry of the second-generation multiplier die, 4.5 layers within half of the multiplier die were simulated for the mismatched 49 PS/PMMA systems; the results are shown in Figure 2.13. As can be seen, N2 distribute more evenly across the die than in the standard, first-generation one (see Figure 2.10). Additionally, the velocity profile is more consistent than that in the first multiplier die, showing nearly flat interfaces that match reasonably well with the experiments, except for the folding edges, which cannot be simulated since they are a consequence of the relaxation and not of the flow. 2.3.4 Reduction of N2: the effect of external lubricant From the results above, it is clear that if further improvement is to be accomplished the problem stemming from non-zero N2 has to be eliminated, since it is at the origin of the elastic instability and, indirectly, the folding of the edges. POLYFLOW® simulations, shown in Figure 2.14, clearly show that as the degree of wall slip increases, N2 is severely reduced and the interface between layers becomes more stable and flat. The low die drag enables most of the elastic deformations in the melts to relax quickly, minimizing the interfacial and elastic instabilities to a level that does not affect the layers’ structure in the second-generation multiplier die. Output profiles are zoomed in on the bottom. Processing aids, especially external lubricants, are able to provide extremely low friction coefficient at the wall, and were used in this work to achieve high levels of slip at the wall, and therefore minimize instability inception and propagation [20, 21]. Specifically, 1% of TR 251 wax and 1.5% of TR 131 wax were used for PS/PMMA or for TPUs, respectively, during layer-multiplying co-extrusion [14]. These amounts of external lubricant were determined experimentally as the ones that offered the best compromise between wall-slip, which is desired, and internal lubrication, which should 50 be avoided. Figures 2.15 and 2.16 show the results with external lubricant for both the rheologically mismatched PS/PMMA (Figure 2.15) and TPU (Figure 2.16) systems. As can be clearly seen, using the second-generation dies in conjunction with the appropriate amount of external results in a quite acceptable layered structure, much better than if no external lubricant is used (Figures 2.11 and 2.12 for PS/PMMA and TPU, respectively). In particular, the folding edges that were observed previously, are now much less significant. Thus, using the external lubricant results in the desired (and predicted computationally) interface stabilization effect due to the formation of an insulating layer between the melt and the metal, which reduces N2 dramatically. This stabilization effect is so dramatic that even for the most difficult to process system, the hard TPU/soft TPU one, it was possible to produce final 65-layer films with a total thickness of only 360 microns (which meant the melts had to go through a further coat-hanger die after the third multiplier). As shown in Figure 2.16 (e), the uniformity of the resulting layer structure in the film is very acceptable. When one considers that the viscosity ratio of the TPUs is over 10:1, the elasticity ratio is around two orders of magnitude, and the contract ratio in coat-hanger die is extremely high, these results represent a notable success. 2.4 Conclusions A new methodology for co-extruding multi-layered films (up to 65 layers) of rheologically mismatched polymers is presented. Flow development was visualized to help understand the kinetics of viscous encapsulation and elastic and interfacial instabilities for both high viscosity and elasticity ratio polymer systems. From this analysis it was evident that most of the low viscosity layers shift to the edge and encapsulation of the high viscosity layers occurred during the expansion section of the 51 multiplier die. These large areas also increased the chance of voids forming in the cooled sample. It was also observed that higher the number of layers, the slower the encapsulation process, due to the progressively lower amount of low viscosity material available for encapsulation. By combining a 9-layer feedblock and a new, secondgeneration multiplier die, viscous encapsulation is minimized and the uniformity of layered structure is dramatically improved. The interfacial and elastic instabilities in multilayer flow are further reduced by resorting to appropriate amounts of external lubricant, which is able to form an insulating layer between the melts and metal and reduce N2 caused by shear during processing in non-axisymmetric channels. The simulations correctly predict the shape and position of the interface between the polymers, and provided guidance into how much slip needs to be promoted at the wall to minimize the phenomenon of folding of the high viscosity, high elasticity layers. 52 2.5 References 1. Wang, H., Keum, J. K., Hiltner, A., Baer, E., Freeman, B., Rozanski, A., Galeski, A., Science, 323, 757 (2009) 2. Mackey, M., Schuele, D. E., Zhu, L., Flandin, L., Wolak, M. A., Shirk, J. S., Hiltner, A., Baer, E., Macromolecules, 45, 1954 (2012) 3. Lai, C.-Y., Ponting, M. T., Baer, E., Polymer, 53, 1393 (2012) 4. Carr, J. M., Mackey, M., Flandin, L., Hiltner, A., Baer, E., Polymer, 54, 1679 (2013) 5. Song, H., Singer, K., Lott, J., Wu, Y., Zhou, J., Andrews, J., Hiltner, A., Weder, C., J. Mater. Chem., 19, 7520 (2009) 6. Jin, Y., Tai, H., Hiltner, A., Baer, E., Shirk, J. S., J. Appl. Polym. Sci., 103, 1834 (2007) 7. Ryan, C., Christenson, C. W., Valle, B., Saini, A., Lott, J., Johnson, J., Schiraldi, D., Weder, C., Baer, E., Singer, K., Shan, J., Adv. Mater., 24, 5222 (2012) 8. Cheng, W., Gomopoulos, N., Fytas, G., Gorishnyy, T., Walish, J., Thomas, E. L., Hiltner, A., Baer, E., Nano Lett., 8, 1423 (2008) 9. Dooley, J.: Viscoelastic Flow Effects in Multilayer Polymer Coextrusion. Ph.D thesis, Eindhoven University of Technology, Netherlands (2002) 10. Anderson, P. D., Dooley, J., Meijer, H. E. H., Appl. Rheol., 16, 198 (2006) 11. Torres, A., Hrymak, A. N., Hilton, T., Rheol. Acta, 525, 513 (1993) 12. Hatzikiriakos, S. G., Migler, K. B. Polymer Processing Instabilities: Control and Understanding, Marcel Dekker, New York, (2005) 13. Nazarenko, S., Snyder, J., Ebeling, T., Schuman, T., Hiltner, A., Baer, E. SPEANTEC ‘96 Proceedings, Indianapolis, Indiana, May 5-9, (1996) 14. Huang, R., Maia, J., Cox, M., U.S. Provisional Patent Appl. No. 61/901,482 (2013) 53 15. Sentmanat, M. L., Rheol. Acta, 43, 657 (2004) 16. Barroso, V. C., Covas, J. a., Maia, J. M., Rheol. Acta, 41, 154 (2002) 17. Harris, P. J., Patz, J., Huntington, B. A., Bonnecaze, R. T., Meltzer, D., Maia, J., Polym. Eng. Sci., 54, 636 (2014) 18. Thien, N. P., Tanner, R. I., J. Non-Newtonian Fluid mech., 2, 353 (1977) 19. Huntington, B. A., Chabert, E., Rahal, Patz, J., S., Silva, J., Harris, P. J., Maia, J., Bonnecaze, R. T., Int. Polym. Proc., 3, 2741 (2013) 20. Joseph, D. D., J. Non-Newtonian Fluid Mech., 70, 187 (1997) 21. Treffler, B., Plastics, Rubber and Composites, 34, 143 (2005) 54 Table 2.1: Relaxation spectra of PS/PMMA. PS 615 Mode i PMMA VS100 PMMA V826 Gi (Pa) λI (s) Gi (Pa) λI (s) Gi (Pa) λI (s) 1 1.82 x 105 3.14 x 10-4 4.20 x 105 5.96 x 10-5 1.84 x 105 2.99 x 10-5 2 7.40 x 104 2.53 x 10-3 1.51 x 105 6.22 x 10-4 7.23 x 104 3.93 x 10-4 3 2.68 x 104 1.26 x 10-2 7.22 x 104 3.24 x 10-3 7.96 x 104 2.35 x 10-3 4 7.11 x 103 5.32 x 10-2 2.27 x 104 1.36 x 10-2 6.59 x 104 1.12 x 10-2 5 9.43 x102 2.33 x 10-1 3.08 x 103 6.02 x 10-2 3.66 x 104 5.12 x 10-2 6 3.62 x101 1.26 x 100 1.91 x 101 7.85 x 10-1 1.11 x 104 2.24 x 10-1 7 9.06 x 102 1.03 x 100 8 4.50 x 101 9.22 x 100 55 Table 2.2: Parameters for POLYFLOW® simulation of PS/PMMA PMMA VS100 PS 615 PMMA V826 ηr (Pa.s) 0.63 0.56 0.015 η (Pa.s) 39.99 102.47 926.50 ξ 0.546 0.510 0.336 ε 0.490 0.072 0.468 λ (s) 0.785 1.260 9.220 56 Figure 2.1: General schematics of the visualization multiplier die. 57 Figure 2.2: Schematics of the cross section of the 9-layer feedblock. 58 Figure 2.3: Schematics of the second-generation modular multiplier die. 59 Figure 2.4: Rheological results for PS/PMMA (a), (b) and TPUs (c), (d): G’- closed symbols, G’’- open symbols. 60 Figure 2.5: Trouton ratio as function of Hencky strain for PS 615 (a), PMMA V100 (b), and PMMA V826 (c); PTT fitting curves are in solid lines. 61 Figure 2.6: Trouton ratio as function of Hencky strain for Isoplast® 2530 (left) and TPU B (right) 62 Figure 2.7: Visualization of layered structure at the end of the 2-layer feedblock and the first generation multiplier dies (only half of the extrudate is shown due to the symmetry). 63 Figure 2.8: Progression of viscosity matched (a-d) and mismatched (e-h) flow along multiplier die for 32 layer films. 64 Figure 2.9: Comparison between experiment and simulation results at the end of multiplier die (only half of the extrudate is shown due to the symmetry). 65 Figure 2.10: N2 in the first generation multiplier die: (a) viscosity matched PS/PMMA, (b) viscosity mismatched PS/PMMA. 66 Figure 2.11: Visualization of viscosity mismatched PS/PMMA by using classical feedblock and the first generation multiplier die (a-c; 8, 32 and 128 layers, respectively), or 9-feedblock and the second-generation multiplier die, (d-g; 9, 17, 33 and 65 layers, respectively). 67 Figure 2.12: Visualization of viscosity mismatched TPUs by using classical feedblock and the first generation multiplier die (a-c; 5, 9 and 17 layers, respectively), or 9-feedblock and the second-generation multiplier die, (d-g; 9, 17, 33 and 65 layers, respectively). 68 Figure 2.13: Simulations of the velocity profile (top) and N2 (bottom) of viscosity mismatched PS/PMMA. 69 Figure 2.14: Simulation results of viscosity mismatched PS/PMMA in the second-generation multiplier die with different wall-slip conditions (from top to bottom: 0%, 25%, 80%, 100%). 70 Figure 2.15: Visualization results of viscosity mismatched PS/PMMA with external lubricant: (a) feedblock, (b)-(d) from the first multiplier die (17 layers) to the third multiplier die (65 layers). 71 (e) Figure 2.16: Visualization results of elasticity mismatched TPUs with external lubricant: (a) feedblock, (b) after the first multiplier die (17 layers), (c) after the second multiplier die (33 layers), (d) after the third multiplier die (65 layers) (e) film after the third multiplier and coathanger die (65 layers). Note the significant improvement in the layering compared to no lubricant as shown in figure 13d-g. 72 CHAPTER 3 Continuous Co-Extrusion of Rheologically Mismatched Polymers Using Rectangular Multiplier Dies NOTE: Parts of this work have been submitted or published in “Huang, R.; Chari, P.; Harris, P.; Zhang, G.; Huntington, B.; Bonnecaze, R.; Cox, M.; Maia, J. M. Polym. Eng. Sci., submitted” Abstract In this chapter, highly rheologically mismatched poly(styrene)/ poly(methylmethacrylate) (PS/PMMA) and polyester based thermoplastic polyurethanes (TPUs) were successfully layered to 65, 129, 257, 513, and 1,025-layer extrudates and films using a 9-layer feedblock, rectangular multiplier dies with an aspect ratio of 4:1 at output, and external lubricants. The extrudates directly from square and rectangular the multiplier dies were cut and polished to study the effect of geometry on the extent of viscous encapsulation, and elastic and interfacial instabilities via optical microscopy. The multilayer films were characterized by atomic force microscopy (AFM) to further study the layer uniformity and distribution of individual layer thickness after extruding from a coat-hanger style die, and the results related to the flow evolution and processing instabilities through the die studied by finite element method (FEM)—ANSYS POLYFLOW®. 3.1 Introduction Multilayer co-extrusion is not only a solvent-free process, but is also easy to be scaled up. By tuning the hierarchical structure and layered configuration, multilayer films 73 can be made that possess outstanding performance in gas barrier, capacitor, Bragg reflector laser, and data storage [1-7]. However, the materials to be co-extruded have to have the matched viscoelasticity to obtain uniform layer structure, which severely narrows the processing window and restricts applications [8, 9]. Many researchers have performed fundamental studies, including both experiments and simulations, to understand and overcome the viscous encapsulation and elastic instabilities during the layer-multiplication process [10-13]. In previous chapter, it was shown that rheologically mismatched polymers could be successfully layered to 65-layer films by re-designing the multiplier dies and using external lubricant. By doing so, instead of squeezing and then spreading the flow in the classical multiplier die, the cross-sectional area of a re-designed multiplier die always keeps constant to simultaneously squeeze and spread the flow so that the pressure drop is reduced by at least 40% [14]. The external lubricant (that is immiscible with most polymers) acts as an insulating layer between polymer melts and the inside walls of the dies, which promotes slip and reduces significantly the second normal-stress difference (N2) at the wall and elastic instabilities. However, the layer thickness of external lubricant will become thinner and thinner as the number of interfaces among multilayer increases. At 65 layers, the external lubricant is too thin to have a significant lubricating effect. Therefore, a solution needs to be found to further improve this process, especially when thousands of layers are necessary for achieving specific properties in specialized applications such as optical lens and high-performance packaging films [15, 16]. As Dooley pointed out in his thesis, even though elastic instabilities are still observed in a rectangular channel with the aspect ratio of 4:1, a fairly flat interface occurs 74 with distortions only near the edges of the channel, which is not the case in a square channel [10]. Therefore, in this work we use a new constant cross-section rectangular multiplier die with an aspect ratio of 4:1 at the outlet, combined with a 9-layer feedblock and external lubricant, to produce films with more than 1,000 layers of highly rheologically mismatched materials. 3.2 Experimental and method 3.2.1 Materials Polystyrene (PS), Styron® 615APR, and poly(methyl methacrylates) (PMMA), Plexiglas® V826, purchased from Styron company and Plexiglas company, respectively, were used as model systems. Two aromatic and polyester-based TPUs provided by Lubrizol Advanced Materials, Inc., ISOPLAST® 2530, consisting of 100% hardsegments and TPU B that contains 52% hard-segments were also used in this study. PMMA and ISOPLAST® 2530 were dried at 90 oC, and TPU B was dried at 70 oC for 48 hours before co-extrusion. 0.25 wt% yellow and red color dye (PE) were added into the resins to observe the layer uniformity of extrudates. 1.5 wt% external lubricants (TR 251, Struktol Company) that were mainly composed by unsaturated primary amide, were dry blended with PS/PMMA or TPUs to prepare the masterbatch for co-extrusion. 3.2.2 Rheological Measurements All the samples were characterized via a rotational rheometry (Thermo Fisher MARS III) according to the method introduced in Chapter 2. 3.2.3 Co-Extrusion System and Conditions 75 The multilayer co-extrusion system is described in Chapter 1, and the processing conditions used in this study are determined based on the rheological results. Since all of the samples are rheologically mismatched, 240 oC for PS/PMMA and 205 oC for TPUs were chosen as the co-extrusion temperature at which viscoelasticity ratio is minimum within the processing window. The combination of a 9-layer feedblock and the rectangular multiplier dies (Figure 3.1) that has an output area of 2.0×0.5 inches (5.08×1.27 cm) and an aspect ratio of 4:1 with a low pressure drop during layer multiplication was used to produce 65, 129, 257, 513, and 1,025 layers extrudates or films [17, 18]. In contrast, the square multiplier dies were also used to produce 65 layers extrudates and films, and the geometrical comparison between these two types of dies is listed in Table 3.1. The flow rate of the melt was set by the gear pumps at 10 rpm. Films were extruded through a 10-inch coat-hanger die and collected on a stainless take-off roller with temperature set at 80 oC. The thickness of the film is around 300 um. 3.2.4 Stretching films Film samples with dimension of 7.6 cm × 5 cm × 0.035 cm were prepared for uniaxial stretching. A MTS Alliance RT/30 testing machine at a gage length of 3 cm was used to stretch the samples along the extrusion direction at 120 oC. At these temperatures, the films were stretched to strain of 25%, 50% and 75% with deformation rate of 50% per min. After stretching, the samples were held tightly and slowly cooled down to room temperature. 3.2.5 Characterization 76 Extrudates directly from the rectangular multiplier dies were collected, cut and polished using 800 and then 4000 grit sandpaper. To analyze the layer uniformity, the polished sample faces were charaterizarized by optical microscopy (OM) involving an Olympus (Miami, FL) BH-2 optical microscope and a CCD camera. The extruded films from the coat-hanger die were also collected and were cut embedded and fixed in epoxy, which is cured at room temperature for 24 hours. To prepare the sample for atomic force microscopy (AFM), a Leica microsystmes EM FC6 ultramicrotome (Buffalo Grove, IL) was used to cut the cross-sections of the films at -70 oC at the direction perpendicular to extrusion. The films were examined by a Digital Laboratories Nanoscope IIIa AFM (Digital Instruments, Santa Barbara, CA) operating in tapping mode at room temperature. AFM phase and height images were analyzed via the NanoScope software to obtain modulus differences and morphology information. A MOCON OX-TRAN 2/20 (Minneapolis, MN) was used to measur the oxygen permeability of the TPU films at 25oC, 0% relative humidity, and 1 atm pressure. Mylar film (NIST certified) with known oxgen permeability was used to calibrate the Mocon machine. Then, both sides of the TPU films were masked by self-adhesive aluminum masks with a testing area of 5 cm2 at the center. Nitrogen was used to remove the atmospheric oxygen inside the chamber for 12 hours prior to testing. The testing method applied was referred to the work studied by Wang et al [9]. The oxygen permeability P(O2) was calculated based on the equation below. 77 In the equation, J is the steady state flux monitored by the Mocon machine, l is the total thickness of TPU film, D is the diffusivity, t is the flux time, and ∆p is the oxygen pressure difference across the film (1 atm). The unit of permeability used is Barrers [9]. 3.2.6 Simulation method The Phan-Thien-Tanner (PTT) model with Gi at the longest relaxation time was applied to fit the rheological behavior and simulate the flow of PS and PMMA, which were considered to be incompressible and isothermal throughout the rectangular multiplier dies by ANSYS POLYFLOW® [18]. The simulation is followed the method performed in Chapter 2. 3.3 Results and discussion 3.3.1 Rheological properties Rheological experiments are performed since rheology plays an important role in multilayer co-extrusion process, which normally requires matched viscoelasticity to obtain uniform layer structures. However, Figure 3.2 shows mismatched shear viscosities and dynamic moduli as function of shear rate or frequency of all the materials. The shear viscosity of PS 615 is one order of magnitude lower than that of PMMA V826 at the range of shear rates in co-extrusion from 0.5 to 1 s-1. PS 615 also shows significantly lower storage moduli than PMMA V826 around 0.5-1 rad/s. ISOPLAST® 2530 and TPU B have a viscosity ratio over 10:1 and an elasticity ratio more than 100:1 in the relevant shear rate or frequency range. It also should be noted that the PTT model fits well the 78 linear viscoelastic behavior of PS 615 and PMMA V826 at all frequencies, which enable the simulation that will be discussed later. 3.3.2 Simulation results POLYFLOW® simulations are able to accurately capture the evolution of the velocity and N2 profiles of PS/PMMA flow inside the die; Figure 3.3 shows that, in contrast to the square die, using the rectangular die results in a flat and stable interface throughout most of the width of the extrudate, with only small distortions being observed near the walls. This matches with the experiment results mentioned above. Our previous work has shown that a reduction of the friction at the walls can severely reduce N2 and improve the layer structure with stable and flat interfaces [12]. Now this wall-slip effect is combined with the high-aspect-ratio design showed in Figure 3.4. As the friction is lowest at the wall, interfacial and elastic instabilities are prevented and a highly uniform layer structure is obtained. 3.3.3 Comparison between the square and rectangular multiplier die Learning the results above, the rectangular multiplier die with aspect ratio of 4:1 at output is designed, which is combined with a 9-layer feedblock and external lubricants to layer rheologically mismatched materials. Figure 3.5 shows the OM results of the extrudates of PS/PMMA directly from the square (a) and rectangular multiplier (b) dies, where the yellow layers represent PMMA the red ones are PS. While the extent of viscous encapsulation in the extrudate of the square die is higher than that in the rectangular die, elastic instability occurs in both. However, given the high aspect ratio of 79 the rectangular die, the distorted interfaces are left near to the wall with much more flat and stable ones in the middle than those in the square die. Besides, as can be seen in Figure 3.1, the input and the “squeezing and spreading” section in rectangular multiplier dies are always kept flat and wide, while these sections in the square dies are vertical and narrow. These factors might lead to different layer structures in the two types of dies. An area where parts of flat interfaces are observed in Figure 3.5, and a related quantitative analysis is shown in Table 3.2. While the length of the flat interfaces in square die is 0.42 cm accounting for 33.60% length of the whole extrudate, a much longer length around 3.28 cm is measured in the rectangular die and accounts for 57.04% of the rectangular extrudate. Also, it is worth noting that: a) Even though the flat surface is relatively limited, a well-defined, if somewhat wavy layered structure is obsereved until close to the edges; b) The exit of the multiplier dies is much thicker than the final film and that inhomogeneities in the former will be minimized in the latter, as shall be seen later. This engineering solution successfully supplements the drawbacks of the material solution—i.e. external lubricants. In fact, even though the external lubricants are able to reduce N2 and elastic instability, the maximum loading of the external lubricants has to be around 1.5 wt%, because beyond this percentage the pressure in the extruder will be too low to push the melt forward in plug-flow conditions. This threshold, on the other hand, limits the thickness of lubricating layer between the polymer melt and metal and fails to decrease N2 enough when more than two multiplier dies are used because the lubricating layer becomes thinner and thinner during layer multiplication (interfacial area increases). 80 The TPU system (Figure 3.6), in which ISOPLAST® 2530 is in yellow and TPU B is in red, shows more viscous encapsulations and elastic instability than PS/PMMA due to the higher viscoelasticity ratio in TPUs. The length of flat interfaces and the relative ratio are lower than those of PS/PMMA (Table 3.2) as well. The rheologically mismatched PS/PMMA were then layered into 65-layer films (thickness~300 µm) through the square or rectangular multiplier dies, and a 10-inch coat hanger die. The layer structure of the cross section of the film is characterized by AFM (Figure 3.7) where the bright area is PMMA and the dark area is PS. Unlike the morphology observed in OM results, the interfaces between the PS/PMMA are very straight and sharp, which is a consequence of the film flatening induced by the coathanger die. The quantitative analyses based on these AFM pictures are performed by normalization and distribution of the individual layer thickness as shown in Figure 3.8 and 3.9. Even though the much longer flat interfaces in the rectangular multiplier die than those in square multiplier die are observed in OM pictures, there is no big difference of layer structures between the two types of films, in the areas of good layering. This is attributed to that the interfaces are fully stretched horizontally in the coat-hanger die, it does not matter how short the flat interfaces are in the multiplier die. The alternated fat/thin layer pattern is observed in films prepared by both types of multiplier dies. For example, the thinnest and thickest individual layer thickness from square dies are 0.86 and 9.46 µm, the average layer thickness being 4.38 µm with standard deviation of 2.42 µm. The thinnest and thickest ones from rectangular dies are 1.61 and 10.48 µm, and the average layer thickness is 4.58 µm with standard deviation of 2.85 µm. The reasons of such a deviation on individual layer thickness are that 1) The 9-layer feedblock has 81 different flow rates in the PMMA and PS channels, and the former flows through five channels, while the latter flows through four; 2) The low-viscousity PS tends to flow towards the edge encapsulating the high-viscosity PMMA, despite the use of a balanced multiplier die and external lubricants, a problem that is especially relevant in the coathanger die, which has a large contract ratio. Figure 3.10 shows the cross-section AFM phase images of the 65-layer TPU films (thickness ~400 µm). A well-defined multilayer structure is obtained even though the viscoelasticity ratio of two TPUs is around 2 orders of magnitude. The alternated fat/thin layer pattern is also observed in TPU films, and is more pronounced than that of PS/PMMA, because the former has higher viscoelasticity ratio than the latter. It should be noted that for TPUs the distribution of individual layer thickness from rectangular dies is more homogeneous than that from square dies. As shown in Figure 3.11 and 3.12, even though the individual layer thicknesses of both square and rectangular dies concentrate at the range of 4~6 µm, the results of square dies show more thick layers of 10~20 µm. While the average layer thickness from the square die is 6.20 µm with a standard deviation of 5.03 µm, the average layer thickness from the rectangular die is slightly more unform at 6.41 µm with a standard deviation of 4.56 µm. This is because that for a very high viscoelasticity ratio system, the flat input and simultaneous “squeezing and spreading” sections in rectangular dies are able to maintain a more homogeneous layer structure than square dies during the layer-muliplication process. 3.3.4 Extrudates with different numbers of layers in rectangular multiplier die 82 With the advantage of the rectangular multiplier die established in terms of relative workable area relatively to total film width, and of layer uniformty for the TPU systems, extrudates with higher numbers of layers were prepared using this multiplier. As can be seen in Figure 3.13, the viscous encapsulation, interfaces and elastic instabilities are progressively reduced and the layered structure becomes more and more uniform as the numbers of the layers increases, due to the increased confinement, which leaves less material available in each layer to propagate the instabilities. For example, at 1,025 layers, the individual layer thickness is around 12 µm, befeore spreading in the coat-hanger die. It should be noted that starting from 513 layers, it seems like there is no big difference between viscosity matched and mismatched system, which is in agreement with our prior findings (chapter 2). This can be better explained by analizing Figure 3.14, which shows that the ratio of the length of the flat interfaces to the extrudate (a/b) increases from 57.04% to 87.50% cm as the number of layers increases from 65 to 1,025. Figure 3.15 shows the OM results for TPU extrudates with numbers of layers from 129 to 1,025. The layer uniformity clearly improves visually as the number of layers increases, showing the same tendency observed in PS/PMMA. It should be noted that some of the interfaces in the 1,025-layer sample are blurred with some layer break-up. This is attributed to the interdiffusion between the two chemical compatible TPUs when the individual layer thickness achieves micro-scale, which will be discussed in details below. Figure 3.16 also shows that the ratio a/b in TPUs are lower than those of PS/PMMA at all numbers of layers. For both PS/PMMA and TPUs, 513-layer sample correponding to individual layer thickness of 25 µm is the threshold value to obtain 83 highly uniform multilayer structure when rheologically mismatched polymers are coextruded. 3.3.5 Films with different numbers of layers using the rectangular multiplier die Once the layered structure of the extrudates was understood, thin multilayered PS/PMMA and TPU films with increasing numbers of layers were also prepared via the rectangular multiplier dies. AFM phase images (Figure 3.17) show that continuous layers with straight and sharp interfaces are obtained in all PS/PMMA samples. Although the alternated fat/thin layer pattern is still observed, the layer structure becomes more and more uniform as the number of the layers increases showing the same trend as observed in extrudates. Figure 3.18 and 3.19 show that while at 65 layers the distribution of the individual layer thickness is very broad and discrete, a Gaussian distribution of the individual layer thickness concentrated at 0.3 µm is formed at 1,025 layers. This indicates a uniform multilayer structure is formed because the measured layer thickness of 300 nm is very close to the 293 nm nominal thickness of the 1,025-layer film. The multilayer structures of TPU films from 65 to 1,025 layers are shown in Figure 3.20. Due to the higher viscoelasticity ratio and interdiffusion, TPU films have worse layer uniformity than PS/PMMA, and there is no well-defined layer structure observed in the 513 and 1,025 layers film. Figure 3.21 and 3.22 show that the 65- and 129-layer TPU films have discrete distribution of inividual layer thickness and 257-layer has periodical ultra-fat/thin layer structure. According to our previous study focused on interdiffusion of co-extruded TPU, the interphase between two aromatic and polyester based TPU has a thickness around 2 µm [19]. Thus, starting from a 129-layer TPU film corresponding to nominally individual layer thickness of 2.3 µm, the interdiffusion 84 between two TPUs becomes very pronounced and they diffuse into each other when 513 and 1,025-layer film are produced. 3.3.6 Gas barrier properties of TPU films Gas (oxygen) permeabilities of TPU films are shown in Table 3.3. The multilayer films show decreased permeability as the number of the layers increases, even though the reduction is very small. The TPU chains, especially in glassy and amorphous Isoplast® 2530, are oriented during the squeezing and spreading process in slit multiplier dies, which leads to forming the impermeable “hard-segments domains” through intermolecular hydrogen bondings along the backbones that contain “–NH” and “C=O” groups. On the other hand, the interdiffusions partially ruin the impermeable structures when the individual layer thickness is reduced to a few microns. Then, the microconfinement effect on gas barrier properties is affected, and the gas permeability decreases by a very small amount only. Uniaxial stretching at 120 oC further helps orienting the TPU chains and forming the impermeable “hard-segments domains”. Table 3.4 shows a decreased permeability as the percentage of stretching increases for 65 layers. However, the reversed trend is observed for 129 and 257 layers, which, again, is due to the interdiffusion of TPUs. In order to exam the enhanced barrier properties that are due to uniaxial stretching, a controlled test, annealing the 65 layers TPU film at 120 oC (with the same time of stretching), is performed. In Figure 3.23, both the as-extruded and the annealed 65 layers films show the same permeability of 0.067 barrer, but the 75% stretched sample shows a 50% improvement of 0.031 barrer. 85 3.4 Conclusions In this study, PS/PMMA with viscoelasticity ratio of 10 and TPUs with viscoelasticity ratio of 100 were successfully co-extruded to 65, 129, 257, 513, and 1,025-layer extrudates and films through a 9-layer feedblock, the rectangular multiplier dies with an aspect ratio of 4:1 at output, and external lubricants. OM results show that the extrudates from rectangular multiplier die have longer, more stable and flatter interfaces than the ones from square die. The layer uniformity and distribution of individual layer thickness of multilayer films improve as the number of the layers increase due to the less amount of low viscous material at the edge available to encapsulate the high viscous one and micro-confinement effect. Simulation results show that the combination of high-aspect-ratio output and low friction at the wall help form the uniform layer structure. Due to inter-diffusion between the two polyester based TPUs, 257-layer film is the top limit to obtain a multilayer structure in TPU and 129 layers is the limit for which good, uniform layering is observed. 86 3.5 References 1. Cheng, W.; Gomopoulos, N.; Fytas, G.; Gorishnyy, T.; Walish, J.; Thomas, E. L.; Hiltner, A.; Baer, E., Nano Lett., 8, 1423 (2008) 2. Tseng, J.-K.; Tang, S.; Zhou, Z.; Mackey, M.; Carr, J. M.; Mu, R.; Flandin, L.; Schuele, D. E.; Baer, E.; Zhu, L., Polymer, 55, 8 (2014) 3. Lai, C.-Y.; Ponting, M. T.; Baer, E., Polymer, 53, 1393 (2012) 4. Singer, K. D.; Kazmierczak, T.; Lott, J.; Song, H.; Wu, Y.; Andrews, J.; Baer, E.; Hiltner, A.; Weder, C.; OPT. EXPRESS, 16, 10358 (2008) 5. Ryan, C.; Christenson, C. W.; Valle, B.; Saini, A.; Lott, J.; Johnson, J.; Schiraldi, D.; Weder, C.; Baer, E.; Singer, K. D.; Shan, J. Adv. Mater., 24, 5222 (2012) 6. Lott, J.; Ryan, C.; Valle, B.; Johnson, J. R.; Schiraldi, D. A.; Shan, J.; Singer, K. D.; Weder, C. Adv. Mater., 23, 2425 (2011) 7. Zhang, G.; Lee, P. C.; Jenkins, S.; Dooley, J.; Baer, E. Polymer, 55, 663 (2014) 8. Ponting, M., Hiltner, A., Baer, E., Macromol. Symp., 294, 19 (2010) 9. Wang, H., Keum, J. K., Hiltner, A., Baer, E., Freeman, B., Rozanski, A., Galeski, A., Science, 323, 757 (2009) 10. Dooley, J.: Viscoelastic Flow Effects in Multilayer Polymer Coextrusion. Ph.D thesis, Eindhoven University of Technology, Netherlands (2002) 11. Yue, P., Zhou, C., Dooley, J., Feng, J. J., J. Rheol., 52, 1027 (2008) 12. Huntington, B. A., Chabert, E., Rahal, Patz, J., S., Silva, J., Harris, P. J., Maia, J., Bonnecaze, R. T., Int. Polym. Proc., 3, 2741 (2013) 13. Anderson, P. D., Dooley, J., Meijer, H. E. H., Appl. Rheol., 16, 198 (2006) 87 14. Harris, P. J., Patz, J., Huntington, B. A., Bonnecaze, R. T., Meltzer, D., Maia, J., Polym. Eng. Sci., 54, 636 (2014) 15. Ji, S., Yin, K., Mackey, M., Brister, A., Ponting, M., Baer, E., Opt Eng., 52, 112105 (2013). 16. Carr, J. M., Langhe, D. S., Ponting, M., Hiltner, A., Baer, E., J. Mater. Res., 27, 1326 (2012). 17. Barroso, V. C., Covas, J. a., Maia, J. M., Rheol. Acta, 41, 154 (2002) 18. Thien, N. P., Tanner, R. I., J. Non-Newtonian Fluid mech., 2, 353 (1977) 19. Silva, J., Maia, J. M., Huang, R., Meltzer, D., Cox, M., Andrade, R., Rheol Acta, 51, 947 (2012). 88 Table 3.1: Geometry parameters of the square and rectangular multiplier die. Multiplier Die Inlet (inch) Outlet (inch) Aspect ratio Square die ¼×½ ½×¼ 1:1 Rectangular die 1 ×½ 2×¼ 4:1 89 Table 3.2: Extrudate dimensions from different multiplier dies Length of flat Length of extrudates Ratio of a and b interfaces (a) (b) (%) PS/PMMA 65L square 0.42 1.25 33.60 PS/PMMA 65L rectangular 3.28 5.75 57.04 TPUs 65L square 0.43 1.25 34.40 TPUs 65L rectangular 3.05 5.15 59.22 90 Table 3.3: Oxygen permeability of multilayer TPU films (thickness: 300 um) Number of layers Norminal individual layer Permeability thickness (um) (Barrer) 65 4.61 0.068 129 2.32 0.067 257 1.16 0.065 513 0.58 0.055 1,025 0.29 0.053 91 Table 3.4: Oxygen permeability of stretched multilayer TPU films Multilayer films with different Permeability (Barrer) percentage of stretching 65L 25% 0.051 65L 50% 0.046 65L 75% 0.031 129L 25% 0.055 129L 50% 0.060 129L 75% 0.062 257L 25% 0.058 257L 50% 0.064 257L 75% 0.070 92 (a) (b) Figure 3.1: The schematics of the square (a) and rectangular (b) multiplier die. 93 Figure 3.2: Rheological results for PS/PMMA (a), (b) and TPUs (c), (d): G’ is represented by closed symbol and G’’ is represented by open symbol. 94 (a) 95 (b) Figure 3.3: Simulations of the velocity profile (a) and N2 (b) of PS/PMMA 96 Figure 3.4: Simulation results of PS/PMMA at the output of the rectangular multiplier die with different friction at the walls (from top to bottom: full, 1/2, 1/6, and no friction). 97 (a) (b) Figure 3.5: OM results of the extrudates of PS/PMMA from: (a) square dies, (b) rectangular dies. 98 (a) (b) Figure 3.6: OM results of the extrudates of TPUs from: (a) square dies, (b) rectangular dies. 99 (a) (b) Figure 3.7: Cross-section AFM phase images of 65-layer PS/PMMA films prepared by square (a) and rectangular (b) multiplier dies. 100 Figure 3.8: Analytical measurements on normalized individual layer thickness of 65-layer PS/PMMA prepared by different multiplier dies. 101 (a) (b) Figure 3.9: Distribution of individual layer thickness of 65-layer PS/PMMA films prepared by (a) square dies, (b) rectangular dies. 102 (a) (b) Figure 3.10: Cross-section AFM phase images of 65-layer TPU films prepared by square (a) and rectangular (b) multiplier dies. 103 Figure 3.11: Analytical measurements on normalized individual layer thickness of 65-layer TPU prepared by different multiplier dies. 104 (a) (b) Figure 3.12: Distribution of individual layer thickness of 65-layer TPU films prepared by (a) square dies, (b) rectangular dies. 105 (a) (b) (c) 106 (d) Figure 3.13: OM results of the extrudates of PS/PMMA with different nominal numbers of layers: (a) 129, (b) 257, (c) 513, (d) 1,025. 107 Figure 3.14: Ratio of the lengths of flat interfaces to PS/PMMA extrudates as function of number of layers. 108 (a) (b) (c) 109 (d) Figure 3.15: OM results of the extrudates of TPUs with different nominal numbers of layers: (a) 129, (b) 257, (c) 513, (d) 1,025 110 Figure 3.16: Ratio of the lengths of flat interfaces to TPU extrudates as function of number of layers. 111 (a) (b) 112 (c) (d) 113 (e) Figure 3.17: Cross-section AFM phase images of PS/PMMA multilayer films with different nominal numbers of layers: (a) 65, (b) 129, (c) 257, (d) 513, (e) 1,025. 114 (a) (b) (c) 115 (d) (e) Figure 3.18: Analytical measurements on normalized individual layer thickness of PS/PMMA multilayer films: (a) 65, (b) 129, (c) 257, (d) 513, and (e) 1,025 layers. 116 (a) (b) (c) 117 (d) (e) Figure 3.19: Distribution of individual layer thickness of PS/PMMA films with different numbers of layers (a) 65, (b) 129, (c) 257, (d) 513, and (e) 1,025. 118 (a) (b) 119 (c) (d) 120 (e) Figure 3.20: Cross-section AFM phase images of TPU multilayer films with different nominal numbers of layers: (a) 65, (b) 129, (c) 257, (d) 513, (e) 1,025. 121 (a) (b) (c) Figure 3.21: Analytical measurements on normalized individual layer thickness of TPU multilayer films: (a) 65, (b) 129, (c) 257 layers. 122 (a) (b) (c) Figure 3.22: Distribution of individual layer thickness of TPU films with different numbers of layers (a) 65, (b) 129, (c) 257. 123 Figure 3.23: Oxygen permeability of 65 layers TPU films with different conditions. 124 CHAPTER 4 Micro-confinement Effect on Gas Barrier and Mechanical Properties of Multilayer Rigid/Soft Thermoplastic Polyurethane Films NOTE: Parts of this work have been submitted or published in “Huang, R.; Chari, P.; Tseng, J-K.; Zhang, G.; Cox, M.; Maia, J. M. J. Appl. Polym. Sci., submitted” Abstract Rigid/soft thermoplastic polyurethane (TPU) films were produced via layermultiplying co-extrusion and the effect of confinement on morphology and gas barrier and mechanical properties is studied. The soft TPU, which has 52% hard-segments, shows phase separation, while the rigid TPU with 100% hard-segments exhibits amorphous structures. Then, the multilayer TPU films are uniaxially stretched to different amounts of deformations, from 0% to 300%. Even though the viscosity ratio of the two TPUs is over 10 and the elasticity ratio around 100, optical and atomic force microscopies show that a multilayer structure is successfully achieved. DSC and WAXS results show that micro-confinement occurs during orientation, upon which a significant reduction in oxygen permeability of multilayer TPU film is observed when the films are stretched at 75% when compared to the mono and bi-layer TPU. In the meanwhile, the dependence of gas barrier properties on temperature and deformation is also investigated. Stress-strain curves of TPU films are obtained through MTS tensile machine, and 100% improvement on elongation at break is found when compared monolayer to multilayer TPU film. 125 4.1 Introduction Thermoplastic polyurethane (TPU) is an important elastomer exhibiting high melt strength, good mechanical properties, and excellent abrasion resistance, with many intricate applications ranging from biomaterials to footwear [1-4]. By tuning the composition of hard-segments and soft-segments during TPU synthesis, the material created can show a wide range of properties. It is well known that the gas barrier and mechanical properties of TPU depend on the amounts of hard-segments, which have a higher glass transition temperature than soft-segments [5-7]. The issue with the particular material is that with more hard-segments, the material becomes more rigid, and as a result, is not flexible enough for a number of applications, e.g., packaging. Soft-segments play an important role in phase separation via different chain lengths, chain extender structures and molecular weight of soft segments [8, 9]. When analyzing the balance of mixing relative fractions of hard and soft phases and its effect on the glass transition temperature, studies have shown that hydrogen bonding with ester groups is stronger than with ether groups [10]. Thus, by integrating ester groups, a stronger and more flexible material can be produced. Finding a good balance between these two phases will yield a material that has hard and soft phases, but also flexibility needed for various applications [7-10]. For example, if a TPU can be designed to contain both good gas barrier and flexibility characteristics, then devices such as biomedical bags/tubes can be produced. Creating multilayered polymeric systems through co-extrusion and biaxial stretching yields favorable characteristics, such as ultra-low gas permeability, high dielectric performance, gradient refractive index lens, 1-D photo crystals, and 3-D storage [11-20]. The purpose of using this layer-multiplying co-extrusion is to control the layer compositions and thickness of two polymers, and in doing so, allowing the maximization 126 of the effect of hierarchical structures and nano-confinement of the polymers [21-25]. Such an effect can also be achieved by adding nano-fillers into polymer matrix forming nanocomposites. For example, Dekun et al. have shown that adding organically modified nanoclays into TPU can decrease the gas permeability of the nanocomposites [26]. However, several issues have to be pointed out: first, such an improvement on barrier properties requires a very high amount of nanoclays, e.g. 10 wt%, which, on the other hand, decreases the elongation at break and tensile strength of TPU. Second, homogeneous distribution and exfoliated dispersion of nanoclays in TPU system is very difficult to achieve, especially at high contents of nanoclays where lots of agglomerations appear. The nano-confinement of polymer chains due to multi-layered co-extrusion is able to not only improve the strength of the material, but also significantly enhance the gas barrier properties especially when the individual layer thickness is around 30 nm, and single crystalline orientation is created [27-29]. This indicates that with a multilayer structure, the orientation of the crystalline structure is altered and can be manipulated to improve the mechanical properties and barrier properties of the TPU while maintaining the flexibility. Even though the structural changes at the micro-scale upon uniaxial stretching of TPU with various ratios of hard-segments are extensively studied, the uniaxial stretching on multilayer TPU under micro-confinement has never been studied [30, 31]. In this paper, a flexible soft TPU, TPU B, and an engineering TPU, Isoplast® 2530, are multilayered by co-extrusion. TPU B works well in applications where the polymer is required to bend and break, but it does not have strong gas barrier properties due to its high free volume. By contrast, Isoplast® 2530 consists of 100% hard-segments and has 127 excellent gas barrier properties, but it is too rigid for various applications. When these two materials are multilayered, the resulting material is aimed to possess both high gas barrier properties, and relatively good flexibility. 4.2 Experimental and method 4.2.1 Materials Two aromatic and polyester-based TPUs provided by Lubrizol Advanced Materials, Inc. were used in this study. A rigid TPU, Isoplast® 2530 consisted of 100% hard-segments, and a soft TPU B with 52% hard-segments were dried at 80 oC for 24 hours prior to processing. 1.5 wt% external lubricants (TR 251) provided by Struktol Company, which mainly compose unsaturated primary amide, were added into TPU during co-extrusion [32, 33]. Extensional rheometry experiments were performed in a SER device coupled to a Paar Physica MCR 501 rheometer. Sample preparation and loading followed the procedure recommended by Barroso et al., in order to ensure the samples were stress-free in not sagging at the beginning of the experiments [34]. 4.2.2 Rheological measurement The co-extrusion processing conditions were determined based on the shear rheological properties of Isoplast® 2530 and TPU B charaterized by rotational rheometry (Thermo Fisher MARS III). Since these two TPUs are rheologically mismatched, 205 oC was chosen as the co-extrusion temperature at which viscoelasticity ratio is minimum within the processing window. The combination of a 9-layer feedblock and a second generation multiplier dies recently developed by the authors is used to produce 65-layer TPU films [32, 33, 35]. The flow rates of the TPU melts were the same and set by 128 identical gear pumps. Films were extruded through a 3 inches coat-hanger die and collected on a stainless take-off roller with temperature set at 80 oC. Mono-layer and bilayer Isoplast® 2530 and TPU B films of 175 microns were also produced. 4.2.3 Stretching films Film samples with dimension of 7.6 cm × 5 cm × 0.035 cm were prepared for uniaxial stretching. A MTS Alliance RT/30 testing machine at a gage length of 3 cm was used to stretch the samples along the extrusion direction at 100 oC, 110 oC, 120 oC, and 130 oC. At these temperatures, the films were stretched to strain of 25%, 50%, 75%, 100%, 200%, and 300% with deformation rate of 50% per min. After stretching, the samples were held tightly and slowly cooled down to room temperature. 4.2.4 Characterization The mechanical tests of TPU films, stress-strain curves, were performed with a MTS Alliance RT/30 testing machine. TPU films were cut into “dog-bone” shape with dimension of 0.44 cm × 0.035 cm and uniaxially stretched until break at room temperature with deformation rate of 50% per min. Differential scanning calorimetric (DSC, TA Instruments Q-100) measurements were performed on both as-extruded and stretched TPU films ranging from -50 to 250 oC at a heating/cooling rate of 10 oC per min with sample sizes of 5-8 mg. Two dimensional wide angle X-ray scattering (WAXS) measurements were carried out on mono-, bi-, nominal 65-layer films with different percentage of stretching in the normal direction (ND) to characterize the molecular structure and orientation of the TPUs. WAXS experiments were performed under vacuum and at room temperature (25 129 o C), with an X-ray beam based on highly focused monochromatic CuKa (λ= 0.1542 nm) generated from a micro-focus X-ray generator (Rigaku, MicroMax-002, Woodlands, TX) that was equipped with two laterally graded multilayer optics side-by-side. This collimated monochromatic X-ray beam was operated at 45 kV and 0.88 mA by using three pinholes, with the diameter of the beam around 700 mm. The images then were taken by using Fujifilm magnetic imaging plates and were processed by a Fujifilm FLA7000 image plate reader. In order to obtain strong reflection patterns, extruded and stretched films were exposed for 8 and 16 h, respectively. TPU films were embedded and fixed in epoxy that is cured at room temperature for 1 day. A Leica microsystmes EM FC6 ultramicrotome (Buffalo Grove, IL) was used to microtome the cross sections of TPU films at -70 oC with direction perpendicular to extrusion. The layer uniformity of extruded and strectched 65-layer TPU films were charaterized by optical microscopy (OM) with an Olympus (Miami, FL) BH-2 optical microscope and a CCD camera. Mono-layer TPU films were examined with a Digital Laboratories Nanoscope IIIa AFM (Digital Instruments, Santa Barbara, CA) operating in tapping mode at room temperature. AFM phase and height images were analyzed via the NanoScope software to obtain modulus differences and morphology information. The oxygen permeability measurements of TPU films were conducted by a MOCON OX-TRAN 2/20 (Minneapolis, MN) at 25 oC, 0% relative humidity, and 1 atm pressure. Prior to testing, Mylar film (NIST certified) with known oxgen permeability was used to calibrate the Mocon machine. Then, both sides of the TPU films were masked by self-adhesive aluminum masks with a testing area of 5 cm2 at the center. Nitrogen was used to remove the atmospheric oxygen inside the chamber for 12 hours. 130 The oxygen permeability P(O2) was calculated from the equation below: P(O2) = J 𝑙 ∆P in which, J is the steady state flux minitored by Mocon machine, l is the total thickness of TPU film, and ∆P is the oxygen pressure difference across the film (1 atm). The unit of permeability used in this study is Barrers. 4.3 Results and discussion 4.3.1 Rheological properties The rheologically mismatched hard/soft TPUs with viscosity ratio over 10 and elasticity ratio of 100 at shear rate/frequency of 1 s-1 during co-extrusion [Figure 4.1 (ab)], were successfully layered to 65-layer films with dimension of 7.5 cm (width) × 0.035 cm (thickness). Extensional rheological tests are also performed on these two TPUs. In Figure 4.1 (c-d), TPU B shows strain-hardening behavior at all deformation rates, while Isoplast® 2530 mostly exhibites strain-softening except at the highest deformation rate of 10 s-1. The reason for the high melt strength of TPU B is the long-range order caused by phase seperation between soft and hard segments. The strong intermolecular interaction leads to high extensional viscosity during stretching. On the other hand, Isoplast® 2530, as an amorphous glassy TPU, consists of bulky polymer chains and yields to the deformation quickly, except at a very high deformation rate, where long-range, crystalline-like structures develop [36]. 4.3.2 Morphology 131 The morphologies of mono-, bi-, and multilayer TPUs films are charaterized by OM and AFM. As shown in Figure 4.2, while TPU B shows the long-range orders in which bright areas represent the hard-domines and the black parts are the soft-domines, Isoplast® 2530 shows an amorphous structure. Due to the chemical compatibility of TPUs, interdiffusion between Isoplast® 2530 and TPU B layer is expected and the crosssection of the bi-layer TPU film shown in Figure 4.3, in which a interphase with 2micron width is observed [37]. AFM phase images of nominal 65-layer TPU films (in Figure 4.4) reveal that good multilayered structures are achieved for both extruded and stretched films. The composition or layer thickness ratio is not 50/50 as expected because: a) despite the use of a balanced multiplier die and external lubricants there is still some residual encapsulation of the high-viscosity Isoplast® 2530 by the low-viscosity TPU B; b) The 9-layer feedblock used in this study yields different flow rates in the Isoplast® 2530 and the TPU B channels, because the total flow rates are the same and the former flows through five channels, while the latter flows through four. However, taking into consideration that the viscoelastic ratio of two TPUs is around 100, the multilayered structure created is a notable success. 4.3.3 Gas barrier properties Gas (oxygen) permeabilities of mono and multilayer TPU films are shown in Figures 4.5 and 4.6. As expected, the rigid Isoplast® 2530 has superior barrier properties than TPU B due to the higher percentage of hard segments. While the bilayer film exhibits a permeability in-between the two TPUs, the nominal 65-layer film shows even lower permeability than Isoplast® 2530. The multilayer films were further uniaxially 132 stretched to different strains at 100 oC. The stretched multilayer films show a decrease in permeability as the deformation increases up to 75%, but a decrease afterwards, up to the maximum stretch of 300%. Thus, the best gas barrier properties of 0.044 barrer were found for the 65-layer film with 75% stretch at this temperature. This represents an almost three-fold improvement relatively to the bilayer film, which has permeability of 0.12 barrer, and a five-fold improvement relatively to TPU B, which has a permeability of 0.235 barrer. Interestingly these variations of gas permeability with stretch are not observed if the monolayer Isoplast® 2530 film is uniaxially stretched. The explanation for this phenonmena will be discussed in next paragraphs. 4.3.4 Thermal properties The thermal properties of TPU films measured by DSC can be used to shed light into the observed tendency in oxygen permeability. In Figures 4.7 and 4.8, there are three pronounced endothermal peaks at 165 oC, 175 oC, and 195 oC, representing dissociation of long-range order in TPU B, fragmented hard-segment domains (see below) and main hard-segment domains in Isoplast® 2530, respectively [5-7, 38, 39]. While both monolayer and bilayer TPU films show almost no endothermal peak around 195 oC, coextruded and stretched (up to 75%) multilayer TPU films exhibit large peaks at this temperature. Further stretching from 100% to 300% on the multilayer films makes the endothermal peak shift from 195 oC to 175 oC. When 75% stretched monolayer Isoplast® 2530 film and multilayer film are compared, the former only shows a tiny bump around 195 oC. Based on the permeability and thermal results of TPU films, the mechanism of enhanced barrier properties is proposed as shown in Figure 4.9. When mono or bilayer 133 TPU film are extruded, the TPU chains, especially in Isoplast® 2530, with isotropic and bucky structure due to the thick individual layer thickness are not able to form impermeable “hard-segments domains” connected by intermolecular hydrogen bondings between “–NH” and “C=O” groups along the backbone [38, 39]. Once the TPUs are layered into multilayer structure with individual layer thickness around 6 microns, under micro-confinement the polymer chains are oriented through the simultaneous squeezing and spreading process happened in multiplier dies, and start constructing “hard-segments domains”. The multilayer films are then stretched to 75% to further orient the polymer chains building up even more and denser “hard-segments domains”, which reduces the permeability by making a tortuous path for oxygen molecules to pass through the films. On the other hand, monolayer Isoplast® 2530 with the same 75% stretching is not able to form such “hard-segments domains”, and reduce the gas permeability, due to the lack of oriented polymer chains under micro-confinement. Stretching the multilayer TPU films from 100% to 300% destroys the “hard-segments domains”, instead of producing more densly packed structures, and micro-crazes start to appear, which causes the gas permeabilities increase [38]. 4.3.5 WAXS In order to confirm the structural model, WAXS measurements in both the normal and transverse directions were performed on extruded and stretched TPU films. 2-D WAXS patterns of monolayer Isoplast® 2530, TPU B and multilayer films are provided in Figure 4.10. In this, all TPU film show a broad amorphous halo and a sharp diffraction ring. In TPU B where the long-range order is observed by AFM and DSC, the sharp ring represents the “hard-segments domains” that have a d-spacing of 7.38 Å, which is in 134 agreement with the results reported by Yunxin et al [7]. As mentioned before, the long length and high ratio of soft segments facilitate microphase seperation and the formation of ordered “hard-segments domains”. Compared to TPU B, the sharp ring in Isoplast® 2530 appears at a place closer to the center meaning a slightly larger d-spacing (=8.84 Å) between the hard-segments sheets because it has no soft segments. While the extruded multilayer film (Figure 4.10c) exhibit the overlapped diffraction rings consisting of those in Isoplast® 2530 and TPU B, the multilayer film with 75% stretch (Figure 4.10d) shows broad relection arcs at the meridian in the center of the pattern presenting the oriented polymer chains. This tend can be more clearly seen in 1-D WAXS profile as shown in Figure 4.11, in which the multilayer film shows a broad peak between the ones of two controlled TPU films at 2Ɵ of 10 and 12 degrees. This peak becomes broader and more pronounced when the multilayer film is 75% stretched. The reason is attributed to the fact that the stretching under micro-confinement helps the polymer chains further oriented forming more and denser “hard-segments domains”. When the multilayer film is stretched beyond 75% (i.e. to 300%), even though the arcs in WAXS pattern become sharper and sharper, a new pair of arcs at 2Ɵ of 4.8 degrees appears due to the fragmented “hard-segments domains” (Figure 4. 10e). 4.3.6 Gas barrier properties dependence on stretching temperature The multilayer TPU films were stretched at different temperatures to examine the gas barrier properties dependence on stretching temperature. As can be seen in Figure 4.12, with the same amount of stretching, i.e. 75%, the permeability decreases as the temperature increases up to 120 oC. It is at this stretching temperature that the lowest permeability of 0.028 barrer is achieved, which is an eight-fold improvement relatively to 135 TPU B, four-fold relatively to the bilayer film, and three-fold relatively to Isoplast® 2530. However, the permeability increases when the temperature is elevated to 130 oC. As mentioned before, the enhancement of gas barrier properties is due to the impermeable “hard-segments domains” that are formed by intermolecular hydrogen bonds. When the temperature is elevated from 100 oC to 120 oC, the mobility of TPU chains increases, and the possibility to form “hard-segments domains” becomes higher. This can be proved by DSC as shown in Figure 4.13 and Table 4.1; the integrated endothermic peak of “hardsegments domains” increases from 9.98 J/g to 12.41 J/g between 100 oC and 120 oC. On the other hand, at 130 oC the “hard-segments domains” are destroyed due to the high energy that deconstructs the intermolecular hydrogen bonds, which shows is in agreement with the findings of Coleman et al [39]. Finally, Figure 4.14 shows the overall dependency of permeability of multilayer TPU films on temperature and stretching ratio, and the set of conditions that lead to the lowest permeability is 75% stretching at 120 oC. 4.3.7 Mechanical properties The effect of micro-confinement on mechanical properties is also pronounced. The stress-strain curve and the tensile properties for mono-, bi-, and multilayer TPU films at room temperature are summarized in Figure 4.15 and Table 4.2. As expected, the rigid Isoplast® 2530 has a high yield stress and a low elongation at break of 95.69%, while the TPU B shows a ductile mechanical behavior. The bilayer, like the gas barrier properties, posseses mechanical properties in-between those of the two components. However, the multilayer film not only shows a high yield stress of 29.17 MPa, but also a high elongation at break that is closed to 195%, a strong and ductile behavior with toughness about 76.07 MPa, and the highest fracture stress at 60.49 MPa. These improvements are 136 due to the fact that the stress relief based on the interaction of the microcraks in Isoplast® 2530 with TPU B layers is able to alleviate crazing [27, 40]. 4.4 Conclusions Extruded and stretched nominal 65-layer rigid/soft TPU films were successfully produced through a novel layer-multiplying co-extrusion and uniaxial stretching and the dependence of gas permeability on deformation and temperature was studied. Uniaxial stretching under micro-confinement has a significant effect on gas barrier properties of TPUs, with up to an eight-fold improvement of 75% stretched multilayer film when compared to the component polymers. Such a reduction in gas permeability is due to oriented “hard-segments domains” in the Isoplast® 2530 layers resulting from intermolecular hydrogen bonds connected between “-NH” and “C=O” groups along the TPU B backbones. This changes the gas-diffusion path into a tortuous way. Multilayer TPU films with stretching beyond 75%, instead of further improving the gas barrier properties, increase the permeability because the “hard-segments domains” start to break up under these circumstances. Finally, the micro-confinement also shows effect on mechanical properties, with 100% improvement on elongation at break being found from monolayer to multilayer TPU film, because the interaction of the microcraks in Isoplast® 2530 with TPU B layers is able to alleviate crazing. 137 4.5 References 1. Furukawa, M.; Mitsui, Y.; Fukumaru, T.; Kojio, K. Polymer, 46, 10817, (2005) 2. Kojio, K.; Kugumiya, S.; Uchiba, Y.; Nishino, Y.; Furukawa, M. Polym. J., 41, 118 (2009) 3. Tang, D.; Macosko, C. 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April 27-30, Las Vegas, accepted 33. Huang, R.; Patz, J.; Silva, J.; Andrade, R.; Harris, P.; Yin, K.; Huntington, B.; Bonnecaze, R.; Cox, M.; Maia, J. M. Int. Polym. Proc. submitted 34. Barroso, V.; Covas, J. A.; Maia, J. M. Rheol. Acta, 41, 154 (2002) 35. Harris, P. J.; Patz, J.; Huntington, B. A.; Bonnecaze, R. T.; Meltzer, D.; Maia, J. Polym. Eng. & Sci., 54, 636 (2014) 36. Silva, J.; Andrade, R.; Huang, R.; Liu, J.; Meltzer, D.; Cox, M.; Maia, J. M. J nonNewtonian Fluid Mech. 2014, submitted. 37. Silva, J.; Maia, J. M.; Huang, R.; Meltzer, D.; Cox, M.; Andrade, R. Rheol. Acta., 51, 947 (2012) 38. Sakurai, S.; Yoshida, H.; Hashimoto, F.; Shibaya, M.; Ishihara, H.; Yoshihara, N.; Nishitsuji, S.; Takenaka, M. Polymer, 50, 1566 (2009) 39. Coleman, M.M.; Lee, K. H.; Skrovanek, D. J.; Painter, P. C. Macromolecules., 19, 2149 (1986) 40. Ponting, M.; Burt, T. M.; Korley, L. T. J.; Andrews, J.; Hiltner, A.; Baer, E. Ind. & Eng. Chem. Res., 49, 12111 (2010) 140 Table 4.1: Comparison of integrated endothermic peak of “hard-segments domains” in nominal 65-layer film with 75% stretching at different temperatures. Temperature Integrated peak (J/g) 100oC 9.98 110oC 12.20 120oC 12.41 130oC 5.9 141 Table 4.2: Mechanical properties of extruded TPU films. Elastic modulus Elongation at Fracture stress Yield stress Toughness (MPa) break (%) (MPa) (MPa) (MJ/m3) Isoplast® 2530 1867.24±98.46 95.69±9.81 46.63±3.81 35.02±3.15 32.02±6.09 TPU B 109.61±3.19 397.86±6.25 41.64±2.23 2.18±0.12 89.61±5.04 Bi-layer 1032.75±100.34 127.40±15.38 34.26±6.86 20.51±2.13 36.65±11.40 65 layers 1265.13±2.38 193.25±1.64 60.49±0.19 29.17±0.71 76.07±2.36 142 Figure 4.1: Rheological results of TPUs: (a) steady shear mode and (b) oscillation shear mode; (c) extensional rheology for Isoplast® 2530, and (d) TPU B. 143 Figure 4.2: AFM phase images of TPU B (left), and Isoplast® 2530 (right). 144 Figure 4.3: AFM phase images of bilayer Isoplast® 2530/TPU B: low magnification (left), high magnification (right). 145 Figure 4.4: Morphologies of nominal 65-layer Isoplast® 2530/TPU B films: (a) OM picture of film as extruded; AFM phase images of (b) extruded, (c) 75% stretched, and (d) 300% stretched films. 146 Figure 4.5: Oxygen permeability of extruded and stretched TPU films. 147 Figure 4.6: Oxygen permeability of 75% stretched TPU films. 148 Figure 4.7: DSC results of extruded and stretched TPU films (heating rate=10 oC/min-1). 149 Figure 4.8: DSC results of 75% stretched TPU films (heating rate=10 oC/min-1). 150 Figure 4.9: Schematic illustration for micro-confinement effect on forming “hard-segments domain” in Isoplast® 2530 layer, and microscopic fracture at very high deformation, in which yellow layer is Isoplast® 2530 and dark blue layer is TPU B, orange boxes are hard segments and light blue spots are chain extenders. 151 (a) (b) (c) 152 (d) (e) Figure 4.10: Normal direction 2-D WAXS patterns for various TPU films: TPU B (a), Isoplast® 2530 (b), 65-layer (c), 65-layer with 75% stretch (d), nominal 65-layer with 300% stretch (e). 153 Figure 4.11: 1-D WAXS profiles of various TPU films. 154 Figure 4.12: Oxygen permeability of 75% stretched nominal 65-layer film as function of temperatures. 155 Figure 4.13: DSC results of nominal 65-layer film with 75% stretching at different temperatures. 156 Figure 4.14: 3-D profile on oxygen permeability of nominal 65-layer film depending on stretching ratio and temperatures. 157 (a) (b) Figure 4.15: Stress-strain curves for various TPU films: (a) full scale, (b) initial area zoomed in. 158 PART II: Twin-screw Compounding Process for Thermoplastic Elastomer 159 CHAPTER 5 Understanding the Distribution and Dispersion of Mineral Oil in Polypropylene/Styrene-Ethylene-Butadiene-Styrene Blends Upon Compounding NOTE: Parts of this work have been submitted or published in “Huang, R.; Chari, P.; Klettlinger, N.; Ling, G.; Tseng, J-K.; Maia, J. M. Int. Polym. Proc., submitted” Abstract This chapter presents a study on the effects of batch and continuous mixing methods of a three component thermoplastic elastomer, TPE, system of mineral oil polypropylene (PP) and Styrene-Ethylene-Butadiene-Styrene (SEBS). The experimental approach keeps the ratios of each TPE component constant, placing emphasis on distribution and dispersion of oil in the two polymer matrices. Through this procedure, the effect of different feeding times on glass transition temperature (Tg) of both the PP and SEBS phases, and the complete TPE system are highlighted. It was observed the well-known affinity of the oil to SEBS phase when compared to PP, which increases the glass-transition temperature, Tg, of the blend and leads to processing defects. Also, increasing residence times of the different phases improves oil absorption in PP, severely reduces the presence of gels, and lowers the Tg of the batch mixed TPE system. These results were then confirmed in twin-screw compounding, where we observed a marked improvement in extrudate appearance and decrease in Tg by adding a second compounding step. 5.1 Introduction 160 Thermoplastic elastomers that exhibit both plastic and rubber characteristics are diverse in applications and exist in many forms, such as styrenic block copolymers, and polyolefin blends [1-6]. Applications of thermoplastic elastomers range from filling the soles of shoes to cables in headphones [7-9]. With many different classes of TPE and range in applications, finding favorable characteristics to strengthen the material will benefit a wide array of products. An important complex included from these classes is the blend of polypropylene (PP) and Styrene-Ethylene-Butylene-Styrene (SEBS), which possesses favorable tensile modulus and strength [10-12]. With PP droplets imbedded in the SEBS matrix, the blend becomes stiffer, more easily processed and cost-effective, and tougher since the SEBS helps prevent the potential crazing of PP at large deformations [13-17]. There are a variety of processing methods to produce styrenic TPE for its many different applications. These include extrusion, injection molding, compression molding, and sometimes blow molding and heat welding [18-23]. Twin-screw extrusion is able to provide the TPE system with the high dispersive and distributive mixing required for proper blending of PP and SEBS. However, due to the high elasticity and viscous dissipating heat of SEBS in the molten state, it is difficult to process this material. Thus, normally a plasticizer such as mineral oil is added to the formulation. At optimal amounts the oil becomes more and more of an extender, which will soften the polymer matrix [2426]. In the meanwhile, due to the polarity difference, the distribution of oil in each PP and SEBS phase plays an important role in determining the mechanical and optical properties of the TPE. In addition to the elongation extension, the addition of a plasticizer 161 also reduces the glass transition of the polymers, allowing the rubbery region of the material to be reached at a faster rate [27]. Even though it has been shown before that increasing the content of oil leads to a decrease in Tg of PP/SEBS blends, the distribution and dispersion kinetics of oil in the polymeric phases is still not well understood [28-30]. In this paper, we begin by studying thermo-rheologically the mixing kinetics of the oil in each of the polymeric phases separately, in an internal batch mixer. Then we repeat the process for the complete TPE, varying the feeding protocol and mixing time in order to minimize the Tg of the final blend. Finally, we upscale the process for twin-screw extrusion. We subjected TPE to one and two passes, and were able to confirm not only the mixing kinetics but also minimize both the Tg of the blend and the presence of gels in the final extruded product with the second extrusion cycle. 5.2. Experimental and method 5.2.1 Materials All the materials used in this work were supplied by Saint-Gobain Performance Plastics. The isotatic polypropylene has a density of ρ=0.9 g/cc as measured by ASTM D1238 and a melt flow rate of 4.2 g/10min. The styrenic block copolymer was an unhydrogentated styrene-ethylene-butadiene-styrene (SEBS) with a hardness of Shore A 60. The mineral oil, which serves as a plasticizer, has a density of ρ=0.88 g/cc 5.2.2 Internal Batch Mixer 162 The PP/SEBS/oil blends, at a constant ratio of 20/35/45 percentage by weight, typical of industrial applications, were prepared in an internal batch mixer (HAAKE™ Rheomix OS Lab Mixers with CAM blades/rotors) at 175 oC and 250 rpm, in different feeding orders. In particular, PP/oil at ratio of 8:1 by weight was first fed into the chamber of mixer, followed by different amounts of oil only, and finally and then the rest of the oil and SEBS/oil at ratio of 1:1 were added. The mixing time of each of these three steps was 75 seconds, and the specifics were shown in the Table 1. After the mixing step, the samples were hot pressed by compression mold (Carver hydraulic compression molder) to make thin films with thickness less than 25 microns at 175 oC. 5.2.3 Twin-screw Compounding PP/SEBS/oil at a constant ratio of 20/35/45 percentage by weight were first dry blended with a KitchenAid Professional 600 Series 6-Quart Stand Mixer for 2 hours at room temperature, and then the mixture was melt compounded in a 24 mm intermeshing co-rotating twin-screw extruder (Thermo Scientific™ TSE 24 MC, L/D=40/1). The screw configuration consists of 5 conveying blocks and 4 kneading blocks, as shown in table 2. The processing temperature was set at 175 oC, and a screw speed of 400 rpm and throughput of 30 lbs/hour were used for each compounding process. After the materials were extruded from a 3-hole strand die, they were quenched through a water tank and diced by a pelletizer. Both the first and second compounding passes were performed under these processing conditions. 5.2.4 Characterization 163 Oscillation shear experiments of the blends were performed via a rotational rheometer (Thermo Fisher MARS III) with 20 mm parallel plates system. A constant shear stress of 100 Pa (within the linear viscoelastic regime) and temperature of 175 oC were used for the frequency sweeps from 100 to 0.01 Hz. Dynamic moduli and complex viscosity were collected to analyze the effect of different compounding processes on oil distribution and dispersion in PP/SEBS. For Atomic Force Microscopy (AFM), the samples were embedded and fixed in epoxy at room temperature for 1 day. A Leica microsystmes EM FC6 ultramicrotome (Buffalo Grove, IL) was applied to cut the cross sections of the sample at -90 oC transveral to the extrusion direction. The samples were examined by a Digital Laboratories Nanoscope IIIa AFM (Digital Instruments, Santa Barbara, CA) operating in tapping mode at room temperature. AFM phase images of the blends with different compounding processes were analyzed via the NanoScope software to obtain modulus differences and morphology information. The glass transition temperatures (Tg) of the blends were determined by Dynamic Mechanical Analysis (DMA). The experiments were performed by using a TA Instruments DMAQ800 within a liquid nitrogen atmosphere and with heating and cooling rate of 3 oC/min. Multi-Frequency-Strain mode at frequency of 1 Hz was applied to all the DMA measurements. The peak temperatures in loss modulus were used to determine the Tg of each sample. Broadband Dielectric Spectroscopy (BDS) measurements were conducted by an Alpha–A broadband dielectric analyzer, Novocontrol. The tested samples were coated with round gold electrodes on both sides (diameter = 1 cm, thickness = 20 nm). The 164 temperature of the sample was controlled by Novocontrol Quatro Cryosystem. Temperature swipe BDS measurement was carried out with the temperature ramp rate of 2 °C/min. 5.3 Results and discussion The first part of the work is concerned with establishing the oil absorption capability of each of the polymeric phases. As seen in Figure 5.1, even for PP/oil ratios as low as 8/1, only a small amount of oil can be absorbed by PP at room temperature, with most staying outside the PP pellets. In contrast, the oil is completely absorbed by SEBS even at the ratio of 1:1. This is majorly attributed to the polarity and free volume difference of between PP and SEBS. The maximum ratio of PP/oil that can be dry-blended prior to feeding in the batch mixer of the extruder is approximately 8:1. Beyond this ratio, the extra oil stays outside the PP pellets at room temperature no matter the duration of the dry blending process. This ratio of PP and oil is first fed into the mixing chamber. The second step is the feeding of extra oil only and finally the rest of the oil and the SEBS are fed at a ratio of 1/1. In order to study the effect of different mixing times, two cycle times of 15-45-15 (seconds) and 15-30-30 (seconds) were imposed in each step. As seen in Figure 5.2, the film with less mixing time in SEBS/oil exhibits white impurities (possible gels), while the other material is totally transparent. This might be attributed to the fact that the time for transferring oil from SEBS phase into PP phase is too short to eliminate the inhomogeneous/unplasticized PP, which causes gel impurities. This is confirmed by DMA, as shown in Figure 5.3. The inhomogeneous/unplasticized PP part in the mixture of 1545-15 (sec) shows a higher Tg than that of 15-30-30 (sec). PP/oil (8:1), SEBS/oil (8:1), and SEBS/oil (1:1) were then compounded twice in the twin-screw extruder. DMA shows that for PP/oil (8:1), Tg decreases from 30 oC to 165 40 oC between the first and second passes in the extruder, as shown in Figure 5.4(a). This means the oil is more homogeneously distributed and dispersed in PP after the second pass. Figure 5.4(b) and (c) show the DMA results of SEBS/oil systems with ratio of 8:1 and 1:1 respectively. Even though the Tg of SEBS/oil at ratio of 1:1 (-60 oC) is 10oC lower than that of 8:1 (-50 oC) due to the plasticizing effect from oil, in both cases there is no shift in Tg between the first and second passes. This means the oil can be easily distributed and dispersed in the SEBS. Therefore, when PP/SEBS/oil are dry blended at room temperature, it is to be expected that most of the oil be absorbed into the SEBS phase. This may cause an inhomogeneous oil distribution in the extruded TPE blend if one compounding step is not sufficient to transfer some of the excess oil in the SEBS phase to the PP phase and distribute equally throughout both. Therefore, the TPE dry blend was also subject to two compounding passes in the extruder. Figure 5.5 shows the DMA results on both extruded samples and it is possible to observe that: a) There is a decline in loss modulus peak between the first and second pass samples as a function of temperature; and b) There is a transition from two glass transition peaks for the one-pass blend to only one in the two-pass blend. The peak at approximately -65 oC is the Tg of the SEBS phase, which is consistent with literature results for ~50 wt% oil in SEBS [28]. The shoulder that can be observed at -45 oC is the Tg of the highly plasticized PP phase. This is a significantly lower value of Tg than that of PP alone, but is again in agreement with previous literature findings for highly plasticized PP [28]. Interestingly, after the second compounding these two Tg peaks merge at -57 oC instead of moving towards lower temperatures. This is a strong 166 indication that the second pass is indeed inducing a transfer of oil from the SEBS to the PP phase, thus increasing the Tg of the former. It is also an indication of the more homogeneous distribution and dispersion of oil in the TPE. Sengers pointed out that oil actually acts as a plasticizer, softening the material as its concentration increases and that, surprisingly, the effect is much more pronounced for PP than for SEBS [28]. In this paper, even though the oil concentration is constant, better distribution and dispersion of oil will create larger surface to volume ratio, leading to the same effect as increasing oil concentration. These mechanical spectroscopy results are confirmed by BDS, Broadband Dielectric Spectroscopy. Since the dielectric response of the molecule depends on the changes in the surrounding viscosity, BDS monitors the mechanical glass transition evolution during the compounding process [26]. Figure 5.6 shows that there are two peaks of loss permittivity (the equivalent of the mechanical loss modulus) for the first pass sample, and only one peak for the second pass. Interestingly, the high Tg peak in the first pass occurs at different temperatures in DMA and BDS experiments. The reason for this discrepancy is not clear. Even though DMA and BDS results show significant differences in the Tg peaks after one and two passes, rotational rheometry data shows that rheologically the two materials have quantitatively the same behavior, see Figure 5.7. In both cases the behavior is typical of elastomers, with moduli showing a very weak dependence on frequency and the storage modulus being much higher than the loss modulus at all frequencies. 167 Atomic Force Microscopy, AFM, was used to investigate the morphology of the blends and the similar rheological behavior between the first and second passes. Figure 5.8(a) and (b) show the phase images of first and second pass samples; the bright areas represent the PP phase and the dark areas represent the SEBS phase. As expected from the rheometry results, a similar morphology is observed for these two samples, therefore confirming that the diffences observed by DMA are due to oil dispersion (which is not visible by AFM) and not to different bulk morphologies (which would be). 5.4 Conclusions Blends of PP/SEBS/oil were successfully prepared by batch mixing and twinscrew compounding. Batch mixing results show that both PP and SEBS are highly plasticized by the oil, and different feeding times would change the optical properties (transparency) and Tg of the film. Even though PP acts as oil resistant material and SEBS is highly affiliated with oil during dry blending at room temperature, PP can be more plasticized by oil upon melt compounding. Extrusion results show that due to the higher affinity of the oil with the SEBS phase, dry blending results in an oil-depleted PP phase upon compounding, with both DMA and BDS showing a two Tg system. Therefore, a 2pass twin-screw compounding is necessary to homogeneously distribute the oil in the TPE system, even if the general morphology, as determined by AFM and rotational rheometry, does not evolve noticeably between the two passes. Tg at -65 oC from the SEBS phase and Tg around -45 oC from PP phase merge towards -57 oC in the second pass. 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Rapid Commun., 26, 542 (2005) 170 Table 5.1: The different feeding time of PP/oil/SEBS in internal batch mixer (unit: second) Samples PP/oil (8:1) Oil SEBS/oil (1:1) TPE 15-45-15 15 45 15 TPE 15-30-30 15 30 30 171 Table 5.2: Twin screw configuration: the order starts from feeder to exit die; each conveying element is 2.4 cm, and each kneading element is 0.6 cm; every 4 kneading elements together have the same twisting angle in arrangement. Order Elements Twisting angle Conveying 1 10 n/a Kneading 2 4×4 30o/60o/60o/90o Conveying 3 4 n/a Reversed conveying 4 0.5 n/a Kneading 5 2×4 60o/60o Conveying 6 4 n/a Reversed conveying 7 0.5 n/a Kneading 8 3×4 60o/60o/90o Conveying 9 3 n/a Kneading 10 2×4 60o/60o Conveying 11 7 n/a Total n/a 40 n/a 172 Figure 5.1: Pictures of oil absorption in PP (a-c), SEBS (d-f) phase at room temperature. 173 Figure 5.2: Optical pictures of PP/oil/SEBS with different mixing time: 15-45-15 (left), 15-30-30 (right). 174 Figure 5.3: DMA results of PP/oil/SEBS with different mixing time. 175 (a) (b) 176 (c) Figure 5.4: DMA results for extruded PP/oil (8:1) (a), SEBS/oil (8:1) (b), and SEBS/oil (1:1) (c) blends. 177 Figure 5.5: DMA results for the extruded TPE system after one and two compounding cycles. 178 Figure 5.6: BDS of the 1st and 2nd pass samples. 179 (a) (b) Figure 5.7: Oscillation shear rheology of 1st and 2nd pass samples: (a) dynamic moduli as function of frequency; (b) complex viscosity as function of frequency. 180 (a) (b) Figure 5.8: AFM phase images of TPE: (a) sample from 1st pass, (b) sample from 2nd pass. 181 APPENDIX 182 APPENDIX Interplay Between Rheological and Structural Evolution of Benzoxazine Resins During Polymerization NOTE: Parts of this work have been submitted or published in “Huang, R.; Carson, S.; Jorge, S.; Agag, T.; Ishida, H.; Maia, J. M. Polymer, 54, 1709 (2013)” A.1 Introduction Polybenzoxazines are a class of phenolic resins that possess various unusual and advantageous properties [1]. While traditional phenolics offer many useful properties and still hold the majority of the share of the thermoset market today, their use also has various problems when considering synthesis, processing, and end use. Examples of these include the use of harsh chemicals during synthesis and polymerization, large volumetric shrinkage during processing, production of water during polymerization which leads to void formation, and an inherent brittleness of the material in the polymerized and crosslinked form [2]. Polybenzoxazines offer the same advantages of traditional phenolics such as excellent mechanical strength, thermal and thermo-oxidative stabilities, good chemical resistance, abrasion resistance, and flame resistance but eliminate most of the problems associated with them [3-8]. Properties such as near-zero volumetric change upon polymerization, very high char yield, low water absorption, and a by-product free polymerization are unique to benzoxazine based resins [3, 9-12]. Polybenzoxazines also show various forms of hydrogen bonding within the final chemical structure, which 183 contribute greatly to its unique properties [13, 14]. Relatively high polymerization temperature can be inconvenient for some applications and, as is for all thermosetting resins, the improvement in toughness may sometimes be needed, although polymeric benzoxazine precursors, such as main-chain and side-chain type polybenzoxazines that can be later cross-linked, offer much better toughness characteristics [15-26]. When compared with traditional thermoset phenolics and epoxies, polybenzoxazines offer a number of useful advantages that make them an attractive alternative, in addition to offering new application opportunities using those unique properties mentioned earlier. The potential for rich molecular design flexibility is one of the most important properties of a benzoxazine-based resin, since it makes it possible for the resin properties to be tailored specifically to an application and still offer all of the same chemical and processing advantages. It is mostly for this reason that polybenzoxazines are very viable materials that find increasing number of applications, from replacements of traditional phenolics and epoxies to specifically tailored high performance materials [1]. Chemically, benzoxazine resins are synthesized through a Mannich condensation of a phenolic derivative, an amine, and formaldehyde. Water is the sole byproduct of this monomer synthesis. The potential for molecular versatility comes from the wide availability of phenolic derivatives and primary amine compounds that can be used in the production of the material. To form a crosslinked thermoset structure, multifunctional phenolics and amines are used. Perhaps the most common form of benzoxazine resin that exemplifies all of the resin family’s typical properties is produced from Bisphenol-A and aniline, commonly designated as BA-a [12, 27-29]. Another common variation of bifuntional benzoxazines, which is more advanced in heat resistance and electrical 184 insulation than BA-a, is based on methylene dianiline, and is designated as P-ddm and its cationic ring-opening mechanism (the same as for BA-a) is shown in Figure A.1 [30]. The aim of this study is to understand the rheological evolution of phenol and methylene dianiline (P-ddm) benzoxazines, which is essential to its successful processing. The polymerization kinetics of benzoxazines by using differential scanning calorimetry (DSC) has been reported elsewhere [27, 31-34]. However, by combining this with rheological means we expect to establish a complete and fundamental understanding of the kinetics, and monitor how benzoxazine acts over different polymerization temperatures. This has not been done before. In particular, the polymerization kinetics was extensively studied using Rheometer, DSC, and Fourier transform infrared spectroscopy (FT-IR). A.2 Experimental and method A.2.1 Preparation of benzoxazine monomer, bis(3-phenyl-3,4-dihydro-2H- benzo[e][1,3]oxazine-6-yl)methane (abbreviated as P-ddm) 110g P-ddm was synthesized according to the modified method of the procedure for the difficult aromatic amines [35]. Some of the possible structures in these assynthesized benzoxazines are shown in Figure A.1. Diaminodiphenylmethane (DDM) (>99%), paraformaldehyde (96%), aniline, 1,4-dioxane, and a mixture of xylene isomers were purchased from Aldrich Chemical Company. All chemicals were used without further purification. A.2.2 Characterization 185 1 H NMR spectra were acquired in deuterated dimethyl sufoxide on a Varian Oxford AS600 at a proton frequency of 600 MHz. The average number of transients for 1H is 64. A relaxation time of 10 s was used for the integrated intensity determination of 1H NMR spectra. Rheological analysis was performed for P-ddm (~0.7g) using an Anton Paar Rheometer (Model Physica MCR 501) and 25mm disposable parallel plates. Small amplitude oscillatory shear (SAOS) time sweep experiments over temperatures ranging from 140°C to 220°C in increments of 20°C and temperature sweep from 140°C to 220°C with heating rate of 3°C/min were performed using a constant frequency of 10 rad/s for all experiments. During the measurements, the stress was continuously increased between 10 Pa and 600 Pa, so as to maintain an acceptable signal strength, i.e., a high enough strain to produce consistent and reproducible results, while keeping the materials’ response in the linear viscoelastic regime as polymerization progresses. Stress relaxation experiments with a shear step strain of 10% were performed on fresh P-ddm samples, as well as on samples corresponding to critical stages during the polymerization process (which will be explained later) at 140oC. In these cases the experiment was stopped and the temperature lowered to 110oC so as to prevent further polymerization within the testing time scale. To study the non-isothermal behavior of P-ddm benzoxazines, differential scanning calorimetric (DSC) analysis was carried out on a TA Instruments Q-100 DSC. Non-isothermal experiments on monomer at a ramp rate of 3oC/min, or products collected at certain polymerization stages at 10oC/min were carried out from 0 to 300°C. The reaction was considered complete when the curves leveled off to the baseline and no 186 more drastic changes in heat were observed. Experiments were always performed below 300°C to prevent any possible degradation inside the chamber. After the exothermic peak, when the DSC curve reached the baseline level again, the sample was cooled rapidly to 0°C. Further heating of the sample was done to determine the residual heat of reaction. Fourier transform infrared (FT-IR) spectra were obtained using a Bomem Michelson MB100 FT-IR spectrometer equipped with a deuterated triglycine sulfate (DTGS) detector and a dry air purge unit. Co-added spectra of 32 scans were recorded at a resolution of 4 cm-1. Transmission spectra were obtained at room temperature using the KBr pellet technique for partially or completely polymerized samples. A.3 Results and discussion A.3.1 Synthesis and characterization of P-ddm H NMR spectrum of P-ddm is shown in Figure A.2 ((CD3)2SO, 600 MHz, δ): 1 6.49-7.39 ppm (Ar-H), 5.33 ppm (O-CH2-N), 4.54 ppm (O-CH2-N), 3.67 ppm (Ar-CH2Ar), 2.47 ppm ((CD3)2SO), 3.30 ppm (H2O), 3.54 ppm (dioxane). The oxazine ring content in the whole composition can be calculated by the following equation: Ring content (%) = I ,× 100 2I where I is the integrated intensity of the methylene protons of Ar-CH2-N in the benzoxazine ring, I’ is the integrated intensity of the methylene protons of Ar-CH2-Ar. The oxazine ring content thus determined for P-ddm is 95%. We did not attempt to further purify the monomer since this level of purity determined is similar to that of technical grades of benzoxazine monomers, so it’s a production-representative sample. 187 A.3.2 Rheological properties evolution of benzoxazine during polymerization The rheological properties of P-ddm are able to provide basic insights about the processability of polybenzoxazine, since the viscoelastic response of the systems is highly sensitive to the structural changes during the polymerization. Figures A.3 and A.4 show the evolution of both viscoelastic moduli (the storage modulus, G’, and the loss modulus, G’’) and tan δ (G’’/G’), clearly revealing the existence of a two transitions during polymerization, especially at the lower temperatures. As with any chemical processes, increasing the temperature at which the reaction takes place increases the polymerization rate, as shown in Figure A.5. For this reason, the first transition is not observed because it occurs too quickly to be detected experimentally. Figure A.3 displays all time sweep data for the P-ddm experiments. Investigation of these curves reveals the unique behavior of benzoxazine polymerization, with all curves up to 180°C showing two transitions in the polymerization process. This can be seen even more clearly in Figure A.4, which depicts the time evolution of tan δ. Peaks in this value indicate that the G” component of the dynamic moduli was at a local relative maximum compared to the G’ component, and were indicators of structural processes, such as relaxation or buildup of molecular network. As the test temperature increases so does the rate of polymerization. Both peaks shift to lower times, while the first peak eventually disappears completely at 220oC. The disappearance of this first peak at high temperatures is due to the fact that the process, whatever its nature, is faster than the time necessary to load the sample and stabilize it at the measurement temperature. Another characteristic of this peak is that its magnitude decreases greatly as temperature increases. 188 Both these facts point to a transient kinetic process that reduces in magnitude and increases in velocity as the polymerization temperature increases. It should also be noted that the elasticity of P-ddm at the beginning of time sweep at 160oC is too low to be detected by rheometer, while the viscosity keeps increasing. This might be due to the temporary intermolecular hydrogen-bonding structures forming between monomers and linear macromolecular chains at 140oC, as can be seen in Figure A.6(a), which disappear when increasing the temperature from 140oC to 160oC [36, 37]. Such structural transformation can take place while the molecular weight of the resin is still small and does not contribute significantly to the elasticity build-up. This is consistent with the finding that the formation of covalent bonds among monomers lags in time of the ring opening reactions, although eventually they match in time [36]. These two transitions during polymerization at lower temperatures (i.e. 140oC, 160oC, 180oC) for P-ddm must be related to the gradual buildup of molecular structure during the entire experiment, with the material going from monomers to oligomers, unentangled polymer chains and eventually to polybenzoxazine with a fully crosslinked structure. Thus, we are in condition to put forward the following hypothesis: i) The first tan δ peak, which was kinetic in nature, probably corresponds to monomer ring-opening and the opened Mannich base hydrogen bonds to each other as shown in Figure A.6 (b). There is very little polymerization taking place at this condition. During this process, the viscosity grows faster than elasticity, which leads to an increase in tan δ. As the polymerization reaction starts later and six-membered intramolecular hydrogen bonds between the hydroxyl group and the nitrogen atom is formed, 189 this behavior was expected to be inverted, with elasticity growing faster than viscosity, thus leading to a decrease in tan δ. Thus, the first peak in tan δ is probably due to the onset of an increased intermolecular interaction and consequent energy dissipation. ii) The second tan δ peak present in the data probably represents the actual polymerization occurring during the experiment. This peak changes its pattern from very distributed over a long period at lower temperatures to very quick and shifted to shorter times at higher temperatures. This is consistent with the fact that once the threshold level of chemically ready linear polymer is reached, a buildup of a large molecular network begins to occur, with phenolic hydroxyl groups formed from benzoxazine ring-opening serving as polymerization catalyst. This is an autocatalytic process of benzoxazine resins as reported in the literature [27]. Thus, the second peak should correspond to the polymerization process, in which polymer chains propagate and crosslink with each other and complete the 3-dimensional network. It is interesting to notice that if one performs a temperature sweep, which is probably the most common way of studying the temperature–induced polymerization processes, two tan δ peaks during polymerization are also observed, as can be seen in Figure A.7. In fact, the continuous increase in temperature destroys the temporary structure of intermolecular hydrogen bond after ring opening, which is attributed to its first tan δ peak. The second tan δ peak is due to the actual polymerization process and 3D network formation. 190 In order to test these hypotheses, further rheological, thermal and chemical experiments were performed. The first of the former was stress relaxation after a step shear on P-ddm at four different stages of the process: beginning, 1st and 2nd tan δ peaks, and at the end of the time sweep. Figure A.8 shows the typical results for the relaxation modulus, G(t). For P-ddm resins at a polymerization temperature of 140oC, it is clear that in the beginning and at the 1st tan δ peak, the material still behaves like a viscoelastic liquid, i.e., a non-zero G(t), decaying to zero over time. The large initial drop in the monomer sample is due to the instrument delay time at the beginning of the experiment, which arises from the very low viscosity of the monomer. On the contrary, by the time the 2nd tan δ peak was reached, G(t) no longer relaxes to 0, but does so to a finite value. This is the behavior typical of a viscoelastic solid and clearly indicates that a permanent solid-like structure has been formed. The finding clearly reinforces the theory that the first relaxation mode corresponds to the transition from monomer to unentangled low molecular weight, intermediates which are loosely connected via hydrogen bonding, whereas the second relaxation process corresponds to the main crosslinking process. A.3.3 Thermal properties Non-isothermal DSC experiments were also performed on benzoxazine as shown in Figure A.9. The thermograms show that the melting and polymerization temperature for P-ddm are around 50oC and 213oC, respectively. In order to find if there is any difference among the polybenzoxazines polymerized at different temperatures, samples were collected after the polymerization process was rheologically complete, i.e., the dynamic moduli had reached a plateau, and characterized by non-isothermal DSC. These results are depicted in Figure A.10 and show the lower the polymerization temperature, 191 the greater the exothermal heat. Therefore, those products polymerized at lower temperature have lower final degrees of polymerization, even though they achieve similar values of the dynamic moduli as the ones at higher polymerization temperatures. This was not expected and is probably due to the limitation of rheometer which was not able to show the dynamic moduli change once the sample tested was crosslinked and reached a threshold of dynamic moduli. Additionally, the polybenzoxazine’s Tg shifts to higher temperatures with higher crosslinking temperatures, which supports the notion of increased crosslink density with increased polymerization temperature. A.3.4 Structural evolution of benzoxazine during polymerization Finally, the polymerization process of P-ddm monomers was also investigated by FT-IR, monitoring the changes of the characteristic peak of benzoxazine. Figure A.11 represents the vibrational spectra of the benzoxazine monomer, the material at the first and second peaks of tan δ, and of the final crosslinked material. The peaks centered at 754 and 694 cm-1, corresponding to the mono-substituted benzene, were present at different stages of the polymerization. However, the characteristic absorption of the benzene ring to which oxazine ring is attached at 947 cm-1, the band at 1496 cm-1 corresponding to the in-plane carbon-carbon stretching of tri-substituted benzene ring, and the absorptions at 1030 and 1231 cm-1 corresponding to the symmetric and asymmetric C-O-C bonds of the benzoxazine all decreased with increasing polymerization time, indicating the ring-opening reaction of benzoxazine had taken place. But, there was no detectable evidence of chain propagation at this stage. On the contrary, a small, heavily overlapped shoulder around 1478 cm-1 appears from the second tan δ peak onward. This corresponds to the in-plane carbon-carbon 192 stretching of the tetra-substituted benzene ring, as the methylene bridges form in the free ortho-positions of the phenolic structures, and is attributed to the polymerization [38]. Figure A.12 shows IR spectra of the final resins at all polymerization temperatures and after a temperature sweep. In it the peak of benzoxazine-related band at 947 cm-1 diminishes, while the peak at 1496 cm-1 gradually shifts to 1478 cm-1 with increasing polymerization temperature, indicating that benzoxazines polymerized at higher temperature have a higher degree of polymerization [39]. A.4 Conclusions P-ddm based benzoxazines polymerized at different temperatures was studied in terms of its chemo-rheological and thermal behavior. Even though benzoxazine polymerizes faster at higher polymerization temperatures, the same ultimate dynamic moduli and tan δ were achieved for all cases. Rheological results of P-ddm at different polymerization temperatures also clearly show there are two transitions during polymerization at lower polymerization temperatures, and one of them at elevated polymerization temperatures. According to the stress relaxation and FT-IR results, the first tan δ peak was assigned to the ring-opening reaction and subsequent hydrogen bond formation of open Mannich base of benzoxazine, while the second tan δ peak is the chain propagation and buildup of a large molecular network. FT-IR and DSC results of benzoxazines reaching the plateau of dynamic moduli at higher polymerization temperature show a higher degree of polymerization with increasing temperature. The reason for the absence of the first peak at elevated temperatures is purely due to its kinetics, which is very fast and is complete before the temperature in the rheometer can be stabilized. 193 A.5 References [1] Ishida H. in "Handbook of Benzoxazine Resins," Ishida H and Agag T, Eds. 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Thermochimica Acta, 441, 150 (2006). 196 Figure A.1: Ring-Opening mechanism of P-ddm. 197 8 7 6 5 4 3 2 Chemical shift (ppm) Figure A.2: 1H NMR spectra of P-ddm. 198 108 107 106 G', G'' (Pa) 105 104 103 102 1400C: 1600C: 1800C: 2000C: 2200C: 1 10 100 10-1 -2 10 10-1 100 G' G' G' G' G' G'' G'' G'' G'' G'' 101 Time (hours) Figure A.3: Influence of polymerization temperature on polymerization kinetics for P-ddm. 199 a 102 tan δ 101 100 0 1 2 3 4 5 Time (hours) b 102 tan δ 101 100 10-1 10-2 0.0 0.5 1.0 1.5 2.0 0.6 0.8 Time (hours) c 101 tan δ 100 10-1 10-2 0.0 0.2 0.4 Time (hours) 200 100 tan δ d 0.0 0.1 0.2 0.3 Time (hours) 100 tan δ e 0.0 0.1 Time (hours) Figure A.4: Polymerization kinetics of P-ddm as a function of tan δ; (a) 140oC, (b) 160oC, (c) 180oC, (d) 200oC, (e) 220oC. 201 5 Time (hours) 4 3 2 1 0 140 160 180 200 220 o Temperature ( C) Figure A.5: Time for P-ddm to reach the final plateau in dynamic moduli. 202 Figure A.6: Intermolecular hydrogen-bonding structure; (a) intermolecular H-bonding structures between monomer and opened benzoxazine, (b) opened Mannich base H-bonds to each other. 203 107 600 6 10 500 105 104 G', G'' (Pa) 102 300 101 G' G'' tan δ 100 10-1 10-2 tan δ 400 103 200 100 -3 10 10-4 0 -5 10 140 160 180 200 220 0 Temperature ( C) Figure A.7: Polymerization kinetics of P-ddm as a function of temperature. 204 101 Monomer 1st tan δ peak 2nd tan δ peak Final product 0 10 Normalized G(t) (Pa) 10-1 10-2 10-3 10-4 10-5 10-6 10-2 10-1 100 101 102 Time (s) Figure A.8: Stress relaxation at different stages of the polymerization process of P-ddm. 205 Heat Flow (mW/g) ∆H= 311.1J/g 0 50 100 150 200 250 300 0 Temperature ( C) Figure A.9: Non-isothermal DSC of P-ddm. 206 Heat Flow (W/g) ∆H=32.7J/g 2000C ∆H=117.5J/g 1800C 1600C ∆H=212.2J/g 1400C ∆H=244.3J/g 50 75 100 125 150 175 200 225 250 275 300 0 Temperature ( C) Figure A.10: Non-isothermal DSC of P-ddm after crosslinking. 207 1496 1231 947 1030 Absorbance d c b a 1800 1600 1400 1200 1000 800 600 -1 Wavelength (cm ) Figure A.11: IR spectra of P-ddm with different polymerization stages at 140oC; (a) Monomer, (b) 1st tan δ peak, (c) 2nd tan δ peak, (d) cured P-ddm. 208 1496 1478 947 Absorbance e d c b a 1800 1600 1400 1200 1000 800 600 -1 Wavelength (cm ) Figure A.12: IR spectra of P-ddm at different polymerization temperatures and temperature sweep; (a) 140oC, (b) 140oC, (c) 140oC, (d) 140oC, (e) T sweep. 209 BIBLIOGRAPHY Chapter 1: 1. 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