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INTERFACE DIFFUSION AND MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS

机译:热塑聚合物共固化的航空航天环氧树脂界面扩散和形貌

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Interfaces formed during the co-curing of an aerospace grade epoxy resin in contact with PEI, PES, and PSU surfaces are examined in this work. The interface found in each scenario is characterized by optical microscopy, and low voltage Scanning Electron Microscopy (SEM) using Energy-Dispersive X-ray spectroscopy (EDX) where applicable. Atomic Force Microscopy (AFM) in tapping mode is also used for high resolution imaging of the interface. The spatial resolution and limitations for each microanalysis technique are defined, and results are interpreted accordingly. The morphology of each interface obtained is correlated with a thermodynamic approach based on the Hansen Solubility Parameter (HSP), which considers dispersion forces, polar forces, hydrogen bonding, and ionic forces between the two materials. The limitations of the HSP thermodynamic approach for this study are discussed. Significant interdiffusion of more than 50 μm is found with PES, PEI and PSU. Nevertheless, a phase separation mechanism was evidenced only for PEI and PSU, and could not be detected with PES. Larger interdiffusion was observed with PSU than PEI.
机译:在这项工作中,研究了航空级环氧树脂与PEI,PES和PSU表面的共固化过程中形成的界面。在每种情况下,通过光学显微镜和使用能量色散X射线光谱仪(EDX)的低压扫描电子显微镜(SEM)来表征每种情况下的界​​面。轻敲模式下的原子力显微镜(AFM)也用于接口的高分辨率成像。定义了每种微分析技术的空间分辨率和局限性,并相应地解释了结果。获得的每个界面的形态都与基于Hansen溶解度参数(HSP)的热力学方法相关,该方法考虑了两种材料之间的分散力,极性力,氢键和离子力。讨论了HSP热力学方法在本研究中的局限性。在PES,PEI和PSU中发现超过50μm的显着相互扩散。然而,仅PEI和PSU证明有相分离机制,而PES无法检测到。与PEI相比,PSU观察到更大的相互扩散。

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