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About the tensile mechanical behaviour of carbon fibers fabrics reinforced thermoplastic composites under very high temperature conditions

机译:关于碳纤维织物增强的热塑性复合材料在非常高温条件下的拉伸力学性能

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摘要

The present work focuses on the thermomechanical behaviour of thermoplastic-based composite materials subjected to the combined action of a mechanical loading in tension and homogeneous temperature conditions. The investigations on the relationship between local temperature resulting from the local atmosphere and the mass losses are essential in understanding the influence of fire on the thermo-mechanical behaviours of polymers and polymer matrix composites. Regardless the testing atmosphere, the decomposition onset temperature is about 500 degrees C. From isothermal tensile tests conducted at temperatures ranging from ambient to 520 degrees C, it appears that the retention of the axial stiffness of quasi-isotropic carbon fibers reinforced polyphenylene sulfide (PPS) laminates is relatively high (about 70% of its initial value) beyond the decomposition temperature. At the same time, the ultimate strength dramatically decreases (about 25% of its initial value). The obtained results also show that melting is instrumental to rule the tensile behaviour of quasi-isotropic C/PPS laminates. Conversely, matrix melting significantly influences the damage mechanisms within the laminate. Finally, for testing temperatures close to the onset decomposition temperature, porosities appear and grow within the laminates, ultimately contributing to the degradation of the mechanical properties.
机译:目前的工作集中在热塑性塑料基复合材料在张力和均匀温度条件下经受机械载荷的综合作用下的热机械行为。为了了解火对聚合物和聚合物基复合材料热力学行为的影响,研究由局部大气引起的局部温度与质量损失之间的关系至关重要。无论测试气氛如何,其分解起始温度均为约500摄氏度。根据在环境温度至520摄氏度的温度下进行的等温拉伸测试,看来准各向同性碳纤维增强聚苯硫醚(PPS)的轴向刚度得以保留。 )层压板在分解温度以上相对较高(约为其初始值的70%)。同时,极限强度急剧下降(约为其初始值的25%)。所得结果还表明,熔融有助于控制准各向同性C / PPS层压板的拉伸性能。相反,基质熔化显着影响层压板内的损坏机理。最后,为了测试接近起始分解温度的温度,在层压制品中出现并生长出孔隙,最终导致机械性能的下降。

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