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Formation and the effects of the thermo-residual stress on mechanical properties of the thermoplastic composites

机译:热残余应力对热塑性复合材料力学性能的形成及其影响

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The thermoplastic composites have widely regarded as high property structural materials for aerospace field for the excellent advantages, which were usually procured based on the moulding process under the high processing temperature and cooling rate. The thermo-residual stresses of the composites will be produced for the mismatch in thermal expansion coefficients between the fiber and matrix, as well as the anisotropy property of the adjacent layers of the plate and temperature gradient of the laminates structures having a certain thickness. The thermo-residual stresses play an important role on the mechanical properties of the obtained thermoplastic composites, which should be taken into consideration in the designing process. It will good to study the formation mechanism and the effects of thermo-residual stresses on the mechanical properties of thermoplastic composites to better utility and control its residual stress level. In present paper, the formation reasons of the thermo-residual stresses were firstly studies and analyzed from three different levels, the methods for controlling and decreasing the thermo-residual stresses were also discussed. In addition, the effects of the residual stresses on the thermoplastic composites properties were also studied from the aspects of dominating by the reinforcement and the polymer matrix.
机译:热塑性复合材料广泛被认为是用于航空航天场的高性能结构材料,用于优异的优点,其通常基于在高加工温度和冷却速率下基于模塑过程采购。复合材料的热残余应力将用于纤维和基质之间的热膨胀系数中的不匹配,以及板的相邻层的各向异性特性和具有一定厚度的层压板结构的温度梯度。热残余应力在所获得的热塑性复合材料的机械性质上发挥着重要作用,这应该在设计过程中考虑。研究形成机制和热残余应力对热塑性复合材料的力学性能,以更好的效用并控制其残余应力水平。在本文中,探讨了热残余应力的形成原因首先研究并分析了三种不同的水平,还讨论了控制和降低热残余应力的方法。此外,还从加强件和聚合物基质主导的方面研究了残留应力对热塑性复合材料的影响。

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