Thermal-force coupling simulation of carbon fibre-reinforced poly-ether-ether-ketone thermoplastic composites during the laser-assisted automated tape placement process

Cheng-Hao Zhang, Fei Wang, Cheng-Shuang Zhang, Yan-Ling Bao, Meng-Jie Wang, Dong Liu, Jing Wu, Zhong-Min Su
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Abstract

To reveal the thermal-force coupling characteristics of the laser in-situ consolidation (ISC) of carbon fibre-reinforced poly-ether-ether-ketone (CF/PEEK) composites, a two-dimensional transient thermal-force model of CF/PEEK composites was constructed using COMSOL Multiphysics finite element simulation software to calculate the temperature history and the thermal stress variation of CF/PEEK composites during the laser-assisted automated tape placement (LATP) process. The results show that the temperature field formed on the surface of each layer by the laser spot during LATP is stable, and the temperature gradient at the front of the spot movement direction is higher than that at the back edge. The maximum stresses in the laminate occur on both sides of the first CF/PEEK layer and the stresses are unevenly distributed along the length and thickness directions of the lay-up. The composite material on both sides of the laminate tends to ‘shrink’ compared to its original position.
碳纤维增强聚醚醚酮热塑性复合材料在激光辅助自动贴带过程中的热力耦合模拟
为了揭示碳纤维增强聚醚醚酮(CF/PEEK)复合材料激光原位固结(ISC)的热-力耦合特性,利用 COMSOL Multiphysics 有限元仿真软件构建了 CF/PEEK 复合材料的二维瞬态热-力模型,计算了激光辅助自动贴带(LATP)过程中 CF/PEEK 复合材料的温度历史和热应力变化。结果表明,LATP 过程中激光光斑在各层表面形成的温度场是稳定的,光斑运动方向前沿的温度梯度高于后沿。层压板的最大应力出现在第一层 CF/PEEK 层的两侧,并且应力沿层压板的长度方向和厚度方向分布不均。与原始位置相比,层压板两侧的复合材料趋于 "收缩"。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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