碳纤维/PEEK层压复合材料的疲劳性能

N.H. Tai , C.C.M. Ma , S.H. Wu
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引用次数: 42

摘要

研究了连续碳纤维增强聚醚醚酮(PEEK)复合材料在拉伸-拉伸(T-T)和拉伸-压缩(T-C)载荷下的疲劳行为。采用准各向同性铺层,即[0/45/90/-45]2s AS-4/PEEK。采用中位数秩法对不同应力幅值下的疲劳寿命和残余抗拉强度试验结果进行了分析。研究了应力幅值对疲劳寿命和残余抗拉强度的影响。S-N曲线由集合威布尔分布函数表示。两段S-N曲线在热塑性复合材料疲劳破坏中表现出不同的破坏模式。此外,利用残余强度退化模型预测了复合材料在多次疲劳循环下的残余强度,并模拟了应力幅值对疲劳寿命的影响。所得结果表明,实验数据与理论预测的相关性较好。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Fatigue behaviour of carbon fibre/PEEK laminate composites

The fatigue behaviour of continuous carbon fibre-reinforced poly(ether ether ketone) (PEEK) composites under tension-tension (T-T) and tension-compression (T-C) loadings was investigated. A quasi-isotropic lay-up was used, namely [0/45/90/-45]2s AS-4/PEEK. The experimental results for fatigue life and residual tensile strength under different stress amplitudes are analysed by the median rank method. The influences of stress amplitude on the fatigue life and the residual tensile strength were investigated. The S-N curve is presented by the pooled Weibull distribution function. Two segments of the S-N curves show a different failure mode in the fatigue failure of the thermoplastic composites. Moreover, a residual strength degradation model is used to predict the residual strength for the composites subjected to a number of fatigue cycles and to simulate the effects of the stress amplitude on the fatigue life. According to the obtained results, the correlation between the experimental data and the theoretical prediction is in good agreement.

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