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Reliability of Thermomechanical Fatigue in Polymer Matrix Composites

机译:聚合物基复合材料中热机械疲劳的可靠性

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摘要

A methodology to compute probabilistic fatigue life of polymer matrix laminated composites has been developed and demonstrated. Matrix degradation effects due to long term environmental exposure and mechanical/thermal cyclic loads are accounted for in the simulation process. Sensitivity of fatigue life reliability to uncertainties in the primitive random variables e.g. constituent properties, fiber volume ratio, void volume ratio, ply thickness, etc. are computed and their significance in the reliability based design for maximum life is discussed. A graphite/epoxy (0/+-45/90) deg_s laminate with ply thickness 0.127 mm, is used to demonstrate the methodology. The results show that at low mechanical cyclic loads and low thermal cyclic amplitudes, fatigue life for 0.999 reliability is most sensitive to matrix compressive strength, matrix modulus, thermal expansion coefficient and ply thickness. Whereas at high mechanical cyclic loads and high thermal cyclic amplitudes, fatigue life at 0.999 reliability is more sensitive to the shear strength of matrix, longitudinal fiber modulus, matrix modulus and ply thickness.
机译:已经开发并证明了一种计算聚合物基层压复合材料的概率疲劳寿命的方法。在模拟过程中考虑了由于长期暴露于环境和机械/热循环载荷造成的基体降解效应。疲劳寿命可靠性对原始随机变量(例如计算出组成特性,纤维体积比,空隙体积比,层厚度等,并讨论了它们在基于可靠性的最大寿命设计中的意义。使用层厚度为0.127 mm的石墨/环氧树脂(0 / +-45/90)degs层压板来演示该方法。结果表明,在低机械循环载荷和低热循环振幅下,疲劳寿命(0.999可靠性)对基体抗压强度,基体模量,热膨胀系数和层厚度最敏感。在高机械循环载荷和高热循环振幅的情况下,可靠性为0.999的疲劳寿命对基体的剪切强度,纵向纤维模量,基体模量和层厚度更敏感。

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