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Experimental and numerical study of fretting fatigue in dovetail assembly using a total life prediction model

机译:使用总寿命预测模型的燕尾组件烦恼疲劳的实验性和数值研究

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The fretting fatigue in dovetail assembly was investigated by experiments and finite element method. A sub-scaled specimen and its fixture were designed and tested under cyclic loading of three load levels. The stress distribution in the contact zone was calculated and several fatigue parameters including SWT and FS parameter were employed to predict the direction and the location of the crack initiation and predict the initiation life. The crack growth path was determined by extended finite element method and crack growth life was predicted after introducing the effect of fretting-contact-induced crack closure. Then based on a total fatigue life prediction model, the total life was obtained by summing up the crack initiation life and the crack growth life using a fixed initial crack length, and the predicted results agreed well with experiments.
机译:通过实验和有限元法研究了燕尾组件中的微动疲劳。 在三个负荷水平的循环负载下设计和测试了亚鳞片样本和其夹具。 计算接触区中的应力分布,并采用包括SWT和FS参数的几个疲劳参数来预测裂纹启动的方向和位置并预测起始寿命。 通过延长的有限元法测定裂纹生长路径,并在引入碎屑诱导的裂纹闭合效果后预测裂纹生长寿命。 然后基于总疲劳寿命预测模型,通过使用固定的初始裂缝长度求出裂缝启动寿命和裂缝生长寿命来获得总寿命,并且预测结果与实验相同。

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