冷膨胀残余应力对2024-T351铝合金疲劳裂纹扩展的影响

M. Benachour, A. Hadjoui, M. Benguediab, N. Benachour
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引用次数: 0

摘要

疲劳寿命和疲劳裂纹扩展速率受应力比、应力水平、裂纹取向、温度、残余应力、腐蚀等因素的控制。采用基于最大应力强度因子失效准则的恒幅循环方法,研究了残余应力对铝合金2024-T351 I型裂纹疲劳裂纹扩展的影响。通过数值试验,对孔口处有双贯通裂纹的试样施加冷胀引起的残余应力场。采用NASGRO模型进行横向-纵向疲劳裂纹扩展试验。分析了应力比和不同程度的残余应力场对疲劳寿命和疲劳裂纹扩展速率的影响。结果表明:压缩残余应力对2024-T351铝合金的疲劳行为有显著影响;
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Effect of residual stress induced by cold expansion on fatigue crack growth of Aluminium alloy 2024-T351
Fatigue life and fatigue crack growth rate are controlled by stress ratio, stress level, orientation of crack, temper-ature, residual stress, corrosion, etc. The effects of residual stress on fatigue crack growth in aluminium (Al) alloy 2024-T351 by Mode I crack were investigated by applying constant amplitude cycles based on maximum stress intensity factor failure criteria. The residual stress fields induced by cold expansion were imposed on the specimen with double through crack at hole by numerical experimentation. The fatigue crack growth tests were performed in transverse-longitudinal orientation using NASGRO model. The effects of stress ratio and different levels of residual stress fields on fatigue life and fatigue crack growth rates were analyzed. The results showed that compressive residual stress has significant effect on fatigue behavior of Al alloy 2024-T351.
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