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A procedure for estimating the total life in fretting fatigue

机译:估算微动疲劳总寿命的程序

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This paper proposes a procedure for estimating the total fatigue life in fretting fatigue. It separately analyses the fatigue crack initiation and propagation lives. The correlation between crack initiation and propagation is made considering a non-arbitrary crack initiation length provided by the model. The number of cycles to initiate a crack is obtained from the stress distribution beneath the contact zone and a multiaxial fatigue crack initiation criterion. The propagation of the crack is considered using different fatigue crack propagation laws, including some modifications in order to take the short crack growth into account. The results obtained by this method are compared with the fatigue lives obtained in various fretting fatigue tests under spherical contact with 7075-T6 aluminium alloy. [References: 30]
机译:本文提出了一种估算微动疲劳总疲劳寿命的方法。它分别分析了疲劳裂纹的萌生和扩展寿命。考虑模型提供的非任意裂纹萌生长度来进行裂纹萌生与扩展之间的相关性。从接触区域下方的应力分布和多轴疲劳裂纹萌生判据可以得出裂纹萌生的循环次数。可以使用不同的疲劳裂纹扩展定律来考虑裂纹的扩展,包括一些修改,以便考虑到短的裂纹扩展。将通过该方法获得的结果与在与7075-T6铝合金进行球形接触的各种微动疲劳试验中获得的疲劳寿命进行比较。 [参考:30]

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