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A new method for modelling the support effect under rotating bending fatigue: application to Ti-6Al-4V alloy, with and without shot peening

机译:一种模拟旋转弯曲疲劳下支撑效果的新方法:适用于有无喷丸处理的Ti-6Al-4V合金

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摘要

The subject of this paper is to investigate the capability of the relative stress gradient to properly represent the beneficial effect of residual stress states on the fatigue life of Ti-6Al-4V specimens, with notches of different severity. The research was developed considering notched and un-notched specimens with different geometries and different shot-peening treatments. The results were determined by running fatigue experimentation under rotating bending and by developing a novel predictive model based on the relationship between the local fatigue limit and a generalized form of the relative stress gradient, accounting for the peening-induced residual stresses. The proposed tool for fatigue limit estimation was completed by a stochastic analysis, which considered the variability of the involved parameters, in particular the residual stress entity. This made it possible to finally determine the component failure probability in a general, efficient and accurate way.
机译:本文的目的是研究相对应力梯度能够正确表示残余应力状态对Ti-6Al-4V试样(具有不同严重程度的缺口)的疲劳寿命的有益影响。这项研究是考虑具有不同几何形状和不同喷丸处理方法的带缺口和无缺口试样而开发的。通过在旋转弯曲下进行疲劳试验并基于局部疲劳极限和相对应力梯度的广义形式之间的关系开发新的预测模型来确定结果,该模型考虑了喷丸引起的残余应力。所提出的疲劳极限估算工具是通过随机分析完成的,该分析考虑了相关参数(尤其是残余应力实体)的可变性。这使得有可能以通用,有效和准确的方式最终确定组件的故障概率。

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