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A simplified and fast method to predict plain and notch fatigue of shot peened high-strength aluminium alloys under reverse bending

机译:一种简化的快速方法来预测喷丸高强度铝合金在反向弯曲下的平整和缺口疲劳

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摘要

A simplified and fast method to predict plain and notch fatigue resistance of shot peened Al-7075-T651 is presented. For this purpose, different shot peening treatments were carried out on plain and notched samples. Reverse bending SN curves were determined for both notched and unnotched conditions. Initial and stabilized residual stresses were measured by X-ray diffraction on plain samples. An evolution to stabilised values of the surface stresses, depending on the applied loads, was observed. Residual stresses measured on plain samples were used for predicting, by means of finite element modelling, respectively the residual stress distributions in the notched samples and the residual stress relaxation in the vicinity of the notch due to the application of different fatigue loads. The results of the numerical analysis were used to validate a simplified analytical approach developed for computing residual stress relaxation and surface residual stress field both in plain and notched samples. The predicted residual stress distribution was finally incorporated into a multiaxial fatigue criterion. Specifically, the critical distances theory was used to predict the fatigue resistance of notched samples in the presence of a compressive residual stress field.
机译:提出了一种简单快速的方法来预测喷丸的Al-7075-T651的平整度和缺口疲劳强度。为此,对普通和有缺口的样品进行了不同的喷丸处理。确定有缺口和无缺口条件的反向弯曲SN曲线。初始应力和稳定残余应力通过X射线衍射对普通样品进行测量。观察到根据施加的载荷,表面应力趋于稳定值的演变。通过有限元建模,在普通样品上测得的残余应力分别用于预测缺口样品中的残余应力分布和由于施加不同的疲劳载荷而造成的缺口附近的残留应力松弛。数值分析的结果用于验证简化的分析方法,该方法可用于计算平原和缺口样品中的残余应力松弛和表面残余应力场。最后将预测的残余应力分布纳入多轴疲劳准则。具体而言,临界距离理论用于预测在存在压缩残余应力场的情况下缺口试样的疲劳强度。

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