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首页> 外文期刊>Tribology Transactions >The fatigue crack initiation life prediction based on several high-cycle fatigue criteria under spherical rolling contact
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The fatigue crack initiation life prediction based on several high-cycle fatigue criteria under spherical rolling contact

机译:基于几种滚动轴承高周疲劳准则的疲劳裂纹萌生寿命预测

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摘要

In this study, the simulation of rolling contact fatigue is conducted under spherical contact. To predict a crack initiation life accurately, it is necessary to calculate contact stress and subsurface stresses accurately. Contact stresses are obtained by contact analysis of a semi-infinite solid based on the use of influence functions and the subsurface stress field is obtained using rectangular patch solutions. Based on these stress values, several multiaxial high-cycle fatigue criteria are used and the critical loads corresponding to fatigue limits are calculated. The criteria were classified into three categories, namely the critical plane approach, the stress invariant approach and the approach based on the meso-scopic scale. The simulation results show that the critical load is decreasing rapidly and the site of crack initiation also moves rapidly to the surface from the subsurface when the friction coefficient exceeds a specific value for all three fatigue criteria.
机译:在这项研究中,滚动接触疲劳的模拟是在球面接触下进行的。为了准确地预测裂纹萌生寿命,必须准确计算接触应力和地下应力。接触应力是通过使用影响函数对半无限固体进行接触分析而获得的,并且地下应力场是使用矩形补丁解决方案获得的。基于这些应力值,使用了多个多轴高周疲劳准则,并计算了与疲劳极限相对应的临界载荷。该标准分为三类,即临界面方法,应力不变方法和基于中观尺度的方法。仿真结果表明,当所有三个疲劳标准的摩擦系数均超过特定值时,临界载荷迅速减小,裂纹萌生部位也从次表面迅速移至表面。

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