首页> 外文期刊>Fatigue & Fracture of Engineering Materials & Structures >Comparison of the cracking energy density and the Smith-Watson-Topper parameters in predicting fretting fatigue lifetime of a steel/aluminum alloy contact
【24h】

Comparison of the cracking energy density and the Smith-Watson-Topper parameters in predicting fretting fatigue lifetime of a steel/aluminum alloy contact

机译:比较开裂能量密度和Smith-Watson-Topper参数在预测钢/铝合金接触件的微动疲劳寿命中的作用

获取原文
获取原文并翻译 | 示例
           

摘要

Many multiaxial fatigue parameters are available to estimate the onset of the crack initiation in mechanical components subjected to fretting fatigue conditions. This study focuses on the ability of the cracking energy density parameter to predict the fretting fatigue life. To estimate this, obtained predictions are compared with those given by another commonly used parameter, namely the Smith-Watson-Topper parameter. First, fretting fatigue experiments were achieved using a new designed setup with a mono-contact configuration (aluminum/steel). A finite element model was used to compute the stress/strain fields around the contact zone. Because of the high stress gradient in the contact zone, the estimates of the two fatigue parameters, when using the mechanical quantities on the most loaded material point, lead to too conservative predicted values. It was therefore necessary to define a kind of process zone in which crack nucleation takes place. Using an averaging method to compute stress and strain in this zone, the obtained results show a quite good agreement between the estimated fatigue life and experimental data, whatever the used fatigue indicator. The size of this zone was then compared with the material microstructure and seems to be in the same magnitude that the average grain size.
机译:许多多轴疲劳参数可用于估计在遭受微动疲劳条件的机械部件中裂纹萌生的开始。这项研究的重点是开裂能量密度参数预测微动疲劳寿命的能力。为了对此进行估计,将获得的预测与另一个常用参数(即Smith-Watson-Topper参数)给出的预测进行比较。首先,使用具有单触点配置(铝/钢)的新设计设置来实现微动疲劳实验。使用有限元模型来计算接触区域周围的应力/应变场。由于接触区中的应力梯度高,因此在最重的物料点上使用机械量时,两个疲劳参数的估计会导致预测值过于保守。因此,必须定义一种在其中发生裂纹成核的工艺区域。使用平均方法计算该区域的应力和应变,无论使用何种疲劳指标,所获得的结果都表明估算的疲劳寿命与实验数据之间有很好的一致性。然后将该区域的大小与材料的微观结构进行比较,似乎与平均晶粒大小相同。

著录项

  • 来源
  • 作者单位

    Universite Lille Nord de France, Lille, France,Universite Lille 1. Laboratoire de Mecanique de Lille (LML), UMR CNRS 8107, F-59650 Villeneuve d'Ascq, France;

    Universite Lille Nord de France, Lille, France,Universite d'Artois. FSA de Bethune, Laboratoire de Genie Civil et geo-Environnement (LGCgE). EA 4515. Technoparc-Futura, 62400 Bethune, France;

    Universite Lille Nord de France, Lille, France,Universite Lille 1. Laboratoire de Mecanique de Lille (LML), UMR CNRS 8107, F-59650 Villeneuve d'Ascq, France;

    Universite Lille Nord de France, Lille, France,Universite Lille 1. Laboratoire de Mecanique de Lille (LML), UMR CNRS 8107, F-59650 Villeneuve d'Ascq, France;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    fretting fatigue; life prediction; cracking energy density; volumetric approach;

    机译:微动疲劳;寿命预测;裂解能密度体积法;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号