首页> 外文期刊>International Journal of Fatigue >From uni- to multi-axial fretting-fatigue crack nucleation: Development of a stress-gradient-dependent critical distance approach
【24h】

From uni- to multi-axial fretting-fatigue crack nucleation: Development of a stress-gradient-dependent critical distance approach

机译:从单轴至多轴微动疲劳裂纹成核:应力梯度相关临界距离方法的发展

获取原文
获取原文并翻译 | 示例
           

摘要

Fretting fatigue is characterized by combined high stress gradients induced by contact loading and more homogeneous stress gradients induced by bulk fatigue stressing. The stress gradients computed at the "hot-spot" located on the surface at the trailing contact border are very high, usually above 10GPa/ mm. For such uncommon stressing conditions, prediction of cracking risk becomes very complex and non-local fatigue approaches must be adopted. The purpose of the present study was to investigate how non-local strategies, such as "critical distance", developed for medium stress gradient conditions such as "notch" configurations, were transposed to predict fretting cracking risk. Elastic crack nucleation conditions of a 35 Ni Cr Mo 16 low alloyed steel at 10E6 cycles have been identified for various cylinder pad radius, contact pressure and fatigue stress conditions. The experimental crack nucleation conditions were then compared to predictions from analytical simulations coupling uni-axial and Crossland's mul-tiaxial fatigue descriptions. The local "hot-spot" analysis systematically overestimated cracking risk and induced more than 30% error with respect to the experimental values. The non-local "critical distance method" based on a constant length scale value still displayed more than 10% dispersion suggesting that a non-constant "critical distance" approach must be considered. By expressing the critical distance evolution as a function of the hydrostatic stress gradient operating next to the stress hot-spot, dispersion was reduced below 5%. Established for the Crossland's stress invariant formulation, this tendency is confirmed by comparing McDiarmid and MWCM critical plane fatigue approaches.
机译:微动疲劳的特征是接触载荷引起的高应力梯度与整体疲劳应力引起的更均匀的应力梯度相结合。在尾部接触边界处位于表面的“热点”处计算出的应力梯度非常高,通常高于10GPa / mm。对于这种不常见的应力条件,开裂风险的预测变得非常复杂,必须采用非局部疲劳方法。本研究的目的是研究如何针对中等应力梯度条件(例如“缺口”构型)开发非局部策略(例如“临界距离”)来预测微动裂纹风险。对于各种气缸垫半径,接触压力和疲劳应力条件,已确定了35 Ni Cr Mo 16低合金钢在10E6循环时的弹性裂纹成核条件。然后,将实验的裂纹成核条件与耦合单轴和Crossland多轴疲劳描述的分析模拟的预测结果进行比较。本地“热点”分析系统地高估了开裂风险,并导致相对于实验值的30%以上的误差。基于恒定长度比例值的非局部“临界距离方法”仍显示出超过10%的离散度,这表明必须考虑非恒定的“临界距离”方法。通过将临界距离演变表示为紧靠应力热点的静水应力梯度的函数,分散度降低到5%以下。为Crossland的应力不变公式建立的这一趋势通过比较McDiarmid和MWCM临界平面疲劳方法得到了证实。

著录项

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