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渗碳M50NiL钢磨削表面完整性特征及疲劳失效机理

娄艳芝 李春志 李旭东 谢孝昌 赵振业

航空材料学报2017,Vol.37Issue(6):25-33,9.
航空材料学报2017,Vol.37Issue(6):25-33,9.DOI:10.11868/j.issn.1005-5053.2017.000127

渗碳M50NiL钢磨削表面完整性特征及疲劳失效机理

Surface Integrity Characteristics and Fatigue Failure Mechanism of Carburized M50NiL Steel

娄艳芝 1李春志 1李旭东 1谢孝昌 1赵振业1

作者信息

  • 1. 中国航发北京航空材料研究院,北京100095
  • 折叠

摘要

Abstract

The surface integrity of carburized M50NiL steel was studied by optical microscopy,scanning electron microscopy (SEM),atomic force microscopy (AFM),microhardness tester and residual stress tester.The fatigue properties of the two specimens were measured by the rotational bending fatigue test,and the fatigue test results were simulated and analyzed.The results show that the rotation bending fatigue of carburized M50NiL steel is originated in the sub-surface in the ideal case without considering the surface processing defects.The surface stress concentration factor produced by general grinding causes the fatigue source to be moved from the surface to the sub-surface.Precise grinding improves the surface quality by optimizing the grinding process,effectively restrains the stress concentration of the working surface,and returns the fatigue source from the surface to the sub-surface.The maximum rotary bending fatigue life can be increased by 30 times and the average is 15 times.

关键词

M50NiL钢/磨削/表面完整性/疲劳/失效机理

Key words

M50NiL steel/grinding/surface integrity/fatigue/failure mechanism

分类

航空航天

引用本文复制引用

娄艳芝,李春志,李旭东,谢孝昌,赵振业..渗碳M50NiL钢磨削表面完整性特征及疲劳失效机理[J].航空材料学报,2017,37(6):25-33,9.

基金项目

973项目资助 ()

航空材料学报

OA北大核心CSCDCSTPCD

1005-5053

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