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微动疲劳寿命预测方法研究综述

李维 杨旭峰 李坚 艾兴 程昊 曾嘉迅

南京航空航天大学学报2025,Vol.57Issue(4):589-600,12.
南京航空航天大学学报2025,Vol.57Issue(4):589-600,12.DOI:10.16356/j.1005-2615.2025.04.001

微动疲劳寿命预测方法研究综述

A Review on Fretting Fatigue Life Prediction Methods

李维 1杨旭峰 1李坚 1艾兴 1程昊 1曾嘉迅1

作者信息

  • 1. 中国航空发动机集团有限公司湖南动力机械研究所,株洲 412002
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摘要

Abstract

Through a review of relevant domestic and international literatures on fretting fatigue research,this paper first introduces the concept and characteristics of fretting fatigue.It summarizes the current research status regarding the mechanisms of fretting map theory and investigations into the microscopic mechanisms of fretting fatigue.Secondly,the main factors influencing fretting fatigue life prediction are summarized,including relative slip amplitude,contact pressure,axial load,coefficient of friction,stress gradient,and temperature.Finally,the widely studied and employed methods for predicting fretting fatigue life are comprehensively reviewed.The development trends in fretting fatigue life prediction and future research prospects are summarized.Considering the wear-fatigue coupling damage mechanism and artificial intelligence(AI)-based fretting fatigue life prediction methods are identified as current research hotspots and represent key directions for future development.

关键词

微动疲劳/寿命预测/表面磨损/磨损-疲劳耦合/人工智能

Key words

fretting fatigue/life prediction/surface wear/wear-fatigue coupling/artificial intelligence(AI)

分类

航空航天

引用本文复制引用

李维,杨旭峰,李坚,艾兴,程昊,曾嘉迅..微动疲劳寿命预测方法研究综述[J].南京航空航天大学学报,2025,57(4):589-600,12.

基金项目

国家科技重大专项(J2022-Ⅳ-0012-0026). (J2022-Ⅳ-0012-0026)

南京航空航天大学学报

OA北大核心

1005-2615

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