紧固件
残余应力
材料科学
微观结构
结构工程
残余物
有限元法
机械工程
复合材料
计算机科学
工程类
冶金
算法
作者
Ru Su,Lei Huang,Changzhou Xu,Peng He,Xiaoliang Wang,Baolin Yang,Dayong Wu,Qian Wang,Huicong Dong,Haikun Ma
出处
期刊:Coatings
[Multidisciplinary Digital Publishing Institute]
日期:2023-12-02
卷期号:13 (12): 2037-2037
被引量:11
标识
DOI:10.3390/coatings13122037
摘要
Cold expansion technology has been widely used in aviation industries as an effective method of improving the fatigue performance of fastener holes. It can improve the fatigue life several times over without adding weight, meeting the growing demand for lightweight and durable aircraft structures. In recent years, it has been extensively studied through extensive experiments and finite element simulations to analyze the residual stresses around the fastener hole. Appropriate process parameters lead to the generation of beneficial residual stresses that influence the material microstructure, thereby improving the fatigue life of the component. This paper summarized factors influencing residual stresses in cold expansion and their effects on fatigue life, and the strengthening mechanism, parameter optimization, and effect of anti-fatigue are discussed from the point of view of the residual stress and microstructure. The development of new cold expansion technologies and the research directions that can realize anti-fatigue technology efficiently are proposed.
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