Affiliation:
1. School of Mechanical and Automotive Engineering, Shanghai University of Engineering Science, Shanghai, China
2. United Automotive Electronic Systems Co., Ltd, Shanghai, China
Abstract
In fatigue test, the fatigue life of metal components is affected by many factors, such as test temperature, stress ratio and loading frequency. In order to study the influence of temperature on fatigue life of bolted joints, thermal stress and fast coefficient are introduced. A numerical method of fatigue crack initiation life is proposed based on Manson-Coffin strain fatigue formula. The crack initiation life of 2024 aluminum alloy at different temperatures can be obtained by this method, which provides a theoretical basis for the fatigue life prediction of metals. Then, the stress severity factor SSF is introduced to calculate fatigue life of plane bolted joints. The data obtained from the model show that the crack initiation life of aluminum alloy specimen decreases significantly with test temperature rises, the same as the fatigue life of bolted joints.
Subject
Mechanical Engineering,Aerospace Engineering
Cited by
4 articles.
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