A fretting fatigue reliability analysis method was developed.The contact area was in a multi-axial stress state under fretting conditions.The multi-axial fatigue parameter based on the critical plane was used to predict the fretting fatigue life.On the basis of calculating determinate life
the randomicity of modulus of elasticity
friction coefficient and material constant in the life model were considered
and the fretting fatigue life reliability model was obtained by Monte-Carlo simulation method along with the response surface method.Finally
the method was applied to analyze fretting fatigue life reliability of dovetail joint
proving the feasibility and validity of this method.
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Related Author
Shijie LIU
Dengfeng LIU
Xiaoqiu MA
Guozhu LIANG
Zheng LIU
Li XIE
Jijun ZHANG
Changjiang LONG
Related Institution
Beijing Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
Laboratory of Science and Technology on Cryogenic Liquid Propulsion,Beijing Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
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