Fretting fatigue in dovetail assembly and bridge-flat model: Verification of a life prediction model based on stress gradient

被引:0
|
作者
Zhang, Xiyuan [1 ,2 ,3 ,4 ]
Wei, Dasheng [1 ,2 ,3 ,4 ]
Yang, Shun [1 ,2 ,3 ,4 ]
机构
[1] Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
[2] Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China
[3] Lab Struct Strength & Vibrat Aero & Astroengines, Beijing 100191, Peoples R China
[4] Beihang Univ, Jiangxi Res Inst, Nanchang 330096, Peoples R China
关键词
Fretting fatigue; Dovetail assembly; Bridge-flat model; Stress gradient; Life prediction model; Combined high and low fatigue; FRACTURE-MECHANICS; CRACK INITIATION; TITANIUM-ALLOY; TI-6AL-4V; CONTACT; WEAR; METHODOLOGY; BEHAVIOR; FAILURE; RISK;
D O I
10.1016/j.ijfatigue.2024.108500
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The dovetail assembly and the bridge-flat model are two typical fretting fatigue tests. This article concentrates on the fretting fatigue of the dovetail assembly, utilizing a sub-scaled specimen tested under cyclic loading. Simultaneously, fretting tests on the bridge-flat and combined high and low cycle fatigue tests on the dovetail assembly were conducted. These tests were analyzed in conjunction with the dovetail assembly to understand the stress state characteristics in the contact region. The results from both tests and finite element analysis highlight that fretting leads to a significant reduction in fatigue life, primarily attributed to stress concentration at the edges of the contact area. Building upon the method of stress gradient correction, a life prediction model for fretting fatigue is proposed, demonstrating good accuracy in predicting fretting fatigue life.
引用
收藏
页数:16
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