Contact-evolution based prediction of fretting fatigue life: Effect of slip amplitude

被引:173
作者
Madge, J. J. [1 ]
Leen, S. B. [1 ]
McColl, I. R. [1 ]
Shipway, P. H. [1 ]
机构
[1] Univ Nottingham, Sch Mech Mat & Mfg Engn, Univ Technol Ctr Gas Turbine Transmiss Syst, Nottingham NG7 2RD, England
关键词
finite element; fretting fatigue; critical plane; wear simulation; contact evolution; fretting wear;
D O I
10.1016/j.wear.2006.11.004
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Fretting fatigue is a complex problem and therefore it has generally been necessary to determine fatigue lives experimentally. This paper describes a method that integrates wear modelling with fretting fatigue analysis to permit the prediction of the effects of material removal, due to fretting wear, on fretting fatigue life. A finite element based method is employed to predict the fretting wear-induced evolution of contact geometry, contact stresses and a multiaxial fatigue damage parameter with cumulative damage effects, as a function of slip amplitude, for a laboratory fretting fatigue test arrangement. The results show that the approach is capable of capturing the experimentally observed effect of slip amplitude on fatigue life. The conditions simulated span across a range of partial slip and gross sliding conditions, corresponding to fretting fatigue tests available from the literature, and giving rise to the well-known phenomenon of a critical range of slip amplitude for reduced fatigue life. The methodology demonstrates that this is primarily due to wear-induced pressure redistribution, the nature of which is highly dependent on the slip regime. (c) 2006 Published by Elsevier B.V.
引用
收藏
页码:1159 / 1170
页数:12
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