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Study of the variation of contact state near the contact boundary in a dovetail attachment under different loads

  • Beihang University
  • AECC Commercial Aircraft Engine Co., Ltd

科研成果: 期刊稿件文章同行评审

摘要

It is very important to characterize the variation of cyclic parameters near the contact edge in dovetail attachments for understanding the fretting fatigue mechanism. In this paper, the variation of contact state in a dovetail attachment was studied by using the finite element method (FEM), which is affected by two key factors i.e. the relative slip and the mutual compaction. When the flank angle and the coefficient of friction are constant, the influence of compaction seems much more obvious under centrifugal loads, and the edge of contact zone would move up along the contact surface. However, the influence of relative slip becomes much more obvious under tensile loads, and the edge of contact zone would move down. The movement of contact edge shows a similar trend under cyclic loads, which may result in the movement of position where the high stress gradient locates, and the numerical results show that the negative stress ratio would occur near the contact edge.

源语言英语
页(从-至)518-526
页数9
期刊Engineering Failure Analysis
105
DOI
出版状态已出版 - 11月 2019

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