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基于寿命预测模型的微动疲劳影响因素

杨茂胜 陈跃良 毕玉泉

海军航空工程学院学报2012,Vol.27Issue(1):39-44,6.
海军航空工程学院学报2012,Vol.27Issue(1):39-44,6.

基于寿命预测模型的微动疲劳影响因素

Research on Influencing Factors of Fretting Fatigue Based on Life Prediction Model

杨茂胜 1陈跃良 1毕玉泉1

作者信息

  • 1. 海军航空工程学院青岛分院,山东青岛266041
  • 折叠

摘要

Abstract

The distributing of contact pressure and tangential stress were calculated based on finite element software/ABAQUS. With them the Ruiz fretting damage parameter was obtained, based on which a new model for predicting fretting fatigue life was presented, and then the rationality and effectiveness of the model were validated according to the contrast of experiment life and predicting life. At last influence of three parameters on fretting fatigue life was investigated with the model. The results showed that life decreased quickly with increasing of contact pressure, and then increased on the contrary, but it always decreased with increasing of axial stress. In lower contact pressure the fretting fatigue life increased with increasing of pad radius, but it almost did not change in the higher values

关键词

微动疲劳/寿命预测/接触压力/轴向应力/压头半径

Key words

fretting fatigue/life prediction/contact pressure/axial stress/pad radius

分类

航空航天

引用本文复制引用

杨茂胜,陈跃良,毕玉泉..基于寿命预测模型的微动疲劳影响因素[J].海军航空工程学院学报,2012,27(1):39-44,6.

基金项目

国家自然科学基金资助项目 ()

海军航空工程学院学报

OACSTPCD

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