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基于临界面法及应变路径多轴疲劳寿命预测模型概述

  • Hongbin Liu*
  • , Wei Chen
  • , Yanrong Wang
  • *此作品的通讯作者
  • Nanjing University of Aeronautics and Astronautics
  • Aero Engine Corporation of China

科研成果: 期刊稿件文章同行评审

摘要

The article has done some research on multiaxial low cycle fatigue life evaluation methods at home and abroad, summarized multiaxial low cycle fatigue life prediction models based on Critical-Plane method and strain path and analyzed the advantages and disadvantages compared with models and applicability. It has been shown that most of the empirical prediction methods could suitable for only one or few materials so far. When they are applied on other materials, the results are usually disappointing. Meanwhile, the multi-axial fatigue failure of materials are very complicated. The current massive research work was mainly done under constant temperature and load while the studies carried out on high temperature, varying temperature and load are few. If taking notch effect, size effect, surface roughness, residual stress into account, the situation would be even more complicated. Current research on multi axis fatigue is interested in establishing life prediction model, To carry out related fatigue test,Little in-depth study of its micro mechanism The multi-axial fatigue is still a problem needing further studies.

投稿的翻译标题Research on multi axis low cycle fatigue life prediction models based on critical plane method and strain path
源语言繁体中文
页(从-至)173-180
页数8
期刊Jixie Qiangdu/Journal of Mechanical Strength
41
1
DOI
出版状态已出版 - 15 2月 2019

关键词

  • Critical-plane
  • Low cycle fatigue life
  • Multi axis
  • Prediction models
  • Strain path

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