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Fatigue life prediction based on equivalent initial flaw size for Al-Li alloy 2297 under spectrum loading

机译:基于等效载荷下Al-Li合金2297初始缺陷尺寸的疲劳寿命预测

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摘要

Fatigue life prediction methods based on the Equivalent Initial Flaw Size (EIFS) concept under variable amplitude (VA) spectrum loading conditions were studied in this paper. Fatigue tests of Al-Li alloy 2297 under constant amplitude (CA) and VA loading cases were carried out. Based on the comparison of predictions and test results, different ways to determine the EIFSs and whether the load-interaction effects should be considered in VA fatigue life prediction were discussed to recommend their applicable cases. A good agreement is observed between EIFS model predictions and experimental data, especially in case of high maximum stresses in VA loading.
机译:研究了基于等效初始缺陷尺寸(EIFS)概念的变幅(VA)频谱加载条件下的疲劳寿命预测方法。在恒定振幅(CA)和VA载荷情况下,对Al-Li合金2297进行了疲劳测试。在比较预测结果和测试结果的基础上,讨论了确定EIFS的不同方法以及在VA疲劳寿命预测中是否应考虑载荷相互作用的影响,以推荐其适用案例。 EIFS模型预测与实验数据之间观察到很好的一致性,尤其是在VA加载中最大应力较高的情况下。

著录项

  • 来源
    《International Journal of Fatigue 》 |2017年第10期| 39-47| 共9页
  • 作者单位

    Institute of Solid Mechanics, Beihang University, Beijing, China;

    Institute of Solid Mechanics, Beihang University, Beijing, China;

    Institute of Solid Mechanics, Beihang University, Beijing, China,Beijing Institute of Aeronautic Materials, Beijing, China;

    Institute of Solid Mechanics, Beihang University, Beijing, China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    AA2297; EIFS; Fatigue crack growth; Life prediction; Spectrum loading;

    机译:AA2297;EIFS;疲劳裂纹扩展;寿命预测;频谱加载;

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