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缺口半径对疲劳寿命影响的有限元分析

金丹 田大将 李江华 林伟 陈旭

金丹, 田大将, 李江华, 林伟, 陈旭. 缺口半径对疲劳寿命影响的有限元分析[J]. 航空动力学报, 2015, 30(7): 1618-1623. doi: 10.13224/j.cnki.jasp.2015.07.012
引用本文: 金丹, 田大将, 李江华, 林伟, 陈旭. 缺口半径对疲劳寿命影响的有限元分析[J]. 航空动力学报, 2015, 30(7): 1618-1623. doi: 10.13224/j.cnki.jasp.2015.07.012
JIN Dan, TIAN Da-jiang, LI Jiang-hua, LIN Wei, CHEN Xu. Finite element analysis for the effect of notched radius on fatigue life[J]. Journal of Aerospace Power, 2015, 30(7): 1618-1623. doi: 10.13224/j.cnki.jasp.2015.07.012
Citation: JIN Dan, TIAN Da-jiang, LI Jiang-hua, LIN Wei, CHEN Xu. Finite element analysis for the effect of notched radius on fatigue life[J]. Journal of Aerospace Power, 2015, 30(7): 1618-1623. doi: 10.13224/j.cnki.jasp.2015.07.012

缺口半径对疲劳寿命影响的有限元分析

doi: 10.13224/j.cnki.jasp.2015.07.012
基金项目: 

国家重点基础研究发展计划(2011CB706504)

国家自然科学基金(11102119)

第48批博士后科学基金面上项目(201000480649)

详细信息
    作者简介:

    金丹(1976-),女,辽宁鞍山人,副教授,博士,主要从事金属材料的疲劳与断裂.

  • 中图分类号: V215.5+5;TG155.5

Finite element analysis for the effect of notched radius on fatigue life

  • 摘要: 针对Mod.9Cr-1Mo铁素体钢缺口件进行了非比例应变路径低周疲劳试验,采用直流电位差法测量裂纹萌生寿命,比较了缺口半径和应变路径对疲劳裂纹萌生寿命的影响.试验结果表明:缺口件裂纹萌生寿命占疲劳寿命的比例与应变路径和缺口半径相关.采用ANSYS软件进行模拟计算,材料弹塑性特性采用von Mises屈服准则、多线性运动硬化律和单轴循环应力应变曲线描述.模拟结果表明:各应变路径下缺口根部处产生了明显的应力集中,等效应力最大值均发生在缺口根部处,随着离缺口根部距离的增加,应力随之而降低.但不同缺口半径下,离缺口根部不同距离处的应力梯度变化趋势随应变路径不同而不同.基于模拟结果,采用Smith-Watson-Topper(SWT)模型进行疲劳寿命预测.结果表明SWT模型针对大缺口半径的预测结果较好,大部分点位于2倍分散带内,但针对小缺口半径预测结果普遍偏低.

     

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出版历程
  • 收稿日期:  2014-02-08
  • 刊出日期:  2015-07-28

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