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平均应力对30CrMnSiA钢多轴疲劳失效的影响

刘天奇 时新红 张建宇 费斌军

刘天奇, 时新红, 张建宇, 费斌军. 平均应力对30CrMnSiA钢多轴疲劳失效的影响[J]. 航空动力学报, 2018, 33(12). doi: 10.13224/j.cnki.jasp.2018.12.018
引用本文: 刘天奇, 时新红, 张建宇, 费斌军. 平均应力对30CrMnSiA钢多轴疲劳失效的影响[J]. 航空动力学报, 2018, 33(12). doi: 10.13224/j.cnki.jasp.2018.12.018
Effect of mean stress on multiaxial fatigue failure of 30CrMnSiA steel[J]. Journal of Aerospace Power, 2018, 33(12). doi: 10.13224/j.cnki.jasp.2018.12.018
Citation: Effect of mean stress on multiaxial fatigue failure of 30CrMnSiA steel[J]. Journal of Aerospace Power, 2018, 33(12). doi: 10.13224/j.cnki.jasp.2018.12.018

平均应力对30CrMnSiA钢多轴疲劳失效的影响

doi: 10.13224/j.cnki.jasp.2018.12.018
基金项目: 国家自然科学基(11172021)

Effect of mean stress on multiaxial fatigue failure of 30CrMnSiA steel

  • 摘要: 对30CrMnSiA高强钢实心圆棒试件进行了存在平均应力及相位差下拉-扭复合加载的多轴高周疲劳试验,对不同平均应力及相位差下的试验数据、平面应力特点进行了分析和研究。试验结果表明,对于不存在平均应力的情况,随着相位差的增大,疲劳寿命逐渐增大。对于存在平均应力的情况,无论是平均拉伸应力还是平均切应力,随着相位差的增大,疲劳寿命逐渐减小。采用最大切应力幅平面上的切应力幅与最大正应力线性组合的准则进行寿命预测发现,对于某些试验情况,随着平均应力的增大,试验寿命与预测寿命变化规律相反。此外,通过测量试件初始起裂的角度并与最大切应力幅平面对比发现,多轴加载下的30CrMnSiA高强钢初始裂纹起裂方向接近最大切应力幅平面。最后通过应力分析说明了采用最大切应力幅平面上的切应力幅与最大正应力线性组合的准则存在的缺陷。

     

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出版历程
  • 收稿日期:  2017-12-19
  • 刊出日期:  2018-12-28

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