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含刮痕缺陷的7050-T7451铝合金板疲劳寿命预估

詹志新 胡伟平 张淼 孟庆春

詹志新, 胡伟平, 张淼, 等 . 含刮痕缺陷的7050-T7451铝合金板疲劳寿命预估[J]. 北京航空航天大学学报, 2015, 41(9): 1678-1685. doi: 10.13700/j.bh.1001-5965.2014.0656
引用本文: 詹志新, 胡伟平, 张淼, 等 . 含刮痕缺陷的7050-T7451铝合金板疲劳寿命预估[J]. 北京航空航天大学学报, 2015, 41(9): 1678-1685. doi: 10.13700/j.bh.1001-5965.2014.0656
ZHAN Zhixin, HU Weiping, ZHANG Miao, et al. Fatigue life prediction for 7050-T7451 aluminum alloy plate with scratch defect[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1678-1685. doi: 10.13700/j.bh.1001-5965.2014.0656(in Chinese)
Citation: ZHAN Zhixin, HU Weiping, ZHANG Miao, et al. Fatigue life prediction for 7050-T7451 aluminum alloy plate with scratch defect[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1678-1685. doi: 10.13700/j.bh.1001-5965.2014.0656(in Chinese)

含刮痕缺陷的7050-T7451铝合金板疲劳寿命预估

doi: 10.13700/j.bh.1001-5965.2014.0656
基金项目: 北京航空航天大学基本科研业务费-博士研究生创新基金
详细信息
    作者简介:

    詹志新(1988—),男,山东聊城人,博士研究生,zzxupc@163.com

    通讯作者:

    胡伟平(1975—),男,湖南常德人,副教授,huweiping@buaa.edu.cn,主要研究方向为疲劳与损伤力学.

  • 中图分类号: O346.5

Fatigue life prediction for 7050-T7451 aluminum alloy plate with scratch defect

  • 摘要: 针对含刮痕缺陷的7050-T7451铝合金板的疲劳损伤问题进行了研究,通过考虑刮擦后残余应力、塑性损伤以及疲劳载荷的共同作用,预估了含刮痕铝合金板的疲劳寿命.对刮痕的产生进行非线性动力学有限元(FE)分析,得到了刮痕处的残余应力场与塑性应变场;根据塑性损伤方程,计算了在刮擦过程中刮痕处由于塑性变形产生的初始损伤场;基于多轴疲劳的损伤力学模型,建立了疲劳损伤分析的有限元数值解法,并对损伤演化方程中的材质参数进行了标定;综合考虑残余应力场、塑性初始损伤和疲劳损伤,对含刮痕的铝合金板进行了疲劳寿命预估,并与试样的疲劳试验结果进行了比较,理论估计和试验得到了相一致的疲劳寿命结果,验证了方法的可行性.本文研究为工程中含刮痕结构的疲劳寿命预估提供了一种本文方法和实用手段.

     

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出版历程
  • 收稿日期:  2014-10-22
  • 刊出日期:  2015-09-20

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