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凹坑型硬物损伤对TC4材料疲劳强度的影响

胡绪腾 贾旭 朱自佳 嵇大伟 宋迎东

胡绪腾, 贾旭, 朱自佳, 嵇大伟, 宋迎东. 凹坑型硬物损伤对TC4材料疲劳强度的影响[J]. 航空动力学报, 2018, 33(4): 969-979. doi: 10.13224/j.cnki.jasp.2018.04.024
引用本文: 胡绪腾, 贾旭, 朱自佳, 嵇大伟, 宋迎东. 凹坑型硬物损伤对TC4材料疲劳强度的影响[J]. 航空动力学报, 2018, 33(4): 969-979. doi: 10.13224/j.cnki.jasp.2018.04.024
Effect of dent-type foreign object damage on fatigue strength of TC4 material[J]. Journal of Aerospace Power, 2018, 33(4): 969-979. doi: 10.13224/j.cnki.jasp.2018.04.024
Citation: Effect of dent-type foreign object damage on fatigue strength of TC4 material[J]. Journal of Aerospace Power, 2018, 33(4): 969-979. doi: 10.13224/j.cnki.jasp.2018.04.024

凹坑型硬物损伤对TC4材料疲劳强度的影响

doi: 10.13224/j.cnki.jasp.2018.04.024
基金项目: 国家自然科学基金(E050401)

Effect of dent-type foreign object damage on fatigue strength of TC4 material

  • 摘要: 针对风扇/压气机叶片中叶盆/叶背遭受的硬物损伤(FOD)凹坑型损伤,进行了不同冲击角度下模拟FOD试验、损伤特征与应力集中分析,开展了冲击后不处理和冲击后去残余应力退火试样的高循环疲劳试验研究和疲劳强度的预测。结果表明:损伤深度和应力集中系数均随着冲击角度的增加而变大,损伤深度范围为0.1~0.5mm,应力集中系数范围为1.3~1.7。不同冲击角度条件下,凹坑型损伤试样疲劳强度相对光滑试样下降程度在50%~70%范围内,与应力集中系数并不是呈单调下降关系,最危险冲击角为60°。去残余应力退火后凹坑型损伤试样的高循环疲劳(HCF)性能有所提高,表明残余应力的影响程度不容忽略。去残余应力试样的HCF性能并不是随应力集中系数的增大而下降,验证了微结构损伤的影响,说明损伤深度作为制定可用极限或维修极限的唯一参量具有一定的局限性。对凹坑型损伤试样的疲劳强度的预测误差在±20%以内。

     

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  • 收稿日期:  2016-11-09
  • 刊出日期:  2018-04-28

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