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航空发动机宽弦风扇叶片鸟撞损伤模型标定

柴象海 侯亮 王志强 汤忠斌

柴象海, 侯亮, 王志强, 汤忠斌. 航空发动机宽弦风扇叶片鸟撞损伤模型标定[J]. 航空动力学报, 2016, 31(5): 1032-1038. doi: 10.13224/j.cnki.jasp.2016.05.002
引用本文: 柴象海, 侯亮, 王志强, 汤忠斌. 航空发动机宽弦风扇叶片鸟撞损伤模型标定[J]. 航空动力学报, 2016, 31(5): 1032-1038. doi: 10.13224/j.cnki.jasp.2016.05.002
CHAI Xiang-hai, HOU Liang, WANG Zhi-qiang, TANG Zhong-bin. Bird strike model calibration for an aero engine wide-chord fan blade[J]. Journal of Aerospace Power, 2016, 31(5): 1032-1038. doi: 10.13224/j.cnki.jasp.2016.05.002
Citation: CHAI Xiang-hai, HOU Liang, WANG Zhi-qiang, TANG Zhong-bin. Bird strike model calibration for an aero engine wide-chord fan blade[J]. Journal of Aerospace Power, 2016, 31(5): 1032-1038. doi: 10.13224/j.cnki.jasp.2016.05.002

航空发动机宽弦风扇叶片鸟撞损伤模型标定

doi: 10.13224/j.cnki.jasp.2016.05.002
基金项目: 

国家自然科学基金(51205377)

上海市科委基础研究重大项目(12DJ1400500)

航空科学基金民发专项(2012ZBN2003)

详细信息
    作者简介:

    柴象海(1979-),男,山东济南人,高级工程师,博士,主要从事航空发动机包容性与外物吸入损伤研究.

  • 中图分类号: V214

Bird strike model calibration for an aero engine wide-chord fan blade

  • 摘要: 为建立航空发动机风扇叶片抗鸟撞载荷能力的量化预测方法,针对特定的航空发动机宽弦风扇叶片设计,依据发动机在典型工作状态下的吸鸟速度、角度等撞击参数开展叶片鸟撞试验,采用显式动力学数值仿真方法,建立叶片鸟撞试验仿真分析模型,并通过对模型中叶片材料参数、鸟体本构模型参数、鸟与叶片耦合接触参数进行敏感度分析,对模型进行标定.结果表明,标定后的鸟撞分析模型所预测的叶片损伤模式与试验结果一致,预测的损伤位置与试验测量结果误差小于10%.

     

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出版历程
  • 收稿日期:  2014-08-11
  • 刊出日期:  2016-05-28

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