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航空发动机风扇叶片的抗鸟撞设计

张海洋 王相平 杜少辉

张海洋, 王相平, 杜少辉. 航空发动机风扇叶片的抗鸟撞设计[J]. 航空动力学报, 2020, 35(6): 1157-1168. doi: 10.13224/j.cnki.jasp.2020.06.005
引用本文: 张海洋, 王相平, 杜少辉. 航空发动机风扇叶片的抗鸟撞设计[J]. 航空动力学报, 2020, 35(6): 1157-1168. doi: 10.13224/j.cnki.jasp.2020.06.005
ZHANG Haiyang, WANG Xiangping, DU Shaohui. Design for anti-bird impact of aero-engine fan blade[J]. Journal of Aerospace Power, 2020, 35(6): 1157-1168. doi: 10.13224/j.cnki.jasp.2020.06.005
Citation: ZHANG Haiyang, WANG Xiangping, DU Shaohui. Design for anti-bird impact of aero-engine fan blade[J]. Journal of Aerospace Power, 2020, 35(6): 1157-1168. doi: 10.13224/j.cnki.jasp.2020.06.005

航空发动机风扇叶片的抗鸟撞设计

doi: 10.13224/j.cnki.jasp.2020.06.005

Design for anti-bird impact of aero-engine fan blade

  • 摘要: 根据航空发动机结构特征和鸟撞后的风扇叶片损伤特征,提出风扇第一级转子叶片是发动机抗鸟撞关键零件,叶片前缘为抗鸟撞设计关键部位。建立一种风扇叶片鸟撞理论分析方法,研究撞击工况、结构参数与鸟撞过程、损伤模式、损伤程度的关系,提出前缘角度是抗鸟撞能力关键结构参数。当撞击工况确定后,前缘角度决定了撞击形式和叶片损伤模式,影响损伤程度。采用显示动力学仿真分析方法,设计了一种带前缘特征的模型,对前缘角度的影响规律进行了验证,并开展了实际风扇叶片改进设计,改进后的叶片被鸟撞击后变形减小最少33%,抗鸟撞击能力明显提升。

     

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出版历程
  • 收稿日期:  2019-12-12
  • 刊出日期:  2020-06-28

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