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不平衡激励作用下周向加肋机匣振动能量传递机理

马英群 张锴 王云飞 赵巍 赵庆军

马英群, 张锴, 王云飞, 赵巍, 赵庆军. 不平衡激励作用下周向加肋机匣振动能量传递机理[J]. 航空动力学报, 2018, 33(11): 2585-2592. doi: 10.13224/j.cnki.jasp.2018.11.003
引用本文: 马英群, 张锴, 王云飞, 赵巍, 赵庆军. 不平衡激励作用下周向加肋机匣振动能量传递机理[J]. 航空动力学报, 2018, 33(11): 2585-2592. doi: 10.13224/j.cnki.jasp.2018.11.003
Vibration energy transmitting mechanism of ring-stiffened casing excited by rotor unbalance[J]. Journal of Aerospace Power, 2018, 33(11): 2585-2592. doi: 10.13224/j.cnki.jasp.2018.11.003
Citation: Vibration energy transmitting mechanism of ring-stiffened casing excited by rotor unbalance[J]. Journal of Aerospace Power, 2018, 33(11): 2585-2592. doi: 10.13224/j.cnki.jasp.2018.11.003

不平衡激励作用下周向加肋机匣振动能量传递机理

doi: 10.13224/j.cnki.jasp.2018.11.003
基金项目: 国家重点研发计划(2016YFB0901402);国家自然科学基金(51406195)

Vibration energy transmitting mechanism of ring-stiffened casing excited by rotor unbalance

  • 摘要: 为了研究周向加肋机匣对整机振动的抑制机理,采用有限元法建立了加肋机匣-支承-转子耦合结构,结合振动功率流法分析了在转子不平衡激励作用下周向加肋机匣中的振动能量传递机理。 结果表明:机匣周向加肋筋诱导出的能量涡流场能够分流和耗散掉部分由转子传递至机匣的振动能量;机匣周向加肋筋改变了振动能量的传递路径,减小了机匣与支板连接处振动能量的回流现象;振动能量传递到机匣周向加肋筋后发生传递波波形的转换,携带大部分振动能量的弯曲波转换为纵波并沿加肋筋周向传递,阻断振动能量沿轴向传递至整机其他部位。 研究结果可为航空发动机结构设计以及整机减振提供参考。

     

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出版历程
  • 收稿日期:  2017-08-25
  • 刊出日期:  2018-11-28

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