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双跨转子系统裂纹-松动耦合故障的非线性响应

罗跃纲 闻邦椿

罗跃纲, 闻邦椿. 双跨转子系统裂纹-松动耦合故障的非线性响应[J]. 航空动力学报, 2007, 22(6): 996-1001.
引用本文: 罗跃纲, 闻邦椿. 双跨转子系统裂纹-松动耦合故障的非线性响应[J]. 航空动力学报, 2007, 22(6): 996-1001.
LUO Yue-gang, WEN Bang-chun. Nonlinear responses of two-span rotor-bearing system with coupling faults of crack and pedestal looseness[J]. Journal of Aerospace Power, 2007, 22(6): 996-1001.
Citation: LUO Yue-gang, WEN Bang-chun. Nonlinear responses of two-span rotor-bearing system with coupling faults of crack and pedestal looseness[J]. Journal of Aerospace Power, 2007, 22(6): 996-1001.

双跨转子系统裂纹-松动耦合故障的非线性响应

基金项目: 国家自然科学基金重点资助(50535010);国家自然科学基金资助(50275024)

Nonlinear responses of two-span rotor-bearing system with coupling faults of crack and pedestal looseness

  • 摘要: 建立了带有裂纹-支承松动耦合故障的具有三轴承支承的双跨弹性转子系统的动力学模型, 并对系统裂纹、松动及其耦合故障对系统非线性动力学响应的影响进行了数值仿真研究.当只有裂纹故障时, 在亚临界转速和超临界转速区均有拟周期运动;当只有松动故障时, 在亚临界转速区为拟周期运动, 而在超临界转速区为混沌运动.当出现裂纹-松动耦合故障时, 松动故障的影响占主要地位, 同时有较大范围的周期3运动区间出现.随着裂纹深度的增加, 其影响作用逐渐增大.研究结果为转子-轴承系统故障诊断、动态设计和安全运行提供了理论参考.

     

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出版历程
  • 收稿日期:  2006-06-01
  • 修回日期:  2006-10-30
  • 刊出日期:  2007-06-28

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