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一种转子动力吸振器的参数优化方法

刘子良 许琦 李文龙 姚红良 闻邦椿

刘子良, 许琦, 李文龙, 姚红良, 闻邦椿. 一种转子动力吸振器的参数优化方法[J]. 航空动力学报, 2018, 33(10): 2359-2366. doi: 10.13224/j.cnki.jasp.2018.10.007
引用本文: 刘子良, 许琦, 李文龙, 姚红良, 闻邦椿. 一种转子动力吸振器的参数优化方法[J]. 航空动力学报, 2018, 33(10): 2359-2366. doi: 10.13224/j.cnki.jasp.2018.10.007
Parameter optimization method of rotor dynamic vibration absorber[J]. Journal of Aerospace Power, 2018, 33(10): 2359-2366. doi: 10.13224/j.cnki.jasp.2018.10.007
Citation: Parameter optimization method of rotor dynamic vibration absorber[J]. Journal of Aerospace Power, 2018, 33(10): 2359-2366. doi: 10.13224/j.cnki.jasp.2018.10.007

一种转子动力吸振器的参数优化方法

doi: 10.13224/j.cnki.jasp.2018.10.007
基金项目: 国家重点基础研究发展计划(2012CB026006);国家自然科学基金(51475085)

Parameter optimization method of rotor dynamic vibration absorber

  • 摘要: 对用于抑制转子系统启机过临界转速时过大振动的动力吸振器进行参数优化设计,以达到最优抑振目的。利用有限元方法建立动力吸振器-转子耦合系统的动力学方程,求得耦合系统的半数值半解析的响应表达式。设计优化策略利用响应解与限边界的坐标轮换法相结合,寻找动力吸振器的最佳设计变量;将所得最优参数的动力吸振器与常规优化设计方法设计的动力吸振器的抑振性能进行对比,并分析动力吸振器对参数最优偏离的敏感性。结果表明:该参数优化方法优化的动力吸振器能降低1阶共振幅值达45.4%,说明了该方法的有效性;该方法比两种有效的常规优化方法优化的动力吸振器的抑振效果分别高11.2%、9%,可见其优化效果的优异性;与阻尼最优偏离相比,该参数优化方法优化的动力吸振器的抑振性能对刚度最优偏离具有更高的敏感性。

     

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出版历程
  • 收稿日期:  2017-05-09
  • 刊出日期:  2018-10-28

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