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复杂结构双转子系统的建模及模型缩减

孙传宗 陈予恕 侯磊

孙传宗, 陈予恕, 侯磊. 复杂结构双转子系统的建模及模型缩减[J]. 航空动力学报, 2017, 32(7): 1747-1753. doi: 10.13224/j.cnki.jasp.2017.07.027
引用本文: 孙传宗, 陈予恕, 侯磊. 复杂结构双转子系统的建模及模型缩减[J]. 航空动力学报, 2017, 32(7): 1747-1753. doi: 10.13224/j.cnki.jasp.2017.07.027
Modeling method and reduction of dual-rotor system with complicated structures[J]. Journal of Aerospace Power, 2017, 32(7): 1747-1753. doi: 10.13224/j.cnki.jasp.2017.07.027
Citation: Modeling method and reduction of dual-rotor system with complicated structures[J]. Journal of Aerospace Power, 2017, 32(7): 1747-1753. doi: 10.13224/j.cnki.jasp.2017.07.027

复杂结构双转子系统的建模及模型缩减

doi: 10.13224/j.cnki.jasp.2017.07.027
基金项目: 国家自然科学基金(11602070); 国家重点基础研究发展计划(2015CB057400); 中国博士后科学基金(2016M590277)

Modeling method and reduction of dual-rotor system with complicated structures

  • 摘要: 建立了包含复杂结构特征的双转子三维实体有限元模型,应用Craig-Bampton模态综合法实现了模型维度的缩减。通过对比临界转速和固有振动特性验证了缩减模型的准确性。在此基础上计算了双转子系统的临界转速谱和特定转速比下的临界转速值。结果表明:Craig-Bampton模态综合法成功地将双转子高维实体有限元模型缩减到仅有数十个(34个)自由度的低维模型,并保持前2阶临界转速误差和前6阶固有频率误差不超过0.43%。基于缩减单转子模型再按照边界条件耦合的分析方案有利于快速求解双转子临界转速等动力学问题。

     

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出版历程
  • 收稿日期:  2016-03-21
  • 刊出日期:  2017-07-28

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