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Bearing loads of dual rotor-bearing system under stationary and transient conditions

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【作者】 刘树辉王国丽朱清乐周年发陈勇

【Author】 LIU Shu-hui,WANG Guo-li,ZHU Qing-le,ZHOU Nian fa,CHEN Yong (1.School of Mechanical Engineering, Beijing Institute of Technology,Beijing 100081, China; 2.Avic Shenyang Liming Aero-Engine (Group) Corporation Ltd, Shenyang 110043, China)

【机构】 School of Mechanical Engineering,Beijing Institute of TechnologyAvic Shenyang Liming Aero-Engine (Group) Corporation Ltd

【摘要】 Aimed at aeroengine vibration failure, bearing loads of dual rotor-bearing system caused by unbalance are calculated under stationary and transient conditions. The three-dimensional (3-D) finite element method (FEM) model of dual rotor-bearing system was established. Applying the rotor dynamics function of Ansys 12.0, bearing loads were calculated under various unbalance force in stationary condition, and the transient vibration characteristics and the effect of acceleration on bearing loads were discussed. On the basis of simulation results, the influence disciplines of unbalance on bearing loads and theoretic reference for reducing bearing loads during start-up were obtained.

【Abstract】 Aimed at aeroengine vibration failure, bearing loads of dual rotor-bearing system caused by unbalance are calculated under stationary and transient conditions. The three-dimensional (3-D) finite element method (FEM) model of dual rotor-bearing system was established. Applying the rotor dynamics function of Ansys 12.0, bearing loads were calculated under various unbalance force in stationary condition, and the transient vibration characteristics and the effect of acceleration on bearing loads were discussed. On the basis of simulation results, the influence disciplines of unbalance on bearing loads and theoretic reference for reducing bearing loads during start-up were obtained.

【基金】 Supported by the National Natural Science Foundation of China (50875022)
  • 【文献出处】 Journal of Beijing Institute of Technology ,北京理工大学学报(英文版) , 编辑部邮箱 ,2012年04期
  • 【分类号】TH774
  • 【下载频次】41
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