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基于整机的中介轴承外圈剥落故障振动分析

陈果 贺志远 尉询楷

陈果, 贺志远, 尉询楷. 基于整机的中介轴承外圈剥落故障振动分析[J]. 航空动力学报, 2020, 35(3): 658-672. doi: 10.13224/j.cnki.jasp.2020.03.022
引用本文: 陈果, 贺志远, 尉询楷. 基于整机的中介轴承外圈剥落故障振动分析[J]. 航空动力学报, 2020, 35(3): 658-672. doi: 10.13224/j.cnki.jasp.2020.03.022
CHEN Guo, HE Zhiyuan, WEI Xunkai. Vibration analysis of peeling fault of intermediate bearing outer ring based on whole aero-engine[J]. Journal of Aerospace Power, 2020, 35(3): 658-672. doi: 10.13224/j.cnki.jasp.2020.03.022
Citation: CHEN Guo, HE Zhiyuan, WEI Xunkai. Vibration analysis of peeling fault of intermediate bearing outer ring based on whole aero-engine[J]. Journal of Aerospace Power, 2020, 35(3): 658-672. doi: 10.13224/j.cnki.jasp.2020.03.022

基于整机的中介轴承外圈剥落故障振动分析

doi: 10.13224/j.cnki.jasp.2020.03.022
基金项目: 国家自然科学基金 (51675263); 国家科技重大专项(2017-Ⅳ-0008-0045)

Vibration analysis of peeling fault of intermediate bearing outer ring based on whole aero-engine

  • 摘要: 针对某典型双转子航空发动机中介轴承外圈疲劳剥落故障诊断问题,基于整机振动耦合动力学模型,导入中介轴承外圈早期剥落故障模型,通过数值积分方法获取故障激励下的整机振动响应。提取并分析了中介轴承外圈剥落故障特征,从信号分析中发现:①出现了4倍外圈故障特征频率及其两侧以外圈旋转频率为间隔的调制边频带;②随着不平衡量增加,特征频率分量基本不变,边频带变得更加突出;③随着轴承游隙的增加,外圈故障引起的冲击更为强烈,特征频率及其调制边频均显著增加。通过比较从轴承座到机匣各测点信号的故障特征,结果表明中介轴承早期疲劳剥落产生的冲击通过轴承座传递到机匣将产生很大程度的衰减,在机匣测点信号中轴承故障特征基本消失。

     

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出版历程
  • 收稿日期:  2019-09-10
  • 刊出日期:  2020-03-28

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