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密封-转子系统气流激振问题数值仿真

罗跃纲 王鹏飞 徐昊 王晨勇 贾海峰

罗跃纲, 王鹏飞, 徐昊, 王晨勇, 贾海峰. 密封-转子系统气流激振问题数值仿真[J]. 航空动力学报, 2019, 34(9): 1857-1865. doi: 10.13224/j.cnki.jasp.2019.09.001
引用本文: 罗跃纲, 王鹏飞, 徐昊, 王晨勇, 贾海峰. 密封-转子系统气流激振问题数值仿真[J]. 航空动力学报, 2019, 34(9): 1857-1865. doi: 10.13224/j.cnki.jasp.2019.09.001
Numerical simulation on seal-rotor system with airflow induced vibration[J]. Journal of Aerospace Power, 2019, 34(9): 1857-1865. doi: 10.13224/j.cnki.jasp.2019.09.001
Citation: Numerical simulation on seal-rotor system with airflow induced vibration[J]. Journal of Aerospace Power, 2019, 34(9): 1857-1865. doi: 10.13224/j.cnki.jasp.2019.09.001

密封-转子系统气流激振问题数值仿真

doi: 10.13224/j.cnki.jasp.2019.09.001
基金项目: 国家自然科学基金(51875085); 辽宁省自然科学基金(20170540205)

Numerical simulation on seal-rotor system with airflow induced vibration

  • 摘要: 对于密封中发生气流激振的故障诊断问题,基于有限元方法,应用Muzynska非线性密封力模型建立了密封-转子系统动力学模型,通过数值积分方法研究了升/降速过程的气流激振失稳规律和振动特性,并分析了在变速和稳速情况下偏心量的影响。结果表明:气流激振力会使系统固有频率升高,使发生共振时的振幅降低;发生气流激振会出现锁频现象并伴有组合频率特征;降速时由于气体的流动性强从而导致切向惯性力很弱,惯性效应不明显;当偏心量较小时频谱上只出现了锁频,随着偏心增大组合频率出现并不断丰富;稳速时气流激振频率随偏心的提高而增大,并出现了频率突变。

     

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

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