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离心压气机不稳定流动的时频特征分析

吴蔚 赵博 薛翔

吴蔚, 赵博, 薛翔. 离心压气机不稳定流动的时频特征分析[J]. 航空动力学报, 2020, 35(8): 1768-1776. doi: 10.13224/j.cnki.jasp.2020.08.022
引用本文: 吴蔚, 赵博, 薛翔. 离心压气机不稳定流动的时频特征分析[J]. 航空动力学报, 2020, 35(8): 1768-1776. doi: 10.13224/j.cnki.jasp.2020.08.022
WU Wei, ZHAO Bo, XUE Xiang. Time-frequency analysis of unsteady flow in centrifugal compressor[J]. Journal of Aerospace Power, 2020, 35(8): 1768-1776. doi: 10.13224/j.cnki.jasp.2020.08.022
Citation: WU Wei, ZHAO Bo, XUE Xiang. Time-frequency analysis of unsteady flow in centrifugal compressor[J]. Journal of Aerospace Power, 2020, 35(8): 1768-1776. doi: 10.13224/j.cnki.jasp.2020.08.022

离心压气机不稳定流动的时频特征分析

doi: 10.13224/j.cnki.jasp.2020.08.022

Time-frequency analysis of unsteady flow in centrifugal compressor

  • 摘要: 离心压气机失稳过程是一个非常复杂的动态过程,提高离心压气机运行的可靠性需要准确获取失稳过程的时频特征。针对带无叶扩压器的高速离心压气机失稳过程中叶轮出口的动态压力数据,采用时空本征模态分解(STIMD)算法和经验模态分解(EMD)算法进行分解,得到了多个本征模态函数(IMF),并结合Hilbert变换对不稳定流动的动态特征进行分析。结果表明,STIMD算法得到了深喘和浅喘的时频信息,观察到了频率在150 Hz附近持续波动的失速现象,并捕捉到了浅喘先兆的频率曲线由抖动向恒定的过渡过程。STIMD算法改善了EMD的模态混叠问题,为压气机失稳分析提供了一种工具。

     

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出版历程
  • 收稿日期:  2019-12-23
  • 刊出日期:  2020-08-28

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