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基于任意传感器排布的叶尖定时信号压缩感知辨识方法

张效溥 田杰 孙宗翰

张效溥, 田杰, 孙宗翰. 基于任意传感器排布的叶尖定时信号压缩感知辨识方法[J]. 航空动力学报, 2020, 35(1): 41-51. doi: 10.13224/j.cnki.jasp.2020.01.005
引用本文: 张效溥, 田杰, 孙宗翰. 基于任意传感器排布的叶尖定时信号压缩感知辨识方法[J]. 航空动力学报, 2020, 35(1): 41-51. doi: 10.13224/j.cnki.jasp.2020.01.005
ZHANG Xiaopu, TIAN Jie, SUN Zonghan. Compressive sensing identification method of blade tip timing signals based on arbitrary sensor arrangement[J]. Journal of Aerospace Power, 2020, 35(1): 41-51. doi: 10.13224/j.cnki.jasp.2020.01.005
Citation: ZHANG Xiaopu, TIAN Jie, SUN Zonghan. Compressive sensing identification method of blade tip timing signals based on arbitrary sensor arrangement[J]. Journal of Aerospace Power, 2020, 35(1): 41-51. doi: 10.13224/j.cnki.jasp.2020.01.005

基于任意传感器排布的叶尖定时信号压缩感知辨识方法

doi: 10.13224/j.cnki.jasp.2020.01.005
基金项目: 中央高校基本科研业务费专项资金

Compressive sensing identification method of blade tip timing signals based on arbitrary sensor arrangement

  • 摘要: 基于叶片振动和叶尖计时系统的特点,推导了任意传感器角度分布下叶片振动响应的分布规律,并基于叶尖定时信号频域的稀疏性,探究了压缩感知方法在叶尖定时信号的重构和倍频辨识上的应用。通过同步信号和非同步信号的大量数值实验,分析了包括信号重构误差、传感器数量、旋转周期数、频率分辨率和信噪比等因素对辨识效果的影响,提出了压缩感知重构叶尖定时信号的基本方法和步骤。进一步将压缩感知方法应用于某型号涡扇发动机钛合金宽弦风扇叶片有限元仿真获得的振动响应数据重构,验证了该方法的有效性。结果表明:在加入了叶尖测点位置误差和30 dB随机噪声的前提下,在80%、90%和100%三种转速工况下均清晰辨识出幅值较大的激励倍频。基于任意传感器角度分布的压缩感知方法对叶尖定时信号辨识效果较好。

     

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出版历程
  • 收稿日期:  2019-06-21
  • 刊出日期:  2020-01-28

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