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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
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.
作者姓名:张效溥  田杰  孙宗翰
作者单位:上海交通大学机械与动力工程学院,上海200240,上海交通大学机械与动力工程学院,上海200240;上海交通大学燃气轮机与民用航空发动机教育部工程研究中心,上海200240,上海交通大学机械与动力工程学院,上海200240,上海交通大学机械与动力工程学院,上海200240;上海交通大学燃气轮机与民用航空发动机教育部工程研究中心,上海200240
基金项目:中央高校基本科研业务费专项资金
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。

关 键 词:叶片振动  叶尖定时  压缩感知  信号重构  有限元仿真
收稿时间:2019/6/21 0:00:00

Compressive sensing identification method of blade tip timing signals based on arbitrary sensor arrangement
ZHANG Xiaopu,TIAN Jie and 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.
Authors:ZHANG Xiaopu  TIAN Jie and SUN Zonghan
Institution:School of Mechanical Engineering,Shanghai Jiao Tong University,Shanghai 200240,China,School of Mechanical Engineering,Shanghai Jiao Tong University,Shanghai 200240,China;Engineering Research Center of Gas Turbine and Civil Aero Engine,Ministry of Education,Shanghai Jiao Tong University,Shanghai 200240,China and School of Mechanical Engineering,Shanghai Jiao Tong University,Shanghai 200240,China
Abstract:Based on the characteristics of blade vibration and tip timing system, the regulation of blade vibration response under arbitrary sensor angle distribution was studied. Based on the sparsity in frequency domain of tip timing signal, the application of compressive sensing method in reconstruction of blade tip timing signal and mode identification was explored. Through a large number of numerical experiments of synchronous and non-synchronous signals, the influences of signal reconstruction errors, number of sensors, number of sampling cycles, frequency resolution and signal to noise ratio on the identification effect were analyzed, and the basic methods and steps of the compressive sensing method to reconstruct the timing signal of blade tip were determined. Finally, the method was applied to the reconstruction of vibration response data of a titanium alloy wide chord fan blade from the finite element simulation. The results show that the excitations with large amplitudes can be accurately identified under three rotating speed conditions of 80%, 90% and 100% with blade tip position error and 30 dB noise signals. The compressive sensing method based on arbitrary sensor angle distribution is effective in identifying the timing signal of blade tip and has value of engineering application and promotion.
Keywords:blade vibration  blade tip timing  compressive sensing  signal reconstruction  finite element simulation
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