航空发动机气路静电信号联合降噪方法
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作者单位:

1.南京航空航天大学民航学院,南京211106;2.安徽工业大学机械工程学院,马鞍山243032;3.南京电子工程研究所,南京210023

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通讯作者:

左洪福, 男, 教授, 博士生导师, E-mail: rms@nuaa.edu.cn。

中图分类号:

V216

基金项目:

国家自然科学基金项目(U2133202); 江苏省研究生科研与实践创新计划项目(KYCX22_0375); 南京航空航天大学博士短期访学项目(ZDGB2022006)。


A Combined Denoising Method for Electrostatic Signals in the Aero-engine Gas Path
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1.College of Civil Aviation, Nanjing University of Aeronautics & Astronautics, Nanjing 211106, China;2.School of Mechanical Engineering, Anhui University of Technology, Maanshan243032, China;3.Nanjing Research Institute of Electronic Engineering, Nanjing 210023, China

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    摘要:

    针对强背景噪声下航空发动机气路静电信号降噪问题,提出一种基于本征模态函数(Intrinsic modal function, IMF)自适应滤波联合小波阈值的静电信号降噪方法。首先,通过互补集合经验模态分解(Complementary ensemble empirical mode decomposition, CEEMD)方法对原始静电信号进行分解,得到若干平稳IMF;然后,构建最优重构自适应低通滤波算法筛选以有用信号为主的IMF分量;再对以噪声为主的IMF分量通过小波阈值算法进行降噪处理;最后,将上述信号重构,得到降噪后的静电信号。进行了仿真和实测信号验证并与传统方法对比,结果表明,该方法对发动机气路静电信号降噪效果良好,在微弱故障信号提取方面更具优越性。

    Abstract:

    Aiming at the problem of noise reduction of electrostatic signals in the aero-engine gas-path under strong background noise, a noise reduction method based on intrinsic modal function (IMF) adaptive filtering combined with wavelet thresholding is proposed. Firstly, the original electrostatic signal is decomposed by the complementary ensemble empirical mode decomposition (CEEMD) method to obtain several smooth IMFs. Secondly, the optimal reconstruction adaptive low-pass filtering algorithm is constructed to filter the signal-dominated IMFs. Thirdly, the noise-dominated IMF components are noise-reduced and reconstructed with the signal-dominated IMFs by the wavelet thresholding method, then the noise-reduced electrostatic signal is obtained. The simulated and measured signals are used to verify the proposed method and compare it with other noise reduction methods, and the results show that the method is effective in noise reduction of engine gas-path electrostatic signals and is superior in extracting weak fault signals.

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引用本文

刘岩,刘珍珍,白芳,郭泽中,左洪福.航空发动机气路静电信号联合降噪方法[J].南京航空航天大学学报,2024,56(6):1036-1047

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  • 收稿日期:2024-03-31
  • 最后修改日期:2024-09-27
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  • 在线发布日期: 2024-12-18
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