Fault Feature Enhancement Method for Main Bearing of Aircraft Engine Based on Optimized Wavelet Packet Decomposition
Received:August 08, 2024  Revised:September 04, 2024
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DOI:10.7643/issn.1672-9242.2024.09.006
KeyWord:main bearing  optimized wavelet packet decomposition  maximum correlation kurtosis deconvolutio  calculation order analysis  fault feature enhancement  fault analysis
              
AuthorInstitution
ZHANG Zhenpeng Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System, Shenyang Aerospace University, Shenyang , China
LUAN Xiaochi Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System, Shenyang Aerospace University, Shenyang , China
SHA Yundong Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System, Shenyang Aerospace University, Shenyang , China
YANG Jie AECC Shenyang Engine Research Institute, Shenyang , China
ZHAO Fengtong Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System, Shenyang Aerospace University, Shenyang , China
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Abstract:
      In order to solve the problem that weak fault features of main bearing of aero-engine are difficult to be identified in high background noise environment and variable speed condition, the work aims to propose an enhancement method of fault features of main bearing of aircraft engine based on optimized wavelet packet decomposition. Firstly, the vibration time domain signal was transformed into vibration angle domain signal by calculation order analysis method. Then, the vibration angle domain signal was decomposed by wavelet packet, and the effective fault feature energy ratio and optimized maximum correlation kurtosis deconvolution method were introduced to enhance the signal fault features, and the fault features were gradually extracted through cyclic iteration. Finally, the signal envelope analysis was carried out and the bearing fault diagnosis was realized by comparing with the theoretical bearing fault order. By analyzing the test data of the main bearing outer ring of the aircraft engine under test conditions, it was verified that the proposed method could effectively enhance the fault feature information in the vibration signal. The results show that compared with the traditional WPD method, the proposed method can effectively enhance the fault feature order of main bearing, and realize fault diagnosis under high background noise environment and variable speed.
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