A Neural Network Weights Initialization Approach for Diagnosing Real Aircraft Engine Inter-Shaft Bearing Faults

被引:2
|
作者
Berghout, Tarek [1 ]
Bentrcia, Toufik [1 ]
Lim, Wei Hong [2 ]
Benbouzid, Mohamed [3 ,4 ]
机构
[1] Univ Batna 2, Lab Automat & Mfg Engn, Batna 05000, Algeria
[2] UCSI Univ, Fac Engn Technol & Built Environm, Kuala Lumpur 56000, Malaysia
[3] Univ Brest, Inst Rech Dupuy Lome, UMR 6027, CNRS, F-29238 Brest, France
[4] Shanghai Maritime Univ, Logist Engn Coll, Shanghai 201306, Peoples R China
关键词
aircraft engine; deep learning; fault diagnosis; inter-shaft bearing; long-short term memory; vibration; weights initialization;
D O I
10.3390/machines11121089
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
The deep learning diagnosis of aircraft engine-bearing faults enables cost-effective predictive maintenance while playing an important role in increasing the safety, reliability, and efficiency of aircraft operations. Because of highly dynamic and harsh operating conditions of this system, such modeling is challenging due to data complexity and drift, making it difficult to reveal failure patterns. As a result, the objective of this study is dual. To begin, a highly structured data preprocessing strategy ranging from extraction, denoising, outlier removal, scaling, and balancing is provided to solve data complexity that resides specifically in outliers, noise, and data imbalance problems. Gap statistics under k-means clustering are used to evaluate preprocessing results, providing a quantitative estimate of the ideal number of clusters and thereby enhancing data representations. This is the first time, to the best of authors' knowledge, that such a criterion has been employed for an important step in a preliminary ground truth validation in supervised learning. Furthermore, to tackle data drift issues, long-short term memory (LSTM) adaptive learning features are used and subjected to a learning parameter improvement method utilizing recursive weights initialization (RWI) across several rounds. The strength of such methodology can be seen by application to realistic, extremely new, complex, and dynamic data collected from a real test-bench. Cross validation of a single LSTM layer model with only 10 neurons shows its ability to enhance classification performance by 7.7508% over state-of-the-art results, obtaining a classification accuracy of 92.03 +/- 0.0849%, which is an exceptional performance in such a benchmark.
引用
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页数:16
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  • [1] Compound faults feature extraction of inter-shaft bearing based on vibration signal of whole aero-engine
    Yu, Mingyue
    Fang, Minghe
    Chen, Wangying
    Cong, Haonan
    [J]. JOURNAL OF VIBRATION AND CONTROL, 2023, 29 (1-2) : 51 - 64
  • [2] Failure Analysis of an Inter-shaft Bearing of an Aero Gas Turbine Engine
    Mishra R.K.
    Muduli S.K.
    Srinivasan K.
    Ahmed S.I.
    [J]. Journal of Failure Analysis and Prevention, 2015, 15 (2) : 205 - 210
  • [3] Composite failure analysis of an aero-engine inter-shaft bearing inner ring
    Hong, Jie
    Liu, Fangming
    Ma, Yanhong
    Chen, Xueqi
    Wang, Yongfeng
    [J]. ENGINEERING FAILURE ANALYSIS, 2024, 165
  • [4] Fault diagnosis of aero-engine inter-shaft bearing based on Deep-GBM
    Tian, Jing
    Li, Youru
    Ai, Yanting
    [J]. Hangkong Dongli Xuebao/Journal of Aerospace Power, 2019, 34 (04): : 756 - 763
  • [5] Nonlinear response analysis for an aero engine dual-rotor system coupled by the inter-shaft bearing
    Zhenyong Lu
    Xiaodong Wang
    Lei Hou
    Yushu Chen
    Xiyu Liu
    [J]. Archive of Applied Mechanics, 2019, 89 : 1275 - 1288
  • [6] Nonlinear response analysis for an aero engine dual-rotor system coupled by the inter-shaft bearing
    Lu, Zhenyong
    Wang, Xiaodong
    Hou, Lei
    Chen, Yushu
    Liu, Xiyu
    [J]. ARCHIVE OF APPLIED MECHANICS, 2019, 89 (07) : 1275 - 1288
  • [7] Motorbike Engine Faults Diagnosing System Using Neural Network
    Paulraj, M. P.
    Shukry, Mohd
    Majid, Abdul
    Yaacob, Sazali
    Zin, Mohd Zubir Md
    [J]. ICED: 2008 INTERNATIONAL CONFERENCE ON ELECTRONIC DESIGN, VOLS 1 AND 2, 2008, : 49 - 54
  • [8] Research on compound faults identification of aeroengine inter-shaft bearing based on CCF-Complexity-VMD-SVD
    Fang, Minghe
    Yu, Mingyue
    Guo, Guihong
    Feng, Zhigang
    [J]. STRUCTURAL HEALTH MONITORING-AN INTERNATIONAL JOURNAL, 2023, 22 (04): : 2688 - 2707
  • [9] Prediction and analysis of paroxysmal impulse vibration in aero-engine inter-shaft bearings induced by localized faults in the outer ring
    Gao, Tian
    Yuan, Si-Min
    Liu, Yong-Qiang
    Cao, Shu-Qian
    Sun, Jian-Qiao
    [J]. NONLINEAR DYNAMICS, 2024, 112 (15) : 12765 - 12794
  • [10] Failure analysis of an aero-engine inter-shaft bearing due to clearance between the outer ring and its housing
    Yang, Zhefu
    Hong, Jie
    Wang, Dong
    Ma, Yanhong
    Cheng, Ronghui
    [J]. ENGINEERING FAILURE ANALYSIS, 2023, 150