Fault prediction of aircraft engine based on adaptive hybrid sampling and BiLSTM

被引:0
|
作者
Junying Hu [1 ]
Xu Jiang [2 ]
Huan Xu [3 ]
Ke Zhang [1 ]
机构
[1] Hefei University,School of Economics and Management
[2] Alibaba (Beijing) Software Services Co.,ECS Sales Department
[3] Ltd,Department of Public Teaching
[4] Hefei Preschool Education College,undefined
关键词
Fault prediction; Aircraft engine; Bidirectional LSTM; Adaptive hybrid sampling;
D O I
10.1038/s41598-025-98756-9
中图分类号
学科分类号
摘要
To address the class imbalance problem in aero-engine fault prediction, we propose a novel framework integrating adaptive hybrid sampling and bidirectional LSTM (BiLSTM). First, a k-means-based adaptive sampling strategy is proposed that dynamically balances datasets by oversampling minority-class boundaries and undersampling redundant majority clusters. Second, a fault prediction model utilizing BiLSTM is built for fault prediction, which can effectively capture bidirectional temporal dependencies. Experiments on real-world sensor data demonstrate that this approach effectively improves the identification of fault samples in imbalanced datasets.
引用
收藏
相关论文
共 50 条
  • [31] Multiple fault-based FDI and reconfiguration for aircraft engine sensors
    Yazar, Isil
    Caliskan, Fikret
    Kiyak, Emre
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2017, 89 (03): : 397 - 405
  • [32] A computer-based intelligent system for fault diagnosis of an aircraft engine
    Mustapha, F
    Sapuan, SM
    Ismail, N
    Mokhtar, AS
    ENGINEERING COMPUTATIONS, 2004, 21 (01) : 78 - 90
  • [33] Fault Detection of Aircraft Piston Engine Based on Exhaustive Database Search
    Miljkovic, Dubravko
    2020 43RD INTERNATIONAL CONVENTION ON INFORMATION, COMMUNICATION AND ELECTRONIC TECHNOLOGY (MIPRO 2020), 2020, : 1018 - 1023
  • [34] Aircraft engine fault detection based on grouped convolutional denoising autoencoders
    Xuyun FU
    Hui LUO
    Shisheng ZHONG
    Lin LIN
    Chinese Journal of Aeronautics , 2019, (02) : 296 - 307
  • [35] DYNAMIC THRESHOLD METHOD BASED AIRCRAFT ENGINE SENSOR FAULT DIAGNOSIS
    Li, Wenfei
    Yedavalli, Rama K.
    PROCEEDINGS OF THE ASME DYNAMIC SYSTEMS AND CONTROL CONFERENCE 2008, PTS A AND B, 2009, : 479 - 485
  • [36] A new proposal for the prediction of an aircraft engine fuel consumption: a novel CNN-BiLSTM deep neural network model
    Metlek, Sedat
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2023, 95 (05): : 838 - 848
  • [37] Fault Prediction Technology Of Civil Aircraft Based On QAR Data
    Li, Rui
    Fang, Hongzheng
    Xiong, Yi
    Wang, Fei
    Pan, Shunliang
    2017 INTERNATIONAL CONFERENCE ON SENSING, DIAGNOSTICS, PROGNOSTICS, AND CONTROL (SDPC), 2017, : 468 - 472
  • [38] Fault Prediction Technique Based on Hybrid Verification
    Zhao Xu
    Wang Yuhong
    Lu Di
    PROCEEDINGS OF THE 29TH CHINESE CONTROL CONFERENCE, 2010, : 1500 - 1505
  • [39] A hybrid onboard adaptive model for aero-engine parameter prediction
    Pang, Shuwei
    Li, Qiuhong
    Feng, Hailong
    AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 105
  • [40] Neural Networks Adaptive Control of Aircraft Engine Based on Genetic Algorithm
    Zhang, Hongmei
    Dong, Ziyun
    Xu, Guangyan
    26TH CHINESE CONTROL AND DECISION CONFERENCE (2014 CCDC), 2014, : 3518 - 3522