TY - GEN
T1 - Identification of Aviation Engine Performance Degradation Paths and Remaining Useful Life Prediction under Multiple Fault Modes Based on DTW-K-Medoids and Informer
AU - Xie, Dongjiang
AU - Li, Mengwei
AU - Jiang, Jinfu
AU - Luo, Tonglin
AU - Ma, Jian
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - The aero-engine, as the core system of an aircraft, has its performance degradation directly affecting flight safety. Accurate life prediction is crucial for its safe and stable operation. Different performance degradation modes of the engine and the trajectory differences under their impacts are one of the challenges faced in achieving universal modeling for life prediction and improving high-impact prediction accuracy. To address the above challenges, a method for adaptive timescale clustering of engine performance degradation trajectories under multiple fault modes and self-matching model life prediction is proposed. First, leveraging the advantage of Dynamic Time Warping (DTW) in measuring the similarity of curves with variable time scales, it is integrated with the K-Medoids method suitable for time-series clustering to achieve clustering of similar trajectories and performance degradation modes unaffected by trajectory length. Then, a life prediction model based on Informer is designed, utilizing its multi-head self-attention mechanism to autonomously mine sensor parameters sensitive to performance degradation and beneficial to life prediction, and to address the accuracy improvement challenge faced by medium and long-term life prediction. Verified by the C-MAPSS dataset, the proposed method has improved prediction accuracy by 25.04% compared with prediction methods without performance degradation path identification, and it has significant accuracy advantages over traditional deep learning prediction models such as LSTM and GRU.
AB - The aero-engine, as the core system of an aircraft, has its performance degradation directly affecting flight safety. Accurate life prediction is crucial for its safe and stable operation. Different performance degradation modes of the engine and the trajectory differences under their impacts are one of the challenges faced in achieving universal modeling for life prediction and improving high-impact prediction accuracy. To address the above challenges, a method for adaptive timescale clustering of engine performance degradation trajectories under multiple fault modes and self-matching model life prediction is proposed. First, leveraging the advantage of Dynamic Time Warping (DTW) in measuring the similarity of curves with variable time scales, it is integrated with the K-Medoids method suitable for time-series clustering to achieve clustering of similar trajectories and performance degradation modes unaffected by trajectory length. Then, a life prediction model based on Informer is designed, utilizing its multi-head self-attention mechanism to autonomously mine sensor parameters sensitive to performance degradation and beneficial to life prediction, and to address the accuracy improvement challenge faced by medium and long-term life prediction. Verified by the C-MAPSS dataset, the proposed method has improved prediction accuracy by 25.04% compared with prediction methods without performance degradation path identification, and it has significant accuracy advantages over traditional deep learning prediction models such as LSTM and GRU.
KW - Aero-engine
KW - Multiple Fault Modes
KW - Performance Degradation Path Identification
KW - RUL
UR - https://www.scopus.com/pages/publications/105032688259
U2 - 10.1109/INDIN64977.2025.11279587
DO - 10.1109/INDIN64977.2025.11279587
M3 - 会议稿件
AN - SCOPUS:105032688259
T3 - IEEE International Conference on Industrial Informatics (INDIN)
BT - 2025 IEEE 23rd International Conference on Industrial Informatics, INDIN 2025
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 23rd International Conference on Industrial Informatics, INDIN 2025
Y2 - 12 July 2025 through 15 July 2025
ER -