TY - GEN
T1 - An EGTM-Based RUL Prediction Method for Auxiliary Power Unit of Aircraft
AU - Han, Xuehao
AU - Su, Zhou
AU - Qi, Boxun
AU - Wang, Benkuan
AU - Liu, Datong
AU - Peng, Yu
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - The performance and health condition of the auxiliary power unit (APU) directly affect the safe operation and economical maintenance of the aircraft. However, due to the limitations of APU report recording mode, the small amount of APU reports makes it difficult for many traditional machine learning methods to evaluate their performance accurately. To address the above problems, this paper proposes a method for predicting the remaining useful life of APU based on the exhaust gas temperature (EGT) margin. First, data preprocessing is performed, and EGT, a key parameter of APU, is extracted from its trend by the X11 method, which is affected by the external environment factors. Then, the remaining useful life of the APU can be obtained by combining the EGT margin with the EGT decay rate. The real APU report is finally applied to verify the efficiency and superiority of the proposed method. Experimental results show that the performance of this proposed method outperforms comparison methods in terms of predicting the remaining useful life of aircraft APU.
AB - The performance and health condition of the auxiliary power unit (APU) directly affect the safe operation and economical maintenance of the aircraft. However, due to the limitations of APU report recording mode, the small amount of APU reports makes it difficult for many traditional machine learning methods to evaluate their performance accurately. To address the above problems, this paper proposes a method for predicting the remaining useful life of APU based on the exhaust gas temperature (EGT) margin. First, data preprocessing is performed, and EGT, a key parameter of APU, is extracted from its trend by the X11 method, which is affected by the external environment factors. Then, the remaining useful life of the APU can be obtained by combining the EGT margin with the EGT decay rate. The real APU report is finally applied to verify the efficiency and superiority of the proposed method. Experimental results show that the performance of this proposed method outperforms comparison methods in terms of predicting the remaining useful life of aircraft APU.
KW - Auxiliary Power Unit
KW - Exhaust Gas Temperature Margin
KW - Remaining Useful Life
UR - https://www.scopus.com/pages/publications/105001672648
U2 - 10.1109/ICSMD64214.2024.10920578
DO - 10.1109/ICSMD64214.2024.10920578
M3 - 会议稿件
AN - SCOPUS:105001672648
T3 - ICSMD 2024 - 5th International Conference on Sensing, Measurement and Data Analytics in the Era of Artificial Intelligence
BT - ICSMD 2024 - 5th International Conference on Sensing, Measurement and Data Analytics in the Era of Artificial Intelligence
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 5th International Conference on Sensing, Measurement and Data Analytics in the Era of Artificial Intelligence, ICSMD 2024
Y2 - 31 October 2024 through 3 November 2024
ER -