Aero Engine Life Prediction Based on KF-TCN Method

Chun-zhi LIU

Science Technology and Engineering ›› 2025, Vol. 25 ›› Issue (27) : 11607 -11613.

PDF
Science Technology and Engineering ›› 2025, Vol. 25 ›› Issue (27) : 11607-11613 DOI: 10.12404/j.issn.1671-1815.2409135
research-article
Aero Engine Life Prediction Based on KF-TCN Method
Author information +
History +
PDF

Abstract

In order to solve the problem of low prediction accuracy of RUL by traditional forecasting methods, a new forecasting method of turbofan engine life based on Kalman filter and time convolutional neural network (KF-TCN) was proposed. Firstly, in order to reduce the noise interference of the sensor when collecting data, Kalman filter algorithm was used to filter the extracted features. Secondly, the KF-TCN model was constructed, and the filtered data was input into the time convolutional network to capture the time dependence of the time series data and output the RUL predicted value. Finally, taking FD001 subset as an example, commercial modular aero-propulsion system simulation (C-MAPSS) aero-engine data set was used to verify the model. The results show that compared with the RUL prediction results of TCN, gated recurrent unit (GRU) and long short-term memory (LSTM) models, the prediction error of KF-TCN model constructed is smaller in the process of engine RUL prediction, which provides a way for engine life prediction.

Keywords

aeroengine / remaining service life prediction / Kalman filtering / time convolutional neural networks

Cite this article

Download citation ▾
Chun-zhi LIU. Aero Engine Life Prediction Based on KF-TCN Method. Science Technology and Engineering, 2025, 25(27): 11607-11613 DOI:10.12404/j.issn.1671-1815.2409135

登录浏览全文

4963

注册一个新账户 忘记密码

References

Funding

PDF (6751KB)

20

Accesses

0

Citation

Detail

Sections
Recommended

/

〈 〉