Vibration prediction of aeroengines based on enhanced SENet model

被引:0
|
作者
Xia C. [1 ]
Zhan Y. [1 ]
机构
[1] College of Aviation Engineering, Civil Aviation Flight University of China, Sichuan, Guanghan
来源
关键词
attention mechanism; convolutional neural network; data-driven; multi-parameter fusion; vibration prediction;
D O I
10.13224/j.cnki.jasp.20220110
中图分类号
学科分类号
摘要
In order to monitor the vibration status of aeroengines and acquire warning signals in real-time, an enhanced SENet (squeeze-and-excitation network) model was proposed based on gas path and vibration parameters. Compared with the previous research which used datasets generated from specific lab situations and simulation data, actual QAR (quick access recorder) data were adopted for random sampling of the datasets. This technique could characterize the real operation status and the interaction of parameters better in vibration systems. The results showed that it is possible to forecast the vibration of aeroengines, and the SENet model could effectively and timely track sudden changes and the fluctuation of vibration. In addition, the applicability of this method into other vibration parameters and different types of aeroengines was tested. Furthermore, compared with other classical learning algorithms, the SENet model may obtain a smaller error in vibration forecasting. At the same time, the experiments showed that compared with previous research only focusing on the vibration, using the fusion of multi parameters could improve the accuracy of the forecast. © 2022 BUAA Press. All rights reserved.
引用
收藏
页码:2807 / 2817
页数:10
相关论文
共 28 条
  • [1] LI Shuming, LI Shidong, ZHANG Ying, Quantitative analysis of aircraft engine compressor performance deterioration impact factor, Science Technology and Engineering, 15, 32, pp. 74-78, (2015)
  • [2] WANG H., A survey of maintenance policies of deteriorating systems, European Journal of Operational Research, 139, 3, pp. 469-489, (2002)
  • [3] CHO D I, PARLAR M., A survey of maintenance models for multi-unit systems, European Journal of Operational Research, 51, 1, pp. 1-23, (1991)
  • [4] WANG R,, LIU M,, MA Y., Fault estimation for aero-engine LPV systems based on LFT, Asian Journal of Control, 23, 1, pp. 351-361, (2021)
  • [5] XIE Xiaolong, Research on aero engine performance evaluation and recession prediction method, (2016)
  • [6] CAO Huiling, LUO Lixiao, Et al., Aero engine surge fault diagnosis based on LS-SVM, Thermal Power Engineering, 28, 1, pp. 23-27, (2013)
  • [7] FU Xuyun, SHAN Zhenyong, LI Zhen, Et al., Time varying fuzzy neural network and its application in aeroengine exhaust temperature prediction, Computer Integrated Manufacturing System, 20, 4, pp. 919-925, (2014)
  • [8] LI Shuming, REN Pei, HUANG Yanxiao, Fitting of aero engine baseline equation, Mechanical Engineering and Automation, 1, 1, pp. 153-154, (2016)
  • [9] LEI Yaguo, JIA Feng, KONG Detong, Et al., Opportunities and challenges of mechanical intelligent fault diagnosis under big data, Journal of Mechanical Engineering, 54, 5, pp. 94-104, (2018)
  • [10] KOHONEN T., An introduction to neural computing, Neural Networks, 1, 1, pp. 3-16, (1988)