Gas Path Fault Diagnosis for Aero-engine Based on Improved Denoising Autoencoder

被引:0
|
作者
Hong J. [1 ]
Wang H. [1 ]
Che C. [1 ]
Ni X. [1 ]
机构
[1] College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing
关键词
Aero engine; Denoising autoencoder; Fault diagnosis; Firefly algorithm; Radial basis function network;
D O I
10.16450/j.cnki.issn.1004-6801.2019.03.022
中图分类号
学科分类号
摘要
Considering the state parameters significant nonlinearity and the vulnerability to noise pollution in the aero-engine gas path faults,a method based on denoising autoencoder (DAE) and integrated with a neural networks of firefly algorithm (FA) and radial basis function (RBF) is proposed to diagnose the gas path faults and improve the diagnostic accuracy. The DAE is adopted through greedy algorithms to identify deeper robust features that helps diagnose the faults. To further improve the diagnostic accuracy of the algorithm, inertia weight and improved FA of self-adaptive light intensity factor are introduced to obtain the firefly radial basis function (FRBF) network after optimizing the RBF network. Then the robust features extracted from the DAE are imported into the FRBF for faults diagnosis. Based on practices, the extracting method is compared with the algorithms which are original DAE, independent FRBF, SVM and RBF. According to the results, the proposed method presents highest diagnostic accuracy of 98.1%, stable performance in the algorithms and more satisfying robustness. © 2019, Editorial Department of JVMD. All right reserved.
引用
收藏
页码:603 / 610
页数:7
相关论文
共 21 条
  • [1] Zhang P., Huang J., Aeroengine fault diagnosis using dual Kalman filtering technique, Journal of Aerospace Power, 23, 5, pp. 952-956, (2008)
  • [2] Lu F., Ju H., Huang J., An im-proved extended Kalman filter with inequality constraintsor gas turbine engine health monitoring, Aerospace Science & Technology, 58, pp. 36-47, (2016)
  • [3] Chen G., Zuo H., Expert systems of engine wear fault diagnosis based on knowledge rule, Journal of Aerospace Power, 19, 1, pp. 23-29, (2004)
  • [4] Zhao W., Jia M., Huang P., Et al., Nonlinear parameters identification of multi-degree-of-freedom systems using sensitivity analysis, Journal of Vib-Ration, Measurement & Diagnosis, 26, 4, pp. 288-290, (2006)
  • [5] Cui J., Yan X., Pu X., Et al., Aero-engine fault diagnosis based on d-ynamic PCA and improved SVM, Journal of Vibration, Measurement & Diagnosis, 35, 1, pp. 94-99, (2015)
  • [6] Lu F., Zhu T., Lv Y., Data dr-iven based gas path fault diagnosis forturbo-shaft engine, Applied Mechanics & Materials, 249-250, pp. 400-404, (2012)
  • [7] Benyounes A., Hafaifa A., Kouzou A., Et al., Gas turbine modeling using adaptive fuzzy neural network approach based on measured data classification, Mathematics-in-Industry Case Studies, 7, 1, pp. 1-4, (2017)
  • [8] Nozari H.A., Banadaki H.D., Shoorehdeli M.A., Et al., Model-based fault detection and isolation using neural networks: an industrial gas turbine case study, International Conference on Systems Engineering, pp. 26-31, (2011)
  • [9] Zhao N., Li S., Yi S., Et al., Fault diagnosis based on rough set and bP neural network (RS-BP) for gas turbine engine, Advanced Materials Research, 732-733, pp. 397-401, (2013)
  • [10] Cao C., Yang S., Zhou X., Et al., Fault diagnosis of rotating machinery based on an improved support vector machines model, Journal of Vibration, Measurement & Diagnosis, 29, 3, pp. 270-273, (2009)