Aero-Engine Wear Fault Diagnosis with Supervised Locally Tangent Space Alignment

被引:0
作者
Zhang Y. [1 ]
Lin X. [1 ]
Wang L. [1 ]
Chen Y. [2 ]
Li P. [1 ]
机构
[1] Aeronautical Basic Institute, Naval Aeronautical University, Yantai, 264001, Shandong
[2] 77120 Unit of PLA, Chengdu
来源
Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University | 2020年 / 54卷 / 04期
关键词
Aero-engine; Locally tangent space alignment; Nonlinear feature extraction; Wear fault diagnosis;
D O I
10.7652/xjtuxb202004022
中图分类号
学科分类号
摘要
To solve the problem that the traditional feature extraction technique is hard to deal with the complex fault data containing nonlinear structure, an aero-engine fault diagnosis method based on supervised locally tangent space alignment is proposed by introducing the non-linear dimensionality reduction method named locally tangent space alignment algorithm. The method learns the intrinsic geometric features of fault manifold data, and non-linearly maps them into a low-dimensional fault feature space to achieve fault feature extraction. The wear fault recognition and diagnosis are carried out in the fault feature space by constructing classifier. The oil spectra data of engine wear fault are used for experiment. Compared with the conventional feature extraction approaches such as PCA and LDA, the proposed approach can effectively extract the nonlinear features embedded in the fault data to improve the fault classification accuracy and provide good fault diagnosis performance with a simple linear classifier. © 2020, Editorial Office of Journal of Xi'an Jiaotong University. All right reserved.
引用
收藏
页码:179 / 185
页数:6
相关论文
共 22 条
  • [1] Zheng B., Gao F., Research on the prediction of aeroengine wear based on the IPSO-SVR, Lubrication Engineering, 39, 11, pp. 81-87, (2014)
  • [2] Ge K., Chen G., Knowledge acquisition of aero-engine wear fault diagnosis expert system based on Weka platform, Mechanical Science and Technology for Aerospace Engineering, 30, 11, pp. 1955-1959, (2011)
  • [3] Chen G., Song L., Chen L., Knowledge acquisition for aero-engine wear fault diagnosis based on rule extraction from neural networks, Journal of Aerospace Power, 23, 12, pp. 2170-2176, (2008)
  • [4] Sun W.X., Chen J., Li J.Q., Decision tree and PCA-based fault diagnosis of rotating machinery, Mechanical Systems and Signal Processing, 21, 3, pp. 1300-1317, (2007)
  • [5] Yang F., Hu J., Chen W., Et al., Application of principal component analysis to fault detection and diagnosis of aeroengines, Mechanical Science and Technology for Aerospace Engineering, 27, 3, pp. 330-333, (2008)
  • [6] Chiang L.H., Kotanchek M.E., Fault diagnosis based on fisher discriminant analysis and support vector machines, Computers and Chemical Engineering, 28, 8, pp. 1389-1401, (2004)
  • [7] Seung H.S., Lee D.D., The manifold ways of perception, Science, 290, pp. 2268-2269, (2000)
  • [8] Scholkopf B., Smola A., Muller K.R., Nonlinear component analysis as a kernel eigenvalue problem, Neural Computation, 10, 5, pp. 1299-1319, (1998)
  • [9] Shi K., Liu S., Zhang H., Et al., Kernel local linear discriminate method for dimensionality reduction and its application in machinery fault diagnosis, Shock and Vibration, 2014, (2014)
  • [10] Mika S., Ratsch G., Weston J., Et al., Constructing descriptive and discriminative nonlinear features: Rayleigh coefficients in kernel feature spaces, IEEE Transactions on Pattern Analysis and Machine Intelligence, 25, 5, pp. 623-628, (2003)