• DocumentCode
    1929670
  • Title

    Vibration analysis via neural network inverse models to determine aircraft engine unbalance condition

  • Author

    Hu, Xiao ; Vian, John ; Slepski, Joseph R. ; Wunsch, Donald C., II

  • Author_Institution
    Appl. Comput. Intelligence Lab., Missouri Univ., Rolla, MO, USA
  • Volume
    4
  • fYear
    2003
  • fDate
    20-24 July 2003
  • Firstpage
    3001
  • Abstract
    This paper describes the use of artificial neural networks (ANNs) with the vibration data from real flight tests for detecting engine health condition - mass imbalance herein. Order-tracking data, calculated from time series is used as the input to the neural networks to determine the amount and location of mass imbalance on aircraft engines. Several neural network methods, including multilayer perceptron (MLP), extended Kalman filter (EKF) and support vector machines (SVMs) are used in the neural network inverse model for the performance comparison. The promising performances are presented at the end.
  • Keywords
    aerospace computing; aerospace engines; condition monitoring; fault diagnosis; mechanical engineering computing; neural nets; vibration measurement; aircraft engine unbalance condition; artificial neural networks; engine health condition; extended Kalman filter; mass imbalance; multilayer perceptron; neural network inverse model; neural network inverse models; order tracking data; real flight tests; support vector machines; time series; vibration analysis; vibration data; Aircraft propulsion; Artificial neural networks; Condition monitoring; Engines; Inverse problems; Multi-layer neural network; Neural networks; Predictive models; Testing; Turbines;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Neural Networks, 2003. Proceedings of the International Joint Conference on
  • ISSN
    1098-7576
  • Print_ISBN
    0-7803-7898-9
  • Type

    conf

  • DOI
    10.1109/IJCNN.2003.1224049
  • Filename
    1224049