• DocumentCode
    3471968
  • Title

    Fault diagnosis of gas turbine engines by using dynamic neural networks

  • Author

    Mohammadi, Reza ; Naderi, Elahe ; Khorasani, K. ; Hashtrudi-Zad, S.

  • Author_Institution
    Dept. of Electr. & Comput. Eng., Concordia Univ., Montreal, QC, Canada
  • fYear
    2011
  • fDate
    14-17 Sept. 2011
  • Firstpage
    25
  • Lastpage
    30
  • Abstract
    The goal of this paper is to present an innovative methodology for performing fault detection in gas turbine engines by utilizing dynamic neural networks. The proposed neural network architecture selected belongs to the class of locally recurrent globally feed-forward networks. The envisaged network is structurally similar to a feed-forward multi-layer perceptron with the difference that the employed processing units are not static and possess dynamic characteristics. The developed and constructed dynamic neural network architecture is then used to perform fault detection of anomalies in a dual-spool turbo fan engine. A number of simulation studies are conducted to demonstrate and verify the advantages and capabilities of our proposed neural network diagnosis methodology.
  • Keywords
    aerospace engineering; fault diagnosis; gas turbines; jet engines; multilayer perceptrons; neural nets; dual-spool turbofan engine; dynamic neural networks; fault diagnosis; feedforward multilayer perceptron; gas turbine engines; innovative methodology; locally recurrent globally feedforward networks; neural network diagnosis methodology; Biological neural networks; Fault detection; Fuels; Jet engines; Mathematical model; Neurons;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Quality and Reliability (ICQR), 2011 IEEE International Conference on
  • Conference_Location
    Bangkok
  • Print_ISBN
    978-1-4577-0626-4
  • Type

    conf

  • DOI
    10.1109/ICQR.2011.6031675
  • Filename
    6031675