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
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