This paper presents a novel methodology for fault detection in gas turbine engines based on the concept of dynamic neural networks. The neural network structure belongs to the class of locally recurrent globally feed-forward networks. The architecture of the network is similar to the feed-forward multi-layer perceptron with the difference that the processing units include dynamic characteristics. The dynamics present in these networks make them a powerful tool useful for identification of nonlinear systems. The dynamic neural network architecture that is described in this paper is used for fault detection in a dual-spool turbo fan engine. A number of simulation studies are conducted to demonstrate and verify the advantages of our proposed neural network diagnosis methodology.
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ASME Turbo Expo 2010: Power for Land, Sea, and Air
June 14–18, 2010
Glasgow, UK
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4398-7
PROCEEDINGS PAPER
Fault Diagnosis of Gas Turbine Engines by Using Dynamic Neural Networks
Rasul Mohammadi,
Rasul Mohammadi
Concordia University, Montreal, QC, Canada
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Esmaeil Naderi,
Esmaeil Naderi
Concordia University, Montreal, QC, Canada
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Khashayar Khorasani,
Khashayar Khorasani
Concordia University, Montreal, QC, Canada
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Shahin Hashtrudi-Zad
Shahin Hashtrudi-Zad
Concordia University, Montreal, QC, Canada
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Rasul Mohammadi
Concordia University, Montreal, QC, Canada
Esmaeil Naderi
Concordia University, Montreal, QC, Canada
Khashayar Khorasani
Concordia University, Montreal, QC, Canada
Shahin Hashtrudi-Zad
Concordia University, Montreal, QC, Canada
Paper No:
GT2010-23586, pp. 365-376; 12 pages
Published Online:
December 22, 2010
Citation
Mohammadi, R, Naderi, E, Khorasani, K, & Hashtrudi-Zad, S. "Fault Diagnosis of Gas Turbine Engines by Using Dynamic Neural Networks." Proceedings of the ASME Turbo Expo 2010: Power for Land, Sea, and Air. Volume 3: Controls, Diagnostics and Instrumentation; Cycle Innovations; Marine. Glasgow, UK. June 14–18, 2010. pp. 365-376. ASME. https://doi.org/10.1115/GT2010-23586
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