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Intelligent performance diagnostics of a gas turbine engine using user‐friendly interface neural networks

Chang‐duk Kong (Department of Aerospace Engineering, Chosun University, Gwangju, Republic of Korea)
Ja‐young Ki (Department of Aerospace Engineering, Chosun University, Gwangju, Republic of Korea)
Myoung‐cheol Kang (Department of Aerospace Engineering, Chosun University, Gwangju, Republic of Korea)
Seong‐hee Kho (Department of Aerospace Engineering, Chosun University, Gwangju, Republic of Korea)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 August 2004

Abstract

In this study, in order to facilitate application of the NNs as well as to provide user‐friendly conditions, a performance diagnostic computer code using MATLAB® was newly proposed. As a result, not only more precise and prompt analysis results can be obtained due to use of the toolbox in MATLAB® on diagnosis and numerical analysis, but also the graphical user interface platform can be realized. The proposed engine diagnostics system is able to train the BPN with each fault pattern and then construct the total training network by assembling the trained BPNs. The database for network learning and test was constructed using a gas turbine performance simulation program. In order to investigate reliability on construction of the database for diagnostic results, an analysis is performed with five combination cases of 40 fault patterns. Finally, a diagnostic application example for the PT6A‐62 turboprop engine is performed using the trained network with the database, which represents the best diagnostic results among test sets.

Keywords

Citation

Kong, C., Ki, J., Kang, M. and Kho, S. (2004), "Intelligent performance diagnostics of a gas turbine engine using user‐friendly interface neural networks", Aircraft Engineering and Aerospace Technology, Vol. 76 No. 4, pp. 391-397. https://doi.org/10.1108/00022660410545500

Publisher

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Emerald Group Publishing Limited

Copyright © 2004, Emerald Group Publishing Limited