Data-Driven Based Gas Path Fault Diagnosis for Turbo-Shaft Engine

Article Preview

Abstract:

In order to improve diagnostic accuracy and reduce the rate of misdiagnosis to the aircraft engine gas path faulty, the methods based on data-driven and information fusion are developed and analyzed. BP neural network (NN) and RBF neural network based on data-driven single gas path fault diagnosis method is introduced firstly. Design gas path performance estimators and the fault type classification for turbo-shaft engine. Then the gas path fused diagnostic structure based on D-S evidence theory and least squares support vector machine are developed. Comparisons of the turbo-shaft engine gas path fault diagnosis verify the feasibility and effectiveness of the gas path fault diagnosis based on information fusion.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

400-404

Citation:

Online since:

December 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Jaiwon S, The NASA Aviation Safety Program: Overview. NASA/TM-2000-209810.

Google Scholar

[2] Michael D G, Ahmet D, Jonathan S L, Model-based fault diagnosis for turboshaft engines, NASA/TM-1998-208825.

Google Scholar

[3] Ogaji S, Li Y G, Sampath S, et al, Gas-path Fault diagnosis of a turbofan engine from transient data using artificial neural networks, GT2003-28423.

DOI: 10.1115/gt2003-38423

Google Scholar

[4] Volponi A J, Data Fusion for Enhanced Aircraft Engine Prognostics and Health Management, NASA/CR-2005-214055.

Google Scholar

[5] Vapnik V. The nature of statistical learning theory. New York: Springer, 1995: 16- 23.

Google Scholar