A method for solving the gas path analysis problem of jet engine diagnostics based on a probabilistic approach is presented. The method is materialized through the use of a Bayesian Belief Network (BBN). Building a BBN for gas turbine performance fault diagnosis requires information of a stochastic nature expressing the probability of whether a series of events occurred or not. This information can be extracted by a deterministic model and does not depend on hard to find flight data of different faulty operations of the engine. The diagnostic problem and the overall diagnostic procedure are first described. A detailed description of the way the diagnostic procedure is set-up, with focus on building the BBN from an engine performance model, follows. The case of a turbofan engine is used to evaluate the effectiveness of the method. Several simulated and benchmark fault case scenarios have been considered for this reason. The examined cases demonstrate that the proposed BBN-based diagnostic method composes a powerful tool. This work also shows that building a diagnostic tool, based on information provided by an engine performance model, is feasible and can be efficient as well.
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ASME Turbo Expo 2004: Power for Land, Sea, and Air
June 14–17, 2004
Vienna, Austria
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
0-7918-4167-7
PROCEEDINGS PAPER
Bayesian Network Approach for Gas Path Fault Diagnosis Available to Purchase
C. Romessis,
C. Romessis
National Technical University of Athens, Athens, Greece
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K. Mathioudakis
K. Mathioudakis
National Technical University of Athens, Athens, Greece
Search for other works by this author on:
C. Romessis
National Technical University of Athens, Athens, Greece
K. Mathioudakis
National Technical University of Athens, Athens, Greece
Paper No:
GT2004-53801, pp. 691-699; 9 pages
Published Online:
November 24, 2008
Citation
Romessis, C, & Mathioudakis, K. "Bayesian Network Approach for Gas Path Fault Diagnosis." Proceedings of the ASME Turbo Expo 2004: Power for Land, Sea, and Air. Volume 2: Turbo Expo 2004. Vienna, Austria. June 14–17, 2004. pp. 691-699. ASME. https://doi.org/10.1115/GT2004-53801
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