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Adaptive Simulation of Gas Turbine Performance PUBLIC ACCESS

[+] Author Affiliations
A. Stamatis, K. Mathioudakis, K. D. Papailiou

National Technical University, Athens, Greece

Paper No. 89-GT-205, pp. V001T01A083; 9 pages
doi:10.1115/89-GT-205
From:
  • ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Toronto, Ontario, Canada, June 4–8, 1989
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7913-9
  • Copyright © 1989 by ASME

abstract

A method is presented allowing the simulation of Gas Turbine performance with the possibility of adapting to engine particularities. Measurements along the gas path are used, in order to adapt a given performance model by appropriate modification of the component maps. The proposed method can provide accurate simulation for engines of the same type, differing due to manufacturing or assembly tolerances. It doesn’t require accurate component maps, as they are derived during the adaptation process. It can also be used for health monitoring purposes, introducing thus a novel approach for component condition assessment. The effectiveness of the proposed method is demonstrated by application to an industrial Gas Turbine.

Copyright © 1989 by ASME
This article is only available in the PDF format.

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