A revolutionary approach to gas turbine condition monitoring is made possible by the recent development of accurate real-time gas turbine performance models. This paper describes an approach for an integrated condition management system operating concurrently with the gas turbine control system for improved availability, safety and economy. This paper considers the system subject to the requirements and constraints of aircraft gas turbines. A system architecture is described based on a primary, gas path performance model with supplementary models representing the secondary air, fuel and lubrication systems and the rotor system dynamics. Measurement and processing requirements for the system are defined. Preflight, in-flight and postflight application and analysis by the gas turbine operator are discussed.
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ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition
June 1–4, 1992
Cologne, Germany
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7894-1
PROCEEDINGS PAPER
On-Board Condition Management for Aircraft Gas Turbines
G. W. Gallops,
G. W. Gallops
United Technologies Corporation
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M. H. Kennedy
M. H. Kennedy
United Technologies Corporation
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G. W. Gallops
United Technologies Corporation
F. D. Gass
United Technologies Corporation
M. H. Kennedy
United Technologies Corporation
Paper No:
92-GT-416, V002T02A037; 7 pages
Published Online:
March 3, 2015
Citation
Gallops, GW, Gass, FD, & Kennedy, MH. "On-Board Condition Management for Aircraft Gas Turbines." Proceedings of the ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. Cologne, Germany. June 1–4, 1992. V002T02A037. ASME. https://doi.org/10.1115/92-GT-416
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