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Exhaust gas temperature measurements in diagnostic examination of naval gas turbine engines. Part I: Steady-state processes

Abstract

The article presents a possible method of detecting failures in the flow section and supply system of a naval gas turbine engine based on the exhaust gas temperature measured behind the gas generator. This temperature is a basic diagnostic parameter use for evaluating the technical state of the turbine engine in operation, and is monitored during engine start-ups, accelerations and decelerations of rotor units, and steady-load states.The first part of the article is limited to the presentation of the results of diagnostic examination of a three-shaft engine with a separate power turbine, operating in steady-load states. The here presented diagnostic analyses and syntheses based on a simplified mathematical model of thermal and flow processes taking place in the combustion chamber, which was used for deriving the equation describing the average steady-state temperature of the exhaust gas flow at the outlet cross-section of the chamber.

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Category:
Articles
Type:
artykuł w czasopiśmie wyróżnionym w JCR
Published in:
Polish Maritime Research no. 18, pages 37 - 43,
ISSN: 1233-2585
Language:
English
Publication year:
2011
Bibliographic description:
Korczewski Z.: Exhaust gas temperature measurements in diagnostic examination of naval gas turbine engines. Part I: Steady-state processes// Polish Maritime Research. -Vol. 18, iss. No. 2(69) (2011), s.37-43
Verified by:
Gdańsk University of Technology

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