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contributor authorRainer Kurz
contributor authorKlaus Brun
contributor authorMeron Wollie
date accessioned2017-05-09T00:32:29Z
date available2017-05-09T00:32:29Z
date copyrightNovember, 2009
date issued2009
identifier issn1528-8919
identifier otherJETPEZ-27086#062401_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/140387
description abstractThis paper provides a discussion on how degradation develops and affects the performance of the gas turbine. Because the function of a gas turbine is the result of the fine-tuned cooperation of many different components, the emphasis of this paper is on the gas turbine and its components as a system. Therefore, the interaction of components is studied in detail. An engine model is subjected to various types of degradation, and the effect on operating parameters is studied. The focus is on three areas: How does component degradation impact the operating points of the engine compressor, how does component degradation impact full load and part load gas turbine performance characteristics, and how does component degradation impact measurable engine operating parameters. Experimental data are provided that supports the theoretical conclusion. Parameters that indicate levels of degradation are outlined, thus providing guidance for condition monitoring practice.
publisherThe American Society of Mechanical Engineers (ASME)
titleDegradation Effects on Industrial Gas Turbines
typeJournal Paper
journal volume131
journal issue6
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3097135
journal fristpage62401
identifier eissn0742-4795
keywordsTemperature
keywordsEngines
keywordsCompressors
keywordsFlow (Dynamics)
keywordsGas turbines
keywordsTurbines
keywordsGenerators
keywordsStress
keywordsPressure AND Heat
treeJournal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 006
contenttypeFulltext


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