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    Degradation Effects on Industrial Gas Turbines

    Source: Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 006::page 62401
    Author:
    Rainer Kurz
    ,
    Klaus Brun
    ,
    Meron Wollie
    DOI: 10.1115/1.3097135
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This 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.
    keyword(s): Temperature , Engines , Compressors , Flow (Dynamics) , Gas turbines , Turbines , Generators , Stress , Pressure AND Heat ,
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      Degradation Effects on Industrial Gas Turbines

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/140387
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    • Journal of Engineering for Gas Turbines and Power

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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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    DSpace software copyright © 2002-2015  DuraSpace
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