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    Optimum Power Boosting of Gas Turbine Cycles With Compressor Inlet Air Refrigeration

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 001::page 124
    Author:
    M. A. Ait-Ali
    DOI: 10.1115/1.2815535
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A conceptual gas turbine cycle with refrigerated air supplied to the compressor inlet is proposed to increase the cycle specific net power significantly and render it practically insensitive to seasonal temperature fluctuations. It is optimized for maximum power per m3 /s and maximum power per kg/s of induced air. These cycle performances are evaluated in a numerical example for two refrigeration cycle efficiencies, based on state-of-the-art isentropic efficiency coefficients of the compressor and turbine. The specific heats of air and products of combustion are treated as temperature-dependent parameters to be determined as integrated mean averages.
    keyword(s): Compressors , Gas turbines , Refrigeration , Cycles , Temperature , Combustion , Fluctuations (Physics) AND Turbines ,
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      Optimum Power Boosting of Gas Turbine Cycles With Compressor Inlet Air Refrigeration

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    https://yetl.yabesh.ir/yetl1/handle/yetl/118730
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. A. Ait-Ali
    date accessioned2017-05-08T23:53:33Z
    date available2017-05-08T23:53:33Z
    date copyrightJanuary, 1997
    date issued1997
    identifier issn1528-8919
    identifier otherJETPEZ-26761#124_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118730
    description abstractA conceptual gas turbine cycle with refrigerated air supplied to the compressor inlet is proposed to increase the cycle specific net power significantly and render it practically insensitive to seasonal temperature fluctuations. It is optimized for maximum power per m3 /s and maximum power per kg/s of induced air. These cycle performances are evaluated in a numerical example for two refrigeration cycle efficiencies, based on state-of-the-art isentropic efficiency coefficients of the compressor and turbine. The specific heats of air and products of combustion are treated as temperature-dependent parameters to be determined as integrated mean averages.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOptimum Power Boosting of Gas Turbine Cycles With Compressor Inlet Air Refrigeration
    typeJournal Paper
    journal volume119
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2815535
    journal fristpage124
    journal lastpage130
    identifier eissn0742-4795
    keywordsCompressors
    keywordsGas turbines
    keywordsRefrigeration
    keywordsCycles
    keywordsTemperature
    keywordsCombustion
    keywordsFluctuations (Physics) AND Turbines
    treeJournal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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