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    Method for Determining the Change in Gas Turbine Firing Temperature

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 009::page 094501-1
    Author:
    Wang, Bo
    ,
    Rosner, Fabian
    ,
    Rao, Ashok
    ,
    Zhao, Lifeng
    ,
    Samuelsen, Scott
    DOI: 10.1115/1.4050859
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The maximum firing temperature of a gas turbine (GT) is limited by material constraints. Critical for the operation of the GT is the blade metal temperature, which is impacted by the heat transfer from the combustor outlet gas to the blade surface. In this study, performance characteristics for an H-class-type GT have been established and two correlations for the change in the maximum permissible firing temperature as function of combustor outlet gas composition or flue gas composition and pressure ratio have been derived: (I) for detailed GT modeling with cooling flows and (II) for simplified GT modeling without specifying cooling flows.
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      Method for Determining the Change in Gas Turbine Firing Temperature

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4278189
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    contributor authorWang, Bo
    contributor authorRosner, Fabian
    contributor authorRao, Ashok
    contributor authorZhao, Lifeng
    contributor authorSamuelsen, Scott
    date accessioned2022-02-06T05:30:44Z
    date available2022-02-06T05:30:44Z
    date copyright5/4/2021 12:00:00 AM
    date issued2021
    identifier issn0742-4795
    identifier othergtp_143_09_094501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4278189
    description abstractThe maximum firing temperature of a gas turbine (GT) is limited by material constraints. Critical for the operation of the GT is the blade metal temperature, which is impacted by the heat transfer from the combustor outlet gas to the blade surface. In this study, performance characteristics for an H-class-type GT have been established and two correlations for the change in the maximum permissible firing temperature as function of combustor outlet gas composition or flue gas composition and pressure ratio have been derived: (I) for detailed GT modeling with cooling flows and (II) for simplified GT modeling without specifying cooling flows.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMethod for Determining the Change in Gas Turbine Firing Temperature
    typeJournal Paper
    journal volume143
    journal issue9
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4050859
    journal fristpage094501-1
    journal lastpage094501-4
    page4
    treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 009
    contenttypeFulltext
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