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    Gas Turbine Emission Characteristics in Perfectly Premixed Combustion

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 006::page 61501
    Author:
    A. M. Elkady
    ,
    D. M. Kalitan
    ,
    R. Akula
    ,
    H. Karim
    ,
    M. Hadley
    ,
    G. Leonard
    ,
    J. Herbon
    DOI: 10.1115/1.4006058
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the present study, a simple perfectly premixed research burner was utilized at temperatures, pressures and residence times representative of an industrial gas turbine cycle to identify the lower limit of NOx and CO emissions, and to establish an emissions benchmark for practical gas turbine combustors. In addition to experimental data, a chemical reactor model has been utilized for the prediction of the NOx and CO, based on detailed chemical reaction mechanisms. Several current kinetics mechanisms were evaluated and subsequently compared to the experimental data. In addition, sensitivity analysis was performed to identify important reactions at the conditions tested, and will be discussed.
    keyword(s): Combustion , Combustion chambers , Gas turbines , Flames , Temperature , Emissions , Mechanisms , Pressure , Chemical kinetics AND Heat losses ,
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      Gas Turbine Emission Characteristics in Perfectly Premixed Combustion

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/148813
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. M. Elkady
    contributor authorD. M. Kalitan
    contributor authorR. Akula
    contributor authorH. Karim
    contributor authorM. Hadley
    contributor authorG. Leonard
    contributor authorJ. Herbon
    date accessioned2017-05-09T00:50:13Z
    date available2017-05-09T00:50:13Z
    date copyrightJune, 2012
    date issued2012
    identifier issn1528-8919
    identifier otherJETPEZ-27196#061501_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148813
    description abstractIn the present study, a simple perfectly premixed research burner was utilized at temperatures, pressures and residence times representative of an industrial gas turbine cycle to identify the lower limit of NOx and CO emissions, and to establish an emissions benchmark for practical gas turbine combustors. In addition to experimental data, a chemical reactor model has been utilized for the prediction of the NOx and CO, based on detailed chemical reaction mechanisms. Several current kinetics mechanisms were evaluated and subsequently compared to the experimental data. In addition, sensitivity analysis was performed to identify important reactions at the conditions tested, and will be discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleGas Turbine Emission Characteristics in Perfectly Premixed Combustion
    typeJournal Paper
    journal volume134
    journal issue6
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4006058
    journal fristpage61501
    identifier eissn0742-4795
    keywordsCombustion
    keywordsCombustion chambers
    keywordsGas turbines
    keywordsFlames
    keywordsTemperature
    keywordsEmissions
    keywordsMechanisms
    keywordsPressure
    keywordsChemical kinetics AND Heat losses
    treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 006
    contenttypeFulltext
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