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    Reaction of Fuel NOx Formation for Gas Turbine Conditions

    Source: Journal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 003::page 474
    Author:
    T. Nakata
    ,
    M. Sato
    ,
    T. Hasegawa
    DOI: 10.1115/1.2818169
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Ammonia contained in coal-gasified fuel is converted to nitrogen oxides (NOx ) in the combustion process of a gas turbine in integrated coal gasification combined cycle (IGCC) system. Research data on fuel-NOx formation are insufficient, and there still remains a wide explored domain. The present research aims at obtaining fundamental knowledge of fuel-NOx formation characteristics by applying reaction kinetics to gas turbine conditions. An instantaneous mixing condition was assumed in the cross section of a gas turbine combustor and both gradual mixing condition and instantaneous mixing condition were assumed at secondary air inlet section. The results may be summarized as follows: (1) in the primary combustion zone under fuel rich condition, HCN and other intermediate products are formed as ammonia contained in the fuel decomposes; (2) formation characteristics of fuel-NOx are affected by the condition of secondary air mixing; and (3) the conversion ratio from ammonia to NOx declines as the pressure inside the combustor rises under the condition of gradual mixing at the secondary air inlet. These results obtained agreed approximately with the experimentation.
    keyword(s): Fuels , Gas turbines , Nitrogen oxides , Combustion , Combustion chambers , Coal , Pressure , Chemical kinetics , Cycles , Fuel gasification AND Integrated gasification combined cycle ,
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      Reaction of Fuel NOx Formation for Gas Turbine Conditions

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    http://yetl.yabesh.ir/yetl1/handle/yetl/120394
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    contributor authorT. Nakata
    contributor authorM. Sato
    contributor authorT. Hasegawa
    date accessioned2017-05-08T23:56:30Z
    date available2017-05-08T23:56:30Z
    date copyrightJuly, 1998
    date issued1998
    identifier issn1528-8919
    identifier otherJETPEZ-26782#474_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120394
    description abstractAmmonia contained in coal-gasified fuel is converted to nitrogen oxides (NOx ) in the combustion process of a gas turbine in integrated coal gasification combined cycle (IGCC) system. Research data on fuel-NOx formation are insufficient, and there still remains a wide explored domain. The present research aims at obtaining fundamental knowledge of fuel-NOx formation characteristics by applying reaction kinetics to gas turbine conditions. An instantaneous mixing condition was assumed in the cross section of a gas turbine combustor and both gradual mixing condition and instantaneous mixing condition were assumed at secondary air inlet section. The results may be summarized as follows: (1) in the primary combustion zone under fuel rich condition, HCN and other intermediate products are formed as ammonia contained in the fuel decomposes; (2) formation characteristics of fuel-NOx are affected by the condition of secondary air mixing; and (3) the conversion ratio from ammonia to NOx declines as the pressure inside the combustor rises under the condition of gradual mixing at the secondary air inlet. These results obtained agreed approximately with the experimentation.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleReaction of Fuel NOx Formation for Gas Turbine Conditions
    typeJournal Paper
    journal volume120
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2818169
    journal fristpage474
    journal lastpage480
    identifier eissn0742-4795
    keywordsFuels
    keywordsGas turbines
    keywordsNitrogen oxides
    keywordsCombustion
    keywordsCombustion chambers
    keywordsCoal
    keywordsPressure
    keywordsChemical kinetics
    keywordsCycles
    keywordsFuel gasification AND Integrated gasification combined cycle
    treeJournal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 003
    contenttypeFulltext
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