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    Test Results of Low NOx Catalytic Combustors for Gas Turbines

    Source: Journal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 003::page 511
    Author:
    Y. Ozawa
    ,
    M. Saiga
    ,
    S. Watanabe
    ,
    J. Hirano
    ,
    M. Sato
    DOI: 10.1115/1.2906849
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Catalytic combustion is an ultralow NOx combustion method, so it is expected that this method will be applied to a gas turbine combustor. However, it is difficult to develop a catalytic combustor because catalytic reliability at high temperature is still insufficient. To overcome this difficulty, we designed a catalytic combustor in which premixed combustion was combined. By this device, it is possible to obtain combustion gas at a combustion temperature of 1300°C while keeping the catalytic temperature below 1000°C. After performing preliminary tests using LPG, we designed two types of combustor for natural gas with a capacity equivalent to one combustor used in a 20 MW class multican-type gas turbine. Combustion tests were conducted at atmospheric pressure using natural gas. As a result, it was confirmed that a combustor in which catalytic combustor segments were arranged alternately with premixing nozzles could achieve low NOx and high combustion efficiency in the range from 1000°C to 1300°C of the combustor exit gas temperature.
    keyword(s): Combustion chambers , Gas turbines , Nitrogen oxides , Combustion , Temperature , Natural gas , Nozzles , Atmospheric pressure , Reliability , Combustion gases AND High temperature ,
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      Test Results of Low NOx Catalytic Combustors for Gas Turbines

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    http://yetl.yabesh.ir/yetl1/handle/yetl/113536
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    contributor authorY. Ozawa
    contributor authorM. Saiga
    contributor authorS. Watanabe
    contributor authorJ. Hirano
    contributor authorM. Sato
    date accessioned2017-05-08T23:44:06Z
    date available2017-05-08T23:44:06Z
    date copyrightJuly, 1994
    date issued1994
    identifier issn1528-8919
    identifier otherJETPEZ-26729#511_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113536
    description abstractCatalytic combustion is an ultralow NOx combustion method, so it is expected that this method will be applied to a gas turbine combustor. However, it is difficult to develop a catalytic combustor because catalytic reliability at high temperature is still insufficient. To overcome this difficulty, we designed a catalytic combustor in which premixed combustion was combined. By this device, it is possible to obtain combustion gas at a combustion temperature of 1300°C while keeping the catalytic temperature below 1000°C. After performing preliminary tests using LPG, we designed two types of combustor for natural gas with a capacity equivalent to one combustor used in a 20 MW class multican-type gas turbine. Combustion tests were conducted at atmospheric pressure using natural gas. As a result, it was confirmed that a combustor in which catalytic combustor segments were arranged alternately with premixing nozzles could achieve low NOx and high combustion efficiency in the range from 1000°C to 1300°C of the combustor exit gas temperature.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTest Results of Low NOx Catalytic Combustors for Gas Turbines
    typeJournal Paper
    journal volume116
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906849
    journal fristpage511
    journal lastpage516
    identifier eissn0742-4795
    keywordsCombustion chambers
    keywordsGas turbines
    keywordsNitrogen oxides
    keywordsCombustion
    keywordsTemperature
    keywordsNatural gas
    keywordsNozzles
    keywordsAtmospheric pressure
    keywordsReliability
    keywordsCombustion gases AND High temperature
    treeJournal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 003
    contenttypeFulltext
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