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    A Study on Low NOx Combustion in LBG-Fueled 1500°C-Class Gas Turbine

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 003::page 534
    Author:
    T. Nakata
    ,
    M. Sato
    ,
    T. Ninomiya
    ,
    T. Hasegawa
    DOI: 10.1115/1.2816680
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Developing integrated coal gasification combined-cycle systems ensures cost-effective and environmentally sound options for supplying future power generation needs. The reduction of NOx emissions and increasing the inlet temperature of gas turbines are the most significant issues in gas turbine development in Integrated Coal Gasification Combined Cycle (IGCC) power generation systems. The coal gasified fuel, which is produced in a coal gasifier of an air-blown entrained-flow type has a calorific value as low as 1/10 of natural gas. Furthermore, the fuel gas contains ammonia when a gas cleaning system is a hot type, and ammonia will be converted to nitrogen oxides in the combustion process of a gas turbine. This study is performed in a 1500°C-class gas turbine combustor firing low-Btu coal-gasified fuel in IGCC systems. An advanced rich-lean combustor of 150-MW class gas turbine was designed to hold stable combustion burning low-Btu gas and to reduce fuel NOx emissions from the ammonia in the fuel. The main fuel and the combustion air are supplied into a fuel-rich combustion chamber with strong swirl flow and make fuel-rich flame to decompose ammonia into intermediate reactants such as NHi and HCN. The secondary air is mixed with primary combustion gas dilatorily to suppress the oxidization of ammonia reactants in fuel-lean combustion chamber and to promote a reducing process to nitrogen. By testing under atmospheric pressure conditions, the authors have obtained a very significant result through investigating the effect of combustor exit gas temperature on combustion characteristics. Since we have ascertained the excellent performance of the tested combustor through our extensive investigation, we wish to report on the results.
    keyword(s): Combustion , Gas turbines , Nitrogen oxides , Fuels , Combustion chambers , Coal , Flow (Dynamics) , Temperature , Cycles , Emissions , Fuel gasification , Integrated gasification combined cycle , Nitrogen , Electric power generation , Firing (materials) , Flames , Sound , Combustion gases , Natural gas , Testing , Atmospheric pressure , Gaseous fuels , Energy / power systems AND Energy generation ,
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      A Study on Low NOx Combustion in LBG-Fueled 1500°C-Class Gas Turbine

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    http://yetl.yabesh.ir/yetl1/handle/yetl/116901
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorT. Nakata
    contributor authorM. Sato
    contributor authorT. Ninomiya
    contributor authorT. Hasegawa
    date accessioned2017-05-08T23:50:02Z
    date available2017-05-08T23:50:02Z
    date copyrightJuly, 1996
    date issued1996
    identifier issn1528-8919
    identifier otherJETPEZ-26756#534_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116901
    description abstractDeveloping integrated coal gasification combined-cycle systems ensures cost-effective and environmentally sound options for supplying future power generation needs. The reduction of NOx emissions and increasing the inlet temperature of gas turbines are the most significant issues in gas turbine development in Integrated Coal Gasification Combined Cycle (IGCC) power generation systems. The coal gasified fuel, which is produced in a coal gasifier of an air-blown entrained-flow type has a calorific value as low as 1/10 of natural gas. Furthermore, the fuel gas contains ammonia when a gas cleaning system is a hot type, and ammonia will be converted to nitrogen oxides in the combustion process of a gas turbine. This study is performed in a 1500°C-class gas turbine combustor firing low-Btu coal-gasified fuel in IGCC systems. An advanced rich-lean combustor of 150-MW class gas turbine was designed to hold stable combustion burning low-Btu gas and to reduce fuel NOx emissions from the ammonia in the fuel. The main fuel and the combustion air are supplied into a fuel-rich combustion chamber with strong swirl flow and make fuel-rich flame to decompose ammonia into intermediate reactants such as NHi and HCN. The secondary air is mixed with primary combustion gas dilatorily to suppress the oxidization of ammonia reactants in fuel-lean combustion chamber and to promote a reducing process to nitrogen. By testing under atmospheric pressure conditions, the authors have obtained a very significant result through investigating the effect of combustor exit gas temperature on combustion characteristics. Since we have ascertained the excellent performance of the tested combustor through our extensive investigation, we wish to report on the results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Study on Low NOx Combustion in LBG-Fueled 1500°C-Class Gas Turbine
    typeJournal Paper
    journal volume118
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2816680
    journal fristpage534
    journal lastpage540
    identifier eissn0742-4795
    keywordsCombustion
    keywordsGas turbines
    keywordsNitrogen oxides
    keywordsFuels
    keywordsCombustion chambers
    keywordsCoal
    keywordsFlow (Dynamics)
    keywordsTemperature
    keywordsCycles
    keywordsEmissions
    keywordsFuel gasification
    keywordsIntegrated gasification combined cycle
    keywordsNitrogen
    keywordsElectric power generation
    keywordsFiring (materials)
    keywordsFlames
    keywordsSound
    keywordsCombustion gases
    keywordsNatural gas
    keywordsTesting
    keywordsAtmospheric pressure
    keywordsGaseous fuels
    keywordsEnergy / power systems AND Energy generation
    treeJournal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 003
    contenttypeFulltext
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