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    Rich-Catalytic Lean-Burn Combustion for Low-Single-Digit NOx Gas Turbines

    Source: Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 001::page 27
    Author:
    Lance L. Smith
    ,
    Vivek Khanna
    ,
    Kenneth O. Smith
    ,
    Hasan Karim
    ,
    Marco J. Castaldi
    ,
    Shahrokh Etemad
    ,
    William C. Pfefferle
    DOI: 10.1115/1.1787510
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new rich-catalytic lean-burn combustion concept (trademarked by PCI as RCL) was tested at industrial gas turbine conditions, in Solar Turbines’ high-pressure (17 atm) combustion rig and in a modified Solar Turbines engine, demonstrating ultralow emissions of NOx<2 ppm and CO<10 ppm for natural gas fuel. For the single-injector rig tests, an RCL catalytic reactor replaced a single swirler/injector. NOx<3 ppm and CO<10 ppm were achieved over a 110°C operating range in flame temperature, including NOx<1 ppm at about 1350°C flame temperature. Combustion noise was less than 0.15% peak to peak. Four RCL catalytic reactors were then installed in a modified (single can combustor) engine. NOx emissions averaged 2.1 ppm over the allowable operating range for this modified engine, with CO<10 ppm and without combustion noise (less than 0.15% peak to peak).
    keyword(s): Temperature , Combustion , Fuels , Engines , Combustion chambers , Ejectors , Catalysts , Emissions , Gas turbines , Stress , Flow (Dynamics) , Air flow AND Flames ,
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      Rich-Catalytic Lean-Burn Combustion for Low-Single-Digit NOx Gas Turbines

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/131818
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorLance L. Smith
    contributor authorVivek Khanna
    contributor authorKenneth O. Smith
    contributor authorHasan Karim
    contributor authorMarco J. Castaldi
    contributor authorShahrokh Etemad
    contributor authorWilliam C. Pfefferle
    date accessioned2017-05-09T00:16:13Z
    date available2017-05-09T00:16:13Z
    date copyrightJanuary, 2005
    date issued2005
    identifier issn1528-8919
    identifier otherJETPEZ-26854#27_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131818
    description abstractA new rich-catalytic lean-burn combustion concept (trademarked by PCI as RCL) was tested at industrial gas turbine conditions, in Solar Turbines’ high-pressure (17 atm) combustion rig and in a modified Solar Turbines engine, demonstrating ultralow emissions of NOx<2 ppm and CO<10 ppm for natural gas fuel. For the single-injector rig tests, an RCL catalytic reactor replaced a single swirler/injector. NOx<3 ppm and CO<10 ppm were achieved over a 110°C operating range in flame temperature, including NOx<1 ppm at about 1350°C flame temperature. Combustion noise was less than 0.15% peak to peak. Four RCL catalytic reactors were then installed in a modified (single can combustor) engine. NOx emissions averaged 2.1 ppm over the allowable operating range for this modified engine, with CO<10 ppm and without combustion noise (less than 0.15% peak to peak).
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRich-Catalytic Lean-Burn Combustion for Low-Single-Digit NOx Gas Turbines
    typeJournal Paper
    journal volume127
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1787510
    journal fristpage27
    journal lastpage35
    identifier eissn0742-4795
    keywordsTemperature
    keywordsCombustion
    keywordsFuels
    keywordsEngines
    keywordsCombustion chambers
    keywordsEjectors
    keywordsCatalysts
    keywordsEmissions
    keywordsGas turbines
    keywordsStress
    keywordsFlow (Dynamics)
    keywordsAir flow AND Flames
    treeJournal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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