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    The Vorbix Burner—A New Approach to Gas Turbine Combustors

    Source: Journal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 001::page 123
    Author:
    S. J. Markowski
    ,
    R. P. Lohmann
    ,
    R. S. Reilly
    DOI: 10.1115/1.3446102
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The vorbix burner (acronym for Vortex Burning and Mixing) represents a new approach to a practical gas turbine combustor design. The concept exploits the Rayleigh instability of swirling flows to enhance the mixing and combustion rates. The combination of a two-stage fuel system with a piloted combustor leads to a unique high rate technique for fuel prevaporization within the combustor proper. This paper presents the fundamental concepts in the definition of the vorbix combustor and the results of exploratory tests conducted on can (tubular) and annular vorbix combustors. The results indicate that this type of combustor has unique performance characteristics that include excellent stability and high combustion efficiency over wide excursions in operating fuel air ratios in addition to substantially reduced emission levels during high power operation.
    keyword(s): Combustion chambers , Gas turbines , Combustion , Fuels , Fuel systems , Design , Vortices , Swirling flow , Emissions , Performance characterization AND Stability ,
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      The Vorbix Burner—A New Approach to Gas Turbine Combustors

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    https://yetl.yabesh.ir/yetl1/handle/yetl/88623
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorS. J. Markowski
    contributor authorR. P. Lohmann
    contributor authorR. S. Reilly
    date accessioned2017-05-08T23:00:40Z
    date available2017-05-08T23:00:40Z
    date copyrightJanuary, 1976
    date issued1976
    identifier issn1528-8919
    identifier otherJETPEZ-26723#123_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88623
    description abstractThe vorbix burner (acronym for Vortex Burning and Mixing) represents a new approach to a practical gas turbine combustor design. The concept exploits the Rayleigh instability of swirling flows to enhance the mixing and combustion rates. The combination of a two-stage fuel system with a piloted combustor leads to a unique high rate technique for fuel prevaporization within the combustor proper. This paper presents the fundamental concepts in the definition of the vorbix combustor and the results of exploratory tests conducted on can (tubular) and annular vorbix combustors. The results indicate that this type of combustor has unique performance characteristics that include excellent stability and high combustion efficiency over wide excursions in operating fuel air ratios in addition to substantially reduced emission levels during high power operation.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Vorbix Burner—A New Approach to Gas Turbine Combustors
    typeJournal Paper
    journal volume98
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3446102
    journal fristpage123
    journal lastpage129
    identifier eissn0742-4795
    keywordsCombustion chambers
    keywordsGas turbines
    keywordsCombustion
    keywordsFuels
    keywordsFuel systems
    keywordsDesign
    keywordsVortices
    keywordsSwirling flow
    keywordsEmissions
    keywordsPerformance characterization AND Stability
    treeJournal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;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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