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    The CIVIC—A Concept in Vortex Induced Combustion, Part II

    Source: Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 004::page 708
    Author:
    J. R. Shekleton
    DOI: 10.1115/1.3230793
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbomach, A Division of Solar Turbines International, An Operating Group of International Harvester, manufactures the small 10kW Gemini gas turbine. The very small size of the combustor precluded the use of conventional gas turbine combustor design techniques. A novel solution was arrived at based primarily on an amalgam of design practices used in furnaces and reciprocating engines. Use was made of the centrifugal force effects of swirl flow (Rayleigh Instability Criteria) both as a method of fuel evaporation and as a method of control of the rate of flame propagation. Substantial advantage can be obtained by this design technique provided that a fine and accurately located fuel spray is achieved. Various applications of this method of combustor design are outlined with emphasis on aerodynamics and fuel atomization and volatility rather than reaction rate criteria as the dominant influences.
    keyword(s): Flow (Dynamics) , Aerodynamics , Combustion , Fuels , Centrifugal force , Volatility , Amalgams , Combustion chambers , Design , Evaporation , Gas turbines , Solar energy , Sprays , Turbines , Vortices , Flames , Furnaces AND Piston engines ,
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      The CIVIC—A Concept in Vortex Induced Combustion, Part II

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/94473
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. R. Shekleton
    date accessioned2017-05-08T23:10:58Z
    date available2017-05-08T23:10:58Z
    date copyrightOctober, 1981
    date issued1981
    identifier issn1528-8919
    identifier otherJETPEZ-26769#708_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94473
    description abstractTurbomach, A Division of Solar Turbines International, An Operating Group of International Harvester, manufactures the small 10kW Gemini gas turbine. The very small size of the combustor precluded the use of conventional gas turbine combustor design techniques. A novel solution was arrived at based primarily on an amalgam of design practices used in furnaces and reciprocating engines. Use was made of the centrifugal force effects of swirl flow (Rayleigh Instability Criteria) both as a method of fuel evaporation and as a method of control of the rate of flame propagation. Substantial advantage can be obtained by this design technique provided that a fine and accurately located fuel spray is achieved. Various applications of this method of combustor design are outlined with emphasis on aerodynamics and fuel atomization and volatility rather than reaction rate criteria as the dominant influences.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe CIVIC—A Concept in Vortex Induced Combustion, Part II
    typeJournal Paper
    journal volume103
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3230793
    journal fristpage708
    journal lastpage717
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsAerodynamics
    keywordsCombustion
    keywordsFuels
    keywordsCentrifugal force
    keywordsVolatility
    keywordsAmalgams
    keywordsCombustion chambers
    keywordsDesign
    keywordsEvaporation
    keywordsGas turbines
    keywordsSolar energy
    keywordsSprays
    keywordsTurbines
    keywordsVortices
    keywordsFlames
    keywordsFurnaces AND Piston engines
    treeJournal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 004
    contenttypeFulltext
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