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    Design and Development of a High-Pressure Combustor for Aero-Gas-Turbines

    Source: Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 001::page 129
    Author:
    K. Suzuki
    ,
    A. Ishii
    ,
    T. Saito
    ,
    M. Matsuki
    ,
    T. Torisaki
    ,
    S. Horiuchi
    DOI: 10.1115/1.3446303
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Research on a high-pressure combustor for turbofan engines has been carried out at National Aerospace Laboratory (Tokyo). In the first step, a design point of research combustor was fixed from a initial program of FJR Turbofan development. Then the combustor-type was developed, and the major dimensions were decided mainly from the experiences of JR-series lift jet engines, and partly from published data. As the next step, various-segment-type and full-annular-type combustors were tested at the pressure up to 15 bar.
    keyword(s): High pressure (Physics) , Combustion chambers , Design , Turbines , Turbofans , Jet engines , Aerospace industry , Pressure , Engines AND Dimensions ,
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      Design and Development of a High-Pressure Combustor for Aero-Gas-Turbines

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/91033
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorK. Suzuki
    contributor authorA. Ishii
    contributor authorT. Saito
    contributor authorM. Matsuki
    contributor authorT. Torisaki
    contributor authorS. Horiuchi
    date accessioned2017-05-08T23:04:47Z
    date available2017-05-08T23:04:47Z
    date copyrightJanuary, 1978
    date issued1978
    identifier issn1528-8919
    identifier otherJETPEZ-26739#129_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/91033
    description abstractResearch on a high-pressure combustor for turbofan engines has been carried out at National Aerospace Laboratory (Tokyo). In the first step, a design point of research combustor was fixed from a initial program of FJR Turbofan development. Then the combustor-type was developed, and the major dimensions were decided mainly from the experiences of JR-series lift jet engines, and partly from published data. As the next step, various-segment-type and full-annular-type combustors were tested at the pressure up to 15 bar.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDesign and Development of a High-Pressure Combustor for Aero-Gas-Turbines
    typeJournal Paper
    journal volume100
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3446303
    journal fristpage129
    journal lastpage135
    identifier eissn0742-4795
    keywordsHigh pressure (Physics)
    keywordsCombustion chambers
    keywordsDesign
    keywordsTurbines
    keywordsTurbofans
    keywordsJet engines
    keywordsAerospace industry
    keywordsPressure
    keywordsEngines AND Dimensions
    treeJournal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;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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