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    Development of a High Temperature Liquid Metal Turbopump

    Source: Journal of Engineering for Gas Turbines and Power:;1963:;volume( 085 ):;issue: 002::page 99
    Author:
    R. W. Kelly
    ,
    G. M. Wood
    ,
    H. V. Marman
    DOI: 10.1115/1.3675239
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High performance, mobile, nuclear power plants utilizing liquid metals require high temperature pumps to circulate these heat transport fluids. These pumps must have moderately high efficiency, small size, low weight, and high reliability. In order to satisfy these requirements, centrifugal pumps directly coupled to gas turbines are utilized. As part of the aircraft nuclear power plant development program, the 3000 gpm stainless steel turbopump described in this paper was designed and tested in NaK at temperatures up to 1300 F.
    keyword(s): Liquid metals , High temperature , Nuclear power stations , Pumps , Aircraft , Centrifugal pumps , Gas turbines , Weight (Mass) , Heat , Temperature , Fluids , Reliability AND Stainless steel ,
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      Development of a High Temperature Liquid Metal Turbopump

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/94467
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorR. W. Kelly
    contributor authorG. M. Wood
    contributor authorH. V. Marman
    date accessioned2017-05-08T23:10:58Z
    date available2017-05-08T23:10:58Z
    date copyrightApril, 1963
    date issued1963
    identifier issn1528-8919
    identifier otherJETPEZ-26628#99_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94467
    description abstractHigh performance, mobile, nuclear power plants utilizing liquid metals require high temperature pumps to circulate these heat transport fluids. These pumps must have moderately high efficiency, small size, low weight, and high reliability. In order to satisfy these requirements, centrifugal pumps directly coupled to gas turbines are utilized. As part of the aircraft nuclear power plant development program, the 3000 gpm stainless steel turbopump described in this paper was designed and tested in NaK at temperatures up to 1300 F.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDevelopment of a High Temperature Liquid Metal Turbopump
    typeJournal Paper
    journal volume85
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3675239
    journal fristpage99
    journal lastpage106
    identifier eissn0742-4795
    keywordsLiquid metals
    keywordsHigh temperature
    keywordsNuclear power stations
    keywordsPumps
    keywordsAircraft
    keywordsCentrifugal pumps
    keywordsGas turbines
    keywordsWeight (Mass)
    keywordsHeat
    keywordsTemperature
    keywordsFluids
    keywordsReliability AND Stainless steel
    treeJournal of Engineering for Gas Turbines and Power:;1963:;volume( 085 ):;issue: 002
    contenttypeFulltext
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