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    Sizing of an Aircraft Fuel Pump

    Source: Journal of Fluids Engineering:;1995:;volume( 117 ):;issue: 002::page 298
    Author:
    U. S. Rohatgi
    DOI: 10.1115/1.2817144
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A need to pump a mixture of two-phase fluid appears naturally in many situations. One example of this situation is aircraft fuel systems, where the pump inlet may have two-phase mixture due to the desorption of the dissolved gases at low pressures at higher altitudes. A simple procedure of selecting proper design conditions for the inlet inducer and a method of sizing the inducer, impeller and volute to meet all the design requirements has been described. This procedure has also been applied to a typical fighter plane boost pump design.
    keyword(s): Fuel pumps , Aircraft , Design , Pumps , Mixtures , Fluids , Gases , Impellers , Fuel systems AND Desorption ,
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      Sizing of an Aircraft Fuel Pump

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    contributor authorU. S. Rohatgi
    date accessioned2017-05-08T23:47:34Z
    date available2017-05-08T23:47:34Z
    date copyrightJune, 1995
    date issued1995
    identifier issn0098-2202
    identifier otherJFEGA4-27096#298_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/115526
    description abstractA need to pump a mixture of two-phase fluid appears naturally in many situations. One example of this situation is aircraft fuel systems, where the pump inlet may have two-phase mixture due to the desorption of the dissolved gases at low pressures at higher altitudes. A simple procedure of selecting proper design conditions for the inlet inducer and a method of sizing the inducer, impeller and volute to meet all the design requirements has been described. This procedure has also been applied to a typical fighter plane boost pump design.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSizing of an Aircraft Fuel Pump
    typeJournal Paper
    journal volume117
    journal issue2
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2817144
    journal fristpage298
    journal lastpage302
    identifier eissn1528-901X
    keywordsFuel pumps
    keywordsAircraft
    keywordsDesign
    keywordsPumps
    keywordsMixtures
    keywordsFluids
    keywordsGases
    keywordsImpellers
    keywordsFuel systems AND Desorption
    treeJournal of Fluids Engineering:;1995:;volume( 117 ):;issue: 002
    contenttypeFulltext
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