Regenerator types applicable to gas turbine engines include liquid metal coupled system, rotary (rotating matrix) system, and direct gas to air heat exchanger; factors which influence regenerator and engine design are engine compression ratio, regenerator characteristics including regenerator type, arrangement effectiveness, total pressure loss, exhaust gas bypass ratio at full power, ratio of air side pressure loss to total pressure loss, etc; mission studies show improvements possible with regenerative gas turbine engine; vehicle mission analysis relating to helicopters, fixed-wing aircraft, cargo transport, and long endurance aircraft.


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    Titel :

    Improved mission capability and economy via regeneration


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Redmond, W.A. (Autor:in) / Beam, Jr., P.E. (Autor:in)

    Kongress:

    SAE Meeting ; 1965 Regenerators



    Erscheinungsdatum :

    1965


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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