Design and testing of 5500-hp experimental engine, developed by Allison Div, General Motors Corp; engine incorporates light weight, tubular regenerator (heat exchanger) in which heat from turbine exhaust is transferred to compressor outlet air reducing fuel consumption; schematic flow diagram for regenerative cycle engine; reduction in specific fuel consumption of 35%, compared to current production nonregenerative turboprop engines, was demonstrated at cruise power test point; program provided background for Allison's new light weight T78 regenerative turboprop engine.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Test of regenerative turboprop aircraft engine


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Beam, Jr., P.E. (Autor:in) / Cutler, R.E. (Autor:in)

    Kongress:

    SAE Meeting ; 1964



    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Test of a Regenerative Turboprop Aircraft Engine

    Beam, Paul E. / Cutler, Roswelt E. | SAE Technical Papers | 1964


    Allison T78 -- Regenerative turboprop for long-endurance aircraft

    Stevens, J.H. | Engineering Index Backfile | 1964


    Regenerative System for Turboprop Engines

    Agrawal, Rishabh / Singh, Deepanshu / Subbarao, PMV | AIAA | 2017


    Aircraft turboprop engine comprising two coaxial propellers

    ANTHONY PASCAL ELOI LOUET / CLEMENT MARCEL MAURICE DEJEU / JONATHAN EVERT VLASTUIN | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT TURBOPROP ENGINE EQUIPPED WITH ELECTRIC MACHINE

    KLONOWSKI THOMAS / LAFARGUE OLIVIER / MOUTAUX ANTOINE et al. | Europäisches Patentamt | 2020

    Freier Zugriff