THIS paper recounts, step by step and model by model, the development of the Allison V-1710 aircraft engine - the first liquid-cooled military aircraft engine in production in this country.Since 1930, when the design of this V-type 12-cyl engine was initiated, the powerplant has been stepped up from 650 hp without supercharging to 1000-1500 hp in its supercharged state, and the weight has increased from about 1000 lb to 1320 lb, the author reveals.The following three underlying reasons are given for building the first V-1710 engine: Additional advantages discussed are flexibility of radiator installation and of engine location.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The ALLISON AIRCRAFT-ENGINE DEVELOPMENT


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    HAZEN, R. M. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    1941-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    ALLISON: AIRCRAFT ENGINE PIONEER

    Jensen, D. T. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003


    Allison t56 turbo-prop aircraft engine

    Wheatley, J.B. / Zimmerman, D.G. / Hicks, R.W. | Engineering Index Backfile | 1955


    Late Developments of the Allison Aircraft Engine

    GERDAN, DIMITRIUS | SAE Technical Papers | 1945


    THE ALLISON T56 TURBO-PROP AIRCRAFT ENGINE

    ZIMMERMAN, D. G. / WHEATLEY, JOHN B. / HICKS, R. W. | SAE Technical Papers | 1955