Paper recounts step by step and model by model, development of Allison V-1710 engine, first liquid cooled military aircraft engine in production in United States; since 1930, when design of this 12-cyl engine was initiated, power plant has been stepped up from 650 hp without supercharging to 1000-1500 hp in its supercharged state, and weight has increased from 1000 to 1320 lb. (Trans)


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    Titel :

    Allison aircraft-engine development


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


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


    Erscheinungsdatum :

    1941


    Format / Umfang :

    13 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The ALLISON AIRCRAFT-ENGINE DEVELOPMENT

    HAZEN, R. M. | SAE Technical Papers | 1941


    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 Allison aircraft engine

    Gerdan, D. | Engineering Index Backfile | 1945


    THE ALLISON T56 TURBO-PROP AIRCRAFT ENGINE

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