Engine so designed that all aircraft accessories are mounted on reduction gear rear case; arrangement favors frontal area at expense of oa length, and results in nacelle of good fineness ratio with extremely low drag; it weighs 1600 lb and delivers 3460 shp and 725 lb jet thrust at 13,800 rpm; test results.


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    Titel :

    Allison t56 turbo-prop aircraft engine


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Wheatley, J.B. (Autor:in) / Zimmerman, D.G. (Autor:in) / Hicks, R.W. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1955 Turbine propeller



    Erscheinungsdatum :

    1955


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    THE ALLISON T56 TURBO-PROP AIRCRAFT ENGINE

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


    ALLISON: AIRCRAFT ENGINE PIONEER

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


    The ALLISON AIRCRAFT-ENGINE DEVELOPMENT

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


    J35-A-15 turbo-jet engine production at Allison

    Geschelin, J. | Engineering Index Backfile | 1948


    Flyover noise measurements for turbo-prop aircraft

    WILFORD, D. / BONNEAU, H. | AIAA | 1983