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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Allison t56 turbo-prop aircraft engine


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1955 Turbine propeller



    Publication date :

    1955


    Size :

    14 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    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


    DESIGN TRENDS IN TURBO-JET AND TURBO-PROP AIRCRAFT ENGINES

    FARRAR, EARL V. | SAE Technical Papers | 1947