Principles of turbofans and their possible cycles, based on 14-yr studies carried out by Pratt and Whitney Aircraft; comparison of jet and turbofan; results of studies with respect to 4-engine, twin-engine, and 3-engine short range transport; 4-engine 200,000-lb, 250, 000-lb, 300,000-lb, 350,000-lb transport; Fleet Air Arm (FAA) climb requirements; present equipment considerations, cargo airplane, and military applications; turbofan improves short range transport by extending range capability at no penalty in direct operating cost. (see also abstract in SAE -- J v 68 n 8 Aug 1960 p 48-9)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Turbofan engine and its application versatility


    Additional title:

    SAE -- Paper


    Contributors:
    Taylor, S.M. (author) / Brame, C.B. (author)

    Conference:

    SAE Meeting ; 1960



    Publication date :

    1960


    Size :

    13 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Turbofan engine and its application versatility

    Taylor, S.M. / Brame, C.B. | Engineering Index Backfile | 1960


    THE TURBOFAN ENGINE AND ITS APPLICATION VERSATILITY

    BRAME, C. B. / TAYLOR, S. M. | SAE Technical Papers | 1960


    Turbofan engine and aircraft comprising turbofan engine

    GARDES PASCAL / MENOU FABIEN / GOUGEON PASCAL et al. | European Patent Office | 2021

    Free access

    Turbofan engine

    NICHOLAS GRECH / CHRISTOPHER A MOSLEY / JOHN R WELLS | European Patent Office | 2020

    Free access

    TURBOFAN ENGINE

    LIESER JAN / BOEHNING PEER | European Patent Office | 2019

    Free access