A new concept for a turbofan engine called the 'Separated Core Turbofan Engine' is proposed and studied under the research program of the ultrahigh bypass turbofan engine for the next generation high-subsonic transport aircraft. The concept engine consists of two subunits, a core engine and a fan engine which are separate from each other. The results of the conceptual study show that this engine has many potential advantages over the current turbofan engines in many respects, including stability of operation and flexibility of configuration, and it also has other applications such as in advanced VTOL transport aircraft.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Separated Core Turbofan Engine


    Contributors:
    Y. Saito (author) / M. Endoh (author) / Y. Matsuda (author) / N. Sugiyama (author) / N. Sugahara (author)

    Publication date :

    1996


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Seperated core turbofan engine

    Saito, Yoshio | TIBKAT | 1996


    Core cowl for a turbofan engine

    CERRA DAVID F / TRETOW PAUL ROBERT / WILLIE ROBERT H et al. | European Patent Office | 2018

    Free access

    Core cowl for a turbofan engine

    DAVID F CERRA / PAUL ROBERT TRETOW / ROBERT H WILLIE et al. | European Patent Office | 2016

    Free access

    TURBOFAN ENGINE AND CORE LINK THEREFORE

    OLVER BRYAN WILLIAM | European Patent Office | 2020

    Free access

    Turbofan engine and core link therefore

    OLVER BRYAN WILLIAM | European Patent Office | 2021

    Free access