A nacelle for use with a gas turbine engine is presented. An integral webbed structure resembling a spoked wheel for rigidly interconnecting the nacelle and engine, provides lightweight support. The inner surface of the nacelle defines the outer limits of the engine motive fluid flow annulus while the outer surface of the nacelle defines a streamlined envelope for the engine.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Integrated gas turbine engine-nacelle


    Contributors:

    Publication date :

    1977-10-25


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Gas turbine engine nacelle

    SMITH ANGUS ROY / ARZOGLOU DIMITRIS | European Patent Office | 2018

    Free access

    Gas turbine engine nacelle

    SMITH ANGUS ROY / ARZOGLOU DIMITRIS | European Patent Office | 2019

    Free access

    Nacelle for gas turbine engine

    CHRISTIE ROBERT E / MACMANUS DAVID G / SHEAF CHRISTOPHER T J | European Patent Office | 2022

    Free access

    NACELLE OF JET-TURBINE ENGINE

    BOUTEILLER XAVIER / BLIN LAURENT ALBERT | European Patent Office | 2015

    Free access

    AIRCRAFT GAS TURBINE ENGINE NACELLE

    BOND JONATHAN M | European Patent Office | 2018

    Free access