An exhaust nozzle for use with a gas turbine engine includes an outer shroud and a nozzle-plug assembly coupled to the outer shroud. The nozzle-plug assembly includes an inner plug and at least one support vane that is coupled to the outer shroud to support the inner plug in an exhaust nozzle flow path.


    Access

    Download


    Export, share and cite



    Title :

    EXHAUST NOZZLE WITH VANE SUPPORT STRUCTURE FOR A GAS TURBINE ENGINE


    Contributors:

    Publication date :

    2021-09-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    Exhaust nozzle with vane support structure for a gas turbine engine

    SUTTERFIELD DAVID L / PETTY JACK D / LERG BRYAN H et al. | European Patent Office | 2022

    Free access

    Turbine engine exhaust nozzle performance

    WEHOFER, S. / MATZ, R. | AIAA | 1973


    EXHAUST NOZZLE FOR GAS TURBINE ENGINE

    HOLT GAVIN JOSEPH / IGLEWSKI TOMASZ / HOLLAND JOHN ROBERT | European Patent Office | 2017

    Free access

    EXHAUST NOZZLE FOR GAS TURBINE ENGINE

    HOLT GAVIN JOSEPH / IGLEWSKI TOMASZ / HOLLAND JOHN ROBERT | European Patent Office | 2017

    Free access

    Variable exhaust nozzle for gas turbine engine

    European Patent Office | 2020

    Free access