A nacelle for a gas turbine engine includes at least one hinge axis extending along the nacelle. At least one cowl is mounted to the nacelle, along the at least one hinge axis, by a plurality of hinges. The plurality of hinges includes at least one latch. The at least one latch includes a clevis and a tang. The clevis and the tang of the at least one latch are configured to receive a hinge pin, through a pin aperture, when the at least one cowl is in a closed condition.


    Access

    Download


    Export, share and cite



    Title :

    Nacelle cowl hinge


    Contributors:

    Publication date :

    2021-02-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    NACELLE COWL HINGE

    SHETZER DANIEL J | European Patent Office | 2020

    Free access

    NACELLE COWL HINGE

    SHETZER DANIEL J | European Patent Office | 2020

    Free access

    NACELLE COWL DEFLECTION LIMITER

    LINDE ERIK | European Patent Office | 2023

    Free access

    Nacelle cowl deflection limiter

    LINDE ERIK | European Patent Office | 2022

    Free access

    Nacelle cowl tangential restraint

    JOEL JASON F | European Patent Office | 2020

    Free access