An aircraft nacelle arrangement includes a compression rod disposed between a first nacelle half and a second nacelle half, wherein the first nacelle half and the second nacelle half are rotatable about a hinge between a closed position and an open position, a compression rod disposed between the first nacelle half and the second nacelle half, and a mounting bracket coupled to an exhaust nozzle flange of the aircraft engine, wherein the compression rod extends through the mounting bracket.


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    Title :

    NACELLE THRUST REVERSER COMPRESSION ROD SUPPORTING SYSTEM


    Additional title:

    DRUCKSTABLAGERUNGSSYSTEM FÜR EINEN GONDELSCHUBUMKEHRER
    SYSTÈME DE SUPPORT DE TIGE DE COMPRESSION D'INVERSEUR DE POUSSÉE DE NACELLE


    Contributors:

    Publication date :

    2024-01-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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