A connection for mounting an aircraft engine to an aircraft pylon includes a plate to be connected to a portion of an engine, and a body that extends rearward from the plate. A back-up connection, including a pin positioned within a slotted hole, is provided between the portion of the engine and the body. When there is a normal connection between the plate and the body, there is clearance between the pin and the slotted hole.


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    Titel :

    GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATHS


    Weitere Titelangaben:

    MONTAGESTRUKTUR MIT SEKUNDÄREN LASTPFADEN FÜR EINEN GASTURBINENMOTOR
    STRUCTURE DE MONTAGE DE MOTEUR À TURBINE À GAZ DOTÉE DE CHEMINS DE CHARGE SECONDAIRES


    Beteiligte:
    ZHENG ZHIJUN (Autor:in) / SANDY DAVID F (Autor:in)

    Erscheinungsdatum :

    21.12.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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