Methods, apparatus, systems and articles of manufacture are disclosed. An apparatus for mounting a gas turbine engine to a pylon, the gas turbine including an upstream section and a downstream section, the gas turbine defining a roll axis, a yaw axis, and a pitch axis, the apparatus including: a first mount to couple the upstream section of the gas turbine engine to the pylon; a second mount to couple the upstream section of the gas turbine engine to the pylon, the second mount downstream of the first mount; a thrust linkage to couple the upstream section to the pylon, wherein the downstream section is decouplable from the upstream section without decoupling the first mount, the second mount, and the thrust linkage.


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    Titel :

    METHODS AND APPARATUS FOR MOUNTING A GAS TURBINE ENGINE


    Weitere Titelangaben:

    TRIEBWERKSAUFHÄNGUNG UND MONTAGEMETHODE
    PROCÉDÉS ET APPAREIL POUR MONTER UN MOTEUR À TURBINE A GAZ



    Erscheinungsdatum :

    2024-07-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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