A mounting system (30) for attaching a gas turbine engine (32) to a pylon (34) of an aircraft. The mounting system comprises a first frame (36) of three elongate members (38) arranged in a triangle. The first frame is arranged such that a core of the gas turbine engine is positioned extending through the area defined between the three elongate members. The first frame forms at least part of a load bearing connection between the pylon and gas turbine engine. The first frame consists of two portions (62,64), one corresponding to each side of the gas turbine engine when attached to the pylon. The triangle is symmetrical about a plane separating the two portions of the first frame.


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    Titel :

    Engine mount


    Weitere Titelangaben:

    Triebwerksaufhängung
    Structure d'accrochage d'un moteur


    Beteiligte:
    STRETTON RICHARD (Autor:in) / UDALL KENNETH (Autor:in)

    Erscheinungsdatum :

    05.09.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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