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.


    Access

    Download


    Export, share and cite



    Title :

    Engine mount


    Additional title:

    Triebwerksaufhängung
    Structure d'accrochage d'un moteur


    Contributors:

    Publication date :

    2018-09-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Engine-mount

    European Patent Office | 2023

    Free access

    Engine mount

    KIM SEUNG WON | European Patent Office | 2019

    Free access

    ENGINE MOUNT

    STRETTON RICHARD GEOFFREY / UDALL KENNETH FRANKLIN | European Patent Office | 2016

    Free access

    ENGINE MOUNT

    European Patent Office | 2024

    Free access

    ENGINE MOUNT

    KIM SEUNG WON | European Patent Office | 2021

    Free access