A mounting arrangement for mounting an aircraft gas turbine engine to an aircraft. The mounting arrangement comprises an engine nacelle. The engine nacelle comprises a distal assembly comprising a part annular engine cowl, a gas turbine engine core housing surrounded by the engine cowl and a distal bifurcation extending between the engine core housing and engine cowl, the distal bifurcation extending in a first direction to define a first axis. The mounting arrangement further comprises a proximal assembly having a mount configured to mount the proximal assembly to the engine core housing. The proximal assembly further comprises a pylon configured to mount the proximal assembly to mounting location such as a wing of the aircraft at an engine mounting location. The pylon extends in a line between the wing and the engine core housing to define a second axis, wherein the second axis is normal to a distal surface of the wing at the engine mounting location and is non-parallel to the vertical axis.


    Access

    Download


    Export, share and cite



    Title :

    GAS TURBINE ENGINE MOUNT ARRANGEMENT


    Additional title:

    MONTAGEANORDNUNG FÜR EINEN GASTURBINENMOTOR
    AGENCEMENT DE MONTAGE D'UN MOTEUR À TURBINE À GAZ


    Contributors:

    Publication date :

    2020-01-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    GAS TURBINE ENGINE MOUNT ARRANGEMENT

    LIM CHIA HUI / STRETTON RICHARD G / SHEAF CHRISTOPHER T J | European Patent Office | 2020

    Free access

    Geared turbofan engine mount arrangement

    COLES DAVID R / ROWNTREE GAVIN M / WILLSHEE MATTHEW J et al. | European Patent Office | 2022

    Free access

    Geared Turbofan Engine Mount Arrangement

    COLES DAVID R / ROWNTREE GAVIN M / WILLSHEE MATTHEW J et al. | European Patent Office | 2019

    Free access

    GAS TURBINE ENGINE MOUNT

    BOWDEN WILLIAM JOSEPH / COLEMAN JONATHAN EDWARD / TIWARI SHARAD et al. | European Patent Office | 2024

    Free access

    A geared turbofan engine mount arrangement

    European Patent Office | 2018

    Free access