An engine assembly for an aircraft, comprising an engine mounting pylon comprising a primary structure forming a box closed by a front closing rib, a front engine mount comprising at least two connecting link rods that are disposed laterally on either side of the box and each comprise a first end mounted on a first fitting of the casing. The rib forms a part of the front mount, comprising at least one transverse fitting made in one piece so as to close a front end of the box and to have lugs protruding laterally on each side of the box, each lug being provided with a first orifice for mounting a second end of one of the link rods.


    Access

    Download


    Export, share and cite



    Title :

    ENGINE ASSEMBLY FOR AN AIRCRAFT, COMPRISING A FRONT ENGINE MOUNT INCORPORATED WITH THE BOX OF THE MOUNTING PYLON


    Contributors:

    Publication date :

    2018-10-25


    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



    Assembly comprising aircraft turbine engine and mounting pylon therefor

    GLEMAREC GUILLAUME / VIGUES JEAN-BAPTISTE / GENTILS ROMUAD MURIEL et al. | European Patent Office | 2023

    Free access

    Assembly for an aircraft, the assembly comprising a pylon and a front engine mount

    DEFORET THOMAS / PUECH JACKY | European Patent Office | 2020

    Free access

    ASSEMBLY FOR AN AIRCRAFT, THE ASSEMBLY COMPRISING A PYLON AND A FRONT ENGINE MOUNT

    DEFORET THOMAS / PUECH JACKY | European Patent Office | 2020

    Free access

    Aircraft engine pylon to wing mounting assembly

    CASTELLI ALBERTO DEI / FERREIRA CLOVIS AUGUSTO EÇA / MONTORO WANDERLEY et al. | European Patent Office | 2018

    Free access

    Aircraft engine pylon to wing mounting assembly

    DA SILVA JULIO ANTONIO BELTRAMI / FERREIRA CLOVIS AUGUSTO EÇA / MONTORO WANDERLEY et al. | European Patent Office | 2018

    Free access