An aircraft turbine engine assembly including a nacelle structure with a strut attachment zone, a first cover forming an air intake lip, a hinged cover arranged on the nacelle upper portion, between the first cover and the attachment zone, a hinge system of the cover comprising, on either side of a mid-plane of the nacelle, a front rod and a rear rod that are one in front of the other. The two ends of each rod are co-planar, parallel to the mid-plane. A first end of each rod is hinged on the cover. A second end of each rod is hinged on the structure. A locking system is actuatable from the outside of the nacelle between a locked and an unlocked positon. The nacelle comprises at least one cylinder with a first end mounted hinged on the structure and the other end mounted hinged on the cover.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft turbine engine assembly comprising a hinged cover


    Contributors:

    Publication date :

    2022-02-15


    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



    Aircraft turbine engine assembly comprising a hinged cover

    LABARTHE CHRISTOPHE / GELIOT JEAN | European Patent Office | 2020

    Free access

    AIRCRAFT TURBINE ENGINE ASSEMBLY COMPRISING A HINGED COVER

    COMBES STÉPHANE / GELIOT JEAN | European Patent Office | 2020

    Free access

    Aircraft nacelle comprising a cover with two hinged flaps

    LABARTHE CHRISTOPHE / GELIOT JEAN | European Patent Office | 2020

    Free access

    Pool cover hinged sliding assembly

    BARLOCKER DANIEL / DALTON MATHEW | European Patent Office | 2024

    Free access

    POOL COVER HINGED SLIDING ASSEMBLY

    BARLOCKER DANIEL / DALTON MATHEW | European Patent Office | 2024

    Free access