The present disclosure relates to a propulsion assembly having a nacelle surrounding a turbojet engine, the nacelle having an upstream structure with an air inlet including an air inlet lip, the air inlet lip defining, with the air inlet lip, an air inlet chamber, the upstream structure being capable of translational movement along an axis parallel to a longitudinal axis of the nacelle, between a closed position and an open position that allows access to the turbojet engine. The propulsion assembly further includes at least one locking/unlocking device allowing and preventing movement of the upstream structure that in one form is fixed to the air inlet lip and to an upstream flange of the turbojet engine.


    Access

    Download


    Export, share and cite



    Title :

    ENSEMBLE PROPULSIF POUR AÉRONEF


    Additional title:

    PROPULSION ASSEMBLY FOR AN AIRCRAFT
    ANTRIEBSBAUGRUPPE FÜR EIN FLUGZEUG


    Contributors:

    Publication date :

    2018-03-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



    ENSEMBLE PROPULSIF POUR AÉRONEF

    CZAPLA LIONEL / VARDELLE EMMANUEL | European Patent Office | 2024

    Free access

    ENSEMBLE PROPULSIF POUR AERONEF

    HURLIN HERVE / CARUEL PIERRE | European Patent Office | 2016

    Free access

    ENSEMBLE PROPULSIF POUR AÉRONEF

    CZAPLA LIONEL / AMARGIER RÉMI | European Patent Office | 2025

    Free access

    ENSEMBLE PROPULSIF POUR AERONEF

    FAUGERAS JOSE | European Patent Office | 2022

    Free access

    ENSEMBLE PROPULSIF POUR AÉRONEF

    CZAPLA LIONEL / VARDELLE EMMANUEL | European Patent Office | 2024

    Free access