A nacelle for an aircraft engine comprising a first fan cowl and a second fan cowl , each fan cowl comprising a hinged end and a closing end , each fan cowl being mobile between a closed operating position and an open maintenance position, the first fan cowl having a larger angular coverage than the second fan cowl, the first fan cowl comprising an upper part connected to a lower part by an intermediate hinge so as to allow the lower part to fold towards the upper part.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT ENGINE NACELLE WITH ASYMMETRIC FAN COWLS


    Beteiligte:
    SCHMITTER OPHÉLIE (Autor:in) / KIOUA HAZEM (Autor:in) / GARDEL ROMAIN (Autor:in) / LEMOINE DAMIEN (Autor:in)

    Erscheinungsdatum :

    24.02.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



    Aircraft engine nacelle with asymmetric fan cowls

    SCHMITTER OPHÉLIE / KIOUA HAZEM / GARDEL ROMAIN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    HOOK LATCH FOR AIRCRAFT NACELLE COWLS

    RENARD LAURENT | Europäisches Patentamt | 2024

    Freier Zugriff

    NACELLE FOR TURBOJET ENGINE, COMPRISING OPENINGS OF FRONT COWLS FOR ACCESS TO FIXING POINTS OF THE NACELLE

    BOILEAU PATRICK / CARUEL PIERRE | Europäisches Patentamt | 2020

    Freier Zugriff

    Nacelle for turbojet engine, comprising openings of front cowls for access to fixing points of the nacelle

    BOILEAU PATRICK / CARUEL PIERRE | Europäisches Patentamt | 2022

    Freier Zugriff

    Aircraft engine pylon having a movable assembly of cowls

    PAUTIS OLIVIER / MESSINA PAOLO | Europäisches Patentamt | 2024

    Freier Zugriff