Double-curved aircraft door having a pair of stops in contact over a contact area. The isobarycentre (31A) of each contact area of a first lateral edge is substantially arranged in a first plane perpendicular to the longitudinal axis (21) and the same applies to a second lateral edge. For each contact area, the normal to the contact area passing through its isobarycentre (31A, 31B) substantially passes through the axis (41) of a medium cylinder (42). For each contact area, the normal to the contact area passing through its isobarycentre (31A, 31B) forms a deflection angle with a plane perpendicular to the longitudinal axis (21), the deflection angles of all the contact areas being equal.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    DOUBLE-CURVED AIRCRAFT DOOR WITH OPTIMISED LOCKING MEANS


    Beteiligte:

    Erscheinungsdatum :

    24.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Double-curved aircraft door with optimised locking means

    DEVILLEZ SÉBASTIEN / DUCASSE JEAN FRANCOIS | Europäisches Patentamt | 2025

    Freier Zugriff

    AIRCRAFT DOOR LOCKING SYSTEM AND AIRCRAFT DOOR ARRANGEMENT

    POPPE ANDREAS / PAPENROTH UWE | Europäisches Patentamt | 2020

    Freier Zugriff

    Aircraft door locking system and aircraft door arrangement

    POPPE ANDREAS / PAPENROTH UWE | Europäisches Patentamt | 2022

    Freier Zugriff

    Door locking assembly for aircraft

    VAISSIERE AURELIEN / RENARD AURELIEN / FRUTET PIERRE et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    LOCKING SYSTEM FOR AN AIRCRAFT DOOR

    PREMRL MIHA | Europäisches Patentamt | 2025

    Freier Zugriff