A door assembly (10), particularly for doors of passenger aircraft, includes a door frame, a guiding rail (15) mounted at a side edge of the door frame and extending vertically along the door frame, a door having a door body (1), and a latch lever (3). The latch lever (3) has a guiding member (6) attached to a first end portion of the latch lever (3) at a first revolute joint (R1) and a latch lever fulcrum (4) attached to a second end portion of the latch lever at a second revolute joint (R2). The guiding member (6) is received in the guiding rail (15) in a prismatic joint (P1), while the latch lever fulcrum (4) is fixedly connected to the door body (1).


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    Titel :

    AIRCRAFT DOOR ASSEMBLY


    Weitere Titelangaben:

    FLUGZEUGTÜRANORDNUNG
    ENSEMBLE PORTE D'AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    2017-05-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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