A door assembly, particularly for doors of passenger aircraft, includes a door frame, a door having a door body hingedly installed in the door frame, at least one hooking pintle (4) attached to the door frame or an edge of the door body extending along a pintle axis, and at least one door latch (2) connected to an edge of the door body or the door frame, respectively, the door latch having a substantially C-shaped latch body (2a) configured to rotate around an axis parallel to the pintle axis of the hooking pintle (4). The door assembly further includes a bistable latch and hook mechanism configured to catch the door latch (2) in hooking engagement with the hooking pintle (4) and to retain the door latch (2) in a direction perpendicular to the door body in an overcenter position.


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    Title :

    AIRCRAFT DOOR ASSEMBLY


    Additional title:

    FLUGZEUGTÜRANORDNUNG
    ENSEMBLE PORTE D'AÉRONEF


    Contributors:

    Publication date :

    2018-06-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / E05B LOCKS , Schlösser



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