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


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    Title :

    Aircraft door assembly


    Contributors:

    Publication date :

    2020-01-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / E05B LOCKS , Schlösser / E05C Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster , BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS



    AIRCRAFT DOOR ASSEMBLY

    ERBEN JOHANN KONRAD | European Patent Office | 2018

    Free access

    AIRCRAFT DOOR ASSEMBLY

    ERBEN JOHANN KONRAD | European Patent Office | 2017

    Free access

    AIRCRAFT DOOR ASSEMBLY

    ERBEN JOHANN KONRAD | European Patent Office | 2017

    Free access

    AIRCRAFT DOOR ASSEMBLY

    ERBEN JOHANN KONRAD | European Patent Office | 2018

    Free access

    AIRCRAFT DOOR ASSEMBLY

    ERBEN JOHANN KONRAD | European Patent Office | 2017

    Free access