A system (1) comprising a door assembly (5) configured to be installed within an aircraft galley, the door assembly (5) including: a door body (7) which is moveable between a closed position and an open position; and a primary latch mechanism (9) configured to secure the door body (7) in the closed position. The primary latch mechanism (9) is moveable between a latched position, a neutral position and an unlatched position. The primary latch mechanism (9) includes: a rotatable plate (13), an electrically operated actuator (17) mechanically coupled to the rotatable plate (13) and configured to rotate the rotatable plate (13), a handle (15) mechanically coupled to the rotatable plate (13) and configured to rotate the rotatable plate (13), and a latching rod (11a) coupled to the rotatable plate, wherein the rotatable plate (13) is configured to convert a rotational movement into linear movement of the latching rod (11a) such that the door assembly (5) may be latched and unlatched.


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    Title :

    AUTOMATIC PRIMARY LATCH MECHANISM


    Additional title:

    AUTOMATISCHER PRIMÄRVERRIEGELUNGSMECHANISMUS
    MECANISME DE VERROUILLAGE PRIMAIRE AUTOMATIQUE


    Contributors:

    Publication date :

    2024-05-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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



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