A door assembly (10), particularly for doors of passenger aircraft, includes a door frame, a door having a door body (1), a guiding rail (15) mounted at a side beam of the door frame and extending vertically along the door frame, and a linkage mechanism (17) coupled between the door frame and the guiding rail. The linkage mechanism is configured to retract and extend the guiding rail perpendicular to the vertical extension of the guiding rail along the door frame.


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    Title :

    AIRCRAFT DOOR ASSEMBLY


    Additional title:

    FLUGZEUGTÜRANORDNUNG
    ENSEMBLE PORTE D'AÉRONEF


    Contributors:

    Publication date :

    2017-05-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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