An aircraft door translation hinge assembly connects a passenger door of an aircraft to the aircraft fuselage structure and enables the passenger door to move through a desired opening motion. The opening motion of the passenger door is controlled by a simplified mechanism that utilizes a pair of linkages connected by a cam surface follower that engages in sliding engagement with a cam surface. The simplified mechanism controls a pivoting movement of the passenger door as the passenger door is first opened, and then controls a translation movement of the passenger door as the passenger door is continued to be opened from a passenger door opening in the aircraft fuselage.


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    Titel :

    DOOR TRANSLATION HINGE ASSEMBLY


    Beteiligte:
    MEANS RYAN M (Autor:in) / HUYNH KENNY K (Autor:in) / PETERSON WAYNE H (Autor:in) / FLEMING MICHAEL A (Autor:in)

    Erscheinungsdatum :

    2021-10-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    E05D Scharniere oder andere Aufhängevorrichtungen für Türen, Fenster oder Flügel , HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS, OR WINGS / B64C AEROPLANES , Flugzeuge



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