A hinge assembly for use with a door, in particular, an aircraft door, that enables the door to remain substantially parallel to the fuselage of the aircraft when the door is open and closed. The hinge assembly includes a door support assembly that couples to the door, and a hinge arm assembly. The hinge arm assembly includes a first gear assembly that couples to the fuselage, a second gear assembly that couples the hinge arm assembly to the door support assembly, and a linkage assembly coupled to the first and second gear assemblies. The first and second gear assemblies and linkage assembly cooperate to move the door support assembly and hinge arm assembly with respect to each other.


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    Titel :

    AIRCRAFT DOOR HINGE ASSEMBLY


    Weitere Titelangaben:

    SCHARNIERBAUGRUPPE FÜR FLUGZEUGTÜREN
    ENSEMBLE CHARNIÈRE DE PORTE D'AVION


    Beteiligte:
    CLAUSEN CHARLES (Autor:in) / FEATHERS JEFF (Autor:in) / KELEHER ANDREW (Autor:in)

    Erscheinungsdatum :

    2018-07-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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