An aircraft door hinge assembly, comprising a door with an outer skin and a frame provided with at least one lug; a fuselage frame provided with at least one clevis configured to be pivotally attached to the lug with a hinge pin so that the door is pivotable relative to the fuselage door frame about a hinge line; a rotatable filler pivotally mounted, at a proximal end, within a gap provided by the clevis; and, a fixed filler having a proximal end fixedly attached to an outermost surface of the lug adjacent to the hinge line, and having a distal end configured to overlap the distal end of the rotatable filler, such that the fixed filler limits of rotation of the rotatable filler.


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    Titel :

    AIRCRAFT DOOR HINGE ASSEMBLY


    Beteiligte:
    HEEREN JENS (Autor:in)

    Erscheinungsdatum :

    2018-10-04


    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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