An aircraft wing system and method comprising: an aircraft wing (102); an edge device (200) coupled to a leading edge or trailing edge of the aircraft wing (102); a drive shaft (804) rotatable about its axis; a crank arm (808, 810), a first end of the crank arm (808, 810) being coupled to the drive shaft (804), and a second end of the crank arm (808, 810) opposite to the first end being coupled to the edge device (200); and a gear system (806) (e.g. a strain wave gear system) coupled between the drive shaft (804) and the first end of the crank arm (808, 810).


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    Titel :

    AIRCRAFT WING SYSTEM


    Weitere Titelangaben:

    FLUGZEUGFLÜGELSYSTEM
    SYSTEME D'AILE D'AERONEF


    Erscheinungsdatum :

    2016-12-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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