A wing is provided, including a high-lift flap arranged on the wing such that it is movable by means of at least two adjustment mechanisms arranged side-by-side in the spanwise direction of the wing and adjustable by means of a drive device. Each adjustment mechanism includes a first adjustment lever, articulated on a main wing surface via a first pivotal articulation, with the formation of a first rotation axis; a second adjustment lever, articulated on the high-lift flap via a second pivotal articulation, with the formation of a second rotation axis; and a central articulation, linking together the first and the second adjustment levers, with the formation of a third rotation axis. An intermediate articulated part is arranged on at least one of the adjustment mechanisms for coupling the first adjustment lever and the main wing surface, or for coupling the second adjustment lever and the high-lift flap.


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    Titel :

    TRAGFLÜGEL MIT EINER HOCHAUFTRIEBSKLAPPE


    Weitere Titelangaben:

    AEROFOIL COMPRISING A HIGH LIFT FLAP
    SURFACE PORTANTE À VOLET HYPERSUSTENTATEUR


    Beteiligte:
    SCHLIPF BERNHARD (Autor:in) / HUE XAVIER (Autor:in)

    Erscheinungsdatum :

    2019-07-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Deutsch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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