An aircraft, in particular an unmanned aerial vehicle with wing-borne flight mode and hover flight mode, comprises a wing structure (4) having a left (6), middle (7), and right wing section (8). A support structure extends from the wing structure (4), and has an upper and lower support section. Each one of the left and right wing section (6, 8), and upper and lower support section (18, 20) has a thrust unit (10, 12, 22, 24). Left and right wingtip sections are rotatable relative to a left and right wing base section, respectively, around an axis extending substantially in a lengthwise direction of the wing structure. The thrust units (10,12) of the left and right wing sections(6, 8) are provided at the respective wingtip sections, in particular at the extremities thereof.


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    Titel :

    AIRCRAFT WITH WING-BORNE FLIGHT MODE AND HOVER FLIGHT MODE


    Beteiligte:
    HULSMAN SANDER (Autor:in) / DE GROOT JURJEN (Autor:in) / MILIS MAARTEN (Autor:in) / DOKTER DIRK LUCAS EDUARD (Autor:in) / BOUMAN JOOST LEON (Autor:in) / KNOOPS RUUD (Autor:in)

    Erscheinungsdatum :

    03.08.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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