An aerial vehicle including at least two side fuselages interconnected via a wing, at least one propulsion mechanism, and two side wings extending from respective ones of the side fuselages. Each side wing has a section as seen from the front that is in the shape of a polygon having at least four sides. The ratio between the height of the side wings and the wingspan of the aerial vehicle is between 0.15 to 0.25. Each side wing has a first wing portion extending in the same plane as the wing, a second wing portion extending vertically above the first wing portion and inclined rearwards and upwards, a third wing portion extending parallel to the first wing portion and extending rearwards while forming an angle with the front plane of the aerial vehicle, and a fourth wing portion extending vertically down to the rear end of the side fuselage.


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    Titel :

    Aircraft With Polygonal Wings


    Beteiligte:

    Erscheinungsdatum :

    2017-04-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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