Aircraft and water-craft adapted to float on main wing

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 35/00 (2006.01)

Patent

CA 2368566

An aircraft has a fuselage, one or more propellers and a main wing. The wing has a central portion located beneath the fuselage and distal portions which extend outwardly from opposite sides of the fuselage. The wing floats on water when the aircraft is stationary and maintains the fuselage above and out of the water. The aircraft optionally has a tail having a horizontal stabilizer which provides additional support to the fuselage to maintain it out of water. The structure of the aircraft can be adapted for use as a water-craft by reducing the length of the wing.

Un avion se compose d'un fuselage, d'une ou de plusieurs hélices et d'une voilure principale. La voilure est dotée d'une partie centrale sous le fuselage et de parties distales qui se prolongent vers l'extérieur, symétriquement, de chaque côté du fuselage. La voilure flotte sur l'eau lorsque l'avion est immobile et garde le fuselage hors de l'eau. L'avion est muni d'une queue dotée d'un plan fixe horizontal qui offre un soutien supplémentaire au fuselage afin de le garder hors de l'eau. La structure de l'avion peut être adaptée pour être utilisée comme navire en raccourcissant la voilure.

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