Hybrid aircraft

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 3/42 (2006.01) B64C 3/38 (2006.01) B64C 27/22 (2006.01) B64C 27/26 (2006.01)

Patent

CA 2572929

A hybrid aircraft (1) comprising an elongated fuselage (2), a rotor (3) having rotor blades (7) and a wing part (4) projecting from each side of the fuselage (2), is disclosed. Each wing part (4) is arranged rotatable about its longitudinal axis to the fuselage (2).

Cet aéronef hybride (1) comprend un fuselage de forme allongée (2), un rotor (3) pourvu de pales (7), et une voilure fixe à ailes (4) dépassant de chaque côté du fuselage. Chaque aile (4) de la voilure est montée sur le fuselage (2) rotative autour de son axe longitudinal.

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