Hovering aircraft

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 27/10 (2006.01) B64B 1/32 (2006.01) B64C 27/16 (2006.01)

Patent

CA 2272413

In a novel hovering aircraft, an airfoil blade structure rotatable about a vertical axis comprises a set of upper blades (30, 32, 34) and a set of lower blades (36, 38), all having variable lift, the upper blades converging toward the lower blades from root to tip. Struts (84), located inboard of the blade tips, keep the tips of the upper and lower blades separate from each other to reduce interference effects, and also supports motors (74, 76) and propellers.

L'invention concerne un nouvel aéronef, capable de vol stationnaire, et à structure de pales en profil aérodynamique, laquelle tourne autour d'un axe verticale et est faite d'une série de pales supérieures (30, 32, 34) et d'une série de pales inférieures (36, 38) ayant toutes une portance variable, les pales supérieures convergeant vers les pales inférieures de la base au bout de pale. Des jambes de force (84), situées sur l'intérieur et entre les bouts de pale, maintiennent espacés les bouts des pales supérieures et inférieures, pour réduire les effets d'interférence, et portent en outre un moteur (74, 76) et une hélice.

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