Aerodynamically stable, high-lift, vertical takeoff aircraft

Details Aerodynamically stable, high-lift, vertical takeoff aircraft Aerodynamically stable, high-lift, vertical takeoff aircraft

B - Operations, Transporting

64

C

B64C 29/00 (2006.01)

Patent

CA 2582798

In a preferred embodiment, a vertical takeoff aircraft (100) body having an inverted hemispherical upper portion (120), a generally cylindrical lower portion (142) with a diameter of its upper end slightly greater than a diameter of its lower end but less than a diameter of the lower end of the upper portion (120), and a truncated inverted generally cone-shaped transition portion (140) joining the upper portion (120) and the lower portion (142); and a plurality of vertical columns (150) attached to the aircraft (100) body and spaced apart from the aircraft (100) body, equidistantly disposed about the aircraft (100) body. The present invention also provides novel landing gears (200) for such an aircraft (100) as well as a novel method of adjusting the pitches of rotating blade (160) thereof.

Dans un mode de réalisation préféré, l'invention concerne un corps d'aéronef (100) à décollage vertical présentant une partie supérieure (120) hémisphérique inversée, une partie inférieure (142) généralement cylindrique dont le diamètre de son extrémité supérieure est légèrement plus grand qu'un diamètre de son extrémité inférieure, mais inférieur à un diamètre de l'extrémité inférieure de la partie supérieure (120), et une partie de transition (140) tronconique inversée généralement conique joignant la partie supérieure (120) et la partie inférieure (142); et une pluralité de colonnes verticales (150) fixées au corps d'aéronef (100) et à distance de celui-ci, installées de manière équidistante autour du corps d'aéronef (100). L'invention concerne également de nouveaux trains d'atterrissage (200) conçus pour un tel aéronef (100), ainsi qu'un nouveau procédé permettant de régler les pas de ses pales en rotation (160).

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