B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 27/22 (2006.01) B64C 39/06 (2006.01)
Patent
CA 2199278
A circular wing aircraft (10) in the form of a helicopter (12) comprising a fuselage (14) and a circular wing assembly (16). A structure (18) is for mounting the circular wing assembly (16) above the fuselage (14) in a stationary manner. An air impeller unit (20) is rotatively carried within the circular wing assembly (16). A device (22) is for driving the air impeller unit (20) to rotate about a central axis (24) within the circular wing assembly (16), so as to provide lift and flight movement while yaw control is maintained.
L'invention se rapporte à un aéronef à ailes circulaires (10) se présentant sous forme d'un hélicoptère (12) comprenant un fuselage (14) et un ensemble aile circulaire (16). Une structure (18) permet la fixation de l'ensemble aile circulaire (16) au-dessus du fuselage (14). Une roue à aubes pneumatique (20) est montée rotative à l'intérieur de l'ensemble aile circulaire (16). Un dispositif (22) est destiné à entraîner la roue à aubes pneumatique (20) pour qu'elle tourne autour d'un axe central (24) à l'intérieur de l'ensemble aile circulaire (16), de manière à assurer la sustentation et le déplacement en vol tout en maintenant le contrôle en lacet.
Mcfadden Fincham
Vass Gabor I.
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