Aircraft

Details Aircraft Aircraft

B - Operations, Transporting

64

C

B64C 3/10 (2006.01) B64C 39/06 (2006.01)

Patent

CA 2129803

ABSTRACT OF THE DISCLOSURE An aircraft (10, 10' or 50) capable of sustained flight including a fuselage (12 or 52) and a spiral-formed flat-section right hand and left hand wing (14 and 16) positioned in generally horizontally opposing relation along either side of the fuselage. Each wing is formed of an elongated flat panel or plate having generally parallel leading (14c and 16c) and trailing edges (14d and 16d), the length of the panel being substantially greater than its width, the width being substantially greater than its thickness. The forward (14a and 16a) and rearward(14b and 16b) ends of each wing are movably connected within forward and rearward longitudinal channels of the fuselage. By appropriate controlled linearand rotational movement of the wing ends, in combination with a conventional rudder (20) of an upright rear stabilizer fin (18) of the fuselage, all aerodynamic flight path variable control is accomplished. Both single (14 and 16) and multiple (54 and 56) spiral-turned wings are provided.

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