Vertical takeoff and landing (VTOL) flying disc

Aeronautics and astronautics – Aircraft – heavier-than-air – Fluid sustained

Patent

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Details

244 122, 244 5, 244 23D, B64C 2900, B64B 120

Patent

active

053519116

ABSTRACT:
A flying disc capable of vertical takeoff, hovering, or powered horizontal flight. The aircraft configuration comprises a circular disc-like airfoil-shaped wing structure having a convex upper surface and a concave lower surface with a leading edge and a trailing edge. At least one thrust-producing unit is attached at each of the leading and trailing edges, respectively. A plurality of other thrust-producing units are mounted symmetrically about the circular wing structure. Each thrust-producing unit has attached thereto a thrust deflector assembly for angularly adjusting the thrust produced by the thrust-producing unit, thereby allowing the aircraft to fly both vertically and horizontally. A substantial volume of helium gas is stored encompassing the inner upper hull of the aircraft, thereby giving the flying disc greater lift capacity. The outer skin of the upper surface consists essentially of a plurality of solar panels for delivering power to a multiplicity of devices.

REFERENCES:
patent: 2933891 (1960-04-01), Britt
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patent: 3503573 (1970-03-01), Modesti
patent: 3525484 (1970-08-01), Mueller
patent: 3915411 (1975-10-01), Surbaugh
patent: 4014483 (1977-03-01), MacNeill
patent: 4023751 (1977-05-01), Richard
patent: 4214720 (1980-07-01), DeSautel
patent: 4433819 (1984-02-01), Carrington
patent: 4799629 (1989-01-01), Mori
patent: 4824048 (1989-04-01), Kim
patent: 5064143 (1991-11-01), Bucher

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