Aircraft with circular wing

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane and fluid sustained

Patent

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Details

244 23C, 244 39, 244 52, B64C 2904, B64C 1706

Patent

active

043124836

ABSTRACT:
An aircraft is provided with a circular wing member which is rotatably mounted to a fuselage member. The circular wing member provides lift for horizontal flight and also provides gyroscopic stabilization of aircraft attitude. The circular wing member is substantially free of aerodynamically active flight control or propulsion members and, in a preferred embodiment, has a concentration of mass at its outer rim. The fuselage is provided with propulsion means for effecting and controlling vertical and horizontal flight. The propulsion means provides horizontal or vertical thrust along vectors which pass through the aircraft center of mass.

REFERENCES:
patent: 989681 (1911-04-01), Woods
patent: 3193214 (1965-07-01), Hollingsworth
patent: 3309041 (1967-03-01), Etchberger
patent: 3321156 (1967-05-01), McMasters
patent: 3514053 (1970-05-01), McGuinness
patent: 3612445 (1971-10-01), Phillips
patent: 3752417 (1973-08-01), Lagace
patent: 3792587 (1974-02-01), Kappus
patent: 3946970 (1976-03-01), Blankenship
patent: 3997131 (1976-12-01), Kling
patent: 4120468 (1978-10-01), Fischer

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