Aircraft

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

Patent

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Details

244 23C, 244 1719, 416114, B64C 2722, B64C 312

Patent

active

041968778

ABSTRACT:
An aircraft comprising a generally annular wing structure surrounding a circular central structure to form an annular air duct, a pair of fuselages extending longitudinally at opposite sides of the aircraft, and rotor blades extending radially across the air duct from the central structure and rotatable relative to the central structure around the duct for inducing airflow through the duct to effect a lift on the aircraft. The annular wing structure consists of forward and rear wings forming air foils, the forward wing having a generally semicircular trailing edge and the rear wing having a generally semicircular leading edge.

REFERENCES:
patent: 1968497 (1934-07-01), Magalis
patent: 2074805 (1937-03-01), Platt
patent: 2410545 (1946-11-01), Main
patent: 2876964 (1959-03-01), Streib
patent: 3002709 (1961-10-01), Cochran
patent: 3253805 (1966-05-01), Taylor
patent: 3456902 (1969-07-01), Visconti
patent: 3640485 (1972-02-01), Mutrux

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