Fixed circular wing aircraft

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

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244 122, 244 2, B64C 2900

Patent

active

050466852

ABSTRACT:
A heavier-than-air craft having a cylindrical external configuration comprising a single annular airfoil forming a circumferential lift wing. This fixed circular wing is surrounded by a circular fuselage of substantially the same diameter, closely spaced axially above and below the outer periphery of the annular airfoil, to allow radial air flow over and under substantially the full circumference of the airfoil. The radial air flow is induced through an axial opening in the center of one surface of the circular fuselage by an engine driven propeller, fan or jet effect.

REFERENCES:
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patent: 2990137 (1961-06-01), Willis
patent: 3034747 (1962-05-01), Lent
patent: 3041009 (1962-06-01), Wharton
patent: 3181811 (1965-05-01), Maksim
patent: 3489374 (1970-01-01), Morcom
patent: 3572613 (1971-03-01), Porter
patent: 3785592 (1974-01-01), Kerruish
patent: 3871602 (1975-03-01), Kissinger
patent: 4044972 (1977-08-01), Anker-Holth
patent: 4312483 (1982-01-01), Bostan
patent: 4601444 (1986-07-01), Lindenbaum

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