Aircraft with a ducted fan in a circular wing

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

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Details

244 122, 244 23B, 244 23D, 244 82, 244 45A, B64C 2900, B64C 3906

Patent

active

053038797

ABSTRACT:
The aircraft comprises a rotor with a vertical axis arranged in a housing for generating a lift exceeding the weight of the aircraft. The housing is essentially shaped as a circular wing. A first way of guiding air is provided for controlling the air stream generated by the rotor, by means of which the position of the aircraft can be controlled in hovering flight. From hovering flight, the aircraft can be moved into a cruise flight, where the lift of the aircraft is generated aerodynamically by the circular wing of the housing and its forward thrust by a propeller. For the transition between hovering flight and cruise flight, a second way of guiding air is provided for controlling the pitch of the aircraft. The structure for the second way of guiding air is arranged outside a zone defined by the air stream of the rotor.

REFERENCES:
patent: 1959270 (1934-05-01), Hedlof
patent: 2717131 (1955-09-01), Barrett
patent: 2843339 (1958-07-01), Streib
patent: 2989269 (1961-06-01), Le Bel
patent: 3049320 (1962-08-01), Fletcher
patent: 3282534 (1966-11-01), Serriades
patent: 3335977 (1967-08-01), Meditz
patent: 4037807 (1977-07-01), Johnston et al.
patent: 4196877 (1980-04-01), Mutrux
patent: 4828203 (1989-05-01), Clifton et al.
patent: 5039031 (1991-08-01), Valverde
patent: 5064143 (1991-11-01), Bucher

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