Canard type aircraft

Details Canard type aircraft Canard type aircraft

1977-12-12

1979-07-17

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

244 46, 244214, 244 90R, B64C 504, B64C 510

Patent

active

041613007

ABSTRACT:
The present canard type of aircraft comprises steering rudder elements which are tiltable substantially about the leading edge of each wing of the aircraft, whereby the respective edge of the rudder element extends alongside said leading edge of the respective wing. Another edge of the rudder element extends alongside a surface portion of the fuselage or body of the aircraft in close conformity with said surface portion, but movable relative thereto. A sealing may be inserted between the rudder element and the fuselage in such a manner that said movement is permitted.

REFERENCES:
patent: 2783956 (1957-03-01), Harriss
patent: 2981504 (1961-04-01), Parker
patent: 3447761 (1969-06-01), Whitener et al.
patent: 3478989 (1969-11-01), Bielefeldt
patent: 3718294 (1973-02-01), Krenz

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