Lightweight aircraft

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244 64, 244 90R, B64C 906, B64C 306, B64C 3104

Patent

active

042068924

ABSTRACT:
An efficient aircraft utilizes a stabilizer spaced from a fixed wing, and supported for controlled rolling about an axis extending generally in a forward direction, to control aircraft yaw. The stabilizer extends generally horizontally in straight forward flight. Pitch of the stabilizer is also controlled.

REFERENCES:
patent: 821393 (1906-05-01), Wright et al.
patent: 1187291 (1916-06-01), Emmons
patent: 1307133 (1919-06-01), Lake
patent: 1839194 (1932-01-01), Blondin
patent: 2681776 (1954-06-01), Howard
patent: 4010920 (1977-03-01), Farner
"American Claims Kremer Man-Power Prize", Flight International, _09/03/77, pp. 676-677.
"Pedal-Powered Plane Flies-80 Feet", Washington PostApr. 22, 1976, p. A4.

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