Apparatus and method to control forward control surface type air

Aeronautics and astronautics – Aircraft control – Rudders and empennage

Patent

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Details

244 45A, B64C 510

Patent

active

040109208

ABSTRACT:
The control surface-type wing, forward of the center of gravity of the aircraft is placed to be shiftable longitudinally with respect to the center of gravity of the aircraft and also adjustable with respect to a transverse and longitudinal axis of the aircraft to thereby provide for sensitive control of the aircraft flight.

REFERENCES:
patent: 2271226 (1942-01-01), Johnson
patent: 2430793 (1947-11-01), Wells

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