Thrust augmented spin recovery device

Aeronautics and astronautics – Aircraft – steering propulsion – Fluid

Patent

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Details

244 87, 244 125, B64C 1502

Patent

active

042366844

ABSTRACT:
Yaw control surfaces are provided for a jet propelled aircraft wherein a thrust augmented rudder is disposed above the jet exhaust stream and a thrust rudder tab extends downward therefrom into the jet exhaust stream with these components being cooperatively deflected to thereby generate yawing moments for directional control of the aircraft.

REFERENCES:
patent: 3515361 (1970-06-01), Blackburn
patent: 3523662 (1970-08-01), Rawcliffe
patent: 3669386 (1972-06-01), Jacobs et al.
patent: 3756542 (1973-09-01), Bertin et al.
patent: 3841588 (1974-10-01), Arnold et al.

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