Nozzle with thrust vectoring in the yaw direction

Details Nozzle with thrust vectoring in the yaw direction Nozzle with thrust vectoring in the yaw direction

1989-04-11

1990-12-18

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

With means controlling amount, shape or direction of...

23926535, 23926541, 244 23D, 244 52, F02K 112

Patent

active

049780719

ABSTRACT:
A vectorable gas turbine engine exhaust nozzle including deployable angled flow deflectors for providing thrust vectoring in the yaw direction. In one embodiment the deflectors are pivotally deployed in the diverging section of a two dimensional nozzle with the use of either electromechanical or pneumatic rotary actuators. The deflectors are preferably employed in a two dimensional convergent divergent exhaust nozzle which includes a means for varying the size of the throat and a means for providing pitch thrust vectoring.

REFERENCES:
patent: 3666044 (1972-05-01), Killian
patent: 3981451 (1976-09-01), Prior et al.
patent: 4128208 (1978-12-01), Ryan et al.
patent: 4176792 (1979-12-01), McCardle, Jr.
patent: 4219156 (1980-08-01), Schwaerzler
patent: 4245787 (1981-01-01), Freid
patent: 4363445 (1982-12-01), Bouiller et al.
patent: 4456178 (1984-06-01), Jones et al.
patent: 4508270 (1985-04-01), Joubert
patent: 4575006 (1986-03-01), Madden
patent: 4848664 (1989-07-01), Thayer
Popular Science, Feb. 1989, X-31 Fighter, Thrust Vectoring of Pitch and Yaw Plane by Deflection of Exhaust, X--31A Aircraft.
ISABE 87-7061, "Thrust Vectoring--Why and How?", Dr. W. B. Herbst, Thrust Vectoring of Pitch and Yaw Plane by Deflection of Exhaust, X-31A Aircraft.

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