Yaw vectoring blade

Details Yaw vectoring blade Yaw vectoring blade

1992-05-11

1993-11-16

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

23926535, 244 23D, 244 52, F02K 112

Patent

active

052616045

ABSTRACT:
A yaw vectoring blade which is alternatively recessed from and extended into an airflow path of an exhaust nozzle of an aircraft gas turbine engine. The yaw vectoring blade is provided with a housing cavity located in a divergent flap of the exhaust nozzle which provides a recess from the airflow path. Actuating means connected to the yaw vectoring blade can move the yaw vectoring blade into and out of the airflow path to produce a desired yawing moment.

REFERENCES:
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patent: 3743184 (1973-07-01), Mancus
patent: 3979067 (1976-09-01), Nash
patent: 4000854 (1977-01-01), Konarski et al.
patent: 4266725 (1981-05-01), Schweikl et al.
patent: 4280660 (1981-07-01), Wooten, Jr. et al.
patent: 4848664 (1989-07-01), Thayer
patent: 4978071 (1990-12-01), MacLean et al.
patent: 5154050 (1992-10-01), Herup et al.

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