Axisymmetric vectoring exhaust nozzle

Details Axisymmetric vectoring exhaust nozzle Axisymmetric vectoring exhaust nozzle

1989-04-11

1991-02-19

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

23926519, 23926535, 23926539, 60228, 60230, 60232, 244 23D, 244 52, B64C 1506

Patent

active

049946609

ABSTRACT:
A thrust vectoring axisymmetric convergent divergent variable exhaust nozzle is provided with a universally pivoting joint between the divergent and convergent flaps and actuating the linkage mechanisms for changing the divergent nozzle section from axisymmetrical to asymmetrical by pivoting the divergent flaps in the radial and tangential directions with respect to the axisymmetric nozzle centerline in a controlled manner.

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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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