Thrust vectoring nozzle assembly

Details Thrust vectoring nozzle assembly Thrust vectoring nozzle assembly

1990-03-01

1991-02-19

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

23926519, 23926539, 60230, F02K 152, F02K 146, F02K 178

Patent

active

049936387

ABSTRACT:
An exhaust nozzle assembly for vectoring the thrust of the exhaust gases from a turbojet engine is disclosed wherein the exhaust gases are vectored by an assembly that is separate from the flaps that are utilized to adjust the cross-sectional area of the exhaust nozzle. The thrust vectoring exhaust nozzle assembly has a moveable thrust vectoring assembly comprised of inner and outer vectoring members, each of which have a generally annular configuration. The vectoring members are pivotally attached to the exhaust nozzle so as to pivot about an axis extending generally perpendicularly to the longitudinal axis of the exhaust duct.

REFERENCES:
patent: 3130544 (1964-04-01), Penza
patent: 3912202 (1975-10-01), Jenkins
patent: 4363445 (1982-12-01), Bouiller et al.
patent: 4508270 (1985-04-01), Joubert
patent: 4778109 (1988-10-01), Jourdain et al.
patent: 4809932 (1989-03-01), Muller

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