Support for a translating nozzle vectoring ring

Details Support for a translating nozzle vectoring ring Support for a translating nozzle vectoring ring

1991-05-10

1992-12-29

Shaver, Kevin P.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

23926519, 23926539, 60228, 60232, B64C 1500

Patent

active

051745020

ABSTRACT:
The present invention provides support for a vectoring ring used to pivot flaps in a gas turbine engine thrust vectoring nozzle. The ring support transfers at least a portion of the side loads acting generated by a gas turbine engine thrust vectoring nozzle to a relatively stationary portion of the engine. The support includes apparatus that provides for allowing two degree of freedom (2 DOF) pivoting or gimballing motion and axial translation of the vectoring ring.

REFERENCES:
patent: 3319892 (1967-05-01), Zirin
patent: 4128208 (1978-12-01), Ryan et al.
patent: 4176792 (1979-12-01), McCardle
patent: 4245787 (1981-01-01), Freid
patent: 4456178 (1984-06-01), Jones et al.
patent: 4508270 (1985-04-01), Joubert
patent: 4994660 (1991-02-01), Hauer
patent: 5076496 (1991-12-01), Lippmeier
patent: 5082182 (1992-01-01), Bruchez, Jr.

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