Variable configuration exhaust discharge opening for a jet propu

Details Variable configuration exhaust discharge opening for a jet propu Variable configuration exhaust discharge opening for a jet propu

1979-09-24

1987-01-27

Bentley, Stephen C.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

23926537, F02K 109

Patent

active

046389466

ABSTRACT:
A gas turbine jet propulsion engine has a rectangular exhaust gas outlet 14. A pair of U-shaped tracks 21,22 one on each side of the outlet and which extend downstream of it, support rollers carrying the plates 24a etc. of a pair of articulated deflectors 24,26, one above and one below the outlet. The deflectors are translatable along the tracks between the final exhaust discharge opening of the engine. The configurations include a convergent divergent nozzle, a thrust vectoring nozzle and thrust reversing outlets.

REFERENCES:
patent: 3519207 (1970-07-01), Clough
patent: 3642209 (1972-02-01), Stahl
patent: 3704829 (1972-12-01), Hall
patent: 4088270 (1978-05-01), Maiden
patent: 4175385 (1979-11-01), Nash

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