Segmented vectoring cruise nozzles

Details Segmented vectoring cruise nozzles Segmented vectoring cruise nozzles

1989-02-08

1990-08-14

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft, heavier-than-air

Fluid sustained

244 23B, 244 125, 23926525, B64C 2900

Patent

active

049480723

ABSTRACT:
A thrust vectoring structure is provided for VSTOL aircraft having a pressurized gas generator and at least one rearward facing outlet with an opening for discharging pressurized gas from the pressurized gas generator. The thrust vectoring structure has a plurality of horizontal dividers extending between the sides of the opening. A front flap is rotatably mounted adjacent the front edge of the dividers and a rear flap is rotatably mounted adjacent the rear edge of the dividers. The flaps are rotatable from a horizontal position to a vertical position. In the horizontal position the pressurized gas is directed

REFERENCES:
patent: 2802333 (1957-08-01), Price et al.
patent: 3081597 (1963-03-01), Kosin et al.

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