Exhaust nozzle assembly for a turbojet engine

Details Exhaust nozzle assembly for a turbojet engine Exhaust nozzle assembly for a turbojet engine

1984-12-19

1987-02-10

Nase, Jeffrey V.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

B64C 938

Patent

active

046417834

ABSTRACT:
An exhaust nozzle assembly for a turbojet engine is described wherein the position of a series of nozzle flaps is controlled by control levels interconnected with an actuating cylinder. The control levers are transversely interconnected in order to synchronize the movement of the flaps and to also permit variation in the transverse distance between adjacent control members. A linkage mechanism is also disclosed which permits the actuation of a second series of flaps from the interconnected control members.

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patent: 3592389 (1971-07-01), Johnson
patent: 3612106 (1971-10-01), Camboulives et al.
patent: 3730436 (1973-05-01), Madden et al.
patent: 3820720 (1974-06-01), Anders et al.
patent: 3837580 (1974-09-01), Camboulives et al.
patent: 4466573 (1984-08-01), Camboulives et al.

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