Supersonic nozzle, in particular for a turbojet engine

Details Supersonic nozzle, in particular for a turbojet engine Supersonic nozzle, in particular for a turbojet engine

1982-11-24

1996-08-06

Bently, Stephen C.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

F02K 112

Patent

active

055426077

ABSTRACT:
A turbojet engine has an outlet duct to which an annular array of actuating cylinders for nozzle flaps are hinged. The housings for the cylinders are connected together by transverse members to form a rigid structure coaxial with the outlet duct. The arrangement includes convergent flaps and slaving devices for divergent flaps, all hinged to the rigid structure and particularly to the housings.

REFERENCES:
patent: 3786992 (1974-01-01), Robinson
patent: 3837580 (1974-09-01), Camboulives et al.
patent: 3954225 (1976-05-01), Camboulives et al.
patent: 4000854 (1977-01-01), Konarski et al.
patent: 4128208 (1978-12-01), Ryan et al.

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