Supersonic nozzle for a turbojet engine

Details Supersonic nozzle for a turbojet engine Supersonic nozzle for a turbojet engine

1981-12-30

1996-10-22

Bentley, Stephen C.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

F02K 112

Patent

active

055668844

ABSTRACT:
Convergent flaps of a jet engine nozzle are controlled by actuating cylinders through actuating levers hinged to the fixed structure of the engine and by connecting rods. Divergent flaps are slaved to the convergent flaps by connecting rods themselves driven by the actuating levers. Cold flaps not hinged to the divergent flaps are slaved to the convergent flaps by further connecting rods connected to the first-named connecting rods.

REFERENCES:
patent: 3899133 (1975-08-01), Camboulives et al.
patent: 3954225 (1976-05-01), Camboulives et al.
patent: 4000854 (1977-01-01), Konarski et al.
patent: 4241876 (1980-12-01), Pedersen

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