Gas turbine spherical exhaust nozzle

Details Gas turbine spherical exhaust nozzle Gas turbine spherical exhaust nozzle

1989-10-26

1991-02-19

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle with jacketed or hollow...

With subsequent mixing in main discharge stream in or...

23926535, 23926537, 60232, F02K 112

Patent

active

049936417

ABSTRACT:
A spherical exhaust nozzle for a gas turbine engine having gimbal mounted convergent-divergent flaps in which cooling air for the flaps is ducted through the convergent flap pivots and the convergent flaps are actuated by actuators connected to the gimbal structure.

REFERENCES:
patent: 4363445 (1982-12-01), Bouiller et al.
patent: 4544098 (1985-10-01), Warburton
patent: 4801087 (1989-01-01), Woodard
patent: 4836451 (1989-06-01), Herrick et al.
patent: 4848664 (1989-07-01), Thayer
patent: 4878617 (1989-11-01), Novotny

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