Sync-ring assembly for a gas turbine engine exhaust nozzle

Details Sync-ring assembly for a gas turbine engine exhaust nozzle Sync-ring assembly for a gas turbine engine exhaust nozzle

1991-09-23

1993-08-31

Bertsch, Richard A.

Power plants

Reaction motor

With thrust direction modifying means

60230, 60271, 23926535, F02K 100, F02K 154

Patent

active

052398153

ABSTRACT:
A sync-ring assembly for use on a axisymmetric gas turbine exhaust nozzle, the sync-ring having a semi-spherical outward surface received within and slidably contacting the cylindrical inner surface of a liner. The sync-ring runs along guide tracks mounted to the case of the nozzle, and is positioned along the liner and rotated with respect to the liner by a plurality of actuators pivotably connected to the sync-ring.

REFERENCES:
patent: 3658253 (1972-04-01), Steffen
patent: 3814325 (1974-06-01), McCardle, Jr. et al.
patent: 3988889 (1976-11-01), Chamay et al.
patent: 4141501 (1979-02-01), Nightingale
patent: 5082182 (1992-01-01), Bruchez, Jr. et al.

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