An exhaust nozzle for use with a gas turbine engine includes an outer shroud and a nozzle-plug assembly coupled to the outer shroud. The nozzle-plug assembly includes an inner plug and at least one support vane that is coupled to the outer shroud to support the inner plug in an exhaust nozzle flow path.
EXHAUST NOZZLE WITH VANE SUPPORT STRUCTURE FOR A GAS TURBINE ENGINE
2021-09-02
Patent
Electronic Resource
English
Exhaust nozzle with vane support structure for a gas turbine engine
European Patent Office | 2022
|Turbine engine exhaust nozzle performance
AIAA | 1973
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