An exhaust system or nozzle for use in a gas turbine engine is disclosed herein. The exhaust system is adapted to adjust various streams of pressurized air produced by the gas turbine engine to control operation of the gas turbine engine.
HYBRID EXHAUST NOZZLE
2017-05-25
Patent
Elektronische Ressource
Englisch
IPC: | F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS |
Exhaust nozzle test techniques
AIAA | 1964
|Mertsheimer's variable exhaust nozzle
Engineering Index Backfile | 1891
Vectoring exhaust nozzle technology
AIAA | 1984
|Improved locomotive exhaust nozzle
Engineering Index Backfile | 1915
|