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Two dimensional gas turbine engine exhaust nozzle

Patent ·
OSTI ID:6776435
;
A two-dimensional variable area gas turbine engine exhaust nozzle is described having thrust reversing capability, the nozzle including spaced apart side wall means and upper and lower flap assemblies connected to the side wall means defining an exhaust gas flow path wihtin the nozzle, the nozzle having a centerline.
Assignee:
United Technologies Corp., Hartford, CT
Patent Number(s):
US 4753392
OSTI ID:
6776435
Country of Publication:
United States
Language:
English

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Related Subjects

33 ADVANCED PROPULSION SYSTEMS
330103* -- Internal Combustion Engines-- Turbine
DESIGN
DUCTS
ENGINES
EXHAUST SYSTEMS
FINS
FLUID FLOW
GAS FLOW
GAS TURBINE ENGINES
HEAT ENGINES
INTERNAL COMBUSTION ENGINES
NOZZLES
WALLS