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Turbofan engine with a low pressure turbine driven supercharger in a bypass duct operated by a fuel rich combustor and an afterburnerA multiple bypass turbofan engine includes a core Brayton Cycle gas generator with a fuel rich burning combustor and is provided with a variable supercharged bypass duct around the gas generator with a supercharging means in the supercharged bypass duct powered by a turbine not mechanically connected to the gas generator. The engine further includes a low pressure turbine driven forward fan upstream and forward of an aft fan and drivingly connected to a low pressure turbine by a low pressure shaft, the low pressure turbine being aft of and in serial flow communication with the core gas generator. A fan bypass duct is disposed radially outward of the core engine assembly and has first and second inlets disposed between the forward and aft fans. An inlet duct having an annular duct wall is disposed radially inward of the bypass duct and connects the second inlet to the bypass duct. A supercharger means for compressing air is drivingly connected to the low pressure turbine and is disposed in the inlet duct. A secondary combustor or augmentor is disposed in an exhaust duct downstream of and in fluid flow communication with the bypass duct and the gas generator.
Document ID
20080004542
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Bartos, James W.
Date Acquired
August 24, 2013
Publication Date
February 9, 1999
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: US-PATENT-5,867,980
Patent Application Number: US-PATENT-APPL-SN-767932
Funding Number(s)
CONTRACT_GRANT: NAS3-26051
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,867,980
Patent Application
US-PATENT-APPL-SN-767932
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