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Variable Cycle Intake for Reverse Core EngineA gas generator for a reverse core engine propulsion system has a variable cycle intake for the gas generator, which variable cycle intake includes a duct system. The duct system is configured for being selectively disposed in a first position and a second position, wherein free stream air is fed to the gas generator when in the first position, and fan stream air is fed to the gas generator when in the second position.
Document ID
20160014450
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Suciu, Gabriel L
Chandler, Jesse M
Staubach, Joseph B
Date Acquired
December 5, 2016
Publication Date
November 8, 2016
Subject Category
Aircraft Propulsion And Power
Funding Number(s)
CONTRACT_GRANT: NNX11AB35A
CONTRACT_GRANT: NNX11AB35A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,488,103
Patent Application
US-Patent-Appl-SN-14/142,966

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