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Gas Turbine Engine Having Fan Rotor Driven by Turbine Exhaust and with a BypassA gas turbine engine has a core engine incorporating a core engine turbine. A fan rotor is driven by a fan rotor turbine. The fan rotor turbine is in the path of gases downstream from the core engine turbine. A bypass door is moveable from a closed position at which the gases from the core engine turbine pass over the fan rotor turbine, and moveable to a bypass position at which the gases are directed away from the fan rotor turbine. An aircraft is also disclosed.
Document ID
20160007316
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Suciu, Gabriel L.
Chandler, Jesse M.
Date Acquired
June 8, 2016
Publication Date
May 31, 2016
Subject Category
Aircraft Propulsion And Power
Funding Number(s)
CONTRACT_GRANT: NNX11AB35A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,352,843
Patent Application
US-Patent-Appl-SN-13/731,371

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