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Unducted-Fan EngineUnducted-fan (UDF(TM) engine advanced counterrotating-pusher-propeller propulsion system for high-subsonic (mach 0.7 to 0.85) aircraft. Combines modern high-pressure-ratio gas-turbine engine with multistage counterrotating power turbine directly coupled to counterrotating, advanced high-speed propellers. Key feature of system is unique direct turbine drive eliminating need for gearbox to transmit power to propeller blades.
Document ID
19870000495
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Meleason, Edward T.
(NASA Lewis Research Center, Cleveland, Ohio.)
Johnson, K. O.
(General Electric Co.)
Date Acquired
August 13, 2013
Publication Date
October 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 9
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-14429
ISSN: 0145-319X
Report Number: LEW-14429
Accession Number
87B10495
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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