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Convertible Gas-Turbine EnginesConvertible engine aircraft gas-turbine is two engines in one. Produces turbofan thrust, turboshaft power, or any combined thrust and shaftpower continously while operating up to full speed. Used to power vertical/short-takeoff-and-landing (V/STOL) airplanes and advanced high-speed rotorcraft. Rotorcraft shows use of convertible engines rather than separate engines for rotor power and forward thrust affords advantages in installation and save 16 percent in fuel and 20 percent in direct operating costs. Engine used for propulsion of new high-speed rotorcraft that needs both thrust and shaft power. Also used to cross-couple fans of two-engine V/STOL aircraft.
Document ID
19880000542
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Abdalla, K. L.
(NASA Lewis Research Center, Cleveland, OH.)
Mcardle, J. G.
(NASA Lewis Research Center, Cleveland, OH.)
Lindsay, H.
(General Electric Co.)
Date Acquired
August 13, 2013
Publication Date
November 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 10
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-14597
ISSN: 0145-319X
Report Number: LEW-14597
Accession Number
88B10542
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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