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Oil-Free Rotor Support Technologies for an Optimized Helicopter Propulsion SystemAn optimized rotorcraft propulsion system incorporating a foil air bearing supported Oil-Free engine coupled to a high power density gearbox using high viscosity gear oil is explored. Foil air bearings have adequate load capacity and temperature capability for the highspeed gas generator shaft of a rotorcraft engine. Managing the axial loads of the power turbine shaft (low speed spool) will likely require thrust load support from the gearbox through a suitable coupling or other design. Employing specially formulated, high viscosity gear oil for the transmission can yield significant improvements (approx. 2X) in allowable gear loading. Though a completely new propulsion system design is needed to implement such a system, improved performance is possible.
Document ID
20070023441
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
DellaCorte, Christopher
(NASA Glenn Research Center Cleveland, OH, United States)
Bruckner, Robert J.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 23, 2013
Publication Date
June 1, 2007
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-15976-1
NASA/TM-2007-214845
ISABE-2007-1145
Report Number: E-15976-1
Report Number: NASA/TM-2007-214845
Report Number: ISABE-2007-1145
Meeting Information
Meeting: 18th ISABE Conference (ISABE 2007)
Location: Beijing
Country: China
Start Date: September 2, 2007
End Date: September 7, 2007
Sponsors: International Society for Air Breathing Engines
Funding Number(s)
WBS: WBS 561581.02.07.03.03.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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