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Variable/Multispeed Rotorcraft Drive System ConceptsSeveral recent studies for advanced rotorcraft have identified the need for variable, or multispeed-capable rotors. A speed change of up to 50 percent has been proposed for future rotorcraft to improve vehicle performance. Varying rotor speed during flight not only requires a rotor capable of performing effectively over the extended operation speed and load range, but also requires an advanced propulsion system to provide the required speed changes. A study has been completed, which investigated possible drive system arrangements to accommodate up to the 50 percent speed change. These concepts are presented. The most promising configurations are identified and will be developed for future validation testing.
Document ID
20090019132
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Stevens, Mark A.
(NASA Glenn Research Center Cleveland, OH, United States)
Handschuh, Robert F.
(Army Research Lab. Cleveland, OH, United States)
Lewicki, David G.
(Army Research Lab. Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
March 1, 2009
Subject Category
Mechanical Engineering
Report/Patent Number
NASA/TM-2009-215456
ARL-TR-4758
E-16649
Funding Number(s)
WBS: WBS 877868.02.07.03.03.10.1
Distribution Limits
Public
Copyright
Public Use Permitted.
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