NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Concepts for Variable/Multi-Speed Rotorcraft Drive SystemIn several recent studies and on-going developments for advanced rotorcraft, the need for variable or multi-speed capable rotors has been raised. A speed change of up to 50 percent has been proposed for future rotorcraft to improve overall vehicle performance. Accomplishing rotor speed changes during operation requires both a rotor that can perform effectively over the operation speed/load range, and a propulsion system that can enable these speed changes. A study has been completed to investigate possible drive system arrangements that can accommodate up to the 50 percent speed change. Several concepts will be presented and evaluated. The most promising configurations will be identified and developed for future testing in a sub-scaled test facility to validate operational capability.
Document ID
20080045530
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
September 1, 2008
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ARL-TR-4564
AHS 080273
NASA/TM-2008-215276
Report Number: ARL-TR-4564
Report Number: AHS 080273
Report Number: NASA/TM-2008-215276
Meeting Information
Meeting: 64th Annual Forum and Technology Display (American Helicopter Society Forum)
Location: Montreal
Country: Canada
Start Date: April 29, 2008
End Date: May 1, 2008
Sponsors: American Helicopter Society, Inc.
Funding Number(s)
WBS: WBS 877868.02.07.03.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available