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Two-Speed Rotorcraft Research Transmission Power-Loss Associated with the Lubrication and Hydraulic Rotating Feed-Through Design FeatureAn investigation was completed into the power loss associated with a rotating feed-through (RFT) design feature used to transfer lubrication and a hydraulic control signal from the static reference frame to a rotating reference frame in the NASA GRC two-speed transmission tests conducted in the Variable-Speed Drive Test Rig. The RFT feature, not commercially available, was created specifically for this research project and is integral to all two-speed transmission configurations tested, as well as a variant concept design for a geared variable-speed transmission presented at AHS Forum 71 in 2015. The experimental set-up and results from measurements in the isolated rotating-feed-through (RFT) experiments are presented. Results were used in an overall power loss assessment for a scaled conceptual 1,000 horsepower inline concentric two-speed transmission to support a NASA Revolutionary Vertical Lift Technologies (RVLT) Technical Challenge, demonstrating 50% speed change with less than 2% power loss while maintaining current power-to-weight ratios.
Document ID
20180005316
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Stevens, Mark A.
(NASA Glenn Research Center Cleveland, OH, United States)
Valco, Mark J.
(Army Research Lab. Cleveland, OH, United States)
LaBerge, Kelsen E.
(Army Research Lab. Cleveland, OH, United States)
Date Acquired
September 17, 2018
Publication Date
July 1, 2018
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
GRC-E-DAA-TN57180
E-19545
NASA/TM-2018-219929
Report Number: GRC-E-DAA-TN57180
Report Number: E-19545
Report Number: NASA/TM-2018-219929
Meeting Information
Meeting: American Helicopter Society (AHS) Annual Forum and Technology Display
Location: Phoenix, AZ
Country: United States
Start Date: May 15, 2018
End Date: May 17, 2018
Sponsors: American Helicopter Society International
Funding Number(s)
WBS: WBS 664817.02.03.02.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Rotorcraft
Drive System
Transmission
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