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Dynamic Testing of a High-Specific-Torque Concentric Magnetic GearThis paper presents initial measurements of the efficiency of NASA's 2nd magnetic gear prototype. A detailed discussion of the test rig's design and capabilities was presented, along with a thorough uncertainty analysis. The reported uncertainties are 95% confidence intervals that include the effects of temperature and parasitic loads. The prototype's response was measured at output speeds between 124 rpm and 744 rpm for a controlled output torque of 10 Nm (8% of the prototype's maximum torque). After correcting for tare losses, the prototype's efficiency was found to decrease from 90.0% to 83.0% as speed increased. If the efficiency is extrapolated to a typical operating condition (85% of maximum torque) using the good assumption that energy loss is approximately independent of the transmitted torque, the expected efficiency would be 99.0% to 98.4%, which exceeds the state of the art for these speeds.
Document ID
20190025467
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Scheidler, Justin J.
(NASA Glenn Research Center Cleveland, OH, United States)
Cameron, Zachary A.
(NASA Glenn Research Center Cleveland, OH, United States)
Tallerico, Thomas F.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
June 1, 2019
Publication Date
May 13, 2019
Subject Category
Mechanical Engineering
Aircraft Design, Testing And Performance
Report/Patent Number
GRC-E-DAA-TN67349
Meeting Information
Meeting: Annual Forum & Technology Display - The Future of Vertical Flight
Location: Philadelphia, PA
Country: United States
Start Date: May 13, 2019
End Date: May 16, 2019
Sponsors: Vertical Flight Society
Funding Number(s)
WBS: 664817.02.03.02.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
magnetic gears
electrified drive systems
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