Dynamic Testing of a High-Specific-Torque Concentric Magnetic Gear

F-0075-2019-14668

5/13/2019

Authors
Abstract
Content

This paper presents measurements of the efficiency of NASA's 2nd magnetic gear prototype. A detailed discussion of the test rig used to make these measurements was presented, including 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.

Meta TagsDetails
DOI
https://doi.org/10.4050/F-0075-2019-14668
Citation
Scheidler, J., Cameron, Z., and Tallerico, T., "Dynamic Testing of a High-Specific-Torque Concentric Magnetic Gear," Vertical Flight Society 75th Annual Forum and Technology Display, Philadelphia, Pennsylvania, May 13, 2019, https://doi.org/10.4050/F-0075-2019-14668.
Additional Details
Publisher
Published
5/13/2019
Product Code
F-0075-2019-14668
Content Type
Technical Paper
Language
English