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Effect of High-Speed Rotation on High-Temperature Superconducting Coils for High Efficiency Megawatt MotorThe use of a superconducting rotor in the High Efficiency Megawatt Motor (HEMM) comes with a number of challenges. The HEMM’s rotor must be designed so that the superconducting coil can tolerate the forces it will encounter during operation. These forces introduce considerable risk to the design of the HEMM. Because this risk cannot be adequately addressed through refined analysis, a set of experiments was deemed necessary to demonstrate that the HEMM’s superconducting coils can survive the stresses imparted by the centrifugal forces acting on the coil during full-speed operation of the machine. These experiments required spin testing a full-scale HEMM coil on a representative rotor structure at room temperature and sequentially higher rotation speeds and measuring the superconductivity response of the coil in liquid nitrogen (LN2) before and after each spin test. Tests were carried out to the full centripetal loading of a recent HEMM design. According to finite element analysis, this load produced stress components in the coil that exceed their design limit by a factor of 1 to 7.4. Although not yet confirmed, the current HEMM design is expected to produce even smaller stresses in the coil due to a 20 percent reduction in the coil’s mass and an increased volume of structural material. The only degradation of the coil that occurred during this testing resulted from a test rig failure and from the voltage taps, which are not part of the final coil design.
Document ID
20240006649
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Justin Scheidler
(Glenn Research Center Cleveland, Ohio, United States)
Thomas Tallerico
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
May 22, 2024
Publication Date
October 1, 2024
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Mechanical Engineering
Report/Patent Number
E-20236
Funding Number(s)
WBS: 081876.02.03.50.10.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Electrified Aircraft Propulsion
Electric Machines
Superconducting Machines
High Temperature Superconductors
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