科技报告详细信息
New Test Rig to Measure Alternating Current Losses of Both Low and High Critical Temperature Superconductors
Hartwig, Jason ; Fraser, Bryan ; Brown, Gerald ; Kohlman, Lee ; Koci, David ; Hunker, Keith ; Bowman, Cheryl ; Schrum, Phillip ; Matten, David
关键词: ALTERNATING CURRENT;    COOLANTS;    DIRECT CURRENT;    ELECTRIC POTENTIAL;    ENERGY STORAGE;    FREQUENCIES;    HIGH TEMPERATURE SUPERCONDUCTORS;    LIMITER CIRCUITS;    LIQUID HYDROGEN;    LIQUID NITROGEN;    MAGNETIC FIELDS;    OPERATING TEMPERATURE;    TRANSFORMERS;    YBCO SUPERCONDUCTORS;   
RP-ID  :  GRC-E-DAA-TN63356,NASA/TM-2019-220046 ,E-19642-TN63356
学科分类:航空航天科学
美国|英语
来源: NASA Technical Reports Server
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【 摘 要 】

This paper presents the design, development, operation, and test capabilities of a proposed superconducting coil testbed to measure alternating current (AC) losses at the NASA Glenn Research Center. Superconducting AC losses are important in the design of electric stators and rotors, power transmission lines, transformers, fault current limiters, magnets, and superconducting energy storage (not batteries). The new liquid-hydrogen-based rig will allow superconducting testing across a wide range of test parameters, including injected current up to 400 A, frequency (0 to 400 Hz), magnetic field (0 to 0.6 T), phase angle between induced voltage and injected current (–180° to 180°), coil coolant temperature (18 to 28 K), and AC power loss (5 to 30 W). While the target application of interest is 20 K superconducting MgB2 (the only superconductor that can presently be made with low losses) stator coils for future electric machines, the rig can accommodate test articles (TAs) with straight wire, tape, cables, coils of any shape, any allowable combination of superconducting wire and fluid (e.g., yttrium barium copper oxide (YBCO) coils and liquid nitrogen), and AC or direct current (DC) testing. The new spin rig builds upon the existing Air Force spin rig through a more flexible mode of fluid control, a wider gap space (up to 10.2 cm) for TAs, and the ability to accommodate TAs over a wider range of operating temperatures (18 to 95 K) using liquid hydrogen, gaseous helium, or liquid nitrogen as the working fluid, thus supporting direct cooled machines below 77 K.

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