Design, Fabrication, and Critical Current Testing of No-Insulation Superconducting Rotor Coils for NASA's 1.4 MW High-Efficiency Megawatt Motor

J. Scheidler, Thomas F. Tallerico
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引用次数: 20

Abstract

NASA Glenn Research Center is developing a 1.4 MW high-efficiency electric machine for future electrified aircraft to reduce energy consumption, emissions, and noise. This wound-field, synchronous machine employs a self-cooled, superconducting rotor to achieve excellent specific power and efficiency. This paper discusses the design and fabrication of the no-insulation high temperature superconducting (HTS) rotor coils and compares them to conventionally insulated HTS coils. Two sub-scale test coils with epoxy on only one axial face were fabricated. Critical current testing of the coils at 77 K and self field was conducted to study the influence of thermal cycling on their critical current and n-value. After two or four aggressive thermal cycles between 77 K and about 278 K (5°C), the critical current and n-value were nearly unchanged, indicating very little to no degradation.
NASA 1.4 MW高效兆瓦电机无绝缘超导转子线圈的设计、制造和临界电流测试
美国宇航局格伦研究中心正在为未来的电气化飞机开发一种1.4兆瓦的高效电机,以降低能耗、排放和噪音。这种绕线场同步电机采用自冷超导转子,以获得优异的比功率和效率。本文讨论了无绝缘高温超导转子线圈的设计和制造,并与常规绝缘高温超导线圈进行了比较。制备了两个只在一个轴向表面涂有环氧树脂的亚比例尺试验线圈。在77 K和自场条件下对线圈进行临界电流测试,研究热循环对其临界电流和n值的影响。在77 K至278 K(5°C)之间剧烈热循环2或4次后,临界电流和n值几乎没有变化,表明几乎没有降解。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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