Investigation of high-speed superconducting electric machines through time-space extrusion numerical modelling

Hongye Zhang
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Abstract

Featured by high power density and efficiency, high temperature superconducting (HTS) electric machines provide a promising solution to heavy-duty electric transport, e.g. electric aircraft. However, designing HTS machines, particularly high-speed HTS motors, presents significant challenges: (1) modelling is highly time-consuming due to the non-linear resistivity of superconductors and complex machine topology; (2) accurately estimating the AC loss of HTS windings remains an open aspiration due to the complicated AC environment. To reduce computational complexity, the thin film approximation (only considering the approximated 1-D HTS film) for HTS coated conductors (CCs) has been widely adopted in simulations, such as the T-formulation models; however, the thin film approximation becomes inadequate for HTS CCs under high-frequency magnetic fields, as encountered in high-speed motors for aerospace. To efficiently and accurately model the AC loss of HTS windings in high-speed superconducting machines, taking a 1 MW superconducting synchronous motor with HTS armature windings as an example, this paper has adopted a time-space extrusion (TSE) method, which demonstrates a >25-fold decrease in modelling time while maintaining comparable accuracy to two benchmark H-A models. The power dissipation in both normal-conducting and superconducting layers of HTS windings has been studied, the AC losses in different turns of the armature winding have been explored, and the slot leakage field harmonics have been illustrated. Results have shown that the losses in Cu and Ag layers for high-speed HTS machines operating at cryo-temperatures (e.g. liquid hydrogen temperature) are not neglectable, especially with a high residual resistance ratio and in the presence of harmonics. The HTS armature winding should be positioned away from the iron tooth and slot opening to minimise exposure to slot leakage fields. The adopted TSE modelling strategy and drawn conclusions have provided valuable insights for the efficient design of high-speed superconducting machines.
通过时空挤压数值建模研究高速超导电机
高温超导(HTS)电机具有功率密度高、效率高的特点,为重型电动交通工具(如电动飞机)提供了一种前景广阔的解决方案。然而,高温超导电机,尤其是高速高温超导电机的设计面临着巨大挑战:(1)由于超导体的非线性电阻率和复杂的机器拓扑结构,建模非常耗时;(2)由于复杂的交流环境,准确估算高温超导绕组的交流损耗仍是一个未知的愿望。为了降低计算复杂性,HTS 涂层导体(CC)的薄膜近似(仅考虑近似的一维 HTS 薄膜)已被广泛用于模拟,如 T 型模型;然而,薄膜近似并不适用于 HTS CC 在高频磁场下的应用,如航空航天领域的高速电机。为了高效、准确地模拟高速超导机器中 HTS 绕组的交流损耗,本文以 1 MW 超导同步电机的 HTS 电枢绕组为例,采用了时空挤压(TSE)方法,在保持与两个基准 H-A 模型相当精度的同时,建模时间缩短了 25 倍。研究了 HTS 绕组常导层和超导层的功率耗散,探讨了电枢绕组不同匝数的交流损耗,并说明了槽漏场谐波。研究结果表明,对于在低温(如液氢温度)下运行的高速 HTS 机器,铜层和银层的损耗是不可忽视的,尤其是在高剩余电阻比和存在谐波的情况下。HTS 电枢绕组的位置应远离铁齿和槽口,以尽量减少槽漏磁场的影响。所采用的 TSE 建模策略和得出的结论为高效设计高速超导机器提供了宝贵的启示。
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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