Conduction cooling of a compact HTS motor for aeropropulsion

被引：10

作者：

Pienkos, JE ^{[1
]}

Masson, PJ

Pamidi, SV

Luongo, CA

机构：

[1] FSU, FAMU, Coll Engn, Tallahassee, FL 32310 USA

[2] Ctr Adv Power Syst, Tallahassee, FL 32310 USA

来源：

IEEE TRANSACTIONS ON APPLIED SUPERCONDUCTIVITY | 2005年 / 15卷 / 02期

关键词：

conduction cooling; HTS motor;

D O I：

10.1109/TASC.2005.849599

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

Thermal aspects of a novel high temperature superconducting motor design are examined for use in the propulsion of an aero-vehicle. To simplify the refrigeration, focus is on conduction cooling of the superconducting material directly from the cold head of the cryocooler. A brief description of the motor is followed by an analysis of the conduction cooling apparatus. An experimental setup has been developed, including a cryocooler, a cryostat, and a mockup of the HTS motor, to validate the system model.

引用

页码：2150 / 2153

页数：4

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