Conduction cooling of a compact HTS motor for aeropropulsion

IEEE Transactions on Applied Superconductivity

Volumn 15, Issue 2 PART II, 2005, Pages 2150-2153

  Pienkos, Jules E ^a   Masson, Philippe J ^a   Pamidi, Sastry V ^b   Luongo, Cesar A ^a  

^a FAMU FSU COLLEGE OF ENGINEERING   (United States)

^b FLORIDA STATE UNIVERSITY   (United States)

Author keywords

Conduction cooling; HTS motor

Indexed keywords

AEROSPACE VEHICLES; AIRCRAFT PROPULSION; COOLING SYSTEMS; CRYOGENICS; CRYOSTATS; ELECTRIC MOTORS; MACHINE DESIGN; REFRIGERATION;

AERO-VEHICLE; COOLING CONDUCTION; CRYOCOOLER; HTS MOTOR;

HIGH TEMPERATURE SUPERCONDUCTORS;

EID: 22144490483     PISSN: 10518223     EISSN: None     Source Type: Journal    
DOI: 10.1109/TASC.2005.849599     Document Type: Conference Paper

References (4)

1. S. W. Van Sciver, "Cryogenic systems for superconducting devices," Physica C, vol. 354, pp. 129-135, 2001.
2. x (Bi-2223) magnet for magnetic separation," Physica C, vol. 350, pp. 76-82, 2001.
3. K. Tasaki et al., "Thermal stability of a cryocooler-cooled HTS pancake coil wound with Bi2223 tape," Physica C, vol. 392-396, pp. 1210-1213, 2003.
4. P. J. Masson and C. A. Luongo, "High power density superconducting motor for all-electric aircraft propulsion," IEEE Trans. ASC, Jun. 2005, to be published.