2007
DOI: 10.1109/tasc.2007.898120
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Design of HTS Axial Flux Motor for Aircraft Propulsion

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Cited by 84 publications
(41 citation statements)
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“…HTS materials have to be cryocooled under a critical temperature of 27-77 K to enable superconducting [32]. Reports from NASA [33], the BHL [34] and Masson et al [35] predict gravimetric power densities between 7-25 kW/kg for HTS motors including cryogenic cooling with efficiencies from 95-99.5%. The efficiency of electric motors is not highly dependent on the rated power output in comparison to gas turbines [14].…”
Section: Electric Propulsion Componentsmentioning
confidence: 99%
“…HTS materials have to be cryocooled under a critical temperature of 27-77 K to enable superconducting [32]. Reports from NASA [33], the BHL [34] and Masson et al [35] predict gravimetric power densities between 7-25 kW/kg for HTS motors including cryogenic cooling with efficiencies from 95-99.5%. The efficiency of electric motors is not highly dependent on the rated power output in comparison to gas turbines [14].…”
Section: Electric Propulsion Componentsmentioning
confidence: 99%
“…Several authors [12]- [23] showed that for a given number of phases, various feasible pole and slot number combinations exist. If S s is the number of slots in the stator and S r is the number of slots in the rotor, or in the present case, the number of radial tapes, the selection should consider the following requirements: 1) To avoid noise and vibrations, the relation between S s and S r must be such that S s −S r = {±1, ±2, ±(p±1), ±(p±2)}.…”
Section: B Rules Applied To Design the Rotor Cagementioning
confidence: 99%
“…The high-power density and efficiency make superconducting motors candidates to replace existing technology for ship and aircraft propulsion [41], [42]. Even with the required cryogenic system, an equivalent superconducting motor takes less space and is significantly lighter.…”
Section: A Transportationmentioning
confidence: 99%