TY - JOUR
T1 - Conceptual Design of Superconducting Induction Motors Using REBa2Cu3Oy Superconducting Tapes for Electric Aircraft
AU - Ozaki, Koichiro
AU - Doi, Yuma
AU - Yoshida, Koichi
AU - Miura, Shun
AU - Sasayama, Teruyoshi
AU - Yoshida, Takashi
AU - Yamamoto, Kaoru
AU - Iwakuma, Masataka
AU - Kawagoe, Akifumi
AU - Tomioka, Akira
AU - Konno, Masayuki
AU - Izumi, Teruo
N1 - Funding Information:
Manuscript received September 24, 2019; accepted January 30, 2020. Date of publication February 5, 2020; date of current version April 3, 2020. This work was supported in part by the New Energy and Industrial Technology Development Organization, in part by the Japan Society for the Promotion of Science Grant-in-Aid-for Scientific Research under Grants JP18H03783 and JP19K14964, and in part by the Japan Science and Technology Agency: Advanced Low Carbon Technology Research and Development Program. (Corresponding author: Koichiro Ozaki.) Yuma Doi, Kaoru Yamamoto, Koichiro Ozaki, Koichi Yoshida, Shun Miura, Teruyoshi Sasayama, Takashi Yoshida, and Masataka Iwakuma are with the Institute of Superconductors Science and Systems, Kyushu University, Fukuoka 819-0395, Japan (e-mail: ozaki@sc.kyushu-u.ac.jp).
PY - 2020/6
Y1 - 2020/6
N2 - High power density motors are required for electric propulsion aircrafts. The highest power density of the conventional motor is reported as 5.2 kW/kg up to now. Superconducting rotating machines have a potential to realize higher power density due to its high current density and a large magnetic field property. In this study, the induction motor with air-cored superconducting armature windings was conceptually designed. The output power range was 3 to 6 MW and the output power density aimed to be over 20 kW/kg. The armature voltage should be below kV-class and joule loss below 122 kW. The target efficiency was over 95%. The electromagnetic design and analysis were carried out by JMAG Designer. The number of magnetic poles and operating temperatures were set as two poles and liquid hydrogen temperature of 20 K, respectively. The parameter was power frequency in the range of 100-250 Hz. As a result, all the requirements were satisfied when the power frequency was 130 Hz. The feasibility of the MW-class superconducting induction motor was investigated, and in conclusion, the superconducting induction motor can be applied to the aircraft propulsion system.
AB - High power density motors are required for electric propulsion aircrafts. The highest power density of the conventional motor is reported as 5.2 kW/kg up to now. Superconducting rotating machines have a potential to realize higher power density due to its high current density and a large magnetic field property. In this study, the induction motor with air-cored superconducting armature windings was conceptually designed. The output power range was 3 to 6 MW and the output power density aimed to be over 20 kW/kg. The armature voltage should be below kV-class and joule loss below 122 kW. The target efficiency was over 95%. The electromagnetic design and analysis were carried out by JMAG Designer. The number of magnetic poles and operating temperatures were set as two poles and liquid hydrogen temperature of 20 K, respectively. The parameter was power frequency in the range of 100-250 Hz. As a result, all the requirements were satisfied when the power frequency was 130 Hz. The feasibility of the MW-class superconducting induction motor was investigated, and in conclusion, the superconducting induction motor can be applied to the aircraft propulsion system.
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U2 - 10.1109/TASC.2020.2971671
DO - 10.1109/TASC.2020.2971671
M3 - Article
AN - SCOPUS:85083256074
VL - 30
JO - IEEE Transactions on Applied Superconductivity
JF - IEEE Transactions on Applied Superconductivity
SN - 1051-8223
IS - 4
M1 - 8984315
ER -