Technology development of high temperature superconducting machine for electric aviation

被引：0
|
作者：
Song D. [1 ]
Yan J. [1 ]
Yang W. [1 ,2 ]
Bai M. [1 ]
Liu R. [3 ]
Wang S. [1 ]
Liu Y. [1 ]
Tian A. [1 ]
机构：
[1] School of Astronautics, Beihang University, Beijing
[2] Ningbo Institute of Technology, Beihang University, Ningbo
[3] Beijing Institute of Aerospace Control Devices, Beijing
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2023年 / 44卷 / 09期
基金：
中国国家自然科学基金;
关键词：
AC superconducting armature; aviation electric propulsion; cryogenic technology; DC superconducting magnet; emerging aviation; insulation technology; superconducting electric drive system; superconducting machine; superconducting rotor technology;
D O I：
10.7527/S1000-6893.2022.27469
中图分类号：
学科分类号：
摘要：
The superconducting machine has prospects of a wide range of applications in aviation electric propulsion due to its advantages such as small size，high power density，and high efficiency. The characteristics and current situation of the superconducting pure/hybrid electric drive systems are compared，showing the importance of the superconducting machine for high power aviation electric propulsion. In view of different requirements for motors and generators for the superconducting electric drive system for high power aviation electric propulsion，the operating principles and structural topologies of those prototypes of High Temperature Superconducting（HTS）machines studied in the past are reviewed and classified，and the advantages and disadvantages are summarized and analyzed. On this basis，the key technologies of superconducting machine are outlined in terms of superconducting technology，AC superconducting armature，rotor technology，cryogenic technology and insulation technology. Under the background of aviation electrification，the progress in the application of superconducting electric drive system in aviation electric propulsion is outlined，and future development of superconducting electric aviation is also discussed. © 2023 AAAS Press of Chinese Society of Aeronautics and Astronautics. All rights reserved.
引用
收藏
相关论文
共 104 条
  • [1] WAHLS R., N+3 technologies and concepts［R］, (2010)
  • [2] HIGH L G O A R., Flightpath 2050：Europe’s vision for aviation，maintaining global leadership & serving society’s needs［R］, (2011)
  • [3] Waypoint 2050：Balancing growth in connectivity with a comprehensive global air transport response to the climate emergency［R］, (2020)
  • [4] FEDDERSEN M., AC loss in MgB2-based fully superconducting electric machines［D］, (2017)
  • [5] ZHAO J, TANG Y D., Study on overall performance scheme of high bypass ratio civil turbofan engine, The 5th Joint Conference on Aerospace Power and the 41st Technical Exchange of China Third Aerospace Information Network, pp. 157-168, (2020)
  • [6] LUONGO C A, NAM T，, Et al., Next generation more-electric aircraft：A potential application for HTS superconductors［J］, IEEE Transactions on Applied Superconductivity, 19, 3, pp. 1055-1068, (2009)
  • [7] LI K S., Summary of research on core technology of electric aircraft［J］, Aeronautical Science & Technology, 30, 11, pp. 8-17, (2019)
  • [8] KONG X H, ZHANG Z R, Et al., Review of electric power system of distributed electric propulsion aircraft［J］, Acta Aeronautica et Astronautica Sinica, 39, 1, (2018)
  • [9] HUANG J, YANG F T., Development and challenges of electric aircraft with new energies［J］, Acta Aeronautica et Astronautica Sinica, 37, 1, pp. 57-68, (2016)
  • [10] HU Y., Design and optimization of a general aircraft’s hybrid electric propulsion system［D］
12345678910