TY - GEN
T1 - Cryogenic Characterization and Modeling of Silicon IGBT for Hybrid Aircraft Application
AU - Hossain, Md Maksudul
AU - Rashid, Arman Ur
AU - Wei, Yuqi
AU - Sweeting, Rosten
AU - Mantooth, H. Alan
N1 - Publisher Copyright:
© 2021 IEEE.
PY - 2021/3/6
Y1 - 2021/3/6
N2 - Cryogenic operation of power electronic converters promises higher density, better efficiency, lower thermal management requirement and higher reliability. However, the wide variation in power semiconductor device performance at deep cryogenic temperatures might cause catastrophic failure if not considered accordingly during the design phase. The work presented in this paper explores a simple cryogenic characterization method for insulated-gate bipolar transistors (IGBT). In addition, an open access physics-based IGBT compact model has been modified with cryo-compatible temperature scaling equations in order to investigate the merit of the chosen device in a power electronic system. A commercial field stop trench IGBT (50A/650V) has been used for the electrical characterization. Furthermore, additional complicated converter circuits (e.g. a buck converter and a 5-level modular multilevel inverter) has been simulated, and loss calculation has been conducted to provide a means for designers to select best devices for appropriate low temperature applications.
AB - Cryogenic operation of power electronic converters promises higher density, better efficiency, lower thermal management requirement and higher reliability. However, the wide variation in power semiconductor device performance at deep cryogenic temperatures might cause catastrophic failure if not considered accordingly during the design phase. The work presented in this paper explores a simple cryogenic characterization method for insulated-gate bipolar transistors (IGBT). In addition, an open access physics-based IGBT compact model has been modified with cryo-compatible temperature scaling equations in order to investigate the merit of the chosen device in a power electronic system. A commercial field stop trench IGBT (50A/650V) has been used for the electrical characterization. Furthermore, additional complicated converter circuits (e.g. a buck converter and a 5-level modular multilevel inverter) has been simulated, and loss calculation has been conducted to provide a means for designers to select best devices for appropriate low temperature applications.
UR - https://www.scopus.com/pages/publications/85111366262
U2 - 10.1109/AERO50100.2021.9438422
DO - 10.1109/AERO50100.2021.9438422
M3 - 会议稿件
AN - SCOPUS:85111366262
T3 - IEEE Aerospace Conference Proceedings
BT - 2021 IEEE Aerospace Conference, AERO 2021
PB - IEEE Computer Society
T2 - 2021 IEEE Aerospace Conference, AERO 2021
Y2 - 6 March 2021 through 13 March 2021
ER -