TY - GEN
T1 - Cryogenic characterization and modeling of silicon superjunction mosfet for power loss estimation
AU - Hossain, Md Maksudul
AU - Rashid, Arman Ur
AU - Sweeting, Rosten
AU - Wei, Yuqi
AU - Woldegiorgis, Dereje
AU - Mhiesan, Haider
AU - Mantooth, H. Alan
N1 - Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - This paper presents a simplified semiconductor device characterization technique at cryogenic temperatures. A commercial silicon superjunction MOSFET (650V CoolMOS™) has been characterized for the DC output, Transfer, and Capacitance-Voltage (C-V) characteristics. The results obtained have been utilized to model the device with an industry standard compact model provided by Saber™. A temperature binning approach has been taken to incorporate the lower temperature behaviors of the device. This model incorporates the non-linear internal capacitance, body diode, and the gate resistance. The model has been used to investigate the merit of using the selected silicon power device at cryogenic temperatures by simulating conduction losses and overall energy losses of a typical buck converter and a 5-level cascaded H-Bridge inverter. From these system-level simulations, it can be beneficial to compare the performance of the power switches for applications like future high efficiency, low emission aviation.
AB - This paper presents a simplified semiconductor device characterization technique at cryogenic temperatures. A commercial silicon superjunction MOSFET (650V CoolMOS™) has been characterized for the DC output, Transfer, and Capacitance-Voltage (C-V) characteristics. The results obtained have been utilized to model the device with an industry standard compact model provided by Saber™. A temperature binning approach has been taken to incorporate the lower temperature behaviors of the device. This model incorporates the non-linear internal capacitance, body diode, and the gate resistance. The model has been used to investigate the merit of using the selected silicon power device at cryogenic temperatures by simulating conduction losses and overall energy losses of a typical buck converter and a 5-level cascaded H-Bridge inverter. From these system-level simulations, it can be beneficial to compare the performance of the power switches for applications like future high efficiency, low emission aviation.
UR - https://www.scopus.com/pages/publications/85091313652
U2 - 10.2514/6.2020-3660
DO - 10.2514/6.2020-3660
M3 - 会议稿件
AN - SCOPUS:85091313652
SN - 9781624106026
T3 - AIAA Propulsion and Energy 2020 Forum
SP - 1
EP - 10
BT - AIAA Propulsion and Energy 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Propulsion and Energy 2020 Forum
Y2 - 24 August 2020 through 28 August 2020
ER -