Module Development for a High Specific Power Density High-Efficiency Cryogenic Solid-State Circuit Breaker for Electrified Aircraft Propulsion

被引:3
作者
Dam, Shimul K. [1 ]
Yang, Ching-Hsiang [1 ]
Dong, Zhou [2 ]
Qin, Dehao [3 ]
Chen, Ruirui [1 ]
Wang, Fred [1 ,4 ]
Bai, Hua [1 ]
Zhang, Zheyu [5 ]
机构
[1] Univ Tennessee, Dept Elect Engn & Comp Sci, Knoxville, TN 37916 USA
[2] ABB Inc, ABB US Res Ctr, Raleigh, NC 27606 USA
[3] Clemson Univ, Coll Engn Comp & Appl Sci, N Charleston, SC 29405 USA
[4] Oak Ridge Natl Lab, Electrificat & Energy Infrastruct Div, Oak Ridge, TN 37830 USA
[5] Rensselaer Polytech Inst, Dept Elect Comp & Syst Engn, Troy, NY 12180 USA
基金
美国国家科学基金会;
关键词
Aircraft propulsion; cryogenic cooling; GaN HEMT; solid-state circuit breaker (SSCB); SYSTEMS; DEVICES; FUTURE; DESIGN;
D O I
10.1109/TPEL.2024.3425586
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Solid-state circuit breaker (SSCB) with high efficiency and high gravimetric power density is required for electrified aircraft propulsion (EAP). A cryogenically cooled gallium nitride (GaN) device-based SSCB module is developed for the EAP system to achieve a higher power density than existing SSCBs. The SSCB module is suitable for medium voltage direct current (MVdc) applications and is designed with low-weight modular cold plates. Each module is rated for 750 V, 100 A, and can interrupt a fault current of 1 kA at cryogenic temperature. The SSCB module structure design, thermal interface design, modular cold plate design, and insulation design are discussed. The developed SSCB module prototype achieves a power density of 329 kW/kg and an efficiency of 99.93%. Experimental results of interrupting a fault of 1 kA and insulation test of the SSCB module are provided to validate its operation.
引用
收藏
页码:13234 / 13247
页数:14
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