PCB Busbar Design and Verification for a Multiphase 250 kW SiC based All-electric Aircraft Powertrain Converter
Author:
Affiliation:
1. Virginia Tech,Center for Power Electronics Systems(CPES),Blacksburg,VA
2. Raytheon Technologies,Raytheon Technology Research Center (RTRC),Hartford,CT,USA
Funder
Advanced Research Projects Agency-Energy (ARPA-E)
U.S. Department of Energy
Texas Instruments
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10131044/10130846/10131311.pdf?arnumber=10131311
Reference11 articles.
1. Adaptive Hysteresis Current Based ZVS Modulation and Voltage Gain Compensation for High-Frequency Three-Phase Converters
2. Submodule Design of a 2 kV 1 MW Integrated Modular Motor Drive for Aviation Applications
3. Design of a 10 kV SiC MOSFET-based high-density, high-efficiency, modular medium-voltage power converter
4. Operation and Control of a Matrix Converter in Current Control Mode with Voltage Boost Capability
5. A general carrier-based modulation and capacitor- voltage balancing method for multilevel matrix converters (AC-AC Stacked Multicell Converters)
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. A SiC MOSFET propulsion inverter design with power redundancy, considering unwanted events, for electrical aircrafts;2024 IEEE Transportation Electrification Conference and Expo (ITEC);2024-06-19
2. High-Density Forced Air-Cooling Duct for 211-kW SiC-Based Aircraft Propulsion Inverters;2023 IEEE Energy Conversion Congress and Exposition (ECCE);2023-10-29
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