Resumen
High power density medium voltage high speed electric motors for aircraft hybrid electric propulsion applications often require high output fundamental frequency from the power inverter. Conventional Si-based medium voltage drive has a switching frequency that is not sufficient to meet the dynamic and harmonic requirements for such application. A 'SiC+Si' hybrid three-level active neutral point clamped (ANPC) inverter has been developed as high-speed motor drive for hybrid electric propulsion. Single-phase and three-phase pump-back tests are performed to validate the power capability and basic control functions. The implementation and test results will be reported in this paper.
| Idioma original | English |
|---|---|
| Título de la publicación alojada | 2019 IEEE International Electric Machines and Drives Conference, IEMDC 2019 |
| Páginas | 1647-1654 |
| Número de páginas | 8 |
| ISBN (versión digital) | 9781538693490 |
| DOI | |
| Estado | Published - may 2019 |
| Evento | 11th IEEE International Electric Machines and Drives Conference, IEMDC 2019 - San Diego, United States Duración: may 12 2019 → may 15 2019 |
Serie de la publicación
| Nombre | 2019 IEEE International Electric Machines and Drives Conference, IEMDC 2019 |
|---|
Conference
| Conference | 11th IEEE International Electric Machines and Drives Conference, IEMDC 2019 |
|---|---|
| País/Territorio | United States |
| Ciudad | San Diego |
| Período | 5/12/19 → 5/15/19 |
Nota bibliográfica
Publisher Copyright:© 2019 IEEE.
Financiación
The authors would like to express sincere thanks to the U.S. National Aeronautics and Space Administration (NASA) and the Department of Energy (DOE) for their partial financial support (NASA Grant No. NNC15CA29C and DOE Grant No. DE-EE0007252) for the work presented in this paper. The authors also wish to acknowledge the contributions of the colleagues at GE Global Research and GE Aviation. ACKNOWLEDGMENT The authors would like to express sincere thanks to the U.S. National Aeronautics and Space Administration (NASA) and the Department of Energy (DOE) for their partial financial support (NASA Grant No. NNC15CA29C and DOE Grant No. DE-EE0007252) for the work presented in this paper. The authors also wish to acknowledge the contributions of the colleagues at GE Global Research and GE Aviation. This work is supported by U.S. National Aeronautics and Space Administration (NASA) and the Department of Energy (DOE).
| Financiadores | Número del financiador |
|---|---|
| U.S. Department of Energy Oak Ridge National Laboratory U.S. Department of Energy National Science Foundation National Energy Research Scientific Computing Center | DE-EE0007252, NNC15CA29C |
| U.S. Department of Energy Oak Ridge National Laboratory U.S. Department of Energy National Science Foundation National Energy Research Scientific Computing Center | |
| National Aeronautics and Space Administration |
ASJC Scopus subject areas
- Energy Engineering and Power Technology
- Electrical and Electronic Engineering
- Mechanical Engineering
Huella
Profundice en los temas de investigación de 'Pump-back validation of a medium voltage high-frequency 'sic+si' hybrid three-level ANPC inverter for hybrid-electric propulsion application'. En conjunto forman una huella única.Citar esto
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver