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Pump-back validation of a medium voltage high-frequency 'sic+si' hybrid three-level ANPC inverter for hybrid-electric propulsion application

  • Di Pan
  • , Di Zhang
  • , Chris Immer
  • , Mark Dame
  • , Jiangbiao He

Producción científica: Conference contributionrevisión exhaustiva

6 Citas (Scopus)

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 originalEnglish
Título de la publicación alojada2019 IEEE International Electric Machines and Drives Conference, IEMDC 2019
Páginas1647-1654
Número de páginas8
ISBN (versión digital)9781538693490
DOI
EstadoPublished - may 2019
Evento11th IEEE International Electric Machines and Drives Conference, IEMDC 2019 - San Diego, United States
Duración: may 12 2019may 15 2019

Serie de la publicación

Nombre2019 IEEE International Electric Machines and Drives Conference, IEMDC 2019

Conference

Conference11th IEEE International Electric Machines and Drives Conference, IEMDC 2019
País/TerritorioUnited States
CiudadSan Diego
Período5/12/195/15/19

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).

FinanciadoresNúmero del financiador
U.S. Department of Energy Oak Ridge National Laboratory U.S. Department of Energy National Science Foundation National Energy Research Scientific Computing CenterDE-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

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