Abstract
Hybrid-electric propulsion system is an enabling technology to make the aircrafts more fuel-saving, quieter, and lower carbide emission. In this paper, a megawatt-scale power inverter based on a three-level active neutral-point-clamped (3L-ANPC) topology will be developed. To achieve high efficiency, the switching devices operating at carrier frequency in the power converter are configured by the emerging Silicon Carbide (SiC) Metal-Oxide Semiconductor Field-Effect Transistors (MOSFETs), while the conventional Silicon (Si) Insulated-Gate Bipolar Transistors (IGBTs) are selected for switches operating at the fundamental output frequency. To reduce system cable weight, the dc-bus voltage is increased to 2.4 kV. Unlike the conventional 400 Hz aircraft electric systems, the rated fundamental output frequency here is boosted to 1.4 kHz to drive the high-speed motor, which can also reduce system weight. Main hardware development and control modulation strategies are presented. Experimental results are presented to verify the performance of this MW-scale medium-voltage 'SiC+Si' hybrid three-level ANPC inverter. It is shown that the 1-MW 3L-ANPC inverter can achieve a high efficiency of 99% and high power density of 12 kVA/kg.
Original language | English |
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Title of host publication | 2018 IEEE Energy Conversion Congress and Exposition, ECCE 2018 |
Pages | 806-813 |
Number of pages | 8 |
ISBN (Electronic) | 9781479973118 |
DOIs | |
State | Published - Dec 3 2018 |
Event | 10th Annual IEEE Energy Conversion Congress and Exposition, ECCE 2018 - Portland, United States Duration: Sep 23 2018 → Sep 27 2018 |
Publication series
Name | 2018 IEEE Energy Conversion Congress and Exposition, ECCE 2018 |
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Conference
Conference | 10th Annual IEEE Energy Conversion Congress and Exposition, ECCE 2018 |
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Country/Territory | United States |
City | Portland |
Period | 9/23/18 → 9/27/18 |
Bibliographical note
Publisher Copyright:© 2018 IEEE.
Funding
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. Thanks are also expressed to all the colleagues at GE-GRC and GE Aviation who provided much support in the power converter tests. 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. Thanks are also expressed to all the colleagues at GE-GRC and GE Aviation who provided much support in the power converter tests
Funders | Funder number |
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Michigan State University-U.S. Department of Energy (MSU-DOE) Plant Research Laboratory | DE-EE0007252, NNC15CA29C |
National Aeronautics and Space Administration |
Keywords
- ANPC inverter
- High efficiency
- High power density
- Hybrid-electric propulsion systems
- Silicon Carbide
ASJC Scopus subject areas
- Energy Engineering and Power Technology
- Renewable Energy, Sustainability and the Environment
- Control and Optimization
- Computer Networks and Communications
- Hardware and Architecture
- Information Systems and Management