Design and implementation of a lightweight high-voltage power converter for electro-aerodynamic propulsion
Name
cpCOMPEL17_Yiou_He_EAD_PID4896709-postconference.pdf
Description
Accepted version
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1.26 MB
Format
Adobe PDF
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Author(s) • •
He, Yiou
Woolston, Mark R.
Perreault, David J
Date Issued
August 2017
Journal
2017 IEEE 18th Workshop on Control and Modeling for Power Electronics (COMPEL)
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Citation
He, Yiou et al. "Design and implementation of a lightweight high-voltage power converter for electro-aerodynamic propulsion." 2017 IEEE 18th Workshop on Control and Modeling for Power Electronics (COMPEL), July 2017, Stanford, California, USA, Institute of Electrical and Electronics Engineers (IEEE), August 2017 © 2017 IEEE
Version
Author's final manuscript
Abstract
Recent studies in electro-Aerodynamic (EAD) propulsion have stimulated the need for lightweight power converters providing outputs at tens of kilovolts and hundreds of watts [1] [2]. This paper demonstrates a design of a lightweight high-voltage converter operating from a 160-200 V dc input and providing dc output of up to 600 W at 40 kV. It operates at around 500 kHz and achieves a specific power of 1.2 kW/kg. This is considerably lighter than comparable industrial and academic designs at this power level. High voltage converters generally comprise an inverter, a step-up transformer and a rectifier, with the large needed voltage gain distributed among these stages. Several means of realizing these stages are compared in terms of weight. The weight of the converter is minimized by properly selecting and optimizing the design and the voltage gain of each stage within the constraints of device limitations and losses. A prototype circuit is developed based on this approach and used to drive an EAD-propulsion system for an unmanned aerial vehicle (UAV). In addition to addressing the power conversion needs for EAD, this research can potentially benefit the development of lightweight high-voltage converters in many other applications where weight and size are important.
MIT Department
Massachusetts Institute of Technology. Department of Electrical Engineering and Computer Science
Lincoln Laboratory
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DOI of Published Version
https://doi.org/10.1109/compel.2017.8013315