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Regeneration in Aircraft Electrical Power Systems?
Technical Paper
2008-01-2898
ISSN: 0148-7191, e-ISSN: 2688-3627
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Sector:
Event:
Power Systems Conference
Language:
English
Abstract
This paper considers a wide range of options for the allowing regeneration onto the aircraft bus for possible inclusion in future aircraft power quality specifications. For many loads, such as actuators, the size and weight of power converters could be significantly reduced if the requirement to avoid regeneration was removed from the specifications.
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Authors
Citation
Wheeler, P., Clare, J., Bozhko, S., and Kulshreshtha, A., "Regeneration in Aircraft Electrical Power Systems?," SAE Technical Paper 2008-01-2898, 2008, https://doi.org/10.4271/2008-01-2898.Also In
References
- Howse M. “All Electric Aircraft” IEE Power Engineer August / September 2003 35 37
- MIL_STD 704 “Revision F - Aircraft Electric Power Characteristics”
- Wheeler, P.W. Rodriguez J. Clare J.C. Empringham L. “Matrix Converter, A technology Review” IEEE Transactions on Industrial Electronics 49 2 April 2002
- Klumpner C. Blaabjerg F. “A new cost-effective multi-drive solution based on a two-stage direct power electronic conversion topology,” Proc. IASV2 1 2002 444 452