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2018 | OriginalPaper | Chapter

3. A Matrix Based Isolated Three Phase AC–DC Converter

Author : Amit Kumar Singh

Published in: Analysis and Design of Power Converter Topologies for Application in Future More Electric Aircraft

Publisher: Springer Singapore

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Abstract

In recent efforts of making aircraft more energy efficient, aircraft-industries are moving towards More Electric Aircraft (MEA). MEA offers several benefits compared to a conventional aircraft system including improved power transmission efficiency, reduced fuel consumption, lesser weight and reduced environmental impact. One of the enabling technologies for MEA is power electronic converter which is required to convert and condition the generated electric power for different aircraft loads (Rosero et al., IEEE Aerosp Electron Syst Mag, 22:3–9, 2007) [1], (Wheeler and Bozhko, IEEE Electrif Mag, 2:6–12, 2014) [2], (Sarlioglu and Morris, IEEE Trans Transp Electrif 1:54–64, 2015) [3].

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previous chapter A Matrix Based Non-isolated Three Phase AC–DC Converter
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Footnotes
1
ESR is reduced by 0.7 factor for high frequency and temperature increase. The size of capacitor is 35 mm (d) and 55 mm (l). The maximum allowable temperature rise is taken as \(10\,^{\circ }\)C.
 
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Metadata
Title
A Matrix Based Isolated Three Phase AC–DC Converter
Author
Amit Kumar Singh
Copyright Year
2018
Publisher
Springer Singapore
Book
Analysis and Design of Power Converter Topologies for Application in Future More Electric Aircraft

Print ISBN: 978-981-10-8212-2

Electronic ISBN: 978-981-10-8213-9

Copyright Year: 2018

DOI
https://doi.org/10.1007/978-981-10-8213-9_3