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Erschienen in:
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2018 | OriginalPaper | Buchkapitel

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

verfasst von : Amit Kumar Singh

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

Verlag: 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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Vorheriges Kapitel A Matrix Based Non-isolated Three Phase AC–DC Converter
Nächstes Kapitel A New Matrix Based Non-isolated Three Phase Buck-Boost Rectifier
Fußnoten
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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Metadaten
Titel
A Matrix Based Isolated Three Phase AC–DC Converter
verfasst von
Amit Kumar Singh
Copyright-Jahr
2018
Verlag
Springer Singapore
Buch
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-Jahr: 2018

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