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A Matrix Based Isolated Three Phase AC–DC Converter

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

Part of the book series: Springer Theses ((Springer Theses))

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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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Notes

  1. 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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Authors and Affiliations

  1. Department of Electrical and Computer Engineering, National University of Singapore, Singapore, Singapore

    Amit Kumar Singh

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  1. Amit Kumar Singh
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Correspondence to Amit Kumar Singh .

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Singh, A.K. (2018). A Matrix Based Isolated Three Phase AC–DC Converter. In: Analysis and Design of Power Converter Topologies for Application in Future More Electric Aircraft. Springer Theses. Springer, Singapore. https://doi.org/10.1007/978-981-10-8213-9_3

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

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  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-10-8212-2

  • Online ISBN: 978-981-10-8213-9

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