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Electrical Systems for Aircraft, Railway and Ship Propulsion 2010
DOI: 10.1109/esars.2010.5665238
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Potential analysis for the optimization of the electrical network of large modern civil and future single aisle aircraft and examples of the network capacity utilisation

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Cited by 16 publications
(2 citation statements)
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“…However, a critical issue of MEA is the weight of the needed electric components and systems as discussed in [4]. Thus, weight reduction is one the main drivers for future aircraft systems [5], [6]. Typical electrical power distribution architectures as applied in today's aircraft can be found in [7] and [8].…”
Section: Introductionmentioning
confidence: 99%
“…However, a critical issue of MEA is the weight of the needed electric components and systems as discussed in [4]. Thus, weight reduction is one the main drivers for future aircraft systems [5], [6]. Typical electrical power distribution architectures as applied in today's aircraft can be found in [7] and [8].…”
Section: Introductionmentioning
confidence: 99%
“…Indeed, modern power networks, in aircrafts for instance, are mainly composed of Power Electronics Converters, interfacing sources and loads to the grid [1], [2]. Therefore, power quality constraints (in the low frequency range), as well as EMC requirements (high frequency) impose adding specific filters.…”
Section: Taking Into Account Interactions Between Converters In the Dmentioning
confidence: 99%