Registro sencillo

dc.rights.licenseAttribution 4.0 International*
dc.contributor.authorBaraia-Etxaburu, Igor
dc.contributor.otherAtutxa Olmos, Unai
dc.contributor.otherLópez, Víctor Manuel
dc.contributor.otherGonzález-Hernando, Fernando
dc.contributor.otherRujas, Alejandro
dc.date.accessioned2022-04-13T13:46:43Z
dc.date.available2022-04-13T13:46:43Z
dc.date.issued2022
dc.identifier.issn2226-4310en
dc.identifier.otherhttps://katalogoa.mondragon.edu/janium-bin/janium_login_opac.pl?find&ficha_no=167657en
dc.identifier.urihttps://hdl.handle.net/20.500.11984/5530
dc.description.abstractAircraft electrification requires reliable, power-dense, high-efficient, and bidirectional rectifiers to improve the overall performance of existing aircrafts. Thus, traditional bulky passive rectifiers must be substituted by active rectifiers, satisfying the requirements imposed by up-to-date standards. However, several challenges are found in terms of power controllability, due to the standardized passive rectifier-based operating conditions. This work presents the implementation of an active rectifier modular architecture for aircraft applications. An analysis of the technical difficulties and limitations was performed and three innovative modular architectures are proposed and designed. In order to find the most suitable architecture, a comparison framework is proposed, focusing on efficiency, volume, and reliability parameters. From the comparative analysis, it can be concluded that the two-stage configuration architecture is a good solution in terms of semiconductor life expectancy and low volume. However, if converter redundancies are required, the single-stage with STATCOM configuration is an excellent trade-off between low volume, redundancy, and cost-effectiveness.en
dc.description.sponsorshipComisión Europea
dc.language.isoengen
dc.publisherMDPIen
dc.rights© 2022 by the authors. Licensee MDPIen
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.subjectmore electric aircraften
dc.subjectelectric power system architectureen
dc.subjectaerospace generation drivesen
dc.subjectAC–DC converteren
dc.subjectthree-phase rectifieren
dc.subjectHVDCen
dc.subjectpower factor correction (PFC)en
dc.titleMulti-Objective Comparative Analysis of Active Modular Rectifier Architectures for a More Electric Aircraften
dcterms.accessRightshttp://purl.org/coar/access_right/c_abf2en
dcterms.sourceAerospaceen
local.contributor.groupSistemas electrónicos de potencia aplicados al control de la energía eléctricaes
local.description.peerreviewedtrueen
local.identifier.doihttps://doi.org/10.3390/aerospace9020098en
local.relation.projectIDinfo:eu-repo/grantAgreement/EC/H2020/783158/EU/first and euRopEAn siC eigTh Inches pilOt liNe/REACTION
local.contributor.otherinstitutionhttps://ror.org/03hp1m080es
local.source.detailsVol. 9. N. 2. N. artículo 98, 2022en
oaire.format.mimetypeapplication/pdf
oaire.file$DSPACE\assetstore
oaire.resourceTypehttp://purl.org/coar/resource_type/c_6501en
oaire.versionhttp://purl.org/coar/version/c_970fb48d4fbd8a85en


Ficheros en el ítem

Thumbnail
Thumbnail

Este ítem aparece en la(s) siguiente(s) colección(es)

Registro sencillo

Attribution 4.0 International
Excepto si se señala otra cosa, la licencia del ítem se describe como Attribution 4.0 International