Modeling and Validation of Passive Rectifier for Airplanes with Variable Frequency and Bipolar DC Buses

Detalhes bibliográficos
Autor(a) principal: Vitoi,Lais Abrantes
Data de Publicação: 2021
Outros Autores: Pomilio,Jose Antenor, Brandão,Danilo Iglesias
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of Aerospace Technology and Management (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462021000100303
Resumo: ABSTRACT Traditional airplanes with fixed frequency and unipolar DC bus (270 V) commonly use 12-pulse passive rectifiers. The increase of power demand and the concern with aircraft efficiency boost the electrification of airplanes using variable frequency(360-800 Hz) and bipolar DC buses (± 270 V). Thus, this paper analyses the 12-pulse passive rectifiers in this new scenario. It is proposed an accurate model, describing its design, to verify if passive rectifiers are suitable for aircraft application complying with current standards. The analysis of the 12-pulse rectifier is done by an association of two 6-pulse rectifiers and considering both sorts of an input filter, L and LC. The mathematical model is presented and considers typical harmonic components, allowing precise analysis of input current and output voltage. Simulation and experimental results are provided to validate the mathematical model. The paper shows that the 12-pulse passive rectifier is not a viable solution when operating under variable frequency, which was verified by the violation of the electricity quality standards.
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spelling Modeling and Validation of Passive Rectifier for Airplanes with Variable Frequency and Bipolar DC BusesBipolar DC busesMore electric aircraftVariable frequency systems12-pulse rectifierABSTRACT Traditional airplanes with fixed frequency and unipolar DC bus (270 V) commonly use 12-pulse passive rectifiers. The increase of power demand and the concern with aircraft efficiency boost the electrification of airplanes using variable frequency(360-800 Hz) and bipolar DC buses (± 270 V). Thus, this paper analyses the 12-pulse passive rectifiers in this new scenario. It is proposed an accurate model, describing its design, to verify if passive rectifiers are suitable for aircraft application complying with current standards. The analysis of the 12-pulse rectifier is done by an association of two 6-pulse rectifiers and considering both sorts of an input filter, L and LC. The mathematical model is presented and considers typical harmonic components, allowing precise analysis of input current and output voltage. Simulation and experimental results are provided to validate the mathematical model. The paper shows that the 12-pulse passive rectifier is not a viable solution when operating under variable frequency, which was verified by the violation of the electricity quality standards.Departamento de Ciência e Tecnologia Aeroespacial2021-01-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462021000100303Journal of Aerospace Technology and Management v.13 2021reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.1590/jatm.v13.1194info:eu-repo/semantics/openAccessVitoi,Lais AbrantesPomilio,Jose AntenorBrandão,Danilo Iglesiaseng2021-02-11T00:00:00Zoai:scielo:S2175-91462021000100303Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2021-02-11T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Modeling and Validation of Passive Rectifier for Airplanes with Variable Frequency and Bipolar DC Buses
title Modeling and Validation of Passive Rectifier for Airplanes with Variable Frequency and Bipolar DC Buses
spellingShingle Modeling and Validation of Passive Rectifier for Airplanes with Variable Frequency and Bipolar DC Buses
Vitoi,Lais Abrantes
Bipolar DC buses
More electric aircraft
Variable frequency systems
12-pulse rectifier
title_short Modeling and Validation of Passive Rectifier for Airplanes with Variable Frequency and Bipolar DC Buses
title_full Modeling and Validation of Passive Rectifier for Airplanes with Variable Frequency and Bipolar DC Buses
title_fullStr Modeling and Validation of Passive Rectifier for Airplanes with Variable Frequency and Bipolar DC Buses
title_full_unstemmed Modeling and Validation of Passive Rectifier for Airplanes with Variable Frequency and Bipolar DC Buses
title_sort Modeling and Validation of Passive Rectifier for Airplanes with Variable Frequency and Bipolar DC Buses
author Vitoi,Lais Abrantes
author_facet Vitoi,Lais Abrantes
Pomilio,Jose Antenor
Brandão,Danilo Iglesias
author_role author
author2 Pomilio,Jose Antenor
Brandão,Danilo Iglesias
author2_role author
author
dc.contributor.author.fl_str_mv Vitoi,Lais Abrantes
Pomilio,Jose Antenor
Brandão,Danilo Iglesias
dc.subject.por.fl_str_mv Bipolar DC buses
More electric aircraft
Variable frequency systems
12-pulse rectifier
topic Bipolar DC buses
More electric aircraft
Variable frequency systems
12-pulse rectifier
description ABSTRACT Traditional airplanes with fixed frequency and unipolar DC bus (270 V) commonly use 12-pulse passive rectifiers. The increase of power demand and the concern with aircraft efficiency boost the electrification of airplanes using variable frequency(360-800 Hz) and bipolar DC buses (± 270 V). Thus, this paper analyses the 12-pulse passive rectifiers in this new scenario. It is proposed an accurate model, describing its design, to verify if passive rectifiers are suitable for aircraft application complying with current standards. The analysis of the 12-pulse rectifier is done by an association of two 6-pulse rectifiers and considering both sorts of an input filter, L and LC. The mathematical model is presented and considers typical harmonic components, allowing precise analysis of input current and output voltage. Simulation and experimental results are provided to validate the mathematical model. The paper shows that the 12-pulse passive rectifier is not a viable solution when operating under variable frequency, which was verified by the violation of the electricity quality standards.
publishDate 2021
dc.date.none.fl_str_mv 2021-01-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462021000100303
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462021000100303
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.1590/jatm.v13.1194
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.13 2021
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
instname_str Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron_str DCTA
institution DCTA
reponame_str Journal of Aerospace Technology and Management (Online)
collection Journal of Aerospace Technology and Management (Online)
repository.name.fl_str_mv Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
repository.mail.fl_str_mv ||secretary@jatm.com.br
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