Modeling and Validation of Passive Rectifier for Airplanes with Variable Frequency and Bipolar DC Buses
Autor(a) principal: | |
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Data de Publicação: | 2021 |
Outros Autores: | , |
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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Journal of Aerospace Technology and Management (Online) |
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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 |
_version_ |
1754732532354514944 |