Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves
Autor(a) principal: | |
---|---|
Data de Publicação: | 2015 |
Tipo de documento: | Dissertação |
Idioma: | por |
Título da fonte: | Repositório Institucional da UFSCAR |
Texto Completo: | https://repositorio.ufscar.br/handle/ufscar/7627 |
Resumo: | In order to reduce the mass of eletrical transformers and generators in aircrafts, many manufacturers have adopted 400 Hz as the operation of these devices. However this frequency causes increased core losses which were disregarded due to the small involved powers and non continuous basis operations. By considering similar sizes, newer aircraft models are more electricity dependent and the generated power increased from 240 kVA to 1000 kVA. In this new scenario losses cannot be neglected and other options for increased efficiency should be considered. Iron-based amorphous transformer cores AEFture reduction by up to 70% loss while operating in 50- 60 Hz. However smaller magnetic saturation induction values result in higher weight than similar cores made of crystalline Fe-Si, therefore, undesirable in aircraft. This work discusses that, when particularities of aeronautical transformers are considered, one can design a power transformer with an amorphous core with smaller mass and losses than a similar with a Fe-Si crystalline based core. For this purpose, a hand-made amorphous core transformer was built to operate at 400 Hz, which has been thermo-magnetically treated to enhance its electromagnetic properties. Through electrical test, equivalent circuits of transformer were obtained for both core conditions: unannealed and annealed. Comparisons of masses and losses between an aircraft transformer with crystalline core and the hand-made amorphous one show that the latter has lower losses and that, when obeyed the particularities for aeronautical transformers, they may have smaller masses. Details and explanations about the thermomagnetic treatment, evidencing by X-ray diffraction of no-crystallization, after core heat-treatment and hand-made transformer evaluation through simulation are also included in this work. |
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Silva, Wagner Angelo daJorge Júnior, Alberto Moreirahttp://lattes.cnpq.br/6360362248108490http://lattes.cnpq.br/5336516408192676090f2c97-1e47-4a12-a8f7-1e8602c636e82016-10-04T17:58:45Z2016-10-04T17:58:45Z2015-04-28SILVA, Wagner Angelo da. Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves. 2015. Dissertação (Mestrado em Ciência e Engenharia de Materiais) – Universidade Federal de São Carlos, São Carlos, 2015. Disponível em: https://repositorio.ufscar.br/handle/ufscar/7627.https://repositorio.ufscar.br/handle/ufscar/7627In order to reduce the mass of eletrical transformers and generators in aircrafts, many manufacturers have adopted 400 Hz as the operation of these devices. However this frequency causes increased core losses which were disregarded due to the small involved powers and non continuous basis operations. By considering similar sizes, newer aircraft models are more electricity dependent and the generated power increased from 240 kVA to 1000 kVA. In this new scenario losses cannot be neglected and other options for increased efficiency should be considered. Iron-based amorphous transformer cores AEFture reduction by up to 70% loss while operating in 50- 60 Hz. However smaller magnetic saturation induction values result in higher weight than similar cores made of crystalline Fe-Si, therefore, undesirable in aircraft. This work discusses that, when particularities of aeronautical transformers are considered, one can design a power transformer with an amorphous core with smaller mass and losses than a similar with a Fe-Si crystalline based core. For this purpose, a hand-made amorphous core transformer was built to operate at 400 Hz, which has been thermo-magnetically treated to enhance its electromagnetic properties. Through electrical test, equivalent circuits of transformer were obtained for both core conditions: unannealed and annealed. Comparisons of masses and losses between an aircraft transformer with crystalline core and the hand-made amorphous one show that the latter has lower losses and that, when obeyed the particularities for aeronautical transformers, they may have smaller masses. Details and explanations about the thermomagnetic treatment, evidencing by X-ray diffraction of no-crystallization, after core heat-treatment and hand-made transformer evaluation through simulation are also included in this work.Para redução de massa dos transformadores e geradores elétricos aeronáuticos, muitos fabricantes adotaram a frequência de 400 Hz para operação destes dispositivos, entretanto o aumento da frequência causa também aumento de perdas em seus núcleos, as quais foram desprezadas devido às pequenas potências envolvidas e por não operarem em regime contínuo. Com o desenvolvimento tecnológico nas aeronaves mais recentes, estas se tornaram mais dependentes de eletricidade e considerando-se o mesmo porte, os valores gerados aumentaram de 240 kVA para 1000 kVA. Neste cenário, perdas não podem ser desprezadas e outras opções para aumento da eficiência devem ser consideradas. Núcleos de transformadores feitos de ligas amorfas à base de Fe apresentam redução em até 70% nas perdas quando operados em 50-60 Hz. Entretanto os menores valores de saturação na indução magnética resultam em núcleos de maior massa que seus similares feitos em Fe-Si cristalino, sendo assim indesejável em aeronaves. Este trabalho discute que, quando consideradas as particularidades dos transformadores aeronáuticos, pode-se projetar um transformador feito com liga amorfa com menores massa e perdas que um similar de mesma potência feito com Fe-Si cristalino. Para tal construiu-se artesanalmente um transformador com núcleo de liga amorfa para operação em 400 Hz, que foi tratado termomagneticamente para melhorar as suas propriedades eletromagnéticas. Através de ensaios elétricos, se obteve circuitos equivalentes do transformador com núcleo sem e com tratamentos termomagnéticos. Comparações de massas e perdas entre um transformador para aeronaves feito de material cristalino e o transformador construído artesanalmente mostram que o último possui menores perdas, e que quando seguidas todas as particularidades dos transformadores aeronáuticos, estes podem ter menores massas. Detalhes e explicações sobre o tratamento termomagnético, constatação da não cristalização do núcleo por difração de raios X após tratamento e avaliação através de simulação do transformador construído artesanalmente também estão incluídos neste trabalho.Não recebi financiamentoporUniversidade Federal de São CarlosCâmpus São CarlosPrograma de Pós-Graduação em Ciência e Engenharia de Materiais - PPGCEMUFSCarAeronavesLiga amorfaTransformadores aeronáuticosENGENHARIASTransformadores elétricos com núcleo de liga amorfa para aplicação em aeronavesApplicability of electric transformers with amorphous alloy core for use in aircraftsinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesisOnline6002b508166-b635-4fb0-a91b-419736667f7finfo:eu-repo/semantics/openAccessreponame:Repositório Institucional da UFSCARinstname:Universidade Federal de São Carlos (UFSCAR)instacron:UFSCARORIGINALDissWAS.pdfDissWAS.pdfapplication/pdf2629604https://repositorio.ufscar.br/bitstream/ufscar/7627/1/DissWAS.pdfc63cb2f3eca6f8313a2ce1352052ed4cMD51LICENSElicense.txtlicense.txttext/plain; charset=utf-81957https://repositorio.ufscar.br/bitstream/ufscar/7627/2/license.txtae0398b6f8b235e40ad82cba6c50031dMD52TEXTDissWAS.pdf.txtDissWAS.pdf.txtExtracted texttext/plain125983https://repositorio.ufscar.br/bitstream/ufscar/7627/3/DissWAS.pdf.txt81d4a9e080a25e3087e9b843201e85fbMD53THUMBNAILDissWAS.pdf.jpgDissWAS.pdf.jpgIM Thumbnailimage/jpeg6153https://repositorio.ufscar.br/bitstream/ufscar/7627/4/DissWAS.pdf.jpgaba96872bdf9146cc1746441f74aa641MD54ufscar/76272023-09-18 18:30:52.484oai:repositorio.ufscar.br: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Repositório InstitucionalPUBhttps://repositorio.ufscar.br/oai/requestopendoar:43222023-09-18T18:30:52Repositório Institucional da UFSCAR - Universidade Federal de São Carlos (UFSCAR)false |
dc.title.por.fl_str_mv |
Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves |
dc.title.alternative.eng.fl_str_mv |
Applicability of electric transformers with amorphous alloy core for use in aircrafts |
title |
Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves |
spellingShingle |
Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves Silva, Wagner Angelo da Aeronaves Liga amorfa Transformadores aeronáuticos ENGENHARIAS |
title_short |
Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves |
title_full |
Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves |
title_fullStr |
Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves |
title_full_unstemmed |
Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves |
title_sort |
Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves |
author |
Silva, Wagner Angelo da |
author_facet |
Silva, Wagner Angelo da |
author_role |
author |
dc.contributor.authorlattes.por.fl_str_mv |
http://lattes.cnpq.br/5336516408192676 |
dc.contributor.author.fl_str_mv |
Silva, Wagner Angelo da |
dc.contributor.advisor1.fl_str_mv |
Jorge Júnior, Alberto Moreira |
dc.contributor.advisor1Lattes.fl_str_mv |
http://lattes.cnpq.br/6360362248108490 |
dc.contributor.authorID.fl_str_mv |
090f2c97-1e47-4a12-a8f7-1e8602c636e8 |
contributor_str_mv |
Jorge Júnior, Alberto Moreira |
dc.subject.por.fl_str_mv |
Aeronaves Liga amorfa Transformadores aeronáuticos |
topic |
Aeronaves Liga amorfa Transformadores aeronáuticos ENGENHARIAS |
dc.subject.cnpq.fl_str_mv |
ENGENHARIAS |
description |
In order to reduce the mass of eletrical transformers and generators in aircrafts, many manufacturers have adopted 400 Hz as the operation of these devices. However this frequency causes increased core losses which were disregarded due to the small involved powers and non continuous basis operations. By considering similar sizes, newer aircraft models are more electricity dependent and the generated power increased from 240 kVA to 1000 kVA. In this new scenario losses cannot be neglected and other options for increased efficiency should be considered. Iron-based amorphous transformer cores AEFture reduction by up to 70% loss while operating in 50- 60 Hz. However smaller magnetic saturation induction values result in higher weight than similar cores made of crystalline Fe-Si, therefore, undesirable in aircraft. This work discusses that, when particularities of aeronautical transformers are considered, one can design a power transformer with an amorphous core with smaller mass and losses than a similar with a Fe-Si crystalline based core. For this purpose, a hand-made amorphous core transformer was built to operate at 400 Hz, which has been thermo-magnetically treated to enhance its electromagnetic properties. Through electrical test, equivalent circuits of transformer were obtained for both core conditions: unannealed and annealed. Comparisons of masses and losses between an aircraft transformer with crystalline core and the hand-made amorphous one show that the latter has lower losses and that, when obeyed the particularities for aeronautical transformers, they may have smaller masses. Details and explanations about the thermomagnetic treatment, evidencing by X-ray diffraction of no-crystallization, after core heat-treatment and hand-made transformer evaluation through simulation are also included in this work. |
publishDate |
2015 |
dc.date.issued.fl_str_mv |
2015-04-28 |
dc.date.accessioned.fl_str_mv |
2016-10-04T17:58:45Z |
dc.date.available.fl_str_mv |
2016-10-04T17:58:45Z |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/masterThesis |
format |
masterThesis |
status_str |
publishedVersion |
dc.identifier.citation.fl_str_mv |
SILVA, Wagner Angelo da. Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves. 2015. Dissertação (Mestrado em Ciência e Engenharia de Materiais) – Universidade Federal de São Carlos, São Carlos, 2015. Disponível em: https://repositorio.ufscar.br/handle/ufscar/7627. |
dc.identifier.uri.fl_str_mv |
https://repositorio.ufscar.br/handle/ufscar/7627 |
identifier_str_mv |
SILVA, Wagner Angelo da. Transformadores elétricos com núcleo de liga amorfa para aplicação em aeronaves. 2015. Dissertação (Mestrado em Ciência e Engenharia de Materiais) – Universidade Federal de São Carlos, São Carlos, 2015. Disponível em: https://repositorio.ufscar.br/handle/ufscar/7627. |
url |
https://repositorio.ufscar.br/handle/ufscar/7627 |
dc.language.iso.fl_str_mv |
por |
language |
por |
dc.relation.confidence.fl_str_mv |
600 |
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2b508166-b635-4fb0-a91b-419736667f7f |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.publisher.none.fl_str_mv |
Universidade Federal de São Carlos Câmpus São Carlos |
dc.publisher.program.fl_str_mv |
Programa de Pós-Graduação em Ciência e Engenharia de Materiais - PPGCEM |
dc.publisher.initials.fl_str_mv |
UFSCar |
publisher.none.fl_str_mv |
Universidade Federal de São Carlos Câmpus São Carlos |
dc.source.none.fl_str_mv |
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UFSCAR |
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Repositório Institucional da UFSCAR |
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