Optimizing the e-beam profile of a single carbon nanotube field emission device for electric propulsion systems

Detalhes bibliográficos
Autor(a) principal: Mologni,Juliano Fujioka
Data de Publicação: 2010
Outros Autores: Alves,Marco Antonio Robert, Braumgratz,Filipe, Fonseca,Edson, Siqueira,Cesareo L. R., Braga,Edmundo Silva
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=S2175-91462010000100009
Resumo: Abstract: Preliminary studies on field emission (FE) arrays comprised of carbon nanotubes (CNT) as an electron source for electric propulsion system show remarkably promising results. Design parameters for a carbon nanotube (CNT) field-emission device operating on triode configuration were numerically simulated and optimized in order to enhance the e-beam focusing quality. An additional focus gate (FG) was integrated to the device to control the profile of the emitted e-beam. An axisymmetric finite element model was developed to calculate the electric field distribution on the vacuum region and a modified Fowler-Nordheim (FN) equation was used to evaluate the current density emission and the effective emitter area. Afterward, a FE simulation was employed in order to calculate the trajectory of the emitted electrons and define the electron-optical properties of the e-beam. The integration of the FG was fully investigated via computational intelligence techniques. The best performance device according to our simulations presents a collimated e-beam profile that suits well for field emission displays, magnetic field detection and electron microscopy. The automated computational design tool presented in this study strongly benefits the robust design of integrated electron-optical systems for vacuum field emission applications, including electrodynamic tethering and electric propulsion systems.
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spelling Optimizing the e-beam profile of a single carbon nanotube field emission device for electric propulsion systemsElectric propulsionCarbon nanotubeFinite element analysisAbstract: Preliminary studies on field emission (FE) arrays comprised of carbon nanotubes (CNT) as an electron source for electric propulsion system show remarkably promising results. Design parameters for a carbon nanotube (CNT) field-emission device operating on triode configuration were numerically simulated and optimized in order to enhance the e-beam focusing quality. An additional focus gate (FG) was integrated to the device to control the profile of the emitted e-beam. An axisymmetric finite element model was developed to calculate the electric field distribution on the vacuum region and a modified Fowler-Nordheim (FN) equation was used to evaluate the current density emission and the effective emitter area. Afterward, a FE simulation was employed in order to calculate the trajectory of the emitted electrons and define the electron-optical properties of the e-beam. The integration of the FG was fully investigated via computational intelligence techniques. The best performance device according to our simulations presents a collimated e-beam profile that suits well for field emission displays, magnetic field detection and electron microscopy. The automated computational design tool presented in this study strongly benefits the robust design of integrated electron-optical systems for vacuum field emission applications, including electrodynamic tethering and electric propulsion systems.Departamento de Ciência e Tecnologia Aeroespacial2010-04-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462010000100009Journal of Aerospace Technology and Management v.2 n.1 2010reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.2010.02010915info:eu-repo/semantics/openAccessMologni,Juliano FujiokaAlves,Marco Antonio RobertBraumgratz,FilipeFonseca,EdsonSiqueira,Cesareo L. R.Braga,Edmundo Silvaeng2017-05-29T00:00:00Zoai:scielo:S2175-91462010000100009Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-29T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Optimizing the e-beam profile of a single carbon nanotube field emission device for electric propulsion systems
title Optimizing the e-beam profile of a single carbon nanotube field emission device for electric propulsion systems
spellingShingle Optimizing the e-beam profile of a single carbon nanotube field emission device for electric propulsion systems
Mologni,Juliano Fujioka
Electric propulsion
Carbon nanotube
Finite element analysis
title_short Optimizing the e-beam profile of a single carbon nanotube field emission device for electric propulsion systems
title_full Optimizing the e-beam profile of a single carbon nanotube field emission device for electric propulsion systems
title_fullStr Optimizing the e-beam profile of a single carbon nanotube field emission device for electric propulsion systems
title_full_unstemmed Optimizing the e-beam profile of a single carbon nanotube field emission device for electric propulsion systems
title_sort Optimizing the e-beam profile of a single carbon nanotube field emission device for electric propulsion systems
author Mologni,Juliano Fujioka
author_facet Mologni,Juliano Fujioka
Alves,Marco Antonio Robert
Braumgratz,Filipe
Fonseca,Edson
Siqueira,Cesareo L. R.
Braga,Edmundo Silva
author_role author
author2 Alves,Marco Antonio Robert
Braumgratz,Filipe
Fonseca,Edson
Siqueira,Cesareo L. R.
Braga,Edmundo Silva
author2_role author
author
author
author
author
dc.contributor.author.fl_str_mv Mologni,Juliano Fujioka
Alves,Marco Antonio Robert
Braumgratz,Filipe
Fonseca,Edson
Siqueira,Cesareo L. R.
Braga,Edmundo Silva
dc.subject.por.fl_str_mv Electric propulsion
Carbon nanotube
Finite element analysis
topic Electric propulsion
Carbon nanotube
Finite element analysis
description Abstract: Preliminary studies on field emission (FE) arrays comprised of carbon nanotubes (CNT) as an electron source for electric propulsion system show remarkably promising results. Design parameters for a carbon nanotube (CNT) field-emission device operating on triode configuration were numerically simulated and optimized in order to enhance the e-beam focusing quality. An additional focus gate (FG) was integrated to the device to control the profile of the emitted e-beam. An axisymmetric finite element model was developed to calculate the electric field distribution on the vacuum region and a modified Fowler-Nordheim (FN) equation was used to evaluate the current density emission and the effective emitter area. Afterward, a FE simulation was employed in order to calculate the trajectory of the emitted electrons and define the electron-optical properties of the e-beam. The integration of the FG was fully investigated via computational intelligence techniques. The best performance device according to our simulations presents a collimated e-beam profile that suits well for field emission displays, magnetic field detection and electron microscopy. The automated computational design tool presented in this study strongly benefits the robust design of integrated electron-optical systems for vacuum field emission applications, including electrodynamic tethering and electric propulsion systems.
publishDate 2010
dc.date.none.fl_str_mv 2010-04-01
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=S2175-91462010000100009
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462010000100009
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.2010.02010915
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.2 n.1 2010
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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