Construction of a Morphing Wing Rib Actuated by a NiTi Wire

Detalhes bibliográficos
Autor(a) principal: Almeida,Thais Campos de
Data de Publicação: 2015
Outros Autores: Santos,Osmar de Sousa, Otubo,Jorge
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=S2175-91462015000400454
Resumo: ABSTRACT: The main goal of this paper is to analyze if it is feasible to employ a trained shape memory alloy wire as a linear actuator to modify the camber of a morphing wing rib. In order to achieve this purpose, a morphing rib with a compliant trailing edge was proposed, developed, and subjected to structural analyses to ensure its flexibility. After the rib configuration was set, it was manufactured by a 3-D printer. The NiTi wire used as actuator was trained by a thermomechanical procedure based on a cycling process with a constant load application to present the two-way shape memory effect. In that way, the wire presents a determined length at its low-temperature phase and a shorter one at its high-temperature phase. Since the wire contraction and the torque applied by it are two crucial factors to define the camber curvature, it was decided to study two different wire lengths: 103.5 and 152.1 mm. The aerodynamic performance of the morphing cambered airfoils was studied using XFOIL software and compared to that of conventional airfoils with single hinged flap. The results show that both morphing airfoils present better aerodynamic performance for small angles of attack.
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spelling Construction of a Morphing Wing Rib Actuated by a NiTi WireNiTiMorphing airfoilCompliant mechanismsShape memory alloy actuatorTwo-way shape memory effectABSTRACT: The main goal of this paper is to analyze if it is feasible to employ a trained shape memory alloy wire as a linear actuator to modify the camber of a morphing wing rib. In order to achieve this purpose, a morphing rib with a compliant trailing edge was proposed, developed, and subjected to structural analyses to ensure its flexibility. After the rib configuration was set, it was manufactured by a 3-D printer. The NiTi wire used as actuator was trained by a thermomechanical procedure based on a cycling process with a constant load application to present the two-way shape memory effect. In that way, the wire presents a determined length at its low-temperature phase and a shorter one at its high-temperature phase. Since the wire contraction and the torque applied by it are two crucial factors to define the camber curvature, it was decided to study two different wire lengths: 103.5 and 152.1 mm. The aerodynamic performance of the morphing cambered airfoils was studied using XFOIL software and compared to that of conventional airfoils with single hinged flap. The results show that both morphing airfoils present better aerodynamic performance for small angles of attack.Departamento de Ciência e Tecnologia Aeroespacial2015-12-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462015000400454Journal of Aerospace Technology and Management v.7 n.4 2015reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v7i4.532info:eu-repo/semantics/openAccessAlmeida,Thais Campos deSantos,Osmar de SousaOtubo,Jorgeeng2017-05-23T00:00:00Zoai:scielo:S2175-91462015000400454Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-23T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Construction of a Morphing Wing Rib Actuated by a NiTi Wire
title Construction of a Morphing Wing Rib Actuated by a NiTi Wire
spellingShingle Construction of a Morphing Wing Rib Actuated by a NiTi Wire
Almeida,Thais Campos de
NiTi
Morphing airfoil
Compliant mechanisms
Shape memory alloy actuator
Two-way shape memory effect
title_short Construction of a Morphing Wing Rib Actuated by a NiTi Wire
title_full Construction of a Morphing Wing Rib Actuated by a NiTi Wire
title_fullStr Construction of a Morphing Wing Rib Actuated by a NiTi Wire
title_full_unstemmed Construction of a Morphing Wing Rib Actuated by a NiTi Wire
title_sort Construction of a Morphing Wing Rib Actuated by a NiTi Wire
author Almeida,Thais Campos de
author_facet Almeida,Thais Campos de
Santos,Osmar de Sousa
Otubo,Jorge
author_role author
author2 Santos,Osmar de Sousa
Otubo,Jorge
author2_role author
author
dc.contributor.author.fl_str_mv Almeida,Thais Campos de
Santos,Osmar de Sousa
Otubo,Jorge
dc.subject.por.fl_str_mv NiTi
Morphing airfoil
Compliant mechanisms
Shape memory alloy actuator
Two-way shape memory effect
topic NiTi
Morphing airfoil
Compliant mechanisms
Shape memory alloy actuator
Two-way shape memory effect
description ABSTRACT: The main goal of this paper is to analyze if it is feasible to employ a trained shape memory alloy wire as a linear actuator to modify the camber of a morphing wing rib. In order to achieve this purpose, a morphing rib with a compliant trailing edge was proposed, developed, and subjected to structural analyses to ensure its flexibility. After the rib configuration was set, it was manufactured by a 3-D printer. The NiTi wire used as actuator was trained by a thermomechanical procedure based on a cycling process with a constant load application to present the two-way shape memory effect. In that way, the wire presents a determined length at its low-temperature phase and a shorter one at its high-temperature phase. Since the wire contraction and the torque applied by it are two crucial factors to define the camber curvature, it was decided to study two different wire lengths: 103.5 and 152.1 mm. The aerodynamic performance of the morphing cambered airfoils was studied using XFOIL software and compared to that of conventional airfoils with single hinged flap. The results show that both morphing airfoils present better aerodynamic performance for small angles of attack.
publishDate 2015
dc.date.none.fl_str_mv 2015-12-01
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=S2175-91462015000400454
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462015000400454
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v7i4.532
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.7 n.4 2015
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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