Characterization of titanium welded joints by the orbital gas tungsten arc welding process for aerospace application
Autor(a) principal: | |
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Data de Publicação: | 2010 |
Outros Autores: | , , , , |
Tipo de documento: | Artigo |
Idioma: | eng |
Título da fonte: | Repositório Institucional da UNESP |
Texto Completo: | http://dx.doi.org/10.5028/jatm.2010.02026710 http://hdl.handle.net/11449/212175 |
Resumo: | In this work, three welding programs for orbital gas tungsten arc welding (GTAW), previously developed, were used, using pulsed current and increasing speed (#A), constant current (#B) and pulsed current and decreasing current (#C). One of these should be used for the propulsion system of the Satellite CBERS (China - Brazil Earth Resources Satellite). Welded joints using tubes of commercially pure titanium were obtained with these procedures, which were characterized by means of mechanical and metallographic tests. The obtained results showed that the three welding procedures produce welded joints free of defects and with adequate shape. Although small differences on mechanical properties and on microstructure have been observed, the three welding programs attained compatible results with international standards used in the aerospace segment. The welding program #B, due to the reduced heat input used, was considered to obtain slightly advantage over the others. |
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Repositório Institucional da UNESP |
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Characterization of titanium welded joints by the orbital gas tungsten arc welding process for aerospace applicationOrbital GTAWTitaniumSatelliteIn this work, three welding programs for orbital gas tungsten arc welding (GTAW), previously developed, were used, using pulsed current and increasing speed (#A), constant current (#B) and pulsed current and decreasing current (#C). One of these should be used for the propulsion system of the Satellite CBERS (China - Brazil Earth Resources Satellite). Welded joints using tubes of commercially pure titanium were obtained with these procedures, which were characterized by means of mechanical and metallographic tests. The obtained results showed that the three welding procedures produce welded joints free of defects and with adequate shape. Although small differences on mechanical properties and on microstructure have been observed, the three welding programs attained compatible results with international standards used in the aerospace segment. The welding program #B, due to the reduced heat input used, was considered to obtain slightly advantage over the others.Instituto de Aeronáutica e EspaçoInstituto Nacional de Pesquisas EspaciaisUnivers. Estadual PaulistaInstituto Tecnológico de AeronáuticaUniversidade Estadual do Norte FluminenseDepartamento de Ciência e Tecnologia AeroespacialInstituto de Aeronáutica e EspaçoInstituto Nacional de Pesquisas EspaciaisUnivers. Estadual PaulistaInstituto Tecnológico de AeronáuticaUniversidade Estadual do Norte FluminenseGarcia, José A. Orlowski DeLima, Gérson Luiz DePereira, Wilson D. BocallãoGuimarães, Valdir AlvesMoura, Carlos DeParanhos, Ronaldo Pinheiro R.2021-07-14T10:35:52Z2021-07-14T10:35:52Z2010info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/article211-218application/pdfhttp://dx.doi.org/10.5028/jatm.2010.02026710Journal of Aerospace Technology and Management. Departamento de Ciência e Tecnologia Aeroespacial, v. 2, n. 2, p. 211-218, 2010.1984-96482175-9146http://hdl.handle.net/11449/21217510.5028/jatm.2010.02026710S2175-91462010000200211S2175-91462010000200211.pdfSciELOreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengJournal of Aerospace Technology and Managementinfo:eu-repo/semantics/openAccess2023-10-28T06:07:07Zoai:repositorio.unesp.br:11449/212175Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T16:14:10.243413Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false |
dc.title.none.fl_str_mv |
Characterization of titanium welded joints by the orbital gas tungsten arc welding process for aerospace application |
title |
Characterization of titanium welded joints by the orbital gas tungsten arc welding process for aerospace application |
spellingShingle |
Characterization of titanium welded joints by the orbital gas tungsten arc welding process for aerospace application Garcia, José A. Orlowski De Orbital GTAW Titanium Satellite |
title_short |
Characterization of titanium welded joints by the orbital gas tungsten arc welding process for aerospace application |
title_full |
Characterization of titanium welded joints by the orbital gas tungsten arc welding process for aerospace application |
title_fullStr |
Characterization of titanium welded joints by the orbital gas tungsten arc welding process for aerospace application |
title_full_unstemmed |
Characterization of titanium welded joints by the orbital gas tungsten arc welding process for aerospace application |
title_sort |
Characterization of titanium welded joints by the orbital gas tungsten arc welding process for aerospace application |
author |
Garcia, José A. Orlowski De |
author_facet |
Garcia, José A. Orlowski De Lima, Gérson Luiz De Pereira, Wilson D. Bocallão Guimarães, Valdir Alves Moura, Carlos De Paranhos, Ronaldo Pinheiro R. |
author_role |
author |
author2 |
Lima, Gérson Luiz De Pereira, Wilson D. Bocallão Guimarães, Valdir Alves Moura, Carlos De Paranhos, Ronaldo Pinheiro R. |
author2_role |
author author author author author |
dc.contributor.none.fl_str_mv |
Instituto de Aeronáutica e Espaço Instituto Nacional de Pesquisas Espaciais Univers. Estadual Paulista Instituto Tecnológico de Aeronáutica Universidade Estadual do Norte Fluminense |
dc.contributor.author.fl_str_mv |
Garcia, José A. Orlowski De Lima, Gérson Luiz De Pereira, Wilson D. Bocallão Guimarães, Valdir Alves Moura, Carlos De Paranhos, Ronaldo Pinheiro R. |
dc.subject.por.fl_str_mv |
Orbital GTAW Titanium Satellite |
topic |
Orbital GTAW Titanium Satellite |
description |
In this work, three welding programs for orbital gas tungsten arc welding (GTAW), previously developed, were used, using pulsed current and increasing speed (#A), constant current (#B) and pulsed current and decreasing current (#C). One of these should be used for the propulsion system of the Satellite CBERS (China - Brazil Earth Resources Satellite). Welded joints using tubes of commercially pure titanium were obtained with these procedures, which were characterized by means of mechanical and metallographic tests. The obtained results showed that the three welding procedures produce welded joints free of defects and with adequate shape. Although small differences on mechanical properties and on microstructure have been observed, the three welding programs attained compatible results with international standards used in the aerospace segment. The welding program #B, due to the reduced heat input used, was considered to obtain slightly advantage over the others. |
publishDate |
2010 |
dc.date.none.fl_str_mv |
2010 2021-07-14T10:35:52Z 2021-07-14T10:35:52Z |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/article |
format |
article |
status_str |
publishedVersion |
dc.identifier.uri.fl_str_mv |
http://dx.doi.org/10.5028/jatm.2010.02026710 Journal of Aerospace Technology and Management. Departamento de Ciência e Tecnologia Aeroespacial, v. 2, n. 2, p. 211-218, 2010. 1984-9648 2175-9146 http://hdl.handle.net/11449/212175 10.5028/jatm.2010.02026710 S2175-91462010000200211 S2175-91462010000200211.pdf |
url |
http://dx.doi.org/10.5028/jatm.2010.02026710 http://hdl.handle.net/11449/212175 |
identifier_str_mv |
Journal of Aerospace Technology and Management. Departamento de Ciência e Tecnologia Aeroespacial, v. 2, n. 2, p. 211-218, 2010. 1984-9648 2175-9146 10.5028/jatm.2010.02026710 S2175-91462010000200211 S2175-91462010000200211.pdf |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
Journal of Aerospace Technology and Management |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.format.none.fl_str_mv |
211-218 application/pdf |
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 |
SciELO reponame:Repositório Institucional da UNESP instname:Universidade Estadual Paulista (UNESP) instacron:UNESP |
instname_str |
Universidade Estadual Paulista (UNESP) |
instacron_str |
UNESP |
institution |
UNESP |
reponame_str |
Repositório Institucional da UNESP |
collection |
Repositório Institucional da UNESP |
repository.name.fl_str_mv |
Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP) |
repository.mail.fl_str_mv |
|
_version_ |
1808128623014576128 |