Construction Methods and Comparative Evaluation of Metal Deployable Load-carrying Shell Structures
Autor(a) principal: | |
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Data de Publicação: | 2018 |
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=S2175-91462018000100332 |
Resumo: | ABSTRACT: This study describes the main regularities for the construction of deployable metal shells of a cylindrical type. The comparative analysis of the efficiency of compact folding methods of thin metal shells of cylindrical and conical types, capable of maintaining the initial load-carrying capacity after unfolding without applying the additional strengthening methods, is presented. The range of possible parameters of long-length structures, constructed on the basis of rigid deployable pressurized shells, is characterized. The paper gives the qualitative and quantitative evaluation of basic functional characteristics of folding inflatable metal structures of cylindrical and conical types under the action of a complex of characteristic external loads, close to the maximum allowable ones. The result of experimental operability confirmation of the proposed structures' configurations is presented. |
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Journal of Aerospace Technology and Management (Online) |
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Construction Methods and Comparative Evaluation of Metal Deployable Load-carrying Shell StructuresTransformable-volume structuresLoad-carrying shellsFoldable shellsDeployable structuresInflatable structuresSurfaces of zero total curvatureABSTRACT: This study describes the main regularities for the construction of deployable metal shells of a cylindrical type. The comparative analysis of the efficiency of compact folding methods of thin metal shells of cylindrical and conical types, capable of maintaining the initial load-carrying capacity after unfolding without applying the additional strengthening methods, is presented. The range of possible parameters of long-length structures, constructed on the basis of rigid deployable pressurized shells, is characterized. The paper gives the qualitative and quantitative evaluation of basic functional characteristics of folding inflatable metal structures of cylindrical and conical types under the action of a complex of characteristic external loads, close to the maximum allowable ones. The result of experimental operability confirmation of the proposed structures' configurations is presented.Departamento de Ciência e Tecnologia Aeroespacial2018-01-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462018000100332Journal of Aerospace Technology and Management v.10 2018reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v10.959info:eu-repo/semantics/openAccessLobanov,LeonidVolkov,ValentinYakimkin,Alexandereng2018-09-04T00:00:00Zoai:scielo:S2175-91462018000100332Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2018-09-04T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false |
dc.title.none.fl_str_mv |
Construction Methods and Comparative Evaluation of Metal Deployable Load-carrying Shell Structures |
title |
Construction Methods and Comparative Evaluation of Metal Deployable Load-carrying Shell Structures |
spellingShingle |
Construction Methods and Comparative Evaluation of Metal Deployable Load-carrying Shell Structures Lobanov,Leonid Transformable-volume structures Load-carrying shells Foldable shells Deployable structures Inflatable structures Surfaces of zero total curvature |
title_short |
Construction Methods and Comparative Evaluation of Metal Deployable Load-carrying Shell Structures |
title_full |
Construction Methods and Comparative Evaluation of Metal Deployable Load-carrying Shell Structures |
title_fullStr |
Construction Methods and Comparative Evaluation of Metal Deployable Load-carrying Shell Structures |
title_full_unstemmed |
Construction Methods and Comparative Evaluation of Metal Deployable Load-carrying Shell Structures |
title_sort |
Construction Methods and Comparative Evaluation of Metal Deployable Load-carrying Shell Structures |
author |
Lobanov,Leonid |
author_facet |
Lobanov,Leonid Volkov,Valentin Yakimkin,Alexander |
author_role |
author |
author2 |
Volkov,Valentin Yakimkin,Alexander |
author2_role |
author author |
dc.contributor.author.fl_str_mv |
Lobanov,Leonid Volkov,Valentin Yakimkin,Alexander |
dc.subject.por.fl_str_mv |
Transformable-volume structures Load-carrying shells Foldable shells Deployable structures Inflatable structures Surfaces of zero total curvature |
topic |
Transformable-volume structures Load-carrying shells Foldable shells Deployable structures Inflatable structures Surfaces of zero total curvature |
description |
ABSTRACT: This study describes the main regularities for the construction of deployable metal shells of a cylindrical type. The comparative analysis of the efficiency of compact folding methods of thin metal shells of cylindrical and conical types, capable of maintaining the initial load-carrying capacity after unfolding without applying the additional strengthening methods, is presented. The range of possible parameters of long-length structures, constructed on the basis of rigid deployable pressurized shells, is characterized. The paper gives the qualitative and quantitative evaluation of basic functional characteristics of folding inflatable metal structures of cylindrical and conical types under the action of a complex of characteristic external loads, close to the maximum allowable ones. The result of experimental operability confirmation of the proposed structures' configurations is presented. |
publishDate |
2018 |
dc.date.none.fl_str_mv |
2018-01-01 |
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=S2175-91462018000100332 |
url |
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462018000100332 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
10.5028/jatm.v10.959 |
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.10 2018 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_ |
1754732531981221888 |