Nonlinear Characteristic of Spherical Joints with Clearance

Detalhes bibliográficos
Autor(a) principal: Jing,Zhang
Data de Publicação: 2015
Outros Autores: Hong-Wei,Guo, Rong-Qiang,Liu, Zong-Quan,Deng
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=S2175-91462015000200179
Resumo: ABSTRACT: Joints in deployable structures can degrade the stiffness and the stability of spacecraft. In this study, the nonlinear stiffness of spherical joints is investigated. The traditional contact model of spherical joints based on non-conforming contact assumption is presented. A new contact model for spherical joints based on the Winkler model and geometric constraints is established to calculate the stiffness of spherical joints with small clearances. The finite element model (FEM) of spherical joints is built to evaluate the accuracy of the theoretical model. The effects of the clearance and the contact force of spherical joints on the deformation of joints are investigated. When compared with FEM results, the error of the new spherical model is smaller than that of the traditional contact model when the clearance of spherical joint is not excessively large. The new contact model for spherical joint is more accurate than the traditional contact model when the clearance of spherical joint is large.
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spelling Nonlinear Characteristic of Spherical Joints with ClearanceDeployable structureNonlinear characteristicJointStiffnessABSTRACT: Joints in deployable structures can degrade the stiffness and the stability of spacecraft. In this study, the nonlinear stiffness of spherical joints is investigated. The traditional contact model of spherical joints based on non-conforming contact assumption is presented. A new contact model for spherical joints based on the Winkler model and geometric constraints is established to calculate the stiffness of spherical joints with small clearances. The finite element model (FEM) of spherical joints is built to evaluate the accuracy of the theoretical model. The effects of the clearance and the contact force of spherical joints on the deformation of joints are investigated. When compared with FEM results, the error of the new spherical model is smaller than that of the traditional contact model when the clearance of spherical joint is not excessively large. The new contact model for spherical joint is more accurate than the traditional contact model when the clearance of spherical joint is large.Departamento de Ciência e Tecnologia Aeroespacial2015-06-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462015000200179Journal of Aerospace Technology and Management v.7 n.2 2015reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v7i2.464info:eu-repo/semantics/openAccessJing,ZhangHong-Wei,GuoRong-Qiang,LiuZong-Quan,Dengeng2017-05-25T00:00:00Zoai:scielo:S2175-91462015000200179Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-25T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Nonlinear Characteristic of Spherical Joints with Clearance
title Nonlinear Characteristic of Spherical Joints with Clearance
spellingShingle Nonlinear Characteristic of Spherical Joints with Clearance
Jing,Zhang
Deployable structure
Nonlinear characteristic
Joint
Stiffness
title_short Nonlinear Characteristic of Spherical Joints with Clearance
title_full Nonlinear Characteristic of Spherical Joints with Clearance
title_fullStr Nonlinear Characteristic of Spherical Joints with Clearance
title_full_unstemmed Nonlinear Characteristic of Spherical Joints with Clearance
title_sort Nonlinear Characteristic of Spherical Joints with Clearance
author Jing,Zhang
author_facet Jing,Zhang
Hong-Wei,Guo
Rong-Qiang,Liu
Zong-Quan,Deng
author_role author
author2 Hong-Wei,Guo
Rong-Qiang,Liu
Zong-Quan,Deng
author2_role author
author
author
dc.contributor.author.fl_str_mv Jing,Zhang
Hong-Wei,Guo
Rong-Qiang,Liu
Zong-Quan,Deng
dc.subject.por.fl_str_mv Deployable structure
Nonlinear characteristic
Joint
Stiffness
topic Deployable structure
Nonlinear characteristic
Joint
Stiffness
description ABSTRACT: Joints in deployable structures can degrade the stiffness and the stability of spacecraft. In this study, the nonlinear stiffness of spherical joints is investigated. The traditional contact model of spherical joints based on non-conforming contact assumption is presented. A new contact model for spherical joints based on the Winkler model and geometric constraints is established to calculate the stiffness of spherical joints with small clearances. The finite element model (FEM) of spherical joints is built to evaluate the accuracy of the theoretical model. The effects of the clearance and the contact force of spherical joints on the deformation of joints are investigated. When compared with FEM results, the error of the new spherical model is smaller than that of the traditional contact model when the clearance of spherical joint is not excessively large. The new contact model for spherical joint is more accurate than the traditional contact model when the clearance of spherical joint is large.
publishDate 2015
dc.date.none.fl_str_mv 2015-06-01
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=S2175-91462015000200179
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462015000200179
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v7i2.464
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.2 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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