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Article: Geometric design and mechanical behavior of a deployable cylinder with Miura origami

TitleGeometric design and mechanical behavior of a deployable cylinder with Miura origami
Authors
Keywordsorigami
Miura-ori
deployable cylinder
Issue Date2015
Citation
Smart Materials and Structures, 2015, v. 24, n. 12, p. 125031 How to Cite?
Abstract© 2015 IOP Publishing Ltd.The folding and deployment of a cylinder with Miura origami patterns are studied in this paper. First, the geometric formulation of the design problem is discussed. Then the loading case of the axial strains and corresponding external nodal loads applied on the vertices of the top polygon during the motion is investigated analytically. The influence of the angle between the diagonal and horizontal fold lines α and β and the number of Miura origami elements n on the dynamic behavior of the basic segment is also discussed. Then the dynamic behavior is analyzed using numerical simulations. Finally, the deployment process of a cylinder with multi-stories is discussed. The numerical results agree well with the analytical predictions. The results show that the range of motion, i.e. the maximal displacement of top nodes, will also increase with the increase of angles α and β. This cylinder, with a smaller n, may have a bistable behavior. When n is larger, the influence of n on the axial strains and external nodal loads is slight. The numerical results agree well with the analytical predictions. Moreover, the deployment of the cylinder with multi-stories is non-uniform, which deploys from the upper story to the lower story.
Persistent Identifierhttp://hdl.handle.net/10722/235950
ISSN
2023 Impact Factor: 3.7
2023 SCImago Journal Rankings: 0.872
ISI Accession Number ID

 

DC FieldValueLanguage
dc.contributor.authorCai, Jianguo-
dc.contributor.authorDeng, Xiaowei-
dc.contributor.authorFeng, Jian-
dc.contributor.authorZhou, Ya-
dc.date.accessioned2016-11-10T07:11:48Z-
dc.date.available2016-11-10T07:11:48Z-
dc.date.issued2015-
dc.identifier.citationSmart Materials and Structures, 2015, v. 24, n. 12, p. 125031-
dc.identifier.issn0964-1726-
dc.identifier.urihttp://hdl.handle.net/10722/235950-
dc.description.abstract© 2015 IOP Publishing Ltd.The folding and deployment of a cylinder with Miura origami patterns are studied in this paper. First, the geometric formulation of the design problem is discussed. Then the loading case of the axial strains and corresponding external nodal loads applied on the vertices of the top polygon during the motion is investigated analytically. The influence of the angle between the diagonal and horizontal fold lines α and β and the number of Miura origami elements n on the dynamic behavior of the basic segment is also discussed. Then the dynamic behavior is analyzed using numerical simulations. Finally, the deployment process of a cylinder with multi-stories is discussed. The numerical results agree well with the analytical predictions. The results show that the range of motion, i.e. the maximal displacement of top nodes, will also increase with the increase of angles α and β. This cylinder, with a smaller n, may have a bistable behavior. When n is larger, the influence of n on the axial strains and external nodal loads is slight. The numerical results agree well with the analytical predictions. Moreover, the deployment of the cylinder with multi-stories is non-uniform, which deploys from the upper story to the lower story.-
dc.languageeng-
dc.relation.ispartofSmart Materials and Structures-
dc.subjectorigami-
dc.subjectMiura-ori-
dc.subjectdeployable cylinder-
dc.titleGeometric design and mechanical behavior of a deployable cylinder with Miura origami-
dc.typeArticle-
dc.description.naturelink_to_subscribed_fulltext-
dc.identifier.doi10.1088/0964-1726/24/12/125031-
dc.identifier.scopuseid_2-s2.0-84948799161-
dc.identifier.hkuros275029-
dc.identifier.hkuros275024-
dc.identifier.volume24-
dc.identifier.issue12-
dc.identifier.spage125031-
dc.identifier.epage125031-
dc.identifier.eissn1361-665X-
dc.identifier.isiWOS:000366111500032-
dc.identifier.issnl0964-1726-

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