Development of bi-stable and millimeter-scale displacement actuator using snap-through effect for reciprocating control fins

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dc.contributor.authorKang, Choon-Gilko
dc.contributor.authorLee, Jun-Seongko
dc.contributor.authorHan, Jae-Hungko
dc.date.accessioned2014-08-27-
dc.date.available2014-08-27-
dc.date.created2014-02-12-
dc.date.created2014-02-12-
dc.date.created2014-02-12-
dc.date.issued2014-01-
dc.identifier.citationAEROSPACE SCIENCE AND TECHNOLOGY, v.32, no.1, pp.131 - 141-
dc.identifier.issn1270-9638-
dc.identifier.urihttp://hdl.handle.net/10203/187203-
dc.description.abstractA new two-step amplifying mechanism combining a lever-arm with flexure hinges and a pre-curved thin shell structure is proposed to make a millimeter-scale linear actuator. A large amplification ratio can be obtained by the snap-through effect of a post-buckled shell structure without losing actuation force. The snap-through phenomenon of pre-curved thin-plate are numerically analyzed by using the finite-element software ABAQUS to specify the trigger force and displacement required to initiate the snap-through. The analytic results are in good agreement with the test results for the pre-curved shell structure. The trigger force and displacement for snap-through are supplied by the lever-arm with the piezo stack actuator. Amplification ratio of the lever-arm is drastically changed according to the external load. The lever-arm mechanism is designed to have enough actuation force and displacement to satisfy requirements such as trigger force and displacement of the bi-stable structure. The components of the designed actuators are manufactured and integrated. The designed two-step amplified actuator is experimentally validated to operate with an 8 mm stroke and 2 Hz bandwidth. (C) 2013 Elsevier Masson SAS. All rights reserved.-
dc.languageEnglish-
dc.publisherELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER-
dc.titleDevelopment of bi-stable and millimeter-scale displacement actuator using snap-through effect for reciprocating control fins-
dc.typeArticle-
dc.identifier.wosid000331921900015-
dc.identifier.scopusid2-s2.0-84892725552-
dc.type.rimsART-
dc.citation.volume32-
dc.citation.issue1-
dc.citation.beginningpage131-
dc.citation.endingpage141-
dc.citation.publicationnameAEROSPACE SCIENCE AND TECHNOLOGY-
dc.identifier.doi10.1016/j.ast.2013.11.007-
dc.embargo.liftdate9999-12-31-
dc.embargo.terms9999-12-31-
dc.contributor.localauthorHan, Jae-Hung-
dc.contributor.nonIdAuthorKang, Choon-Gil-
dc.type.journalArticleArticle-
dc.subject.keywordAuthorBi-stable-
dc.subject.keywordAuthorSnap-through-
dc.subject.keywordAuthorPost-buckling-
dc.subject.keywordAuthorPiezo stack actuator-
dc.subject.keywordAuthorDisplacement amplification-
dc.subject.keywordAuthorReciprocating control fin-
dc.subject.keywordPlusPIEZOELECTRIC ACTUATORS-
dc.subject.keywordPlusCOMPOSITES-
dc.subject.keywordPlusMECHANISMS-
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AE-Journal Papers(저널논문)
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