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contributor authorStacey, Jonathan P.
contributor authorO'Donnell, Matthew P.
contributor authorSchenk, Mark
date accessioned2019-03-17T10:09:23Z
date available2019-03-17T10:09:23Z
date copyright2/22/2019 12:00:00 AM
date issued2019
identifier issn1942-4302
identifier otherjmr_011_02_020908.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4255952
description abstractThis paper explores the ability to tailor the mechanical properties of composite compliant shell mechanisms, by exploiting the thermal prestress introduced during the composite laminate cure. An extension of an analytical tape spring model with composite thermal analysis is presented, and the effect of the thermal prestress is studied by means of energy landscapes for the cylindrical composite shells. Tape springs that would otherwise be monostable structures become bistable and exhibit greater ranges of low-energy twisting with thermally induced prestress. Predicted shell geometries are compared with finite element (FE) results and manufactured samples, showing good agreement between all approaches. Wider challenges around the manufacture of prestressed composite compliant mechanisms are discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermal Prestress in Composite Compliant Shell Mechanisms
typeJournal Paper
journal volume11
journal issue2
journal titleJournal of Mechanisms and Robotics
identifier doi10.1115/1.4042476
journal fristpage20908
journal lastpage020908-8
treeJournal of Mechanisms and Robotics:;2019:;volume( 011 ):;issue: 002
contenttypeFulltext


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