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contributor authorJ. C. Yee
contributor authorS. Pellegrino
date accessioned2017-05-08T21:16:14Z
date available2017-05-08T21:16:14Z
date copyrightOctober 2005
date issued2005
identifier other%28asce%290893-1321%282005%2918%3A4%28224%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45040
description abstractThis paper is concerned with self-powered, self-latching tube hinges, made by cutting three parallel slots in a thin-walled carbon fiber reinforced plastic tube with a circular cross section. Thus, a hinge consists of two short tubes connected by three transversally curved strips of material (known as tape springs). A particular tube hinge design is considered, with a diameter of about one-third that of the hinges used previously; this requires the tape springs to reach strains close to failure when the hinge is folded. Three analyses of the peak strains in a tube hinge are presented. The first analysis obtains general analytical expressions for the longitudinal fold radius of a tape spring and the associated peak fiber strains. The second analysis is a finite-element simulation of the folding of a single tape spring and the third analysis is a simulation of a complete tube hinge. It is found that the largest fiber strains in one- and two-ply hinges can be predicted analytically with very good accuracy. It is also found that the contact and interaction between the three tape springs that form a tube hinge, modeled in the third analysis, do not affect the peak strains significantly.
publisherAmerican Society of Civil Engineers
titleComposite Tube Hinges
typeJournal Paper
journal volume18
journal issue4
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2005)18:4(224)
treeJournal of Aerospace Engineering:;2005:;Volume ( 018 ):;issue: 004
contenttypeFulltext


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