| contributor author | J. C. Yee | |
| contributor author | S. Pellegrino | |
| date accessioned | 2017-05-08T21:16:14Z | |
| date available | 2017-05-08T21:16:14Z | |
| date copyright | October 2005 | |
| date issued | 2005 | |
| identifier other | %28asce%290893-1321%282005%2918%3A4%28224%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/45040 | |
| description abstract | This 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. | |
| publisher | American Society of Civil Engineers | |
| title | Composite Tube Hinges | |
| type | Journal Paper | |
| journal volume | 18 | |
| journal issue | 4 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2005)18:4(224) | |
| tree | Journal of Aerospace Engineering:;2005:;Volume ( 018 ):;issue: 004 | |
| contenttype | Fulltext | |