Analytical solution of the bending of a bi-convex boom

This paper derives closed-form solutions for the local deformation of a bi-convex boom under circular bending, and the resulting strain energy and self-extending force. Convex tapes and bi-convex booms that consists of a pair of convex tapes can be stored into a small volume and have high specific r...

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Autores principales: Yasuyuki MIYAZAKI, Shota INOUE, Akihiro TAMURA
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Lenguaje:EN
Publicado: The Japan Society of Mechanical Engineers 2015
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Acceso en línea:https://doaj.org/article/ac3616a3c34845839aa8ff8b8e6d5a51
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spelling oai:doaj.org-article:ac3616a3c34845839aa8ff8b8e6d5a512021-11-26T06:32:15ZAnalytical solution of the bending of a bi-convex boom2187-974510.1299/mej.15-00465https://doaj.org/article/ac3616a3c34845839aa8ff8b8e6d5a512015-11-01T00:00:00Zhttps://www.jstage.jst.go.jp/article/mej/2/6/2_15-00465/_pdf/-char/enhttps://doaj.org/toc/2187-9745This paper derives closed-form solutions for the local deformation of a bi-convex boom under circular bending, and the resulting strain energy and self-extending force. Convex tapes and bi-convex booms that consists of a pair of convex tapes can be stored into a small volume and have high specific rigidity. They extert a self-extending force when stored cylindrically. Therefore, they have been proposed as members of deployable space structures. In this paper, two types of bi-convex booms are considered. In the first, the tapes of the bi-convex boom are bonded to each other at their edges; in the second, the tapes are wrapped in a cylindrical braid mesh. The latter is called a BCON (braid-coated bi-convex) boom. The tape of a BCON boom can slip on each other, and do not separate from each other because of the tension of the mesh net. Consequently, the BCON boom can be used in an ultralight self-deployable structure with quite high stowage volume efficiency and specific rigidity. However, structures using convex tapes or BCON booms have been designed and developed through a trial-and-error process because there is no appropriate formula for the self-extending force of convex tapes. This paper proposes a formula for the deformation of a convex tape that is initially bent into a circular shape. The deviation from the circular shape is obtained by solving the equilibrium equations. The deformation of a bi-convex boom is also derived by using the solution for a convex tape. Thus the theory described in this paper contributes to the design of space structures using convex tapes in bi-convex booms, as well as to the structural mechanics of flexible beams.Yasuyuki MIYAZAKIShota INOUEAkihiro TAMURAThe Japan Society of Mechanical Engineersarticleflexible structureself-deployable structureconvex boomnonlinear deformationanalytical solutionMechanical engineering and machineryTJ1-1570ENMechanical Engineering Journal, Vol 2, Iss 6, Pp 15-00465-15-00465 (2015)
institution DOAJ
collection DOAJ
language EN
topic flexible structure
self-deployable structure
convex boom
nonlinear deformation
analytical solution
Mechanical engineering and machinery
TJ1-1570
spellingShingle flexible structure
self-deployable structure
convex boom
nonlinear deformation
analytical solution
Mechanical engineering and machinery
TJ1-1570
Yasuyuki MIYAZAKI
Shota INOUE
Akihiro TAMURA
Analytical solution of the bending of a bi-convex boom
description This paper derives closed-form solutions for the local deformation of a bi-convex boom under circular bending, and the resulting strain energy and self-extending force. Convex tapes and bi-convex booms that consists of a pair of convex tapes can be stored into a small volume and have high specific rigidity. They extert a self-extending force when stored cylindrically. Therefore, they have been proposed as members of deployable space structures. In this paper, two types of bi-convex booms are considered. In the first, the tapes of the bi-convex boom are bonded to each other at their edges; in the second, the tapes are wrapped in a cylindrical braid mesh. The latter is called a BCON (braid-coated bi-convex) boom. The tape of a BCON boom can slip on each other, and do not separate from each other because of the tension of the mesh net. Consequently, the BCON boom can be used in an ultralight self-deployable structure with quite high stowage volume efficiency and specific rigidity. However, structures using convex tapes or BCON booms have been designed and developed through a trial-and-error process because there is no appropriate formula for the self-extending force of convex tapes. This paper proposes a formula for the deformation of a convex tape that is initially bent into a circular shape. The deviation from the circular shape is obtained by solving the equilibrium equations. The deformation of a bi-convex boom is also derived by using the solution for a convex tape. Thus the theory described in this paper contributes to the design of space structures using convex tapes in bi-convex booms, as well as to the structural mechanics of flexible beams.
format article
author Yasuyuki MIYAZAKI
Shota INOUE
Akihiro TAMURA
author_facet Yasuyuki MIYAZAKI
Shota INOUE
Akihiro TAMURA
author_sort Yasuyuki MIYAZAKI
title Analytical solution of the bending of a bi-convex boom
title_short Analytical solution of the bending of a bi-convex boom
title_full Analytical solution of the bending of a bi-convex boom
title_fullStr Analytical solution of the bending of a bi-convex boom
title_full_unstemmed Analytical solution of the bending of a bi-convex boom
title_sort analytical solution of the bending of a bi-convex boom
publisher The Japan Society of Mechanical Engineers
publishDate 2015
url https://doaj.org/article/ac3616a3c34845839aa8ff8b8e6d5a51
work_keys_str_mv AT yasuyukimiyazaki analyticalsolutionofthebendingofabiconvexboom
AT shotainoue analyticalsolutionofthebendingofabiconvexboom
AT akihirotamura analyticalsolutionofthebendingofabiconvexboom
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