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    Accommodating Thickness in Origami Based Deployable Arrays1

    Source: Journal of Mechanical Design:;2013:;volume( 135 ):;issue: 011::page 111005
    Author:
    Zirbel, Shannon A.
    ,
    Lang, Robert J.
    ,
    Thomson, Mark W.
    ,
    Sigel, Deborah A.
    ,
    Walkemeyer, Phillip E.
    ,
    Trease, Brian P.
    ,
    Magleby, Spencer P.
    ,
    Howell, Larry L.
    DOI: 10.1115/1.4025372
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The purpose of this work is to develop approaches to accommodate thickness in origamibased deployable arrays with a high ratio of deployedtostowed diameter. The origami flasher model serves as a basis for demonstrating the approach. A thicknessaccommodating mathematical model is developed to describe the flasher. Practical modifications are presented for the creation of physical models and two options are proposed: allowing the panels to fold along their diagonals or applying a membrane backing with specified widths at foldlines. The mathematical model and hardware modifications are employed to create several physical models. The results are general and apply to a range of applications. An example is provided by the application that motivated the work: a deployable solar array for space applications. The model is demonstrated in hardware as a 1/20th scale prototype with a ratio of deployedtostowed diameter of 9.2 (or 1.25 m deployed outer diameter to 0.136 m stowed outer diameter).
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      Accommodating Thickness in Origami Based Deployable Arrays1

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    http://yetl.yabesh.ir/yetl1/handle/yetl/152586
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    • Journal of Mechanical Design

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    contributor authorZirbel, Shannon A.
    contributor authorLang, Robert J.
    contributor authorThomson, Mark W.
    contributor authorSigel, Deborah A.
    contributor authorWalkemeyer, Phillip E.
    contributor authorTrease, Brian P.
    contributor authorMagleby, Spencer P.
    contributor authorHowell, Larry L.
    date accessioned2017-05-09T01:01:07Z
    date available2017-05-09T01:01:07Z
    date issued2013
    identifier issn1050-0472
    identifier othermd_135_11_111005.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/152586
    description abstractThe purpose of this work is to develop approaches to accommodate thickness in origamibased deployable arrays with a high ratio of deployedtostowed diameter. The origami flasher model serves as a basis for demonstrating the approach. A thicknessaccommodating mathematical model is developed to describe the flasher. Practical modifications are presented for the creation of physical models and two options are proposed: allowing the panels to fold along their diagonals or applying a membrane backing with specified widths at foldlines. The mathematical model and hardware modifications are employed to create several physical models. The results are general and apply to a range of applications. An example is provided by the application that motivated the work: a deployable solar array for space applications. The model is demonstrated in hardware as a 1/20th scale prototype with a ratio of deployedtostowed diameter of 9.2 (or 1.25 m deployed outer diameter to 0.136 m stowed outer diameter).
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAccommodating Thickness in Origami Based Deployable Arrays1
    typeJournal Paper
    journal volume135
    journal issue11
    journal titleJournal of Mechanical Design
    identifier doi10.1115/1.4025372
    journal fristpage111005
    journal lastpage111005
    identifier eissn1528-9001
    treeJournal of Mechanical Design:;2013:;volume( 135 ):;issue: 011
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian