Conceptual model study using origami for membrane space structures

M. C. Natori, Nobuhisa Katsumata, Hiroshi Yamakawa, Hiraku Sakamoto, Naoko Kishimoto

    研究成果: Conference contribution

    14 被引用数 (Scopus)

    抄録

    Some attempts to get efficient membrane space structure designs using various conceptual origami models are introduced, and their basic design considerations to fit their concepts to actual space structural hardware are presented. They cover cylindrical shell elements with axially buckled patterns for inflatable tubes, and deployable flat membrane structures for light weight large aperture spacecraft including their thickness effects and their various variations driven from geometrical dual properties. Some examples of deployable concepts in nature with reference to better designs of membrane space structures are also shown, and some limitations of their origami models are discussed.

    本文言語English
    ホスト出版物のタイトルProceedings of the ASME Design Engineering Technical Conference
    出版社American Society of Mechanical Engineers
    6 B
    ISBN(印刷版)9780791855942
    DOI
    出版ステータスPublished - 2013
    イベントASME 2013 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2013 - Portland, OR
    継続期間: 2013 8 42013 8 7

    Other

    OtherASME 2013 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2013
    CityPortland, OR
    Period13/8/413/8/7

    ASJC Scopus subject areas

    • 機械工学
    • コンピュータ グラフィックスおよびコンピュータ支援設計
    • コンピュータ サイエンスの応用
    • モデリングとシミュレーション

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