A study on the design of deployable cable-panel structure

    研究成果: Conference contribution

    抄録

    Recently, large space structures are being developed. From the point of view of payload capacity and transportation efficiency, large space structures are required to be lightweight and highly efficient in their folding. Cable-panel structures are also expected to satisfy the above conditions mainly due to the omission of frames that hold panels structures. However, the deployment of three-dimensional membranes is difficult to control accurately because of the small stiffness normal to membranes. In this study, we discuss the wire location design in the wire-based deployment of three-dimensional plates. And, through experiments, we evaluate 27 design locations of wires for deployment and compare the deployed shape between the designed dimensions and the measured surface. Then, we confirmed the increment of 2.2 percent in height dimension. Furthermore, we confirmed that our proposed deployment method is feasible, and obtained several design criteria for wire design: First, it is necessary to consider an order of deployment to deploy from the outside surface. Second, the design needs to intersect folds at right angles. Third, extending the length of designs without changing the route shape of the designs leads to higher accuracy of the deployment shape without causing a large increase in the required forces. The multi particle system model was applied to predict the deformation of the structure reasonablly.

    元の言語English
    ホスト出版物のタイトル4th AIAA Spacecraft Structures Conference, 2017
    出版者American Institute of Aeronautics and Astronautics Inc, AIAA
    ISBN(印刷物)9781624104558
    出版物ステータスPublished - 2017
    イベント4th AIAA Spacecraft Structures Conference, 2017 - Grapevine, United States
    継続期間: 2017 1 92017 1 13

    Other

    Other4th AIAA Spacecraft Structures Conference, 2017
    United States
    Grapevine
    期間17/1/917/1/13

    Fingerprint

    Cables
    Wire
    Membranes
    Stiffness
    Experiments

    ASJC Scopus subject areas

    • Electrical and Electronic Engineering
    • Aerospace Engineering
    • Mechanical Engineering
    • Computer Science Applications

    これを引用

    Seino, K., Parque Tenorio, V., & Miyashita, T. (2017). A study on the design of deployable cable-panel structure. : 4th AIAA Spacecraft Structures Conference, 2017 American Institute of Aeronautics and Astronautics Inc, AIAA.

    A study on the design of deployable cable-panel structure. / Seino, Koujirou; Parque Tenorio, Victor; Miyashita, Tomoyuki.

    4th AIAA Spacecraft Structures Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, 2017.

    研究成果: Conference contribution

    Seino, K, Parque Tenorio, V & Miyashita, T 2017, A study on the design of deployable cable-panel structure. : 4th AIAA Spacecraft Structures Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, 4th AIAA Spacecraft Structures Conference, 2017, Grapevine, United States, 17/1/9.
    Seino K, Parque Tenorio V, Miyashita T. A study on the design of deployable cable-panel structure. : 4th AIAA Spacecraft Structures Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA. 2017
    Seino, Koujirou ; Parque Tenorio, Victor ; Miyashita, Tomoyuki. / A study on the design of deployable cable-panel structure. 4th AIAA Spacecraft Structures Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, 2017.
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