发明名称 Large membrane space structure and method for its deployment and expansion
摘要 <p>A large membrane space structure deployed and spanned by centrifugal force owing to the spin motion, contains a hub (2) located at a central portion thereof and a sail (4) including a plurality of petals (6) attached to the hub (2) by supports (8). Each of the petals has regions symmetrical to an imaginary center line (OX) passing through the center of the hub (2). Membranes are spanned on the regions. Each of the membranes is divided into parts of suitable shapes, and adjacent membranes are discretely connected to each other by bridge belts (10) to suppress the residual crease strain. The petals (6) are symmetric with respect to the center of the hub (2). Deployment force is provided in the circumferential direction by the introduction of imaginary tension lines. The petals may be connected to each other to help deployment. <IMAGE></p>
申请公布号 EP1280228(A2) 申请公布日期 2003.01.29
申请号 EP20010129966 申请日期 2001.12.17
申请人 THE DIRECTOR-GENERAL OF THE INSTITUTE OFSPACE AND ASTRONAUTICAL SCIENCE 发明人 KAWAGUCHI, JUNICHIRO
分类号 B64G1/22;B64G1/24;B64G1/40;B64G1/44;H01Q1/28;H01Q15/16;(IPC1-7):H01Q1/28 主分类号 B64G1/22
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