首页> 外国专利> legere deployable structure and rigidifiable after unfolding, its advantages of, and its application to the equipment of a spatial

legere deployable structure and rigidifiable after unfolding, its advantages of, and its application to the equipment of a spatial

机译:Legere可展开结构,展开后可固定,其优点及其在空间设备中的应用

摘要

The structure comprises a line (1 - 2) consisting of at least one flexible rope (1,2) impregnated with a thermosetting material, the hardening controllable, intended to stiffen the said at least one rope after its deployment and extension. The structure may comprise at least a mesh in line with at least one flexible rope (1,2) is impregnated with thermosetting material and connected to it - same and / or at least one other chord of the rope by at least one strap (6) .elle may also comprise a deployment device (3) which is independent of the line and by extension, the cords (1,2) of the structure and the maintaining in tension during the hardening of the material durcissant.application in particular to deployable structures and and rigidifiable on board spacecraft
机译:该结构包括由至少一根浸渍有热固性材料的柔性绳索(1,2)组成的线(1-2),该绳索可硬化,该硬化绳索是可控制的,旨在在所述至少一根绳索在其展开和延伸之后变硬。该结构可以包括至少一个与至少一根柔性绳索(1,2)成一直线的网孔,该柔性绳索浸渍有热固性材料并连接到其上-通过至少一条带子(6)与绳索的相同和/或至少另一个弦相连接)还可以包括展开装置(3),该展开装置(3)独立于生产线,并且通过延伸,结构的绳索(1,2)以及在材料durissant硬化期间保持张力。结构和可固定在航天器上

著录项

  • 公开/公告号FR2887523B1

    专利类型

  • 公开/公告日2008-11-07

    原文格式PDF

  • 申请/专利权人 EADS ASTRIUM SAS;

    申请/专利号FR20050006342

  • 发明设计人 RENE JEAN CHEYNET DE BEAUPRE;

    申请日2005-06-22

  • 分类号B64G1/64;

  • 国家 FR

  • 入库时间 2022-08-21 19:47:22

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号