首页> 外国专利> DEPLOYABLE LIGHTWEIGHT STRUCTURE CAPABLE OF BEING RIGIDIFIED AFTER BEING DEPLOYED, METHOD FOR MAKING THE SAME, AND USE THEREOF FOR EQUIPPING A SPACECRAFT

DEPLOYABLE LIGHTWEIGHT STRUCTURE CAPABLE OF BEING RIGIDIFIED AFTER BEING DEPLOYED, METHOD FOR MAKING THE SAME, AND USE THEREOF FOR EQUIPPING A SPACECRAFT

机译:可部署后可刚性化的可部署轻量级结构,相同方法以及使用该结构来安装航天飞机

摘要

The invention concerns a structure comprising a rigging (1-2) consisting of at least one flexible rope (1, 2) impregnated with a hardening substance, with controllable hardening, designed to rigidify at least one rope after it has been deployed and extended. The structure may comprise at least one rigging mesh, whereof at least one flexible rope (1, 2) is impregnated with the hardening substance and bound to itself and/or to another rope of the rigging by at least one bond (6). Said structure is independent of any means of deployment, but may also comprise a deploying device (3) independent of the rigging and extending the ropes (1, 2) of the structure and maintaining them taut while the hardening material is cured. The invention is in particular applicable to deployable structures capable of being rigidified on board space crafts.
机译:本发明涉及一种包括索具(1-2)的结构,该索具(1-2)由至少一根浸渍有硬化物质并具有可控制的硬化性的柔性绳索(1、2)组成,该绳索被设计成在至少一根绳索被展开和伸展之后硬化。该结构可以包括至少一个索具网,其中至少一根柔性绳(1、2)被硬化物质浸渍并且通过至少一个结合件(6)结合到自身和/或索具的另一根绳上。所述结构不依赖于任何展开方式,但是还可以包括独立于索具和伸展结构的绳索(1、2)并在硬化材料固化时保持绷紧的部署装置(3)。本发明尤其适用于能够在航天器上硬化的可展开结构。

著录项

  • 公开/公告号EP1893489B1

    专利类型

  • 公开/公告日2009-09-30

    原文格式PDF

  • 申请/专利权人 ASTRIUM SAS;

    申请/专利号EP20060764782

  • 发明设计人 CHEYNET DE BEAUPRE RENE JEAN;

    申请日2006-06-13

  • 分类号B64G1/64;

  • 国家 EP

  • 入库时间 2022-08-21 19:17:22

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