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    • 3. 发明申请
    • Large Rigid Deployable Structures and Method of Deploying and Locking Such Structures
    • 大型刚性可部署结构和部署和锁定这种结构的方法
    • US20120325973A1
    • 2012-12-27
    • US13333744
    • 2011-12-21
    • Stéphane VEZAINYannick BAUDASSENicolas DANDOLudovic SCHREIDER
    • Stéphane VEZAINYannick BAUDASSENicolas DANDOLudovic SCHREIDER
    • B64G1/22
    • B64G1/222B64G1/66
    • The invention is situated in the field of telecommunication satellites. A deployable structure with which such a satellite may be equipped and a method of deploying the deployable structure is provided. The deployable structure includes: a set of primary panels, a set of secondary panels, primary articulation systems, each primary articulation system enabling a primary panel to be caused to pivot relative to another primary panel about a primary axis, the primary axes being substantially parallel to the primary panels, and secondary articulation systems, each secondary articulation system being associated with a secondary panel and enabling said panel to be caused to pivot relative to another panel about a secondary axis parallel to said panels, the deployable structure being configured in such a manner that, in a deployed configuration, the front surfaces of the panels form a substantially continuous overall surface.
    • 本发明位于电信卫星领域。 提供了可以配备这样的卫星的可部署结构以及部署可部署结构的方法。 可部署的结构包括:一组主面板,一组次面板,主要关节运动系统,每个主要关节运动系统使主要面板相对于另一主面板围绕主轴线枢转,主轴线基本平行 所述主要面板和次要关节运动系统,每个次要关节运动系统与次级面板相关联,并且使所述面板相对于另一个面板绕平行于所述面板的副轴线枢转,所述可部署结构被配置为 在部署结构中,面板的前表面形成基本上连续的整个表面。