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    • 73. 发明申请
    • Lightweight, compactly deployable support structure with telescoping members
    • 轻便,紧凑的部署支撑结构与伸缩构件
    • US20020063660A1
    • 2002-05-30
    • US10004334
    • 2001-10-25
    • Harris Corporation, Corporation of the State of Delaware
    • Richard I. Harless
    • H01Q015/14H01Q015/20
    • B64G1/222B64G9/00H01Q15/161
    • A compactly stowable and deployable support architecture, such as may be used for supporting an energy directing surface, includes radial and hoop support members including upwardly and downwardly extending strut members for deploying a surface, such as a mesh-configured antenna reflector. In one aspect, at least one strut is formed as a telescoping tube member. A multi-sided foldable hoop structure has a plurality of foldable joints, and generally radial struts that extend from and are foldable about corner joints of the hoop structure. At least one drive mechanism is coupled to torque tubes that drive geared hinges of the multi-sided hoop structure. The hinges and drive linkages are geared to synchronously unfold the multi-sided foldable hoop structure and the radial struts, so that the antenna surface may be smoothly deployed from its stowed condition.
    • 可以用于支撑能量引导表面的紧凑的可收起和展开的支撑结构包括径向和环箍支撑构件,包括用于展开表面的向上和向下延伸的支柱构件,例如网状配置的天线反射器。 在一个方面,至少一个支柱形成为伸缩管构件。 多侧可折叠箍结构具有多个可折叠接头,并且大体上是径向支柱,其从环箍结构的拐角接头延伸并可折叠。 至少一个驱动机构联接到驱动多侧箍结构的齿轮铰链的扭矩管。 铰链和驱动联动装置适于同时展开多侧可折叠箍结构和径向支柱,使得天线表面可以从其收起状态平滑地展开。