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Solar arrays, deployment mechanisms therefor, and related methods

机译:太阳能电池板,其部署机制以及相关方法

摘要

Mechanisms for deploying a solar array include an elongated deployment member routed along a first panel, along an extension, and at least partially along a second panel. The elongated deployment member is configured to, upon retraction of the elongated deployment member by a deployment motor, move the extension into an extended position and rotate the second panel about a hub located at a distal end of the extension. Solar array assemblies include such a mechanism. Methods of deploying a solar array include retracting an elongated deployment member to rotate an extension into an extended position and further retracting the elongated deployment member to rotate a panel coupled to the extension approximately 360° about a hub of the extension.
机译:用于展开太阳能电池阵列的机构包括沿着第一面板,沿着延伸部并且至少部分地沿着第二面板布置的细长的展开构件。细长的展开构件构造成在通过展开马达使细长的展开构件缩回时,将延伸部移动到延伸位置,并使第二面板绕位于延伸部的远端的毂旋转。太阳能电池阵列组件包括这种机制。展开太阳能电池阵列的方法包括缩回细长的展开构件以将延伸部旋转到延伸位置,并且进一步缩回细长的展开构件以使联接至延伸部的面板绕延伸部的毂旋转大约360°。

著录项

  • 公开/公告号US9352853B2

    专利类型

  • 公开/公告日2016-05-31

    原文格式PDF

  • 申请/专利权人 ORBITAL ATK INC.;

    申请/专利号US201313804331

  • 申请日2013-03-14

  • 分类号H01L31/042;H02S30/20;B64G1/44;B64G1/22;H01L31/02;H01L31/18;

  • 国家 US

  • 入库时间 2022-08-21 14:29:49

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