首页> 外国专利> Compact Structures and Methods for Deploying Foldable Origami Solar Arrays, Solar Sails, and Antenna Structures

Compact Structures and Methods for Deploying Foldable Origami Solar Arrays, Solar Sails, and Antenna Structures

机译:用于部署可折叠折纸太阳能电池板,太阳帆和天线结构的紧凑型结构和方法

摘要

The Structural Origami ARray (SOAR) concept is an extremely high performance, deployable solar array system that delivers high power output and exceeds state-of-the-art packaging efficiencies. Unlike existing Z-folding panels or rolled architectures, this approach utilizes an origami-inspired two-dimensional packaging scheme of a flexible blanket/substrate that is coupled with a simple and compact deployable supporting structure that stabilizes the array by external tension or internal support. This enables large deployed areas populated with high efficiency photovoltaic (PV) cells or antenna elements, which compactly stows in a square form factor with thin stack height that minimizes impingement on spacecraft bus internal volume.
机译:结构折纸ARray(SOAR)概念是一种极高性能,可部署的太阳能电池阵列系统,可提供高功率输出并超过最先进的包装效率。与现有的Z形折叠面板或卷式结构不同,此方法利用了折纸启发的柔性毯子/基材的二维包装方案,该方案与简单而紧凑的可部署支撑结构相结合,该支撑结构通过外部张力或内部支撑来稳定阵列。这样可以在大面积部署区域中布满高效光伏(PV)电池或天线元件,以紧凑的堆栈高度紧凑地收纳在方形形状中,从而将对航天器总线内部体积的影响降至最低。

著录项

  • 公开/公告号US2018278200A1

    专利类型

  • 公开/公告日2018-09-27

    原文格式PDF

  • 申请/专利权人 SUNGEUN K. JEON;JOSEPH N. FOOTDALE;

    申请/专利号US201715466731

  • 发明设计人 SUNGEUN K. JEON;JOSEPH N. FOOTDALE;

    申请日2017-03-22

  • 分类号H02S30/20;F16M11/38;F16M11/20;

  • 国家 US

  • 入库时间 2022-08-21 12:58:23

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