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Flexible, foldable solar generator for spacecraft, contg. foldable array(s) with integrated system of current conductor strips and blankets carrying solar cells

机译:航天器的柔性,可折叠太阳能发电机,续。可折叠阵列,带有集成的电流带和承载太阳能电池的毯子系统

摘要

The individual blankets (2) are interconnected by hinges vertically w.r.t the unfolding direction of the array (1). The solar cells are fitted in several parallel and series circuits. The current conductor strip system consists of an inner system (4) and an outer one (5) outside of the cell carrying blanket. The parallel circuits are meander-shaped, and the series circuits are U-shaped, electric conductors (10) provide interconnection of cells in the parallel circuits, while conductors (9) carry the current from the inner system to the energy processors of the spacecraft.
机译:各个毯子(2)通过铰链在阵列(1)的展开方向上垂直互连。太阳能电池安装在多个并联和串联电路中。电流导体带系统由一个内部系统(4)和一个在电池承载毯外面的外部系统(5)组成。并联电路是曲折形的,串联电路是U形的,电导体(10)提供并联电路中单元的互连,而导体(9)将电流从内部系统传送到航天器的能量处理器。

著录项

  • 公开/公告号DE19836272A1

    专利类型

  • 公开/公告日2000-02-17

    原文格式PDF

  • 申请/专利权人 DAIMLERCHRYSLER AG;

    申请/专利号DE1998136272

  • 发明设计人 KUECHLER GUNTER;MEURER RENE;

    申请日1998-08-11

  • 分类号B64G1/44;H01L31/05;

  • 国家 DE

  • 入库时间 2022-08-22 01:42:40

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