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Spacecraft multi-directional loop heat pipe thermal systems

机译:航天器多向回路热管热系统

摘要

Multi-directional (reversible and parallel) loop heat pipe thermal systems for use on a spacecraft. The multi-directional loop heat pipe thermal systems may comprise reversible or parallel loop heat pipes that provide efficient thermal pathways that are directionally independent between any combination of equipment mounting panels and radiator panels. Loop heat pipes of the reversible loop heat pipe thermal system are coupled between opposite ends of respective evaporator/condenser flanges. The evaporator/condenser flanges each comprise a condenser and an evaporator. The parallel loop heat pipe thermal system comprises pairs or sets of parallel heat pipes that are respectively coupled between a condenser flange and an evaporator flange. The reversible or parallel loop heat pipes may be routed to a multiple number of radiator panels in order to optimize the use of a radiator panel by always transporting heat to the coolest radiator panel.
机译:用于航天器的多向(可逆和并行)回路热管热系统。多向回路热管热系统可以包括可逆或平行回路热管,其提供有效的热路径,该热路径在设备安装面板和散热器面板的任何组合之间在方向上是独立的。可逆回路热管热系统的回路热管连接在相应的蒸发器/冷凝器法兰的相对端之间。蒸发器/冷凝器凸缘各自包括冷凝器和蒸发器。平行回路热管热系统包括成对或成组的平行热管,它们分别连接在冷凝器凸缘和蒸发器凸缘之间。可逆或并联回路热管可被路由到多个散热器面板,以便通过始终将热量传输到最冷的散热器面板来优化散热器面板的使用。

著录项

  • 公开/公告号US6591899B1

    专利类型

  • 公开/公告日2003-07-15

    原文格式PDF

  • 申请/专利权人 SPACE SYSTEMS/LORAL INC.;

    申请/专利号US20000717585

  • 发明设计人 EDDY M. YEE;

    申请日2000-11-21

  • 分类号F28D150/00;

  • 国家 US

  • 入库时间 2022-08-22 00:06:51

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