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Thermomechanical structure suitable for a space environment

机译:适用于太空环境的热机械结构

摘要

The structure (1) has walls formed with a hole (2) and lined with filaments (3), where the filaments are greater in length than distance separating an outside of a liquid ammonia heat pipe (4) from an inside of the hole such that the filaments bend when the pipe is introduced. The hole is equipped with the pipe. The walls are included between 30 and 100 filaments per square centimeter, where length of the filaments is between 0.2 and 5 mm and diameter of the filaments is between 0.3 and 0.8 mm. The walls are covered with grease for allowing better thermal conduction. An independent claim is also included for a process for producing a monolithic metal mechanical-thermal structure.
机译:结构(1)具有形成有孔(2)并衬有细丝(3)的壁,其中细丝的长度大于将液氨热管(4)的外部与孔的内部分开的距离,例如引入管道时细丝会弯曲。该孔配有管道。壁包括在每平方厘米30至100根细丝之间,其中细丝的长度在0.2到5 mm之间,细丝的直径在0.3到0.8 mm之间。壁上覆盖有油脂,以实现更好的热传导。还包括用于制造整体式金属机械热结构的方法的独立权利要求。

著录项

  • 公开/公告号PL2711299T3

    专利类型

  • 公开/公告日2016-08-31

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号PL20130185352T

  • 申请日2013-09-20

  • 分类号B23P15/26;B64G1/50;F28D15/02;

  • 国家 PL

  • 入库时间 2022-08-21 14:23:36

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