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heat exchanger, especially as a radiator air cooling for hypersonic propulsion, with spacing for the pipes of its matrix.

机译:换热器,特别是作为用于超音速推进的散热器空气冷却器,其矩阵管之间有一定间距。

摘要

Spacer supports are connected to a matrix of heat exchange tubes of a heat exchanger to maintain the heat exchange tubes in spaced relation and resist overheating by hot fluid flowing around the tubes and the spacer supports. The spacer supports are in the form of hollow tubular bodies in which the heat exchange tubes are supported in spaced relation. The heat exchange tubes communicate with the interior of the hollow bodies so that flow of a heatable fluid in the heat exchange tubes is conveyed through the hollow body to wet the interior thereof and cool the same.
机译:间隔器支撑件连接到热交换器的热交换管的矩阵,以使热交换管保持间隔开的关系,并抵抗在管和间隔器支撑件周围流动的热流体引起的过热。间隔件支撑件为中空管状体的形式,其中,热交换管以间隔关系支撑在其中。热交换管与中空体的内部连通,从而使热交换管中的可加热流体的流动通过中空体以润湿其内部并对其进行冷却。

著录项

  • 公开/公告号IT1256058B

    专利类型

  • 公开/公告日1995-11-23

    原文格式PDF

  • 申请/专利权人

    申请/专利号IT1992MI02654

  • 发明设计人

    申请日1992-11-20

  • 分类号6F28FA;

  • 国家 IT

  • 入库时间 2022-08-22 03:52:17

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