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Aircraft signal computer system having a plurality of modular signal computer units

机译:具有多个模块化信号计算机单元的飞机信号计算机系统

摘要

An aircraft signal computer system includes a plurality of modular signal computer units and a liquid cooling device for cooling the modular signal computer units. The liquid cooling device includes a coolant line, which is connectable to a central liquid cooling system of an aircraft in order to supply a liquid coolant medium at a desired low temperature to the liquid cooling device. The coolant line of the liquid cooling device is in thermal surface contact with the modular signal computer units in order to dissipate heat from the modular signal computer units. A heat-emitting component of the modular signal computer units may be in thermal contact with a coolant bath or an internal heat conductor for removing heat energy.
机译:飞机信号计算机系统包括多个模块化信号计算机单元和用于冷却模块化信号计算机单元的液体冷却装置。液体冷却装置包括冷却剂管线,该冷却剂管线可连接到飞机的中央液体冷却系统,以便将期望的低温下的液体冷却剂介质供应到液体冷却装置。液体冷却装置的冷却剂管线与模块化信号计算机单元热表面接触,以散发来自模块化信号计算机单元的热量。模块化信号计算机单元的散热部件可以与冷却剂浴或内部热导体热接触以去除热能。

著录项

  • 公开/公告号US8508934B2

    专利类型

  • 公开/公告日2013-08-13

    原文格式PDF

  • 申请/专利权人 SEBASTIAN ROERING;

    申请/专利号US200913059528

  • 发明设计人 SEBASTIAN ROERING;

    申请日2009-08-13

  • 分类号H05K7/20;

  • 国家 US

  • 入库时间 2022-08-21 16:48:19

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