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Improvements in and relating to closed liquid-circulating cooling systems

机译:封闭式液体循环冷却系统及其相关方面的改进

摘要

969,804. Closed liquid coolant circulation systems. G. BAYARD. April 30, 1962 [May 13, 1961], No. 16412/62. Heading F4U. Apparatus for cooling the liquid coolant, e.g. of electronic equipment in an aircraft, comprises an air cooled heat exchanger 11, means 7 capable of causing the liquid to bypass the heat exchanger when the temperature of the cooling air rises above a predetermined value, means leading from the heat exchanger and from the by-pass to convey the liquid to a pair of evaporators 16, 17 arranged in series, the evaporators containing a second liquid, e.g. methyl alcohol, and means capable of controlling the boiling temperature of said second liquid. As shown, liquid to be cooled enters distribution cock 7 which is controlled by a heat sensitive probe 9 which records the temperature of the air-cooling heat exchanger 11. If the temperature sensed is below e.g. 50‹ C. then cock 7 diverts the liquid through the heat exchanger 11, if above, then the heat exchanger is by-passed. Both by-pass and heat exchanger liquid enters evaporators 16 and 17 before finally flowing back to the equipment to be cooled via pipe 5. The required amount of cooling of the liquid in the evaporators is obtained when the methyl alcohol is subjected to a pressure of 700 gm. per sq. cm. equivalent to an altitude of 3000 metres. When the aircraft rises above this altitude regulator 32 acts as an exhaust valve for both evaporators and restores the pressure in the evaporators to 700 gm. per sq. cm. via stacks 26 and 27 and valve 31. When the aircraft descends below 3000 metres the regulator 32 is set directly in communication with the atmosphere and the methyl alcohol in evaporator 16 boils off at a higher temperature and does not sufficiently cool the liquid. The evaporator 17 however is subjected to a depression through regulator 33 which communicates with extractor 35 which restores inside evaporator 17 a pressure of 700 gm. per sq. cm. Valve 31 remains closed while extractor 35 is in operation.
机译:969,804。封闭的液体冷却剂循环系统。 G.拜亚德。 1962年4月30日[1961年5月13日],编号16412/62。标题为F4U。用于冷却液体冷却剂的设备,例如飞机中的电子设备包括一个空气冷却的热交换器11,当冷却空气的温度升高到预定值以上时,能够使液体绕过热交换器的装置7,该装置从热交换器和从-通过以将液体输送到串联布置的一对蒸发器16、17,所述蒸发器包含第二液体,例如甲醇,以及能够控制所述第二液体的沸腾温度的装置。如图所示,要冷却的液体进入分配旋塞7,该分配旋塞由热敏探头9控制,该探头记录空气冷却热交换器11的温度。然后在50℃下旋塞7将液体转移通过热交换器11,如果在上方,则旁路热交换器。旁路液体和热交换器液体均进入蒸发器16和17,然后最终通过管道5流回要冷却的设备。当甲醇承受的压力为10时,蒸发器中的液体需要冷却的量。 700克每平方厘米相当于3000米的高度。当飞机升起时,高度调节器32充当两个蒸发器的排气门,并将蒸发器中的压力恢复到700 gm。每平方厘米当飞机下降到3000米以下时,调节器32直接与大气连通,蒸发器16中的甲醇在较高的温度下沸腾,并且不能充分冷却液体。然而,蒸发器17通过调节器33承受低压,该调节器33与提取器35连通,提取器35在蒸发器17内部恢复700gm的压力。每平方厘米当抽取器35运行时,阀31保持关闭。

著录项

  • 公开/公告号GB969804A

    专利类型

  • 公开/公告日1964-09-16

    原文格式PDF

  • 申请/专利权人 GASTON BAYARD;

    申请/专利号GB19620016412

  • 发明设计人

    申请日1962-04-30

  • 分类号B64D13/08;F25B49/02;

  • 国家 GB

  • 入库时间 2022-08-23 16:15:57

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