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Cooling system for travelling wave tube of telecommunications satellite includes radiator and heat exchange fluid circuit to remove heat from travelling wave tubes

机译:用于电信卫星行波管的冷却系统包括散热器和热交换流体回路,用于从行波管中散热

摘要

The cooling device comprises a radiator (15) thermally uncoupled from the satellite body, and placed to disperse heat by radiation into space. A heat exchange fluid loop (25) links a exchangers (34,33) on the collectors (28) to a cold exchanger (32) belonging to the radiator (15). The device provides cooling for travelling wave tubes (26) having a collector (28) preferably operating at high temperature and thermally insulated from the rest of the tube. The device comprises a radiator (15) thermally uncoupled from the satellite body, and placed in an orientation such that it disperses heat by radiation into space. A heat exchange fluid loop (25) links hot exchangers (34,33) thermally coupled to the collectors (28) and emitting units of the tubes (26) carried by the satellite, and a cold exchanger (32) belonging to the radiator (15). The fluid loop is monophase, and the fluid flow is controlled by a link (38,40) between the input and the output of the cold exchanger (32). The fluid loop may includes include at least one flexible section (50).
机译:该冷却装置包括散热器(15),该散热器与卫星主体热解耦,并且被放置以通过辐射将热量散布到太空中。热交换流体回路(25)将集热器(28)上的交换器(34,33)连接到属于散热器(15)的冷交换器(32)。该装置为行波管(26)提供冷却,该行波管具有优选在高温下操作并与管的其余部分绝热的收集器(28)。该装置包括与卫星主体热解耦的辐射器(15),辐射器(15)的放置方向使其通过辐射将热量散布到太空中。热交换流体回路(25)连接与卫星(28)的收集器(28)和由卫星携带的管(26)的发射单元热耦合的热交换器(34,33)和属于散热器( 15)。流体回路是单相的,并且流体的流动由冷交换器(32)的输入和输出之间的连接(38,40)控制。流体回路可包括至少一个柔性部分(50)。

著录项

  • 公开/公告号FR2840881A1

    专利类型

  • 公开/公告日2003-12-19

    原文格式PDF

  • 申请/专利权人 ASTRIUM SAS;

    申请/专利号FR20020007265

  • 发明设计人 POULAIN BERTRAND;

    申请日2002-06-13

  • 分类号B64G1/46;H01J23/033;H01J25/34;

  • 国家 FR

  • 入库时间 2022-08-21 22:39:30

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