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SPACECRAFT EAST-WEST RADIATOR ASSEMBLY

机译:航天飞机东-西散热器总成

摘要

A heat transfer assembly (HTA) includes an equipment panel having a first longitudinal length and a first radiator panel that is coupled to one of an east end and a west end of the equipment panel. The first radiator panel is longer in the longitudinal direction than the equipment panel and has least one longitudinal heat pipe. The HTA also includes at least one flexible heat pipe having a first rigid tube coupled to the equipment panel, a second rigid tube thermally coupled to the first longitudinal heat pipe, and a flexible tube coupled between the first and second rigid tubes. The equipment panel is configured to retain an equipment module in thermal contact with the first rigid tube.
机译:传热组件(HTA)包括具有第一纵向长度的设备面板和联接至设备面板的东端和西端中的一个的第一散热器面板。第一散热器面板在纵向上比设备面板长,并且具有至少一个纵向热管。该HTA还包括至少一个挠性热管,该挠性热管具有与设备面板连接的第一刚性管,与第一纵向热管热耦合的第二刚性管以及在第一和第二刚性管之间耦合的挠性管。设备面板被配置为保持设备模块与第一刚性管热接触。

著录项

  • 公开/公告号EP3003862B1

    专利类型

  • 公开/公告日2019-10-30

    原文格式PDF

  • 申请/专利权人 LOCKHEED MARTIN CORPORATION;

    申请/专利号EP20140807496

  • 发明设计人 WONG HAMILTON;BUCKLEY ROK PARK;

    申请日2014-06-05

  • 分类号B64G1/50;F28D15/02;

  • 国家 EP

  • 入库时间 2022-08-21 12:30:50

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