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dehumidification system for use on an aircraft assembly, and method for mounting a dehumidification system for use on an aircraft assembly

机译:用于飞机组件的除湿系统,以及安装用于飞机组件的除湿系统的方法

摘要

dehumidification system for use on an aircraft assembly, and method for mounting a dehumidification system for use on an aircraft assembly. a dehumidification system (222) for use in an aircraft assembly (102) is provided. the system includes a thermally conductive member (230) coupled to an outer shell (218) of the aircraft assembly, and a duct (238) at least partially circumscribing the thermally conductive member so that an airflow passage (240) is provided. between the duct and the thermally conductive element. the thermally conductive member is configured to transmit a temperature of the outer casing to moisture-laden air (244) through the air flow passage.
机译:用于飞机组件的除湿系统,以及用于安装用于飞机组件的除湿系统的方法。提供了一种用于飞机组件(102)的除湿系统(222)。该系统包括联接至飞机组件的外壳(218)的导热构件(230),以及至少部分地围绕导热构件的管道(238),从而提供了气流通道(240)。在管道和导热元件之间。导热构件被构造成通过空气流动通道将外壳的温度传递到载有湿气的空气(244)。

著录项

  • 公开/公告号BR102014031298A2

    专利类型

  • 公开/公告日2015-10-06

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号BR20141031298

  • 发明设计人 FUE CHUE VUE;

    申请日2014-12-12

  • 分类号B64D33/04;B64D13/06;F24F3/14;F24F13/04;

  • 国家 BR

  • 入库时间 2022-08-21 15:16:17

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