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Lightweight plenum system for spacecraft application

机译:用于航天器的轻质通风系统

摘要

A gas distribution system for use in an enclosed volume wherein the system includes a distribution duct and a first inflatable duct portion in fluid communication with the distribution duct. The system further includes a passageway defining an opening which extends through the passageway, wherein: the opening is in fluid communication with the first inflatable duct portion; the passageway includes a valve with a flapper positioned within the opening of the passageway; and the flapper is moveable in relationship to the opening by way of a bi-metallic temperature sensing member. The system further includes an inflatable enclosure in fluid communication with the opening of the passageway, wherein the inflatable enclosure is configured to define a volume within and separated from the enclosed volume.
机译:一种用于封闭空间的气体分配系统,其中,该系统包括分配管道和与分配管道流体连通的第一可充气管道部分。该系统还包括通道,该通道限定了延伸穿过该通道的开口,其中:所述开口与第一可充气管道部分流体连通;该通道包括一个阀,该阀的挡板位于该通道的开口内。并且挡板通过双金属温度感测构件相对于开口可移动。该系统还包括与通道的开口流体连通的可充气外壳,其中该可充气外壳被配置为在所包围的体积内限定一个体积,并与该所包围的体积分开。

著录项

  • 公开/公告号US9915958B2

    专利类型

  • 公开/公告日2018-03-13

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201715592744

  • 发明设计人 GALEN DUFF CARROLL;

    申请日2017-05-11

  • 分类号G05D23/08;B64G1/00;B64G1/40;B64G1/50;

  • 国家 US

  • 入库时间 2022-08-21 12:59:03

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