Vacuum filtration device sealable vacuum vent
    2.
    发明授权
    Vacuum filtration device sealable vacuum vent 失效
    真空过滤装置可密封真空排气口

    公开(公告)号:US5725763A

    公开(公告)日:1998-03-10

    申请号:US670752

    申请日:1996-06-24

    CPC分类号: F16K7/20 B01D36/001 F16K24/04

    摘要: Disclosed is a vacuum filtration device including; (a)filter body including a filter membrane; (b) a passageway extending through the body and communicating with the upstream side of the filter for receiving a fluid to be filtered; (c) a junction mounted on the body on the downstream side of the filter and adapted to receive a closed container for receiving the filtered fluid and including sealing for creating a fluid tight seal between the container and the body; (d) a vacuum port communicating with said junction and adapted to be connected to a vacuum source for drawing the fluid through the filter and comprising a sealable vacuum vent which, when open, provides fluid communication between the vacuum port and a gas source. The device also includes a vacuum vent cap and a filter body vent and vent cap.

    摘要翻译: 公开了一种真空过滤装置,包括: (a)包括过滤膜的过滤体; (b)延伸穿过本体并与过滤器的上游侧连通的通道,用于接收待过滤的流体; (c)在过滤器的下游侧安装在主体上并且适于容纳用于接收过滤流体的密封容器并且包括用于在容器和主体之间形成流体密封的密封件的接头; (d)与所述接合部连通并且适于连接到真空源的真空端口,用于将流体抽吸通过过滤器并且包括可密封的真空通气口,其在打开时提供真空端口和气体源之间的流体连通。 该装置还包括一个真空排气盖和一个过滤器主体通风口和排气盖。

    Aircraft engine firewall seal
    3.
    发明授权
    Aircraft engine firewall seal 失效
    飞机发动机防火墙密封

    公开(公告)号:US5458343A

    公开(公告)日:1995-10-17

    申请号:US288856

    申请日:1994-08-11

    摘要: An aircraft engine firewall seal includes a plurality of discrete, stacked-together sealing disks each have a central hole sized for receiving a feed-through member therethrough, with the disks being larger in outer diameter than the firewall aperture through which the feed-through member extends, and with the central holes being smaller in inner diameter than the firewall aperture. The disks are retained against the firewall by a retainer which fixedly clamps together the disks around the feed-through member for sealing gas flow through the firewall aperture.

    摘要翻译: 飞机发动机防火墙密封件包括多个离散的,堆叠在一起的密封盘,每个密封盘具有大小适于容纳通过其中的馈通构件的中心孔,其中盘的外径大于防火墙孔径,穿过构件 延伸,并且中心孔的内径小于防火墙孔径。 磁盘通过保持器保持抵靠防火墙,该保持器将盘周围固定地夹在馈通构件上,以密封通过防火墙孔的气体流。