Cover for Gas Cylinder Tap
    4.
    发明申请
    Cover for Gas Cylinder Tap 有权
    气瓶盖盖

    公开(公告)号:US20170067601A1

    公开(公告)日:2017-03-09

    申请号:US15123283

    申请日:2015-02-23

    IPC分类号: F17C13/00

    摘要: The invention is directed to a cover (4) for a tap of a gas cylinder (6), comprising a shell (7, 8) for housing the tap; and a hook (12) pivotally mounted on the shell (8), configured for securing the gas cylinder (6) to a horizontal bar (28). The shell (8) comprises reservations (30) on its external surface configured for receiving the hook (12) in a folded position so as to generally conform to said external surface. The invention is also directed to a gas storage assembly comprising a gas cylinder (6), a tap and a cover (4).

    摘要翻译: 本发明涉及一种用于气瓶(6)的龙头的盖(4),包括用于容纳龙头的外壳(7,8) 以及枢转地安装在所述壳体(8)上的钩(12),构造成用于将所述气瓶(6)固定到水平杆(28)。 壳体(8)在其外表面上包括预定位置(30),该外表面被构造成用于在折叠位置接纳钩子(12),从而大体上符合所述外表面。 本发明还涉及一种包括气瓶(6),龙头和盖(4)的气体存储组件。

    Method of manufacturing liquefied natural gas carrier
    5.
    发明授权
    Method of manufacturing liquefied natural gas carrier 有权
    制造液化天然气载体的方法

    公开(公告)号:US09376174B2

    公开(公告)日:2016-06-28

    申请号:US14234991

    申请日:2012-07-25

    摘要: Provided a LNG ship that is manufactured in a short construction period by assembling a LNG tank on land and mounting the LNG tank in a hold of the ship.A cold insulator and a membrane are affixed on an inner side of a prismatic tank to fabricate a LNG tank, which is mounted in a hold having a double hull structure. In order to prevent the prismatic tank from deforming at the time of the mounting, strength members are welded to an outer surface of the prismatic tank before a thermal insulation work for the purpose of sufficient reinforcement. After the tank is mounted in the hold, the strength members of the prismatic tank are coupled to the inner hull of the ship to integrate the LNG tank and the hull, so that the weight of a liquid cargo is supported by the prismatic tank and the hull together.

    摘要翻译: 提供一种通过在陆地上组装LNG罐并将LNG罐安装在船舶的船舶上,在短的施工期内制造的LNG船。 冷却绝缘体和膜固定在棱柱形罐的内侧以制造LNG罐,其安装在具有双层船体结构的保持架中。 为了防止棱镜箱在安装时发生变形,为了充分的加强,加强部件在进行绝热工作之前被焊接在棱柱形箱体的外表面上。 在罐被安装在搁板中之后,棱柱箱的强度构件联接到船的内部船体以将LNG罐和船体结合在一起,使得液体货物的重量由棱柱箱和 船体在一起

    Fuel tank with specialized tank outlet for spacecraft
    8.
    发明申请
    Fuel tank with specialized tank outlet for spacecraft 有权
    燃油箱,专门用于航天器出油口

    公开(公告)号:US20070145194A1

    公开(公告)日:2007-06-28

    申请号:US11641182

    申请日:2006-12-18

    IPC分类号: B64G1/00

    摘要: A fuel tank of a spacecraft stores a liquid fuel and a pressurized propellant gas that drives the fuel out of the tank though a fuel extraction arrangement including a reservoir or fuel collection container and a tank outlet. A spiraling or J-shaped or hook-shaped fuel collection channel and plural obliquely sloping fuel flow channels connect the fuel collection container to an outlet pipe of the tank outlet. The channels are configured, dimensioned, oriented and arranged to ensure that fuel will be retained in the outlet pipe without leaking back into the fuel tank, even when the tank is oriented horizontally and has a low tank filling level. These structures produce a capillary pumping effect and use the surface tension to separate the fuel from the propellant gas, and allow the inner space of the collection container to be completely filled with liquid fuel.

    摘要翻译: 航天器的燃料箱存储液体燃料和加压推进剂气体,其通过包括储存器或燃料收集容器和罐出口的燃料提取装置将燃料驱出罐外。 螺旋式或J型或钩状燃料收集通道和多个倾斜倾斜的燃料流动通道将燃料收集容器连接到罐出口的出口管。 通道的构造,尺寸,定向和布置,以确保燃料将被保留在出口管中,而不会泄漏回燃料箱,即使水箱水平定向并具有低的罐装水平。 这些结构产生毛细管抽吸效应,并使用表面张力将燃料与推进剂气体分离,并允许采集容器的内部空间完全充满液体燃料。