Pressure Vessel Closure Apparatus and Method
    52.
    发明申请
    Pressure Vessel Closure Apparatus and Method 审中-公开
    压力容器封闭装置及方法

    公开(公告)号:US20150323136A1

    公开(公告)日:2015-11-12

    申请号:US14705909

    申请日:2015-05-06

    发明人: Matthew Southam

    IPC分类号: F17C13/06

    摘要: Embodiments of the invention provide a pressure vessel closure apparatus for a pressure vessel having a shell wall, a removable end cap, and an internal retaining groove along an interior surface of the shell wall. The retaining member can include a main-portion outer profile and an end-portion outer profile. The end-portion outer profile can deviate from the main-portion outer profile in order to provide a clearance between the interior surface of the shell wall and the retaining member for the insertion of the retaining member into the retaining groove. A stop can be secured in place with respect to the end cap or the shell wall in order to retain the retaining member within the retaining groove. The retaining member, as retained within the retaining groove by the stop, can retain the end cap within the pressure vessel when the pressure vessel is pressurized.

    摘要翻译: 本发明的实施例提供了一种用于压力容器的压力容器封闭装置,其具有壳壁,可移除的端盖和沿着壳壁的内表面的内部保持槽。 保持构件可以包括主要部分外部轮廓和端部部分外部轮廓。 端部外部轮廓可以偏离主要部分外部轮廓,以便在壳体壁的内表面和保持构件之间提供间隙,用于将保持构件插入保持槽中。 相对于端盖或壳壁可以将止动件固定在适当位置,以便将保持构件保持在保持槽内。 通过止动件保持在保持槽内的保持构件可以在压力容器加压时将端盖保持在压力容器内。

    Aircraft fire extinguishing device and mounting method
    54.
    发明授权
    Aircraft fire extinguishing device and mounting method 有权
    飞机灭火装置及安装方法

    公开(公告)号:US08800675B2

    公开(公告)日:2014-08-12

    申请号:US12718754

    申请日:2010-03-05

    IPC分类号: A62C25/00

    摘要: A fire extinguisher device for aircraft has a hanger structure and a reservoir of extinguishing agent, the aforementioned reservoir being hung beneath the aforementioned hanger structure by metal fittings held by fasteners to the aforementioned hanger structure. The aforementioned extinguisher wherein the reservoir has means of suspension and the hanger structure has carriers complementary to the means of suspension, the aforementioned means of suspension and the aforementioned carriers being such that when the fasteners are withdrawn, the reservoir is in a position called the “intermediate position,” in which the metal fittings are free and the reservoir is suspended by interaction of the means of suspension and the carriers. The disclosed embodiments also relate to a method for fastening such an extinguishing device.

    摘要翻译: 用于飞机的灭火器装置具有衣架结构和灭火剂储存器,上述储存器通过紧固件固定在上述衣架结构上的金属配件悬挂在上述衣架结构的下面。 上述灭火器,其中储存器具有悬挂装置,并且悬挂结构具有与悬挂装置互补的载体,上述悬挂装置和上述载体使得当紧固件被拉出时,储存器处于称为“ 中间位置“,其中金属配件是自由的,并且通过悬挂装置和载体的相互作用来悬浮储存器。 所公开的实施例还涉及用于紧固这种灭火装置的方法。

    METALLIC SEALED DOUBLE CONTAINER
    56.
    发明申请
    METALLIC SEALED DOUBLE CONTAINER 有权
    金属密封双重容器

    公开(公告)号:US20140158683A1

    公开(公告)日:2014-06-12

    申请号:US14234556

    申请日:2012-08-16

    申请人: MIRAPRO CO., LTD.

    IPC分类号: B65D1/40

    摘要: The metallic sealed double container of the present invention includes an outer container, an inner container, an outer lid for the outer container, and an inner lid for the inner container, all of which being formed from thin metallic sheet. Connection holes are formed in the outer lid and the inner lid by burring, and both end parts of thin-walled pipes are respectively connected while inserted in the connection holes. The inner lid is joined to the inner container, and the outer lid is joined to the outer container, thereby constituting a metallic sealed double container in which the inner container is isolated in the outer container. As a result, the weight of the metallic sealed double container is reduced, the temperature in the inner container can be maintained over long periods of time, and the heat-insulating effect of the resulting sealed double container is high.

    摘要翻译: 本发明的金属密封双层容器包括外容器,内容器,用于外容器的外盖和用于内容器的内盖,所述内盖均由金属薄片形成。 通过翻边在外盖和内盖中形成连接孔,并且在插入连接孔时分别连接薄壁管的两端部。 内盖与内容器接合,外盖与外容器接合,构成内容器与外容器隔离的金属密封双重容器。 结果,金属密封双层容器的重量减少,内部容器中的温度可以长时间保持,并且所得到的密封双层容器的绝热效果高。

    KEY FOR GAS CYLINDERS
    57.
    发明申请
    KEY FOR GAS CYLINDERS 审中-公开
    关键气罐

    公开(公告)号:US20140021393A1

    公开(公告)日:2014-01-23

    申请号:US13555380

    申请日:2012-07-23

    IPC分类号: F16K31/60

    摘要: There is a key for use with pressurized gas cylinders. The key includes a sleeve configured to fit over a lever arm of a gas cylinder. The key includes a handle extending from the sleeve, and having a body. The handle includes a first slot and a second slot extending through the body of the handle and configured to fit over a valve toggle of a gas cylinder. The handle includes a washer storage device extending substantially orthogonally from the body of the handle. The handle includes a flange coupled to an end of the washer storage device, opposite the body. The handle also includes a recess portion disposed about a base of the washer storage device of the handle and sized and shaped to receive a plurality of gas cylinder washers.

    摘要翻译: 加压气瓶有一个关键。 钥匙包括配置成装配在气瓶的杠杆臂上的套筒。 钥匙包括从套筒延伸并具有主体的把手。 手柄包括延伸穿过手柄主体的第一槽和第二槽,并且构造成装配在气瓶的阀瓣上。 手柄包括从手柄主体基本正交地延伸的洗衣机存储装置。 手柄包括与主体相对的联接到洗衣机存储装置的端部的凸缘。 手柄还包括设置在手柄的垫圈存储装置的基部周围的凹部,其尺寸和形状被容纳以容纳多个气瓶垫圈。

    TANK MOUNTING MECHANISM AND VEHICLE EQUIPPED WITH TANK
    59.
    发明申请
    TANK MOUNTING MECHANISM AND VEHICLE EQUIPPED WITH TANK 有权
    坦克安装机构和装有油罐的车辆

    公开(公告)号:US20100045018A1

    公开(公告)日:2010-02-25

    申请号:US12531579

    申请日:2009-02-05

    IPC分类号: B60K15/067 A47B96/06

    摘要: A tank mounting technique of the invention effectively responds to a variation in size of a high-pressure tank T in its longitudinal direction and allows positioning of the high-pressure tank T around its longitudinal axis. A tank receiving recess 110 provided below a vehicle platform F has a pair of a front inclined surface 112F and a rear inclined surface 112R arranged to face each other across a concave groove 114. A side face of the high pressure tank T is brought into contact with both the inclined surfaces 112F and 112R. An end face of a tank positioning groove TVS formed on the high pressure tank T is brought into contact with a contact structure 121 of a tank edge bracket 120. This arrangement enables the high-pressure tank T to be positioned in a vehicle vertical direction and a vehicle front-back direction, as well as in the tank longitudinal direction (in a vehicle width direction). The tank positioning groove TVS is aligned with a notch 122 formed in the tank edge bracket 120 to specify a rotational position of the high-pressure tank T around its longitudinal axis.

    摘要翻译: 本发明的罐安装技术有效地响应高压罐T在其纵向上的尺寸变化,并且允许高压罐T围绕其纵向轴线定位。 设置在车辆平台F下方的油箱接收凹部110具有一对前倾斜面112F和后倾斜面112R,该倾斜面112F和后倾斜面112R相对于凹槽114彼此相对配置。高压罐T的侧面接触 同时具有倾斜表面112F和112R。 形成在高压罐T上的罐定位槽TVS的端面与罐边支架120的接触结构121接触。这种布置使得高压罐T能够在车辆垂直方向上定位,并且 车辆前后方向以及油箱纵向(车宽方向)。 油箱定位槽TVS与形成在油箱边缘支架120中的切口122对准,以指定高压罐T围绕其纵向轴线的旋转位置。

    Fuel tank with specialized tank outlet for spacecraft
    60.
    发明授权
    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:US07621291B2

    公开(公告)日:2009-11-24

    申请号:US11641182

    申请日:2006-12-18

    IPC分类号: B67D5/54

    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。