Propellant tank and vapor jet emitting device including same
    121.
    发明授权
    Propellant tank and vapor jet emitting device including same 有权
    推进剂罐和包括其的蒸气喷射发射装置

    公开(公告)号:US08881501B2

    公开(公告)日:2014-11-11

    申请号:US13039915

    申请日:2011-03-03

    IPC分类号: F02K9/60 B64G1/40 F02K9/42

    CPC分类号: B64G1/402 F02K9/42 F02K9/605

    摘要: A propellant tank for storing a liquid propellant A and supplying vapor produced by evaporation of part of the liquid propellant A to an external location comprises a tank body for storing the liquid propellant A, a mesh member arranged inside the tank body to cover a liquid surface of the liquid propellant A to divide an interior of the tank body into a liquid propellant storing area LA and a gas storing area GA by utilizing surface tension of the liquid propellant, and a heater arranged to a gas storing area GA side of the tank body to keep the gas storing area GA at higher temperature than temperature in the liquid propellant storing area LA. The tank body has a propellant inlet open into the liquid propellant storing area LA and a gas outlet open into the gas storing area GA.

    摘要翻译: 用于储存液体推进剂A并将部分液体推进剂A蒸发产生的蒸气的推进剂罐用于外部位置包括用于储存液体推进剂A的罐体,设置在罐体内部以覆盖液体表面的网状构件 的液体推进剂A通过利用液体推进剂的表面张力将罐体的内部分成液体推进剂存储区域LA和气体存储区域GA,以及布置在罐体的气体存储区域GA侧的加热器 以保持气体存储区域GA在液体推进剂存储区域LA中比温度更高的温度。 罐体具有通向液体推进剂存储区域LA的推进剂入口和通向气体存储区域GA的气体出口。

    Crystallization device
    122.
    发明授权
    Crystallization device 有权
    结晶装置

    公开(公告)号:US08876972B2

    公开(公告)日:2014-11-04

    申请号:US11879694

    申请日:2007-07-17

    IPC分类号: C30B29/58 B01D9/00

    CPC分类号: B01D9/005

    摘要: A crystallization device is for protein crystallization with a small amount of a sample in the liquid to liquid diffusion method. It is easy to fill the device with protein solution and precipitant solution and easy to pick up grown crystals from the device. The device comprises a channel plate made of polydimethylsiloxane (PDMS) and the first and second cover sheets made of polyethylene terephthalate. The channel plate includes at least one elongated channel having one side which extends in the longitudinal direction of the channel, the one side being exposed at the bottom surface of the channel plate. The channel has both ends which communicate with a protein solution inlet and a precipitant solution inlet respectively. The channel also communicates midway with a gel inlet and a vent hole. When picking up grown crystals from the device, the second cover sheet is cut off with a cutter knife so that the channel is exposed.

    摘要翻译: 结晶装置用于在液体/液体扩散方法中用少量样品进行蛋白质结晶。 使用蛋白质溶液和沉淀剂溶液容易填充设备,并容易从设备中取出生长的晶体。 该装置包括由聚二甲基硅氧烷(PDMS)制成的通道板和由聚对苯二甲酸乙二醇酯制成的第一和第二覆盖片。 通道板包括至少一个细长通道,其具有在通道的纵向方向上延伸的一侧,一侧在通道板的底表面处露出。 通道的两端分别与蛋白质溶液入口和沉淀剂溶液入口分别连通。 该通道还与凝胶入口和通气孔中途连通。 当从设备拾起生长的晶体时,用切割刀切割第二覆盖片,使得通道暴露。

    OPERATION STABILIZATION METHOD AND OPERATION STABILIZATION APPARATUS FOR SUPERSONIC INTAKE
    123.
    发明申请
    OPERATION STABILIZATION METHOD AND OPERATION STABILIZATION APPARATUS FOR SUPERSONIC INTAKE 审中-公开
    操作稳定方法和操作稳定装置用于超声波摄取

    公开(公告)号:US20140196436A1

    公开(公告)日:2014-07-17

    申请号:US14155472

    申请日:2014-01-15

    发明人: Yasushi Watanabe

    IPC分类号: F02K1/38

    CPC分类号: F02C7/042

    摘要: An object of the present invention is to provide a technique of enlarging a stable operating range of an intake in accordance with an operating condition of an engine without using a complicated control system so that a wide operating range of the engine can be covered. In an operation stabilization method for a supersonic intake according to the present invention, an enlarged duct between a cowl and a ramp of the intake is divided by a splitter plate such that an opening angle of the enlarged duct decreases. Further, in the operation stabilization method for a supersonic intake according to the present invention, when the duct is divided by the splitter plate, the splitter plate is disposed such that, from among a cowl side duct and a ramp side duct, cross-section variation in one duct, in which an effect of a flow is larger, is reduced within an allowable range of total pressure loss in the other duct.

    摘要翻译: 本发明的目的是提供一种根据发动机的运行状态来扩大进气口的稳定运行范围的技术,而不使用复杂的控制系统,从而能够覆盖发动机的宽的运行范围。 在根据本发明的用于超音速摄入的操作稳定方法中,前罩和进气道的斜坡之间的扩大的管道被分离板分隔,使得扩大的管道的打开角度减小。 此外,在本发明的超声波进气口的操作稳定方法中,当通过分流板分隔管道时,分离板被设置成从前侧管道和斜坡侧管道的横截面 一个管道中的流量影响较大的变化在另一个管道的总压力损失的允许范围内减小。

    GAS TURBINE COMBUSTOR
    124.
    发明申请
    GAS TURBINE COMBUSTOR 有权
    气体涡轮搅拌机

    公开(公告)号:US20140083105A1

    公开(公告)日:2014-03-27

    申请号:US14091619

    申请日:2013-11-27

    IPC分类号: F23R3/28

    摘要: An annular type gas turbine combustor having a plurality of fuel nozzle assemblies (10) on a circumference includes a pilot nozzle unit (12) for spraying a fuel for diffusive combustion from a pilot outer peripheral nozzle (34) into a combustion chamber (8), a main nozzle unit (14) provided so as to surround the pilot nozzle unit (12) for spraying a fuel for premix combustion, and a flow guide (27) disposed on a downstream side of each of the fuel nozzle assemblies (10) and having a sectional area of a passage for air and air-fuel mixture from each of the fuel nozzle assemblies (10), which gradually increase in a downstream direction.

    摘要翻译: 在圆周上具有多个燃料喷嘴组件(10)的环形燃气轮机燃烧器包括用于将用于扩散燃烧的燃料从先导外周喷嘴(34)喷射到燃烧室(8)中的先导喷嘴单元(12) 设置为围绕用于预混燃烧的燃料喷射的先导喷嘴单元(12)设置的主喷嘴单元(14),以及设置在每个燃料喷嘴组件(10)的下游侧的流动引导件(27) 并且具有从下游方向逐渐增加的每个燃料喷嘴组件(10)的空气和空气 - 燃料混合物的通道的截面面积。

    Crawler type travelling device
    125.
    发明授权
    Crawler type travelling device 有权
    履带式行走装置

    公开(公告)号:US08657043B2

    公开(公告)日:2014-02-25

    申请号:US12810509

    申请日:2008-12-24

    IPC分类号: B62D55/253

    CPC分类号: B62D55/253

    摘要: To provide a crawler type traveling device with few rotating wheel mechanisms and equalizing the pressure contacting the ground. A crawler type traveling device comprises a driving wheel driven by a driving axis; idler wheels having axes parallel to that of the driving wheel; and a crawler belt which is spooled around the driving wheel and the idler wheels and travels around the driving wheel and the idler wheels. The crawler belt comprises an inner crawler belt having an engaging structure engaging with the driving wheel, the inner crawler belt being driven by the driving wheel; an outer crawler belt encircling circumferentially the outside of the inner crawler belt; a plurality of elastic members connecting the inner crawler belt to the outer crawler belt; and a plurality of crawler plates mounted to the outer crawler belt, and having lag for engaging with the ground.

    摘要翻译: 提供具有少量旋转轮机构的履带式行走装置,并使接触地面的压力相等。 履带式行驶装置包括由驱动轴驱动的驱动轮; 惰轮具有与驱动轮平行的轴; 以及履带,其围绕驱动轮和惰轮缠绕并围绕驱动轮和惰轮行进。 履带包括具有与驱动轮接合的接合结构的内履带,内履带由驱动轮驱动; 外履带,其周向地包围所述内履带的外侧; 将所述内侧履带与所述外侧履带连接的多个弹性部件; 以及安装在外履带上的多个履板,并且具有与地面接合的滞后。

    Shock absorbing apparatus for aircraft seat
    126.
    发明授权
    Shock absorbing apparatus for aircraft seat 有权
    飞机座椅减震装置

    公开(公告)号:US08573690B2

    公开(公告)日:2013-11-05

    申请号:US13057442

    申请日:2009-08-03

    IPC分类号: B60N2/42

    摘要: A shock absorbing apparatus for an aircraft seat that attenuates shock to passengers and crews includes; an airbag 11 being expanded in a plate shape in a state of less than maximum expansion; an upper flat plate 12 arranged on one side of the airbag 11; a lower flat plate 13 arranged on another side of the airbag 11; a gas supply device 15 for supplying a gas to the airbag 11; and a detector sending a signal to activate the gas supply device 15 by a preset condition. The shock is absorbed by expanding the airbag 11 before the shock is applied to the passenger.

    摘要翻译: 一种用于减轻对乘客和船员的冲击的飞机座椅的减震装置包括: 气囊11在小于最大膨胀的状态下膨胀成板状; 布置在气囊11一侧的上平板12; 布置在气囊11的另一侧的下平板13; 用于向气囊11供给气体的气体供给装置15; 以及检测器,其发送信号以使预定条件激活气体供给装置15。 在冲击应用于乘客之前,通过使气囊11膨胀来吸收冲击。

    Dielectric ceramic composition
    127.
    发明授权
    Dielectric ceramic composition 有权
    介电陶瓷组合物

    公开(公告)号:US08293668B2

    公开(公告)日:2012-10-23

    申请号:US12991601

    申请日:2008-05-15

    IPC分类号: C04B35/468

    摘要: Dielectric ceramic composition comprising a barium titanate including barium titanate having hexagonal structure as a main component, and an element “M”, an effective ionic radius of the “M” is within ±20% with respect to an effective ionic radius of 12-coordinated Ba2+ or with respect to an effective ionic radius of 6-coordinated Ti4+, an ionic valence of the “M” is larger than that of the Ba or Ti.

    摘要翻译: 包含钛酸钡的电介质陶瓷组合物,包括具有六方结构的钛酸钡作为主要成分,元素M,M的有效离子半径相对于12配位Ba2 +的有效离子半径相对于±20% 到6配位Ti4 +的有效离子半径,M的离子价态大于Ba或Ti的离子价。

    ELECTRIC ENERGY STORAGE APPARATUS CAPABLE OF AC OUTPUT
    128.
    发明申请
    ELECTRIC ENERGY STORAGE APPARATUS CAPABLE OF AC OUTPUT 有权
    交流输出电力储能装置

    公开(公告)号:US20120200163A1

    公开(公告)日:2012-08-09

    申请号:US13411483

    申请日:2012-03-02

    IPC分类号: H02J1/00

    摘要: An electric energy storage apparatus can generate an AC output in a low-loss and low-noise manner without using a DC-DC converter or an inverter. The electric energy storage apparatus comprises: an electric energy storage module group formed by connecting in series electric energy storage modules each comprising one or more electric energy storage elements; a balancing circuit electrically connected to the electric energy storage module group and configured to adjust a voltage to be applied to each of the electric energy storage modules; a first switch group comprising switches each in a path connecting a first terminal and a terminal of one of the series-connected electric energy storage modules; and a second switch group comprising switches each in a path connecting a second terminal and a terminal of one of the series-connected electric energy storage modules. The electric energy storage apparatus may perform a switch changeover in the switch groups.

    摘要翻译: 电能存储装置可以在不使用DC-DC转换器或逆变器的情况下以低损耗和低噪声的方式产生AC输出。 电能存储装置包括:电力存储模块组,其通过串联连接各自包含一个或多个电能存储元件的电能存储模块而形成; 电连接到电能存储模块组并被配置为调节施加到每个电能存储模块的电压的平衡电路; 第一开关组,其包括在连接所述串联连接的电能存储模块之一的第一端子和端子的路径中的开关; 以及第二开关组,其包括在连接所述串联连接的电能存储模块之一的第二端子和端子的路径中的开关。 电力存储装置可以在开关组中进行开关切换。

    DEPLOYABLE ANTENNA
    129.
    发明申请
    DEPLOYABLE ANTENNA 有权
    可配天线

    公开(公告)号:US20120193498A1

    公开(公告)日:2012-08-02

    申请号:US13361234

    申请日:2012-01-30

    IPC分类号: H01Q1/08

    CPC分类号: H01Q15/161 H01Q1/288

    摘要: A deployable antenna which has a larger aperture diameter by four-side links provided in at least three stages and which includes: six deployment link mechanisms (20) arranged radially from a central shaft so as to support an outer edge portion of a flexible reflector mirror surface; and one deployment driving mechanism (30) arranged at a lower portion of a center of arrangement of the six deployment link mechanisms, for unfolding the six deployment link mechanisms. Each of the six deployment link mechanisms includes a first four-side link (5), a second four-side link (6), and a third four-side link (7) arranged in an order from a position of the central shaft, around which the six deployment link mechanisms are arranged, toward an outer side of the each of the six deployment link mechanisms so that the each of the six deployment link mechanisms is structured to be foldable in three stages.

    摘要翻译: 一种可展开的天线,其具有通过设置在至少三个级中的四侧链路具有较大孔径的直径,并且包括:从中心轴径向布置的六个展开连杆机构(20),以支撑柔性反射镜的外缘部分 表面; 以及布置在六个部署链接机构的布置中心的下部的一个部署驱动机构(30),用于展开六个部署链接机构。 六个展开连杆机构中的每一个包括从中心轴的位置起依次布置的第一四侧连杆(5),第二四侧连杆(6)和第三四侧连杆(7) 六个部署链接机构围绕着六个部署链接机构排列,朝向六个部署链接机构中的每一个的外侧,使得六个部署链接机构中的每一个被构造成可分三个阶段折叠。

    AIRBORNE LIDAR FOR DETECTING MATTER SUSPENDED IN AIR
    130.
    发明申请
    AIRBORNE LIDAR FOR DETECTING MATTER SUSPENDED IN AIR 有权
    用于检测空气中悬挂物品的AIRBORNE LIDAR

    公开(公告)号:US20120182544A1

    公开(公告)日:2012-07-19

    申请号:US13343152

    申请日:2012-01-04

    IPC分类号: G01N21/49 G01N21/21 G01N21/55

    CPC分类号: G01S17/95 G01S7/499 Y02A90/19

    摘要: An object of the present invention is to provide a device which detects matter suspended in air, represented by, for example, ice crystals, volcanic ash, in the forward direction of the flight of an aircraft. A method of detecting matter suspended in air of this invention is characterized in that, in airborne Doppler LIDAR using laser light, components of matter subjected to laser light reflection and scattering are remotely measured on a basis of an angular difference in planes of polarization of transmitted light which is laser light radiated into the atmosphere, and received light scattered by matter suspended in air in a remote region.

    摘要翻译: 本发明的目的在于提供一种在飞行器的飞行方向上检测悬浮在空气中的物质,例如由冰晶,火山灰表示的装置。 本发明的悬浮在空气中的物质的检测方法的特征在于,在使用激光的机载多普勒激光雷达中,经受激光反射和散射的物质的成分基于透射的极化面的角度差进行远程测量 激光照射到大气中的光,并接收由悬浮在偏远地区的空气中的物质散射的光。