Flow field plate module for fuel cell system
    121.
    发明授权
    Flow field plate module for fuel cell system 失效
    燃料电池系统流场板模块

    公开(公告)号:US08101313B2

    公开(公告)日:2012-01-24

    申请号:US11905212

    申请日:2007-09-28

    IPC分类号: H01M8/24 H01M8/04

    CPC分类号: H01M8/0258 H01M8/04186

    摘要: A flow field plate module for a fuel cell system includes at least one flow field plate defining a fuel transporting channel thereon. The fuel transporting channel is divided into a middle converging zone having a group of first flow guiding plates arranged therein, and two diverging zones located at two lateral sides of the middle converging zone and each having a group of second flow guiding plates arranged therein. The second flow guiding plates are symmetrically arranged in the two diverging zones and are directed at respective inner end toward a space between two adjacent first flow guiding plates in the middle converging zone to thereby offset from each of the two adjacent first flow guiding plates by a predetermined distance in a fuel flowing direction, so that a fluid path is formed between any two adjacent first and second flow guiding plates.

    摘要翻译: 用于燃料电池系统的流场板模块包括在其上限定燃料输送通道的至少一个流场板。 燃料输送通道被分成具有一组布置在其中的一组第一导流板的中间会聚区域,以及位于中间会聚区域的两个侧面处的两个发散区域,每个具有布置在其中的一组第二导流板。 第二流动引导板对称地布置在两个发散区域中并且在相应的内端处朝向中间会聚区域中的两个相邻的第一导流板之间的空间引导,从而从两个相邻的第一流动引导板中的每一个偏移一个 在燃料流动方向上的预定距离,使得在任何两个相邻的第一和第二导流板之间形成流体路径。

    HYDROGEN GENERATION DEVICE AND FUEL CELL USING THE SAME
    122.
    发明申请
    HYDROGEN GENERATION DEVICE AND FUEL CELL USING THE SAME 失效
    氢气发生装置和使用它的燃料电池

    公开(公告)号:US20110189563A1

    公开(公告)日:2011-08-04

    申请号:US12908002

    申请日:2010-10-20

    IPC分类号: H01M8/06 B01J19/00

    CPC分类号: B01J19/00 H01M8/06

    摘要: A hydrogen generation device and a fuel cell using the same are provided. The hydrogen generation device includes a first containing groove, a cover, a second containing groove, and a rotating device. The first containing groove contains liquid water. The cover is fixed on the first containing groove and covers the liquid water. The cover has an opening for exposing the liquid water. The second containing groove is stacked on the cover and divided into a plurality of containing compartments, wherein each containing compartment contains a solid fuel. The opening is aligned with one containing compartment so that the corresponding solid fuel reacts with the liquid water generate hydrogen. The rotating device is connected with the first or the second containing groove. The opening is moved and aligned with another containing compartment when the rotating device drives the first containing groove and the second containing groove to relatively rotate.

    摘要翻译: 提供了一种氢生成装置和使用其的燃料电池。 氢产生装置包括第一容纳槽,盖,第二容纳槽和旋转装置。 第一容纳槽包含液态水。 盖固定在第一容纳槽上并覆盖液态水。 盖具有用于暴露液态水的开口。 第二容纳槽堆叠在盖上并分成多个容纳隔室,其中每个容纳室包含固体燃料。 开口与一个容纳隔间对准,使得相应的固体燃料与液态水反应产生氢气。 旋转装置与第一或第二容纳槽连接。 当旋转装置驱动第一容纳槽和第二容纳槽相对旋转时,开口移动并与另一容纳隔间对准。

    FUEL MIXING TANK AND FUEL CELL SYSTEM
    123.
    发明申请
    FUEL MIXING TANK AND FUEL CELL SYSTEM 审中-公开
    燃料混合罐和燃料电池系统

    公开(公告)号:US20110129761A1

    公开(公告)日:2011-06-02

    申请号:US12850646

    申请日:2010-08-05

    IPC分类号: H01M8/04

    CPC分类号: H01M8/04208 H01M8/04201

    摘要: A fuel mixing tank adapted for supplying fuel to a fuel cell unit of a fuel cell system is provided. The fuel mixing tank includes a storage room, a supplying pipe, and a fuel recycling pipe. The storage room is adapted for communicating with the fuel cell unit to supply fuel to the fuel cell unit. The supplying pipe supplies fuel or water to the storage room and is thermally and adjacently connected to the storage room. The fuel recycling pipe is adapted for communicating with the fuel cell unit to recycle fuel from the fuel cell unit, and the fuel recycling pipe and the supplying pipe are connected at a convergence place communicating with the storage room. The fuel mixing tank has superior power generation efficiency.

    摘要翻译: 提供了一种用于向燃料电池系统的燃料电池单元供应燃料的燃料混合罐。 燃料混合罐包括储藏室,供给管和燃料循环管。 存储室适于与燃料电池单元连通以向燃料电池单元供应燃料。 供应管道向储藏室供应燃料或水,并且热和相邻地连接到储藏室。 燃料循环管适于与燃料电池单元连通以从燃料电池单元再循环燃料,并且燃料回收管和供应管在与储藏室连通的会聚处连接。 燃料混合罐具有优异的发电效率。

    LOOP HEAT PIPE AND MANUFACTURING METHOD THEREOF
    125.
    发明申请
    LOOP HEAT PIPE AND MANUFACTURING METHOD THEREOF 有权
    环形管及其制造方法

    公开(公告)号:US20100307721A1

    公开(公告)日:2010-12-09

    申请号:US12789421

    申请日:2010-05-27

    申请人: Cheng Wang

    发明人: Cheng Wang

    IPC分类号: F28D15/04 B21D53/02

    摘要: A loop heat pipe for dissipating heat generated by a heat source includes a pipe, a first capillary structure, a second capillary structure, and a working fluid in the pipe. The pipe has a condensing section, an evaporating section adapted to contact the heat source thermally, and an obstructing section adjacent to the evaporating section. The first capillary structure on an inner surface of the pipe is disposed between the condensing section and the obstructing section. The second capillary structure has a first and a second parts connected with each other. The first part on the inner surface of the pipe is extended from the evaporating section to the obstructing section. The second part passing through the obstructing section is extended from the obstructing section to the condensing section. A space between the first capillary structure and the second part of the second capillary structure defines a compensation room.

    摘要翻译: 用于散发由热源产生的热的回路热管包括管道,第一毛细管结构,第二毛细管结构和管道中的工作流体。 管道具有冷凝部分,适于热接触热源的蒸发部分和与蒸发部分相邻的阻塞部分。 管的内表面上的第一毛细结构设置在冷凝部分和阻塞部分之间。 第二毛细管结构具有彼此连接的第一和第二部分。 管的内表面上的第一部分从蒸发部分延伸到阻塞部分。 通过阻塞部分的第二部分从阻塞部分延伸到冷凝部分。 第一毛细管结构与第二毛细管结构的第二部分之间的空间限定了补偿室。

    Fuel cell system
    126.
    发明申请
    Fuel cell system 审中-公开
    燃料电池系统

    公开(公告)号:US20100279189A1

    公开(公告)日:2010-11-04

    申请号:US12003877

    申请日:2008-01-03

    IPC分类号: H01M8/04

    摘要: A fuel cell system having uniform temperature field, includes at least one fuel cell stack. The fuel cell stack includes a housing, a fuel cell module, and an air guiding device. The housing defines an internal receiving space, and has an air outlet zone and at least two air inlet zones. The fuel cell module is disposed in the receiving space and includes a plurality of membrane electrode assemblies are disposed at intervals along a first sidewall toward a second sidewall on a plane of the receiving space of the housing. Each of the membrane electrode assemblies corresponds to at least one of the air inlet zones. The air guiding device is disposed on of the housing for generating airflows via the air inlet zones into the housing. The airflows flow along cathode surfaces of the membrane electrode assemblies and finally flow out of the housing via the air outlet zone.

    摘要翻译: 具有均匀温度场的燃料电池系统包括至少一个燃料电池堆。 燃料电池堆包括壳体,燃料电池模块和空气引导装置。 壳体限定内部容纳空间,并且具有空气出口区域和至少两个空气入口区域。 燃料电池模块设置在容纳空间中,并且包括多个膜电极组件,其沿着第一侧壁间隔地设置在壳体的容纳空间的平面上的第二侧壁。 每个膜电极组件对应于至少一个空气入口区域。 空气引导装置设置在壳体上,用于经由空气入口区域产生气流进入壳体。 气流沿着膜电极组件的阴极表面流动,并且最终经由空气出口区域流出壳体。

    Illumination apparatus
    127.
    发明申请
    Illumination apparatus 审中-公开
    照明装置

    公开(公告)号:US20100246166A1

    公开(公告)日:2010-09-30

    申请号:US12659790

    申请日:2010-03-22

    IPC分类号: F21L4/02 F21V29/00 F21L4/00

    摘要: An illumination apparatus includes a housing, a light source, a centrifugal fan, and a heat sink. The housing has an accommodation, a plurality of inlets, and a plurality of outlets. The accommodation communicates with the outside of the housing through the inlets and the outlets. The light source, the centrifugal fan, and the heat sink are disposed in the accommodation. The heat sink includes a base and a plurality of fins connected to the base. The base is connected to the light source, the fins radially surround the centrifugal fan. An air channel is disposed between two adjacent fins. An air from the outside of the housing is capable of flowing into the accommodation through the inlets and then into the centrifugal fan in an axial direction of the centrifugal fan, and flow out of the accommodation in a radial direction of the centrifugal fan through the air channel and outlets.

    摘要翻译: 照明装置包括壳体,光源,离心风扇和散热器。 壳体具有容纳物,多个入口和多个出口。 住宿通过入口和出口与住房的外部通信。 光源,离心风扇和散热片设置在住宅内。 散热器包括基座和连接到基座的多个鳍片。 基座连接到光源,散热片径向包围离心式风扇。 空气通道设置在两个相邻的翅片之间。 来自壳体外部的空气能够通过入口流入容纳物,然后沿离心风扇的轴向流入离心式风扇,并通过空气沿着离心式风扇的径向流出容器 渠道和网点。

    Germanium doped n-type aluminum nitride epitaxial layers
    128.
    发明授权
    Germanium doped n-type aluminum nitride epitaxial layers 失效
    锗掺杂n型氮化铝外延层

    公开(公告)号:US07682709B1

    公开(公告)日:2010-03-23

    申请号:US08550195

    申请日:1995-10-30

    IPC分类号: B32B18/00

    摘要: A method of preparing an n-type epitaxial layer of aluminum nitride conductively doped with germanium comprises directing a molecular beam of aluminum atoms onto the growth surface of a substrate that provides an acceptable lattice match for aluminum nitride; directing a molecular beam of activated nitrogen to the growth surface of the substrate; and directing a molecular beam of germanium to the growth surface of the substrate; while maintaining the growth surface of the substrate at a temperature high enough to provide the surface mobility and sticking coefficient required for epitaxial growth, but lower than the temperature at which the surface would decompose or the epitaxial layer disassociate back into atomic or molecular species.

    摘要翻译: 制备导电掺杂锗的氮化铝的n型外延层的方法包括将铝原子的分子束引导到提供氮化铝可接受的晶格匹配的衬底的生长表面上; 将活性氮的分子束引导到基底的生长表面; 并将锗的分子束引导到所述衬底的生长表面; 同时将衬底的生长表面保持在足够高的温度以提供外延生长所需的表面迁移率和粘附系数,但低于表面将分解的温度或外延层解离成原子或分子物质。

    AIRCRAFT FLIGHT DISPLAY WITH A NON-LINEAR PITCH SCALE
    129.
    发明申请
    AIRCRAFT FLIGHT DISPLAY WITH A NON-LINEAR PITCH SCALE 有权
    具有非线性尺寸的飞机飞行显示

    公开(公告)号:US20090121901A1

    公开(公告)日:2009-05-14

    申请号:US11940112

    申请日:2007-11-14

    IPC分类号: G01C23/00

    摘要: A display image for use in an aircraft is produced in response to receiving aircraft location, heading, altitude, and pitch data. The location and heading data are employed to access a topographical database and obtain terrain information for a region on the earth's surface ahead of the aircraft. A terrain image is produced from the terrain information and a non-linear pitch scale is superimposed over the terrain image. The non-linear pitch scale corresponds to the relationship of the aircraft pitch and the terrain image. Additional data designating other aircraft operational parameters, such as speed and altitude, are depicted by graphical objects. The terrain image, the non-linear pitch scale, and the graphical objects are combined into the display image. The terrain image and the non-linear pitch scale move in the display image in response to changes in the pitch of the aircraft.

    摘要翻译: 响应于接收飞行器的位置,航向,高度和俯仰数据而产生用于飞行器的显示图像。 采用位置和标题数据来访问地形数据库,并获取飞机前方地球表面上的区域的地形信息。 从地形信息产生地形图像,并且在地形图像上叠加非线性俯仰尺度。 非线性俯仰尺度对应于飞机俯仰和地形图像的关系。 图形对象描绘了指定其他飞机操作参数(如速度和高度)的附加数据。 地形图像,非线性俯仰尺度和图形对象被组合到显示图像中。 响应于飞行器的俯仰变化,地形图像和非线性俯仰比例在显示图像中移动。