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    ENERGY STORAGE SYSTEM
    1.
    发明申请
    ENERGY STORAGE SYSTEM 审中-公开
    能源储存系统

    公开(公告)号：US20100055512A1

    公开(公告)日：2010-03-04

    申请号：US12589914

    申请日：2009-10-30

    Applicant: Bart D. Hibbs ,  William M. Parks ,  Omourtag A. Velev

    Inventor： Bart D. Hibbs ,  William M. Parks ,  Omourtag A. Velev

    IPC: H01M8/00

    CPC classification number: B64D27/24 ,  B64C2201/042 ,  B64D2041/005 ,  B64D2211/00 ,  H01M8/04097 ,  H01M8/04164 ,  H01M8/04373 ,  H01M8/04768 ,  H01M8/0656 ,  H01M8/186 ,  Y02E60/368 ,  Y02E60/528 ,  Y02P20/134 ,  Y02T50/44 ,  Y02T50/55 ,  Y02T50/62 ,  Y02T90/36

    Abstract: A closed loop energy storage system configured with a hydrogen tank, an oxygen tank, a fuel cell stack and an electrolyzer. A heat exchanger freeze-dries the hydrogen and oxygen prior to their storage in their respective tanks. The heat exchanger also uses excess fuel cell heat to preheat streams of hydrogen and oxygen coming from the tanks. Phase separators serve both to separate water from hydrogen and oxygen, and to store the water. A thermal management system encloses all the system components except the tanks. An airfoil-shaped shell covers the system, and the larger of the two tanks extends substantially across the shell at its point of greatest camber thickness. The tanks are composed of polymer liners integral with composite shells.

    Abstract translation: 一种闭环储能系统，其配置有氢罐，氧气罐，燃料电池堆和电解槽。 热交换器在将氢气和氧气储存在各自的储罐中之前将其冷冻干燥。 热交换器还使用过量的燃料电池热来预热来自罐的氢气和氧气流。 相分离器用于将水与氢气和氧气分开，并储存水分。 一个热管理系统包含除坦克之外的所有系统组件。 翼型壳体覆盖系统，并且两个坦克中的较大的壳体在其最大外倾厚度的点处基本上延伸穿过壳体。 这些罐由聚合物衬垫组成，与复合壳一体。

    Portable electrically powered blower apparatus
    2.
    发明授权
    Portable electrically powered blower apparatus 有权
    便携式电动鼓风机

    公开(公告)号：US06105206A

    公开(公告)日：2000-08-22

    申请号：US291504

    申请日：1999-04-13

    Applicant: Phillip T. Tokumaru ,  Bart D. Hibbs ,  Scott C. Newbern ,  Thomas Zambrano

    Inventor： Phillip T. Tokumaru ,  Bart D. Hibbs ,  Scott C. Newbern ,  Thomas Zambrano

    IPC: A01G1/12 ,  A47L5/14 ,  A47L5/24 ,  A47L5/36 ,  A47L9/00 ,  A47L9/32 ,  E01H1/08 ,  F04D19/00

    CPC classification number: A47L5/14 ,  A01G1/125 ,  A47L5/24 ,  A47L5/36 ,  A47L9/0081 ,  A47L9/322 ,  E01H1/0809 ,  F04D19/002

    Abstract: An improved portable electrically powered leaf blower is disclosed that can provide levels of air flow and velocity comparable to those of gasoline-powered blowers, yet that generates substantially reduced noise, eliminates exhaust emissions and emissions from spilled fuel, and is lightweight and convenient to operate. The leaf blower incorporates a sound-insulated duct that encloses an electric motor and fan assembly, and a handle projects above the duct's inlet end. Electrical power is provided by a battery pack carried in a backpack worn by the operator. Positioning the primary noise sources within a duct that in use is positioned close to the ground minimizes noise levels both at the operator's ears and at a distance.

    Abstract translation: 公开了一种改进的便携式电动叶片鼓风机，其可以提供与汽油发动机相当的空气流量和速度水平，但是产生显着降低的噪音，消除溢出燃料的废气排放和排放，并且重量轻且操作方便 。 叶片风机包括隔音管道，其包围电动机和风扇组件，并且手柄在管道的入口端上方突出。 电力由操作者佩戴的背包中携带的电池组提供。 将主要噪声源定位在使用中的导管内靠近地面的位置，使操作者的耳朵和远处的噪声水平最小化。

    Hydrogen powered aircraft
    3.
    发明授权
    Hydrogen powered aircraft 有权
    氢动力飞机

    公开(公告)号：US08308106B2

    公开(公告)日：2012-11-13

    申请号：US13200466

    申请日：2011-09-23

    Applicant: Paul B. MacCready ,  Bart D. Hibbs ,  Robert F. Curtin

    Inventor： Paul B. MacCready ,  Bart D. Hibbs ,  Robert F. Curtin

    IPC: B64D27/24 ,  B64D27/00

    CPC classification number: B64C1/26 ,  B64C3/10 ,  B64C3/14 ,  B64C9/24 ,  B64C39/024 ,  B64C39/10 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/086 ,  B64C2201/104 ,  B64C2201/122 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/187 ,  B64D27/02 ,  B64D27/24 ,  B64D37/30 ,  B64D2041/005 ,  Y02T50/12 ,  Y02T50/32 ,  Y02T50/44 ,  Y02T50/64 ,  Y02T90/36

    Abstract: Disclosed is an aircraft, configured to have a wide range of flight speeds, consuming low levels of power for an extended period of time, while supporting a communications platform with an unobstructed downward-looking view. The aircraft includes an extendable slat at the leading edge of the wing, and a reflexed trailing edge. The aircraft comprises a flying wing extending laterally between two ends and a center point. The wing is swept and has a relatively constant chord. The aircraft also includes a power module configured to provide power via a fuel cell. The fuel cell stores liquid hydrogen as fuel, but uses gaseous hydrogen in the fuel cell. A fuel tank heater is used to control the boil-rate of the fuel in the fuel tank. The fuel cell compresses ambient air for an oxidizer, and operates with the fuel and oxidizer at pressures below one atmosphere.

    Abstract translation: 公开了一种被配置为具有宽范围的飞行速度的飞机，在延长的时间段内消耗低水平的功率，同时以无阻碍的向下观看的方式支持通信平台。 飞机在翼的前缘包括可延伸的板条，以及反射的后缘。 飞机包括在两端之间横向延伸的飞翼和中心点。 机翼被扫掠并具有相对恒定的和弦。 该飞机还包括被配置为经由燃料电池提供电力的功率模块。 燃料电池将液态氢作为燃料储存，而在燃料电池中使用气态氢。 燃料箱加热器用于控制燃料箱中的燃料的沸腾率。 燃料电池压缩氧化剂的环境空气，并在低于一个大气压的燃料和氧化剂下操作。

    High altitude platform deployment system
    4.
    发明授权
    High altitude platform deployment system 有权
    高空平台部署系统

    公开(公告)号：US08180341B2

    公开(公告)日：2012-05-15

    申请号：US12387388

    申请日：2009-04-30

    Applicant: Bart D. Hibbs ,  Earl C. Cox

    Inventor： Bart D. Hibbs ,  Earl C. Cox

    IPC: H04W4/04 ,  H04B7/185 ,  G01C21/26 ,  G01S13/58

    CPC classification number: H04B7/18504

    Abstract: A communication system for supporting communications with a target market area. The system includes one or more solar-powered aircraft maintained in, or successively passing through, flight stations or flight patterns around the market area. Each of the aircraft targets limited beamwidth communication antennas on a substantial portion of the target market area. The control system is configured to fly selective flight patterns depending on the aircraft characteristics and the flight conditions. The flight patterns may emphasize high-power-generation patterns such as flying away from the sun for aircraft with wing-mounted solar cells.

    Abstract translation: 一种用于支持与目标市场区域通信的通信系统。 该系统包括一个或多个维护在市场区域附近或相继通过飞行站或飞行模式的太阳能飞机。 每个飞机在目标市场区域的大部分上瞄准有限的波束宽度通信天线。 控制系统被配置为根据飞机特性和飞行条件飞行选择性飞行模式。 飞行模式可能会强调高功率发电模式，例如用飞机安装的太阳能电池飞离太阳。

    Enhancements to high efficiency ceiling fan
    8.
    发明授权
    Enhancements to high efficiency ceiling fan 有权
    增强高效吊扇

    公开(公告)号：US07210910B1

    公开(公告)日：2007-05-01

    申请号：US11027242

    申请日：2004-12-31

    Applicant: Danny S. Parker ,  Guan Hua Su ,  Bart D. Hibbs

    Inventor： Danny S. Parker ,  Guan Hua Su ,  Bart D. Hibbs

    IPC: F04D29/38

    CPC classification number: F04D25/088 ,  F04D29/384

    Abstract: Twisted ceiling fan blades for low, medium and high speed operation of less than approximately 250 rpm. The novel blades twisted blades can be configured for 60″ and 64″ diameter fans, and have less blades (3 for example) than conventional flat type bladed fans having 4, 5 blades and have greater air flow and less power draw results than the conventional flat 54 inch fans. Any of the novel twisted blades of 54″, 60″ and 64″ can be run at reduced speeds, drawing less Watts than conventional fans and still perform better with more air flow and less problems than conventional flat type conventional blades.

    Abstract translation: 用于低，中，高速操作的扭转天花板叶片小于约250rpm。 新型叶片扭转叶片可以配置为直径为60“和64”的风扇，并且具有比具有4,5叶片的传统扁平型叶片风扇更少的叶片（例如3），并且具有更大的气流和更少的功率抽取结果 传统平板54寸风扇。 54“，60”和64“的任何新颖的扭转叶片都可以以较低的速度运行，比常规风扇的瓦数小得多，并且与传统的扁平型传统叶片相比，仍然具有更好的空气流动和更少的问题。

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