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20 条记录 (耗时 0.025 秒)

    Self contained marine air conditioner
    2.
    发明授权
    Self contained marine air conditioner 失效
    自备海洋空调

    公开(公告)号：US5848536A

    公开(公告)日：1998-12-15

    申请号：US897632

    申请日：1997-07-21

    申请人： David Dodge ,  James Harper ,  Frank Marciano

    发明人： David Dodge ,  James Harper ,  Frank Marciano

    IPC分类号： B63J2/04 ,  B63B25/26 ,  F25B27/00 ,  F25D17/06

    CPC分类号： B63J2/04 ,  F24F2203/02

    摘要： A marine air conditioner (which may also be used as a heat pump) has a low volume to cooling capacity ratio, and high efficiency. A blower is connected to a shroud, and within the shroud are a water cooled tube-in-tube condenser coil and a raised lance fin evaporator coil. The condenser coil is mounted between the evaporator coil and the blower so that air is drawn past the evaporator coil, then past the condenser coil, and then discharged by the blower. The shroud and blower are mounted, along with a rotary compressor connected to the coils by refrigerant lines, in a condensate drain pan having side walls of 1.5 inches or more in height and a plurality of widely spaced drain plugs or fittings. The cooling water inlet and outlet for the condenser coil pass through a wall of the shroud, and the inlet is connected to a water pump below the water line of the boat in which the condensate pan is mounted.

    摘要翻译： 船用空调（也可以用作热泵）具有体积小，冷却能力高，效率高的优点。 鼓风机连接到护罩，并且在护罩内是水冷的管中管冷凝器盘管和升高的喷枪翅片蒸发器盘管。 冷凝器盘管安装在蒸发器盘管和鼓风机之间，使得空气被抽过蒸发器盘管，然后经过冷凝器盘管，然后由鼓风机排出。 护罩和鼓风机与连接到线圈的旋转式压缩机一起安装在具有高度为1.5英寸或更大的侧壁的冷凝水排放盘中，以及多个间隔开的排水塞或配件。 冷凝器盘管的冷却水入口和出口通过护罩的壁，并且入口连接到安装有冷凝盘的船的水线下方的水泵。

    Electrolytic reactor and related methods for supplementing the air intake of an internal combustion engine
    3.
    发明授权
    Electrolytic reactor and related methods for supplementing the air intake of an internal combustion engine 失效
    电解反应器及补充内燃机进气口的相关方法

    公开(公告)号：US08347829B2

    公开(公告)日：2013-01-08

    申请号：US12476385

    申请日：2009-06-02

    申请人： James Harper

    发明人： James Harper

    IPC分类号： F02B43/08

    CPC分类号： C25B9/20 ,  C25B1/08 ,  F02B2043/106 ,  F02M25/12 ,  Y02E60/366 ,  Y02T10/121

    摘要： An electrolytic reactor and related methods are provided for supplementing the air-intake of an internal combustion engine with hydrogen. In one embodiment, the reactor has a core defined by a plurality of whole metal plates separated by peripheral gaskets; an inlet for providing an electrolyte to the core; a gas and effluent outlet, and a pump to force an electrolyte through the core.

    摘要翻译： 提供一种电解反应器和相关方法，用于用氢气补充内燃机的进气口。 在一个实施方案中，反应器具有由多个由外围垫片分隔开的整个金属板限定的芯; 用于向芯提供电解质的入口; 气体和流出物出口，以及迫使电解质通过芯的泵。

    Method and apparatus to facilitate cooling of a diffusion tip within a gas turbine engine
    8.
    发明授权
    Method and apparatus to facilitate cooling of a diffusion tip within a gas turbine engine 有权
    有助于冷却燃气涡轮发动机内的扩散尖端的方法和装置

    公开(公告)号：US08479519B2

    公开(公告)日：2013-07-09

    申请号：US12350083

    申请日：2009-01-07

    申请人： Wei Chen ,  William Lawrence Byrne ,  Xiaoguang Yu ,  James Harper

    发明人： Wei Chen ,  William Lawrence Byrne ,  Xiaoguang Yu ,  James Harper

    IPC分类号： F02C1/00 ,  F02G3/00

    CPC分类号： F23R3/283 ,  F23D14/78 ,  F23D2214/00 ,  F23D2900/00016 ,  Y10T29/4932

    摘要： A method and apparatus for a diffusion tip for use with a fuel nozzle is described. The diffusion tip has a substantially circular body including an outer surface and an opposite inner surface. The diffusion tip body extends from a discharge end to an inlet end. The diffusion tip includes an inlet surface adjacent to the discharge end and defined within the body. A discharge surface is defined opposite the inlet surface. A plurality of diffusion apertures each extend between the discharge surface and the inlet surface, each aperture is oriented relative to the body to discharge a diffusion flow outward therefrom at an angle γ (gamma) measured in an X-Z plane between a centerline of the aperture and an X-axis extending tangentially to the outer surface, and at an angle θ (theta) measured in a Y-Z plane between the centerline of the aperture and a Y-axis extending radially outward from the centerline.

    摘要翻译： 描述了用于与燃料喷嘴一起使用的扩散尖端的方法和装置。 扩散尖端具有包括外表面和相对的内表面的基本圆形的主体。 扩散尖端体从排出端延伸到入口端。 扩散尖端包括邻近放电端并限定在体内的入口表面。 排出表面限定与入口表面相对。 多个扩散孔各自在排出表面和入口表面之间延伸，每个孔相对于主体定向，以在XZ平面中在孔的中心线和 与外表面相切地延伸的X轴，并且以在孔的中心线和从中心线径向向外延伸的Y轴的YZ平面中测量的角度θ（θ）延伸。

    Method for managing data in a shared computing environment
    9.
    发明授权
    Method for managing data in a shared computing environment 失效
    在共享计算环境中管理数据的方法

    公开(公告)号：US08352999B1

    公开(公告)日：2013-01-08

    申请号：US11490676

    申请日：2006-07-21

    申请人： Kaijun Zhan ,  James Harper

    发明人： Kaijun Zhan ,  James Harper

    IPC分类号： H04L29/06

    CPC分类号： H04L63/083 ,  H04L63/104

    摘要： A method of storing secret data in a shared computing environment includes defining secret data, such as a password and administration policies according to a schema of a directory server such as a LDAP server. The secret data and administration polices are centrally stored on the LDAP server. The secret data can be encrypted. Administration polices include authorization and authentication policies, and a security zone can be defined for a collection of entities with a common security characteristic, such as a common password. A security zone defines a group of users and the secret data that can be accessed by the group of users. Multiple security zones can be defined. The secret data can be accessed directly from the server of the directory service without accessing another server or data store assuming the administration policies are satisfied.

    摘要翻译： 在共享计算环境中存储秘密数据的方法包括根据诸如LDAP服务器的目录服务器的模式定义秘密数据，例如密码和管理策略。 秘密数据和管理策略集中存储在LDAP服务器上。 秘密数据可以加密。 管理政策包括授权和认证策略，并且可以为具有公共安全特性的实体集合定义安全区域，例如通用密码。 安全区域定义一组用户和可由该组用户访问的秘密数据。 可以定义多个安全区域。 秘密数据可以直接从目录服务的服务器访问，而不需要访问另一个服务器或数据存储，假设管理策略得到满足。

    Methods and systems for operating gas turbine engines
    10.
    发明授权
    Methods and systems for operating gas turbine engines 有权
    运行燃气涡轮发动机的方法和系统

    公开(公告)号：US08122725B2

    公开(公告)日：2012-02-28

    申请号：US11933898

    申请日：2007-11-01

    申请人： Geoffrey David Myers ,  David August Snider ,  Eric Motter ,  Daniel R. Tegel ,  James Harper ,  Stephen R. Watts ,  Joseph Citeno

    发明人： Geoffrey David Myers ,  David August Snider ,  Eric Motter ,  Daniel R. Tegel ,  James Harper ,  Stephen R. Watts ,  Joseph Citeno

    IPC分类号： F02C7/22 ,  F02C9/26 ,  F02C9/00 ,  F02C3/00

    CPC分类号： F02C7/228

    摘要： Methods and systems for delivering fuel in a gas turbine engine are provided. The system includes a plurality of can annular combustors that includes at least a first set of combustors of the plurality of can annular combustors and at least a second set of combustors of the plurality of can annular combustors wherein each set of combustors is supplied by a separately controllable respective fuel delivery system. The method includes supplying fuel at a first fuel schedule to the first set of combustors and supplying fuel at a second fuel schedule to the second set of combustors during a first mode of operation wherein the second fuel schedule is different than the first fuel schedule, and supplying fuel at the second fuel schedule to the first and second sets of combustors during a second mode of operation.

    摘要翻译： 提供了用于在燃气涡轮发动机中输送燃料的方法和系统。 该系统包括多个罐式环形燃烧器，其包括多个罐环形燃烧器中的至少第一组燃烧器和多个罐形环形燃烧器的至少第二组燃烧器，其中每组燃烧器由单独的 可控的燃油输送系统。 该方法包括以第一燃料排程向第一组燃料供应燃料，并在第一燃料运行方式中将第二燃料的燃料供应给第二组燃料，其中第二燃料计划与第一燃料计划不同，以及 在第二工作模式期间将第二燃料计划的燃料供应到第一和第二组燃烧器。