利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

12 条记录 (耗时 0.016 秒)

    RETRACTABLE GAS TURBINE INLET COILS
    2.
    发明申请
    RETRACTABLE GAS TURBINE INLET COILS 有权
    可回收气体涡轮机入口线圈

    公开(公告)号：US20130051994A1

    公开(公告)日：2013-02-28

    申请号：US13215498

    申请日：2011-08-23

    申请人： Eric Milton LAFONTAINE ,  Michael Adelbert SULLIVAN ,  Huong Van VU ,  Bhalchandra Arun DESAI ,  Mark Andrew COURNOYER

    发明人： Eric Milton LAFONTAINE ,  Michael Adelbert SULLIVAN ,  Huong Van VU ,  Bhalchandra Arun DESAI ,  Mark Andrew COURNOYER

    IPC分类号： F02C7/04 ,  B23P17/00 ,  F02C7/00

    CPC分类号： F02C7/143 ,  Y10T29/49229

    摘要： A gas turbine inlet heat exchange coil assembly includes a gas turbine inlet housing formed to include an inlet and an outlet and a flow path therebetween. A plurality of adjacent coils are located in proximity to the inlet, and moveable between a closed operative position where the coils are aligned substantially in a plane so as to maximize resistance to flow along the flow path, and an open inoperative position where said coils are individually rotated substantially 90° such that the coils lie in individual, parallel planes so as to minimize resistance to flow along the flow path.

    摘要翻译： 燃气轮机入口热交换线圈组件包括形成为包括入口和出口的燃气轮机入口壳体和它们之间的流动路径。 多个相邻的线圈位于入口附近，并且在闭合的操作位置之间运动，其中线圈基本上在一个平面中对齐，以便最大化沿着流动路径的流动阻力，以及开放的不工作位置，其中所述线圈是 单独旋转大约90°，使得线圈位于单独的平行平面中，以便最小化沿着流动路径的流动阻力。

    VARIABLE TEMPERATURE CHILLER COILS
    4.
    发明申请
    VARIABLE TEMPERATURE CHILLER COILS 审中-公开
    可变温度冷却器线圈

    公开(公告)号：US20130048265A1

    公开(公告)日：2013-02-28

    申请号：US13215583

    申请日：2011-08-23

    申请人： Bhalchandra Arun DESAI ,  Michael Adelbert SULLIVAN ,  Huong Van VU ,  Eric Milton LAFONTAINE ,  Mark Andrew COURNOYER

    发明人： Bhalchandra Arun DESAI ,  Michael Adelbert SULLIVAN ,  Huong Van VU ,  Eric Milton LAFONTAINE ,  Mark Andrew COURNOYER

    IPC分类号： F28F27/00 ,  F28D15/00

    CPC分类号： F02C7/143 ,  F02C7/1435

    摘要： A chiller coil system for an asymmetric gas turbine filter house includes a plurality of chiller coil modules arranged in a substantially vertical array, each chiller coil module provided with a cooled fluid inlet pipe and a fluid outlet pipe. Each outlet pipe is connected to a common return pipe and at least some of the inlet pipes are connected to the common return pipe. A mixing control valve is provided for controlling an amount of cooling fluid in the common return pipe to be added to at least some of the inlet pipes.

    摘要翻译： 用于不对称燃气涡轮机过滤器房屋的冷却器盘管系统包括以基本垂直的阵列布置的多个冷却器盘管模块，每个冷却器盘管模块设置有冷却的流体入口管和流体出口管。 每个出口管连接到公共回流管，并且至少一些入口管连接到公共回流管。 提供了一种混合控制阀，用于控制要添加到至少一些入口管道的公共回流管中的冷却流体的量。

    Retractable gas turbine inlet coils
    7.
    发明授权
    Retractable gas turbine inlet coils 有权
    伸缩式燃气轮机入口线圈

    公开(公告)号：US08894356B2

    公开(公告)日：2014-11-25

    申请号：US13215498

    申请日：2011-08-23

    申请人： Eric Milton Lafontaine ,  Michael Adelbert Sullivan ,  Huong Van Vu ,  Bhalchandra Arun Desai ,  Mark Andrew Cournoyer

    发明人： Eric Milton Lafontaine ,  Michael Adelbert Sullivan ,  Huong Van Vu ,  Bhalchandra Arun Desai ,  Mark Andrew Cournoyer

    IPC分类号： F02C7/143

    CPC分类号： F02C7/143 ,  Y10T29/49229

    摘要： A gas turbine inlet heat exchange coil assembly includes a gas turbine inlet housing formed to include an inlet and an outlet and a flow path therebetween. A plurality of adjacent coils are located in proximity to the inlet, and moveable between a closed operative position where the coils are aligned substantially in a plane so as to maximize resistance to flow along the flow path, and an open inoperative position where said coils are individually rotated substantially 90° such that the coils lie in individual, parallel planes so as to minimize resistance to flow along the flow path.

    摘要翻译： 燃气轮机入口热交换线圈组件包括形成为包括入口和出口的燃气轮机入口壳体和它们之间的流动路径。 多个相邻的线圈位于入口附近，并且在闭合的操作位置之间运动，其中线圈基本上在一个平面中对齐，以便最大化沿着流动路径的流动阻力，以及开放的不工作位置，其中所述线圈是 单独旋转大约90°，使得线圈位于单独的平行平面中，以便最小化沿着流动路径的流动阻力。

    System and method for conditioning air flow to a gas turbine
    8.
    发明授权
    System and method for conditioning air flow to a gas turbine 有权
    调节到燃气轮机的气流的系统和方法

    公开(公告)号：US08465573B2

    公开(公告)日：2013-06-18

    申请号：US13253273

    申请日：2011-10-05

    申请人： Michael Adelbert Sullivan ,  Huong Van Vu ,  Bhalchandra Arun Desai ,  Eric M. Lafontaine ,  Mark Andrew Cournoyer

    发明人： Michael Adelbert Sullivan ,  Huong Van Vu ,  Bhalchandra Arun Desai ,  Eric M. Lafontaine ,  Mark Andrew Cournoyer

    IPC分类号： B01D46/00

    CPC分类号： F02C7/05 ,  F02C7/143 ,  F05D2250/70 ,  F05D2250/71 ,  F05D2300/522 ,  F28F13/14

    摘要： A system for conditioning air flow to a gas turbine includes a filter housing and a conditioning media inside the filter housing to adjust the temperature of the air flowing through the filter housing. At least one of a depth or a density of the conditioning media varies across the filter housing. A method for conditioning air flow to a gas turbine includes flowing air through a filter housing connected to the gas turbine and flowing the air across a conditioning media in the filter housing. The method further includes conditioning the air flow to reduce the temperature difference of the air exiting the filter housing across a dimension of the filter housing.

    摘要翻译： 用于调节到燃气轮机的空气流的系统包括过滤器壳体和过滤器壳体内部的调节介质，以调节流过过滤器壳体的空气的温度。 调节介质的深度或密度中的至少一个在过滤器壳体上变化。 用于调节到燃气轮机的空气流的方法包括使空气流过连接到燃气轮机的过滤器壳体并使空气流过过滤器壳体中的调节介质。 该方法还包括调节空气流量以减小过滤器壳体的空气在过滤器壳体的尺寸上的温度差。