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    Turbocharger system
    3.
    发明申请
    Turbocharger system 审中-公开
    涡轮增压器系统

    公开(公告)号：US20070144175A1

    公开(公告)日：2007-06-28

    申请号：US11646416

    申请日：2006-12-28

    申请人： Thomas Sopko ,  Michael Vanderham ,  Kent Casey ,  Brian Kuras

    发明人： Thomas Sopko ,  Michael Vanderham ,  Kent Casey ,  Brian Kuras

    IPC分类号： F02D23/00 ,  F02B33/44

    CPC分类号： F02D13/0226 ,  F02B29/0412 ,  F02B39/10 ,  F02B2275/14 ,  F02D13/0269 ,  F02D15/04 ,  F02D23/02 ,  F02D41/0007 ,  F02D2200/0406 ,  F02M26/08 ,  F02M26/23 ,  Y02T10/142 ,  Y02T10/144

    摘要： A system for controlling intake pressure of a combustion engine operably coupled to a power generation system includes at least one turbocharger operably coupled to the intake system of the combustion engine. The at least one turbocharger is configured to increase the intake pressure in the intake system of the combustion engine. A turbocharger controller is configured to compare actual and desired intake pressures and control operation of the at least one turbocharger based on the comparison such that the turbocharger supplies a desired intake pressure to the combustion engine.

    摘要翻译： 用于控制可操作地耦合到发电系统的内燃机的进气压力的系统包括可操作地联接到内燃机的进气系统的至少一个涡轮增压器。 所述至少一个涡轮增压器构造成增加所述内燃机的进气系统中的进气压力。 涡轮增压器控制器被配置为基于比较来比较实际和期望的进气压力和至少一个涡轮增压器的控制操作，使得涡轮增压器向内燃机提供期望的进气压力。

    Electric drive system having DC bus voltage control
    5.
    发明申请
    Electric drive system having DC bus voltage control 有权
    电动驱动系统具有直流母线电压控制

    公开(公告)号：US20050263329A1

    公开(公告)日：2005-12-01

    申请号：US10852137

    申请日：2004-05-25

    申请人： Brian Kuras ,  Thomas Sopko

    发明人： Brian Kuras ,  Thomas Sopko

    IPC分类号： E02F9/20 ,  B60K1/00 ,  B60K6/46 ,  B60L11/08 ,  B60L11/12 ,  B60W10/08 ,  B60W20/00 ,  B61C9/38 ,  H01M10/48 ,  H02P9/04

    CPC分类号： B60W20/10 ,  B60K6/46 ,  B60L11/123 ,  B60L2200/40 ,  B60L2220/18 ,  B60W10/08 ,  B60W10/26 ,  B60W20/00 ,  B60W2300/17 ,  H01M10/482 ,  Y02T10/6217 ,  Y02T10/7005 ,  Y02T10/7022 ,  Y02T10/7077 ,  Y02T90/16

    摘要： An electric drive system has a power source and a generator operatively connected to the power source. The generator is configured to produce a power output. The electric drive system also has at least one capacitor configured to store a supply of power. The electric drive system further has a common bus configured to direct the power output to the capacitor. The electric drive system also has at least one motor configured to receive power from the common bus. The electric drive system additionally has a controller in communication with the at least one motor and the generator. The controller is configured to receive at least one input associated with the motor, to determine a requested motor power as a function of the at least one input, and to operate the generator to produce the requested motor power.

    摘要翻译： 电驱动系统具有电源和可操作地连接到电源的发生器。 发电机被配置为产生功率输出。 电驱动系统还具有至少一个配置成存储电力供应的电容器。 电驱动系统还具有配置成将功率输出引导到电容器的公共总线。 电驱动系统还具有至少一个被配置为从公共总线接收电力的电动机。 电驱动系统还具有与至少一个电动机和发电机连通的控制器。 控制器被配置为接收与电动机相关联的至少一个输入，以根据至少一个输入来确定所请求的电动机功率，并且操作发电机以产生所请求的电动机功率。

    Retarding and filter cleaning method and system
    7.
    发明申请
    Retarding and filter cleaning method and system 审中-公开
    清洗和过滤清洗方法和系统

    公开(公告)号：US20070119146A1

    公开(公告)日：2007-05-31

    申请号：US11289321

    申请日：2005-11-30

    申请人： James Callas ,  Kevin Martin ,  Cody Renshaw ,  Thomas Sopko ,  Andrew Tonsor

    发明人： James Callas ,  Kevin Martin ,  Cody Renshaw ,  Thomas Sopko ,  Andrew Tonsor

    IPC分类号： F02C7/052

    CPC分类号： F02C7/052 ,  B01D46/0068 ,  F05D2260/607 ,  Y02T50/675

    摘要： A filter cleaning system is provided for a gas turbine engine including a compressor section and a combustor section. A mechanism is operatively connected to the gas turbine engine and is configured to be driven by the gas turbine engine in a first mode and configured to drive the gas turbine engine in a second mode. A first flow path is for delivering compressed air to the compressor section. At least one air filter is configured to filter air entering the first flow path. A second flow path is for delivering compressed air from the compressor section to the combustor section in the first mode. A third flow path is for delivering compressed air from the compressor section to the at least one air filter during the second mode.

    摘要翻译： 为包括压缩机部分和燃烧器部分的燃气涡轮发动机提供过滤器清洁系统。 机构可操作地连接到燃气涡轮发动机并且被构造成在第一模式中被燃气涡轮发动机驱动，并被构造成以第二模式驱动燃气涡轮发动机。 第一流路是用于将压缩空气输送到压缩机部分。 至少一个空气过滤器被配置为过滤进入第一流动路径的空气。 第二流路用于在第一模式中将压缩空气从压缩机部分输送到燃烧器部分。 第三流路是用于在第二模式期间将压缩空气从压缩机部分输送到至少一个空气过滤器。

    Multiple turbine system with a single recuperator
    8.
    发明申请
    Multiple turbine system with a single recuperator 失效
    具有单个换热器的多个涡轮机系统

    公开(公告)号：US20070137211A1

    公开(公告)日：2007-06-21

    申请号：US11305112

    申请日：2005-12-19

    申请人： James Callas ,  Kevin Martin ,  Cody Renshaw ,  Thomas Sopko ,  Andrew Tonsor

    发明人： James Callas ,  Kevin Martin ,  Cody Renshaw ,  Thomas Sopko ,  Andrew Tonsor

    IPC分类号： F02C7/10

    CPC分类号： F02C6/02 ,  F02C7/08 ,  F05D2220/76 ,  F05D2240/40

    摘要： A turbine system is provided including a plurality of gas turbine engines, each having a compressor section for producing compressed air, a combustor section, and a turbine section yielding hot exhaust gas. A single, common recuperator section is shared by and operatively associated with the plurality of gas turbine engines. A first flow path within the single, common recuperator section is configured to receive compressed air produced by the compressor section of each gas turbine engine. A second flow path, separated from the first flow path and within the single, common recuperator section is configured to receive hot exhaust gases yielded by the turbine section of each gas turbine engine.

    摘要翻译： 提供一种涡轮机系统，其包括多个燃气涡轮发动机，每个具有用于产生压缩空气的压缩机部分，燃烧器部分和产生热废气的涡轮部分。 一个单一的常见的换热器部分由多个燃气涡轮发动机共享并与其可操作地相关联。 单个公共换热器部分内的第一流动路径被配置为接收由每个燃气涡轮发动机的压缩机部分产生的压缩空气。 与第一流动路径分离并且在单个公共换热器部分内的第二流动路径被配置为接收由每个燃气涡轮发动机的涡轮部分产生的热废气。