Turbine inlet air heat pump-type system
    1.
    发明授权
    Turbine inlet air heat pump-type system 有权
    涡轮进风机热泵式系统

    公开(公告)号:US09470149B2

    公开(公告)日:2016-10-18

    申请号:US12332383

    申请日:2008-12-11

    摘要: A heating and cooling system for inlet air of a turbine compressor. The heating and cooling system may include a thermal energy storage tank charging loop, a cooling loop in communication with the thermal energy storage charging loop, and a heating loop in communication with the cooling loop and the inlet air of the turbine compressor.

    摘要翻译: 一种用于涡轮压缩机入口空气的加热和冷却系统。 加热和冷却系统可以包括热能储存箱充电回路,与热能存储充电回路连通的冷却回路,以及与冷却回路和涡轮压缩机的入口空气连通的加热回路。

    Inlet air heating and cooling system
    2.
    发明授权
    Inlet air heating and cooling system 有权
    进气加热和冷却系统

    公开(公告)号:US08468830B2

    公开(公告)日:2013-06-25

    申请号:US12332380

    申请日:2008-12-11

    IPC分类号: F02C1/00 F02C3/30 F25D9/00

    摘要: A heating and cooling system for inlet air of a turbine compressor. The heating and cooling system may include a fluid coil positioned about the turbine compressor and a thermal energy storage tank. The fluid coil and the thermal energy storage tank are in fluid communication such that fluid is both provided to the fluid coil from the thermal energy storage tank for exchanging heat with the inlet air and returned to the thermal energy storage tank without further heat exchange.

    摘要翻译: 一种用于涡轮压缩机入口空气的加热和冷却系统。 加热和冷却系统可以包括围绕涡轮压缩机和热能储存器定位的流体盘管。 流体盘管和热能储存罐是流体连通的,使得流体都从热能储存罐提供给流体盘管,用于与入口空气进行热交换并返回到热能储存罐而不需要进一步的热交换。

    System and method for changing the efficiency of a combustion turbine
    3.
    发明授权
    System and method for changing the efficiency of a combustion turbine 有权
    改变燃气轮机效率的系统和方法

    公开(公告)号:US08266910B2

    公开(公告)日:2012-09-18

    申请号:US12257731

    申请日:2008-10-24

    IPC分类号: F02C1/00

    摘要: An application and process that incorporates an external heat source to increase the temperature of the airstream entering a compressor section of a combustion turbine. The application and process may perform an anti-icing operation that may not require an Inlet Bleed Heat system (IBH) to operate. Additionally, the application and process may perform an anti-icing operation that may allow for the IGV angle to remain nearly constant. The application and process may increase the output and efficiency of a combustion turbine operating at partload by delaying IBH operation and delaying the closing IGVs.

    摘要翻译: 包括外部热源以增加进入燃气轮机的压缩机部分的气流的温度的应用和过程。 应用程序和过程可以执行防冰操作,这可能不需要入口泄放热系统(IBH)的操作。 另外,应用和过程可以执行可以使IGV角度几乎保持恒定的防冰操作。 应用和过程可以通过延迟IBH操作和延迟闭合IGV来增加在部分负载下工作的燃气轮机的输出和效率。

    Gas Turbine Base Load Control by Chilling Modulation
    4.
    发明申请
    Gas Turbine Base Load Control by Chilling Modulation 审中-公开
    燃气轮机基础负荷控制通过冷却调制

    公开(公告)号:US20100146978A1

    公开(公告)日:2010-06-17

    申请号:US12332378

    申请日:2008-12-11

    IPC分类号: F02C1/00

    CPC分类号: F02C7/057 F02C7/143 F02C9/16

    摘要: A control system for a base load output of a gas turbine engine. The control system may include an inlet chilling coil system for providing air to the gas turbine engine at a desired temperature, a temperature control valve in communication with the inlet chilling coil system, a temperature sensor positioned about the gas turbine engine, and a temperature controller in communication with the temperature control valve and the temperature sensor. The temperature controller modulates the temperature control valve until the air provided to the gas turbine engine by the inlet chilling coil system reaches the desired temperature as sensed by the temperature sensor.

    摘要翻译: 一种用于燃气涡轮发动机的基本负载输出的控制系统。 控制系统可以包括用于在期望温度下向燃气涡轮发动机提供空气的入口冷却盘管系统,与入口冷却盘管系统连通的温度控制阀,围绕燃气涡轮发动机定位的温度传感器和温度控制器 与温度控制阀和温度传感器通信。 温度控制器调节温度控制阀,直到由入口冷却线圈系统提供给燃气涡轮发动机的空气达到温度传感器感测到的所需温度。

    TURBINE INLET AIR TREATMENT APPARATUS
    5.
    发明申请
    TURBINE INLET AIR TREATMENT APPARATUS 审中-公开
    涡轮入口空气处理设备

    公开(公告)号:US20080098891A1

    公开(公告)日:2008-05-01

    申请号:US11552535

    申请日:2006-10-25

    IPC分类号: B01D47/00

    摘要: An inlet air treatment system. The inlet air treatment system includes a housing with more than two symmetric sides. Each of the sides includes a number of air filters and a number of spray arrays. A central air deflector is positioned within the housing.

    摘要翻译: 进气处理系统。 入口空气处理系统包括具有多于两个对称侧的壳体。 每个侧面包括多个空气过滤器和多个喷射阵列。 中央空气导流板位于壳体内。

    Low grade heat recovery system for turbine air inlet
    6.
    发明授权
    Low grade heat recovery system for turbine air inlet 有权
    用于涡轮进气口的低档热回收系统

    公开(公告)号:US08356466B2

    公开(公告)日:2013-01-22

    申请号:US12332385

    申请日:2008-12-11

    IPC分类号: F02C6/00 F02C3/30

    摘要: A heating and cooling system for inlet air of a gas turbine engine in a combined cycle power plant having a steam turbine. The heating and cooling system may include a fluid coil positioned about the gas turbine engine, a heat exchanger in communication with the fluid coil, and a condenser in communication with the steam turbine and the heat exchanger such that waste heat from the steam turbine is forwarded to the fluid coil.

    摘要翻译: 一种具有蒸汽涡轮机的联合循环发电厂中的燃气涡轮发动机的入口空气的加热和冷却系统。 加热和冷却系统可以包括围绕燃气涡轮发动机定位的流体线圈,与流体线圈连通的热交换器以及与蒸汽轮机和热交换器连通的冷凝器,使得来自蒸汽涡轮机的废热被转发 到流体盘管。

    Turbine Inlet Air Heat Pump-Type System
    7.
    发明申请
    Turbine Inlet Air Heat Pump-Type System 有权
    涡轮进气空气热泵型系统

    公开(公告)号:US20100146981A1

    公开(公告)日:2010-06-17

    申请号:US12332383

    申请日:2008-12-11

    IPC分类号: F02C7/08

    摘要: A heating and cooling system for inlet air of a turbine compressor. The heating and cooling system may include a thermal energy storage tank charging loop, a cooling loop in communication with the thermal energy storage charging loop, and a heating loop in communication with the cooling loop and the inlet air of the turbine compressor.

    摘要翻译: 一种用于涡轮压缩机入口空气的加热和冷却系统。 加热和冷却系统可以包括热能储存箱充电回路,与热能存储充电回路连通的冷却回路,以及与冷却回路和涡轮压缩机的入口空气连通的加热回路。

    Inlet Air Heating and Cooling System
    8.
    发明申请
    Inlet Air Heating and Cooling System 有权
    进气加热和冷却系统

    公开(公告)号:US20100146976A1

    公开(公告)日:2010-06-17

    申请号:US12332380

    申请日:2008-12-11

    IPC分类号: F02C7/141 F25B29/00 F02C1/00

    摘要: A heating and cooling system for inlet air of a turbine compressor. The heating and cooling system may include a fluid coil positioned about the turbine compressor and a thermal energy storage tank. The fluid coil and the thermal energy storage tank are in fluid communication such that fluid is both provided to the fluid coil from the thermal energy storage tank for exchanging heat with the inlet air and returned to the thermal energy storage tank without further heat exchange.

    摘要翻译: 一种用于涡轮压缩机入口空气的加热和冷却系统。 加热和冷却系统可以包括围绕涡轮压缩机和热能储存器定位的流体盘管。 流体盘管和热能储存罐是流体连通的,使得流体都从热能储存罐提供给流体盘管,用于与入口空气进行热交换并返回到热能储存罐而不需要进一步的热交换。

    Low Grade Heat Recovery System for Turbine Air Inlet
    9.
    发明申请
    Low Grade Heat Recovery System for Turbine Air Inlet 有权
    用于涡轮空气入口的低等级热回收系统

    公开(公告)号:US20100146930A1

    公开(公告)日:2010-06-17

    申请号:US12332385

    申请日:2008-12-11

    IPC分类号: F02C7/10 F01K23/04

    摘要: A heating and cooling system for inlet air of a gas turbine engine in a combined cycle power plant having a steam turbine. The heating and cooling system may include a fluid coil positioned about the gas turbine engine, a heat exchanger in communication with the fluid coil, and a condenser in communication with the steam turbine and the heat exchanger such that waste heat from the steam turbine is forwarded to the fluid coil.

    摘要翻译: 一种具有蒸汽涡轮机的联合循环发电厂中的燃气涡轮发动机的入口空气的加热和冷却系统。 加热和冷却系统可以包括围绕燃气涡轮发动机定位的流体线圈,与流体线圈连通的热交换器以及与蒸汽轮机和热交换器连通的冷凝器,使得来自蒸汽涡轮机的废热被转发 到流体盘管。

    SYSTEM AND METHOD FOR CHANGING THE EFFICIENCY OF A COMBUSTION TURBINE
    10.
    发明申请
    SYSTEM AND METHOD FOR CHANGING THE EFFICIENCY OF A COMBUSTION TURBINE 有权
    改变燃油效率的系统和方法

    公开(公告)号:US20100101209A1

    公开(公告)日:2010-04-29

    申请号:US12257731

    申请日:2008-10-24

    IPC分类号: F02K3/08

    摘要: An embodiment of the present invention takes the form of an application and process that incorporates an external heat source to increase the temperature of the airstream entering a compressor section of a combustion turbine. An embodiment of the present invention may perform an anti-icing operation that may not require an Inlet Bleed Heat system (IBH) to operate. An embodiment of the present invention may perform an anti-icing operation that may allow for the IGV angle to remain nearly constant. An embodiment of the present invention may increase the output and efficiency of a combustion turbine operating at partload by delaying IBH operation and delaying the closing IGVs.

    摘要翻译: 本发明的实施例采用包含外部热源以增加进入燃气轮机的压缩机部分的气流的温度的应用和过程的形式。 本发明的一个实施例可以执行防冰操作,该操作可能不需要入口放热加热系统(IBH)的操作。 本发明的一个实施例可以执行防冰操作,其可以允许IGV角保持几乎恒定。 本发明的一个实施例可以通过延迟IBH操作并延迟关闭IGV来增加在部分负载下工作的燃气轮机的输出和效率。