Wet dry integrated circulation cooling system

    公开(公告)号:US12247520B2

    公开(公告)日:2025-03-11

    申请号:US16902794

    申请日:2020-06-16

    Abstract: An integrated circulating water cooling system includes at least one load; an air cooling sub-system; a wet surface cooling sub-system; at least one temperature sensor; a control; and a coolant circulation sub-system for fluidly circulating coolant from the at least one load to the air cooling sub-system to the wet surface cooling sub-system and back to the at least one load. The control selectively operates the wet surface cooling sub-system and the air cooling sub-system based on at least one of temperature sensed in the water circulation sub-system; or sensed ambient temperature.

    SYSTEM FOR TURBINE COMBUSTOR FUEL MIXING
    3.
    发明申请

    公开(公告)号:US20160084160A1

    公开(公告)日:2016-03-24

    申请号:US14961131

    申请日:2015-12-07

    CPC classification number: F02C3/30 F23K5/005 F23K5/12 F23L7/002 F23R3/36

    Abstract: A system includes a plurality of interconnected mixing assemblies configured to mix a first fuel and water to generate a first mixture, and mix a second fuel and the water to generate a second mixture. The first and second fuel mixtures are configured to combust in a plurality of combustors of a gas turbine. The interconnected mixing assemblies include first and second fuel passages, a water passage, first and second mixers, first and second fuel valves, and first and second water valves disposed in an integrated housing. The first fuel valve has a first fuel flow coefficient between approximately 1.0 to 1.5, the second fuel valve has a second fuel flow coefficient between approximately 3.0 to 5.0, the first water valve has a first water flow coefficient between approximately 0.4 to 0.55, and the second water valve has a second water flow coefficient between approximately 3.5 to 5.0.

    System for turbine combustor fuel mixing

    公开(公告)号:US10227921B2

    公开(公告)日:2019-03-12

    申请号:US14961131

    申请日:2015-12-07

    Abstract: A system includes a plurality of interconnected mixing assemblies configured to mix a first fuel and water to generate a first mixture, and mix a second fuel and the water to generate a second mixture. The first and second fuel mixtures are configured to combust in a plurality of combustors of a gas turbine. The interconnected mixing assemblies include first and second fuel passages, a water passage, first and second mixers, first and second fuel valves, and first and second water valves disposed in an integrated housing. The first fuel valve has a first fuel flow coefficient between approximately 1.0 to 1.5, the second fuel valve has a second fuel flow coefficient between approximately 3.0 to 5.0, the first water valve has a first water flow coefficient between approximately 0.4 to 0.55, and the second water valve has a second water flow coefficient between approximately 3.5 to 5.0.

    WET DRY INTEGRATED CIRCULATION COOLING SYSTEM

    公开(公告)号:US20210388765A1

    公开(公告)日:2021-12-16

    申请号:US16902794

    申请日:2020-06-16

    Abstract: An integrated circulating water cooling system includes at least one load; an air cooling sub-system; a wet surface cooling sub-system; at least one temperature sensor; a control; and a coolant circulation sub-system for fluidly circulating coolant from the at least one load to the air cooling sub-system to the wet surface cooling sub-system and back to the at least one load. The control selectively operates the wet surface cooling sub-system and the air cooling sub-system based on at least one of temperature sensed in the water circulation sub-system; or sensed ambient temperature.

    APPARATUS AND METHOD FOR PURGING A GAS TURBOMACHINE NOZZLE
    7.
    发明申请
    APPARATUS AND METHOD FOR PURGING A GAS TURBOMACHINE NOZZLE 审中-公开
    燃气涡轮喷嘴的装置和方法

    公开(公告)号:US20160178203A1

    公开(公告)日:2016-06-23

    申请号:US14573696

    申请日:2014-12-17

    CPC classification number: F23R3/28 F01D25/002 F02C3/30 F05D2240/35

    Abstract: A gas turbomachine includes a compressor portion, a turbine portion operatively connected to the compressor portion, and a combustor assembly fluidically connected to the turbine portion. The combustor assembly includes at least one nozzle including at least one fuel gas injector portion and at least one water injector portion. A fuel system is fluidically connected to the at least one nozzle. The fuel system includes at least one fuel gas manifold, a water injector purge manifold and a water injector manifold. The at least one fuel gas manifold is selectively fluidically connectable to the water injector portion of the nozzle through the water injector purge manifold.

    Abstract translation: 气体涡轮机包括压缩机部分,可操作地连接到压缩机部分的涡轮机部分和与涡轮部分流体连接的燃烧器组件。 燃烧器组件包括至少一个喷嘴,其包括至少一个燃料气体喷射器部分和至少一个喷水器部分。 燃料系统与至少一个喷嘴流体连接。 燃料系统包括至少一个燃料气体歧管,喷水器清洗歧管和注水器歧管。 所述至少一个燃料气体歧管通过所述喷水器清洗歧管选择性地流体连接到所述喷嘴的所述喷水器部分。

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