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公开(公告)号：US20100092896A1
公开(公告)日：2010-04-15
申请号：US12250875
申请日：2008-10-14
Applicant: Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Glenn David Nelson , Robert Joseph Rohrssen , John Drake Vanselow
Inventor： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Glenn David Nelson , Robert Joseph Rohrssen , John Drake Vanselow
CPC classification number: F23R3/04 , F23L7/005 , F23L2900/07002 , F23L2900/07003 , F23L2900/07009 , F23R3/283 , F23R3/44 , F23R3/60 , F23R2900/00017 , Y02E20/342
Abstract: Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. At least one shroud is secured to the baffle plate and includes at least one piston ring disposed at the shroud. The at least one piston ring is configured to meter a flow of diluent between the at least one shroud and the at least one fuel nozzle. Further disclosed is a method for providing diluent to a combustor including providing a piston ring gap defined by at least one piston ring disposed at a baffle plate and a fuel nozzle extending through a through hole in the baffle plate. The diluent is flowed through the piston ring gap toward at least one airflow hole in the fuel nozzle.
Abstract translation: 公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。 至少一个护罩固定在挡板上并且包括设置在护罩上的至少一个活塞环。 所述至少一个活塞环构造成测量所述至少一个护罩和所述至少一个燃料喷嘴之间的稀释剂流。 还公开了一种向燃烧器提供稀释剂的方法，包括提供由设置在挡板上的至少一个活塞环限定的活塞环间隙和延伸穿过挡板中的通孔的燃料喷嘴。 稀释剂通过活塞环间隙朝向燃料喷嘴中的至少一个气流孔流动。
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公开(公告)号：US20090284013A1
公开(公告)日：2009-11-19
申请号：US12153231
申请日：2008-05-15
Applicant: Ashok Kumar Anand , James Anthony West , Gilbert Otto Kraemer , Hasan Ul Karim , Sam David Draper , Jonathan Dwight Berry
Inventor： Ashok Kumar Anand , James Anthony West , Gilbert Otto Kraemer , Hasan Ul Karim , Sam David Draper , Jonathan Dwight Berry
CPC classification number: F02C3/34 , B01D53/8625 , B01D53/8643 , B01D2255/1021 , B01D2255/204 , B01D2255/206 , B01D2255/20715 , B01D2255/2092 , F02C6/18 , Y02E20/16 , Y02T10/22
Abstract: A power generation system capable of eliminating NO, components in the exhaust gas by using a 3-way catalyst, comprising a gas compressor to increase the pressure of ambient air fed to the system; a combustor capable of oxidizing a mixture of fuel and compressed air to generate an expanded, high temperature exhaust gas; a gas turbine engine that uses the force of the high temperature gas; an exhaust gas recycle (EGR) stream back to the combustor; a 3-way catalytic reactor downstream of the gas turbine engine outlet which treats the exhaust gas stream to remove substantially all of the NOx components; a heat recovery steam generator (HRSG); an EGR compressor; and an electrical generator.
Abstract translation: 一种能够通过使用三元催化剂消除废气中的NO的发电系统，其包括气体压缩机以增加供给到系统的环境空气的压力; 能够氧化燃料和压缩空气的混合物以产生膨胀的高温废气的燃烧器; 使用高温气体的力的燃气轮机; 废气再循环（EGR）流回燃烧器; 在燃气涡轮发动机出口下游的三元催化反应器，其处理排气流以去除基本上所有的NOx组分; 热回收蒸汽发生器（HRSG）; 一个EGR压缩机; 和发电机。
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13.发明授权Fuel nozzles with mixing tubes surrounding a liquid fuel cartridge for injecting fuel in a gas turbine combustor 有权燃料喷嘴，其具有围绕液体燃料盒的混合管，用于在燃气轮机燃烧器中喷射燃料公开(公告)号：US09366440B2
公开(公告)日：2016-06-14
申请号：US13343417
申请日：2012-01-04
Applicant: Jonathan Dwight Berry
Inventor： Jonathan Dwight Berry
IPC: F23R3/28
CPC classification number: F23R3/286 , F23D2900/00008 , Y02E20/16
Abstract: Fuel nozzles for gas turbines are provided that include liquid fuel cartridges. In one embodiment, a fuel nozzle includes a fuel plenum plate separating an air plenum from a fuel plenum. The fuel nozzle also includes a plurality of mixing tubes extending through the fuel plenum from the fuel plenum plate to a face plate. Each mixing tube includes an air inlet configured to receive air from the air plenum, a fuel inlet disposed in a tube wall within the fuel plenum to direct fuel from the fuel plenum into the mixing tube to produce a fuel-air mixture, and a fuel-air outlet configured to discharge the fuel-air mixture away from the face plate into a combustion region. The fuel nozzle further includes a liquid fuel cartridge extending through the air plenum and the fuel plenum to the face plate. The liquid fuel cartridge includes a liquid fuel passage.
Abstract translation: 提供了用于燃气轮机的燃料喷嘴，其包括液体燃料盒。 在一个实施例中，燃料喷嘴包括将空气增压室与燃料增压室分开的燃料增压板。 燃料喷嘴还包括多个混合管，其通过燃料增压室从燃料增压板延伸到面板。 每个混合管包括被配置为从空气压力室接收空气的空气入口，设置在燃料增压室内的管壁中的燃料入口以将来自燃料增压室的燃料引导到混合管中以产生燃料 - 空气混合物，以及燃料 空气出口构造成将燃料 - 空气混合物从面板排出到燃烧区域中。 燃料喷嘴还包括延伸穿过空气压力室和燃料增压室到液面板的液体燃料盒。 液体燃料盒包括液体燃料通道。
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公开(公告)号：US09121609B2
公开(公告)日：2015-09-01
申请号：US12250875
申请日：2008-10-14
Applicant: Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Glenn David Nelson , Robert Joseph Rohrssen , John Drake Vanselow
Inventor： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Glenn David Nelson , Robert Joseph Rohrssen , John Drake Vanselow
CPC classification number: F23R3/04 , F23L7/005 , F23L2900/07002 , F23L2900/07003 , F23L2900/07009 , F23R3/283 , F23R3/44 , F23R3/60 , F23R2900/00017 , Y02E20/342
Abstract: Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. At least one shroud is secured to the baffle plate and includes at least one piston ring disposed at the shroud. The at least one piston ring is configured to meter a flow of diluent between the at least one shroud and the at least one fuel nozzle. Further disclosed is a method for providing diluent to a combustor including providing a piston ring gap defined by at least one piston ring disposed at a baffle plate and a fuel nozzle extending through a through hole in the baffle plate. The diluent is flowed through the piston ring gap toward at least one airflow hole in the fuel nozzle.
Abstract translation: 公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。 至少一个护罩固定在挡板上并且包括设置在护罩上的至少一个活塞环。 所述至少一个活塞环构造成测量所述至少一个护罩和所述至少一个燃料喷嘴之间的稀释剂流。 还公开了一种向燃烧器提供稀释剂的方法，包括提供由设置在挡板上的至少一个活塞环限定的活塞环间隙和延伸穿过挡板中的通孔的燃料喷嘴。 稀释剂通过活塞环间隙朝向燃料喷嘴中的至少一个气流孔流动。
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公开(公告)号：US09052112B2
公开(公告)日：2015-06-09
申请号：US13405564
申请日：2012-02-27
Applicant: Jonathan Dwight Berry , Michael John Hughes
Inventor： Jonathan Dwight Berry , Michael John Hughes
CPC classification number: F23R3/10 , F23D2209/30 , F23R3/286
Abstract: A combustor includes an end cap. The end cap includes a first surface and a second surface downstream from the first surface, a shroud that circumferentially surrounds at least a portion of the first and second surfaces, a plate that extends radially within the shroud, a plurality of tubes that extend through the plate and the first and second surfaces, and a first purge port that extends through one or more of the plurality of tubes, wherein the purge port is axially aligned with the plate.
Abstract translation: 燃烧器包括端盖。 端盖包括第一表面和第二表面，在第一表面的下游，围绕第一和第二表面的至少一部分的护罩，在护罩内径向延伸的板，延伸穿过该护罩的多个管 板和第一和第二表面，以及延伸穿过多个管中的一个或多个的第一吹扫口，其中吹扫口与板轴向对准。
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Patent Agency Ranking
公开(公告)号：US08991187B2
公开(公告)日：2015-03-31
申请号：US12901648
申请日：2010-10-11
Applicant: Michael John Hughes , Jonathan Dwight Berry , Jason Thurman Stewart , Almaz Valeev , Chunyang Wu
Inventor： Michael John Hughes , Jonathan Dwight Berry , Jason Thurman Stewart , Almaz Valeev , Chunyang Wu
CPC classification number: F23R3/286 , F23C2900/07001 , F23C2900/9901 , F23R3/36
Abstract: The present application provides for a combustor for combusting a flow of fuel and a flow of air. The combustor may include a number of fuel nozzles, a lean pre-nozzle fuel injection system positioned upstream of the fuel nozzles, and a premixing annulus positioned between the fuel nozzles and the lean pre-nozzle fuel injection system to premix the flow of fuel and the flow of air.
Abstract translation: 本申请提供了一种用于燃烧燃料流和空气流的燃烧器。 燃烧器可以包括多个燃料喷嘴，位于燃料喷嘴上游的稀薄预喷嘴燃料喷射系统以及位于燃料喷嘴和稀薄预喷嘴燃料喷射系统之间的预混合环，以预混合燃料流和 空气流动。
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17.发明授权公开(公告)号：US08925324B2
公开(公告)日：2015-01-06
申请号：US12898267
申请日：2010-10-05
Applicant: Jonathan Dwight Berry , Chunyang Wu , Baifang Zuo
Inventor： Jonathan Dwight Berry , Chunyang Wu , Baifang Zuo
CPC classification number: F23R3/286 , F23D2900/00003 , F23R3/12
Abstract: A turbomachine includes a compressor section, a combustor operatively connected to the compressor section, an end cover mounted to the combustor, and an injection nozzle assembly operatively connected to the combustor. The injection nozzle assembly includes a plurality of mixing tube elements. Each of the plurality of mixing tube elements includes a conduit having a first fluid inlet, a second fluid inlet arranged downstream from the first fluid inlet, a discharge end arranged downstream from the first and second fluid inlets, and a vortex generator arranged between the first and second fluid inlets. The vortex generator is configured and disposed to create multiple vortices within the conduit to mix first and second fluids passing through each of the plurality of mixing tube elements.
Abstract translation: 涡轮机包括压缩机部分，可操作地连接到压缩机部分的燃烧器，安装到燃烧器的端盖以及可操作地连接到燃烧器的喷嘴组件。 注射喷嘴组件包括多个混合管元件。 多个混合管元件中的每一个包括具有第一流体入口，布置在第一流体入口下游的第二流体入口，布置在第一和第二流体入口下游的排放端，以及设置在第一流体入口之间的涡流发生器 和第二个流体入口。 涡流发生器被配置和设置成在管道内产生多个涡流以混合通过多个混合管元件中的每一个的第一和第二流体。
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公开(公告)号：US20130305725A1
公开(公告)日：2013-11-21
申请号：US13475882
申请日：2012-05-18
Applicant: Jonathan Dwight Berry
Inventor： Jonathan Dwight Berry
IPC: F23R3/28
CPC classification number: F23R3/14 , F23C2900/07001 , F23D2900/14004 , F23R3/283 , F23R3/286 , F23R2900/00012 , F23R2900/00017 , Y02T50/675
Abstract: Certain embodiments include a first individual sector having a first outer perimeter configured to fit together with outer perimeters of a plurality of individual sectors to form a combustor cap assembly of a turbine combustor, wherein the first individual sector comprises a first inner perimeter configured to fit about a nozzle outer perimeter of a first fuel nozzle, and the first individual sector is configured to fixedly attach to the first fuel nozzle.
Abstract translation: 某些实施例包括具有第一外周边的第一单独扇区，该第一外周边配置成与多个独立扇区的外周配合在一起，以形成涡轮机燃烧器的燃烧器盖组件，其中，第一单独扇区包括配置成围绕 第一燃料喷嘴的喷嘴外周边，并且第一单独扇区构造成固定地附接到第一燃料喷嘴。
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公开(公告)号：US08528337B2
公开(公告)日：2013-09-10
申请号：US12017364
申请日：2008-01-22
Applicant: Jonathan Dwight Berry , Gilbert Otto Kramer
Inventor： Jonathan Dwight Berry , Gilbert Otto Kramer
IPC: F23R3/30
CPC classification number: F23R3/286 , F23C2900/07001 , F23D14/62
Abstract: An injection system for fuel and air that includes a number of lobes positioned adjacent to each other. Each of the lobes has a trailing end. A number of jets may be positioned adjacent to the trailing end.
Abstract translation: 一种用于燃料和空气的喷射系统，其包括彼此相邻定位的多个叶片。 每个裂片具有尾端。 可以将多个喷嘴定位成与尾端相邻。
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公开(公告)号：US08381532B2
公开(公告)日：2013-02-26
申请号：US12694544
申请日：2010-01-27
Applicant: Jonathan Dwight Berry , Michael John Hughes
Inventor： Jonathan Dwight Berry , Michael John Hughes
Abstract: The present subject matter provides a system for modifying static pressure recoveries and emissions formation within a gas turbine. The system includes a bled diffuser positioned downstream from a compressor section of the gas turbine and a bleed duct extending from the bled diffuser. The bleed duct may be configured to direct bleed air from the pressurized airflow exiting the compressor section to a secondary combustion system located downstream from the main combustion system in a combustor. The bleed air flowing into the secondary combustion system may be mixed with fuel to form an air/fuel mixture.
Abstract translation: 本主题提供了一种用于改变燃气轮机内静压回收率和排放物形成的系统。 该系统包括位于燃气涡轮机的压缩机部分下游的排放扩散器和从流血扩散器延伸的排放管道。 排放管道可以被配置为将排出压缩机部分的加压气流的排出空气引导到位于燃烧器中的主燃烧系统下游的二次燃烧系统。 流入二次燃烧系统的排出空气可与燃料混合以形成空气/燃料混合物。
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