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21. 发明授权

US08925324B2 Turbomachine including a mixing tube element having a vortex generator 有权
标题翻译：涡轮机包括具有涡流发生器的混合管元件
公开(公告)号：US08925324B2
公开(公告)日：2015-01-06
申请号：US12898267
申请日：2010-10-05
申请人： Jonathan Dwight Berry , Chunyang Wu , Baifang Zuo
发明人： Jonathan Dwight Berry , Chunyang Wu , Baifang Zuo
IPC分类号： F02C1/00 , F02G3/00 , F23R3/28
CPC分类号： F23R3/286 , F23D2900/00003 , F23R3/12
摘要： 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.
摘要翻译：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。

22. 发明申请

US20130305725A1 FUEL NOZZLE CAP 审中-公开
标题翻译：燃油喷嘴盖
公开(公告)号：US20130305725A1
公开(公告)日：2013-11-21
申请号：US13475882
申请日：2012-05-18
申请人： Jonathan Dwight Berry
发明人： Jonathan Dwight Berry
IPC分类号： F23R3/28
CPC分类号： F23R3/14 , F23C2900/07001 , F23D2900/14004 , F23R3/283 , F23R3/286 , F23R2900/00012 , F23R2900/00017 , Y02T50/675
摘要： 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.
摘要翻译：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。

23. 发明授权

US08528337B2 Lobe nozzles for fuel and air injection 有权
标题翻译：喷嘴用于燃料和空气注入
公开(公告)号：US08528337B2
公开(公告)日：2013-09-10
申请号：US12017364
申请日：2008-01-22
申请人： Jonathan Dwight Berry , Gilbert Otto Kramer
发明人： Jonathan Dwight Berry , Gilbert Otto Kramer
IPC分类号： F23R3/30
CPC分类号： F23R3/286 , F23C2900/07001 , F23D14/62
摘要： 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.
摘要翻译：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。

24. 发明授权

US08381532B2 Bled diffuser fed secondary combustion system for gas turbines 有权
标题翻译：燃气轮机的Bled扩散器二次燃烧系统
公开(公告)号：US08381532B2
公开(公告)日：2013-02-26
申请号：US12694544
申请日：2010-01-27
申请人： Jonathan Dwight Berry , Michael John Hughes
发明人： Jonathan Dwight Berry , Michael John Hughes
IPC分类号： F02C9/00 , F02C1/00
CPC分类号： F02C7/222 , F01D9/06 , F23R3/346
摘要： 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.
摘要翻译：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。

25. 发明授权

US08381526B2 Systems and methods of providing high pressure air to a head end of a combustor 有权
标题翻译：向燃烧器的头端提供高压空气的系统和方法
公开(公告)号：US08381526B2
公开(公告)日：2013-02-26
申请号：US12705737
申请日：2010-02-15
申请人： Jonathan Dwight Berry , Constantin Dinu , Carl Robert Barker , Krishna Kumar Venkataraman
发明人： Jonathan Dwight Berry , Constantin Dinu , Carl Robert Barker , Krishna Kumar Venkataraman
IPC分类号： F02C3/14
CPC分类号： F23R3/02
摘要： A combustor includes a first flow path and a second flow path. The first flow path places a diffuser in indirect fluid communication with a combustor cap assembly by way of an intervening lower combustor annular passageway. The second flow path places the diffuser in direct fluid communication with the combustor cap assembly.
摘要翻译：燃烧器包括第一流路和第二流路。第一流路通过中间的下部燃烧器环形通道将扩散器与燃烧器盖组件间接流体连通。第二流路将扩散器与燃烧器盖组件直接流体连通。

26. 发明申请

US20120305677A1 SYSTEM FOR CONDITIONING FLOW THROUGH A NOZZLE 审中-公开
标题翻译：通过喷嘴调节流量的系统
公开(公告)号：US20120305677A1
公开(公告)日：2012-12-06
申请号：US13153506
申请日：2011-06-06
申请人： Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Jonathan Dwight Berry
发明人： Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Jonathan Dwight Berry
IPC分类号： F23D11/38
CPC分类号： F23D14/70 , F23R3/16
摘要： A system for conditioning flow through a plurality of nozzles arranged in a combustor includes a shield circumferentially surrounding at least a portion of the plurality of nozzles and a plurality of baffles disposed circumferentially around the shield. Each baffle is circumferentially disposed between adjacent nozzles.
摘要翻译：用于调节流过布置在燃烧器中的多个喷嘴的流动系统包括周向围绕多个喷嘴的至少一部分的屏蔽件和围绕屏蔽件周向设置的多个挡板。每个挡板周向地设置在相邻喷嘴之间。

27. 发明授权

US08252251B2 Fluid cooled reformer and method for cooling a reformer 有权
标题翻译：流体冷却重整器和冷却重整器的方法
公开(公告)号：US08252251B2
公开(公告)日：2012-08-28
申请号：US12749985
申请日：2010-03-30
申请人： Jonathan Dwight Berry , Hasan Karim , Abdul Rafey Khan
发明人： Jonathan Dwight Berry , Hasan Karim , Abdul Rafey Khan
IPC分类号： B01J8/00 , H01M8/06
CPC分类号： C01B3/386 , B01J8/0278 , B01J2208/00176 , B01J2208/00221 , B01J2208/00371 , B01J2208/0053 , B01J2208/00849 , C01B2203/0261 , C01B2203/0877 , C01B2203/0883 , C01B2203/84 , C10J3/466 , C10J2200/09 , C10J2300/0959 , C10J2300/0989 , C10J2300/1861 , C10J2300/1884 , F23C2900/03002
摘要： The present subject matter discloses a fluid cooled reformer for gas turbine systems and a method for cooling both a fuel reformer and a heated reformate stream produced by such fuel reformer. The fluid cooled reformer may include a pressure vessel and a reactor assembly disposed within the pressure vessel. The reactor assembly may include a reactor and may be configured to receive and reform an oxygen/fuel mixture to produce a heated reformate stream. Additionally, the fluid cooled reformer may include an inlet configured to direct a fluid stream into the pressure vessel. At least a portion of the fluid stream may be used to cool the reactor assembly. A reformate cooling section may be disposed downstream of the reactor of the reactor assembly and may be configured to cool the heated reformate stream.
摘要翻译：本发明公开了一种用于燃气轮机系统的流体冷却重整器和用于冷却由这种燃料重整器产生的燃料重整器和加热的重整产品流的方法。流体冷却的重整器可以包括压力容器和设置在压力容器内的反应器组件。反应器组件可以包括反应器，并且可以被配置为接收和改造氧/燃料混合物以产生加热的重整产物流。此外，流体冷却的重整器可以包括构造成将流体流引导到压力容器中的入口。流体流的至少一部分可用于冷却反应器组件。重整物冷却段可以设置在反应器组件的反应器的下游，并且可以被配置为冷却加热的重整产物流。

28. 发明申请

US20110197586A1 Systems and Methods of Providing High Pressure Air to a Head End of a Combustor 有权
标题翻译：向燃烧器头端提供高压空气的系统和方法
公开(公告)号：US20110197586A1
公开(公告)日：2011-08-18
申请号：US12705737
申请日：2010-02-15
申请人： Jonathan Dwight Berry , Constantin Dinu , Carl Robert Barker , Krishna Kumar Venkataraman
发明人： Jonathan Dwight Berry , Constantin Dinu , Carl Robert Barker , Krishna Kumar Venkataraman
IPC分类号： F02C3/14
CPC分类号： F23R3/02
摘要： A combustor includes a first flow path and a second flow path. The first flow path places a diffuser in indirect fluid communication with a combustor cap assembly by way of an intervening lower combustor annular passageway. The second flow path places the diffuser in direct fluid communication with the combustor cap assembly.
摘要翻译：燃烧器包括第一流路和第二流路。第一流路通过中间的下部燃烧器环形通道将扩散器与燃烧器盖组件间接流体连通。第二流路将扩散器与燃烧器盖组件直接流体连通。

29. 发明申请

US20110162375A1 Secondary Combustion Fuel Supply Systems 审中-公开
标题翻译：二次燃油供应系统
公开(公告)号：US20110162375A1
公开(公告)日：2011-07-07
申请号：US12652181
申请日：2010-01-05
申请人： Jonathan Dwight Berry
发明人： Jonathan Dwight Berry
IPC分类号： F02C7/22
CPC分类号： F02C7/222 , F23R3/60
摘要： Systems are provided for supplying fuel to secondary combustion zones within gas turbine engines. In one embodiment, a system includes a transition piece support structure extending from a compressor casing and configured to support a combustor transition piece of a gas turbine engine. A fuel passageway is integrated with the support structure.
摘要翻译：提供用于向燃气涡轮发动机内的二级燃烧区供应燃料的系统。在一个实施例中，系统包括从压缩机壳体延伸并且构造成支撑燃气涡轮发动机的燃烧器过渡件的过渡件支撑结构。燃料通道与支撑结构集成。

30. 发明授权

US07921653B2 Internal manifold air extraction system for IGCC combustor and method 有权
标题翻译： IGCC燃烧器内部歧管空气抽取系统及方法
公开(公告)号：US07921653B2
公开(公告)日：2011-04-12
申请号：US11984925
申请日：2007-11-26
申请人： Abhijit Som , Jonathan Dwight Berry
发明人： Abhijit Som , Jonathan Dwight Berry
IPC分类号： F02C6/06 , F23R3/26 , F23R3/46
CPC分类号： F01D9/023
摘要： A combustor for a turbine including a combustor liner; a first flow sleeve surrounding the combustor liner with a first flow annulus therebetween, the first flow sleeve having at least one cooling aperture formed about a circumference thereof for directing compressor discharge air as cooling air into the first flow annulus; a casing surrounding first flow sleeve with a second flow annulus therebetween, the first flow sleeve having at least one air extraction opening formed about a circumference thereof for directing compressor discharge air from the first flow annulus as extraction air into the second flow annulus; and an extraction port operatively coupled to the casing for extracting the extraction air from the second flow annulus.
摘要翻译：一种用于涡轮机的燃烧器，包括燃烧器衬套; 围绕所述燃烧器衬套的第一流动套筒，其间具有第一流动环空，所述第一流动套筒具有围绕其圆周形成的至少一个冷却孔，用于将压缩机排出的空气作为冷却空气引导到所述第一流动环空中; 围绕其间具有第二流动环的第一流动套管的壳体，所述第一流动套筒具有围绕其周边形成的至少一个空气抽取开口，用于将来自所述第一流动环空间的压缩机排出的空气作为抽出空气引导到所述第二流动环空中; 以及可操作地联接到所述壳体以从所述第二流动环空提取抽取空气的抽出端口。

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