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公开(公告)号：US09856768B2
公开(公告)日：2018-01-02
申请号：US14753064
申请日：2015-06-29
Applicant: General Electric Company
Inventor： Lewis Berkley Davis, Jr. , Gilbert Otto Kraemer , Parag Prakash Kulkarni , Hua Zhang
IPC: F01D15/10 , F01N3/04 , F01N3/10 , F01N3/20 , F02C3/04 , F02C7/141 , F02C7/16 , F01D25/30 , F02C3/30
CPC classification number: F01N3/04 , F01D15/10 , F01D25/305 , F01N3/103 , F01N3/2066 , F01N2590/10 , F01N2610/02 , F01N2610/08 , F02C3/04 , F02C3/30 , F02C7/141 , F02C7/16 , F05D2220/32 , F05D2220/76 , F05D2240/24 , F05D2240/35 , F05D2240/60 , F05D2260/212 , F05D2270/082 , Y02T10/24
Abstract: A turbomachine system according to an embodiment includes: a gas turbine system including a compressor component, a combustor component, and a turbine component; a mixing area for receiving an exhaust gas stream produced by the gas turbine system; a fluid injection system for injecting a fluid into the mixing area to reduce a temperature of the exhaust gas stream; and an exhaust processing system for processing the reduced temperature exhaust gas stream.
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公开(公告)号：US20170184310A1
公开(公告)日：2017-06-29
申请号：US15458545
申请日：2017-03-14
Applicant: General Electric Company
IPC: F23R3/34
Abstract: A system for injecting a liquid fuel into a combustion gas flow field includes an annular liner that defines a combustion gas flow path. The annular liner includes an inner wall, an outer wall and a fuel injector opening that extends through the inner wall and the outer wall. The system further includes a gas fuel injector that is coaxially aligned with the fuel injector opening. The gas fuel injector includes an upstream end and a downstream end. The downstream end terminates substantially adjacent to the inner wall. A dilution air passage is at least partially defined by the gas fuel injector. A liquid fuel injector extends partially through the dilution air passage. The liquid fuel injector includes an injection end that terminates upstream from the inner wall.
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公开(公告)号：US20160376954A1
公开(公告)日：2016-12-29
申请号：US14753064
申请日：2015-06-29
Applicant: General Electric Company
Inventor： Lewis Berkley Davis, JR. , Gilbert Otto Kraemer , Parag Prakash Kulkarni , Hua Zhang
CPC classification number: F01N3/04 , F01D15/10 , F01D25/305 , F01N3/103 , F01N3/2066 , F01N2590/10 , F01N2610/02 , F01N2610/08 , F02C3/04 , F02C3/30 , F02C7/141 , F02C7/16 , F05D2220/32 , F05D2220/76 , F05D2240/24 , F05D2240/35 , F05D2240/60 , F05D2260/212 , F05D2270/082 , Y02T10/24
Abstract: A turbomachine system according to an embodiment includes: a gas turbine system including a compressor component, a combustor component, and a turbine component; a mixing area for receiving an exhaust gas stream produced by the gas turbine system; a fluid injection system for injecting a fluid into the mixing area to reduce a temperature of the exhaust gas stream; and an exhaust processing system for processing the reduced temperature exhaust gas stream.
Abstract translation: 根据实施例的涡轮机系统包括：包括压缩机部件，燃烧器部件和涡轮机部件的燃气轮机系统; 用于接收由所述燃气轮机系统产生的废气流的混合区域; 用于将流体注入混合区域以降低排气流的温度的流体注入系统; 以及用于处理降温废气流的废气处理系统。
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公开(公告)号：US09381462B2
公开(公告)日：2016-07-05
申请号：US13932157
申请日：2013-07-01
Applicant: General Electric Company
Inventor： Robert Thomas Thatcher , Gilbert Otto Kraemer , Andrew Mitchell Rodwell , Brett Matthew Thompson
IPC: F01N3/04 , B01D53/14 , B01D53/86 , F01N3/20 , F01N5/02 , B01D53/48 , B01D53/54 , B01D53/72 , B01D53/75 , B01D53/78 , F01N13/00
CPC classification number: B01D53/14 , B01D53/48 , B01D53/54 , B01D53/72 , B01D53/75 , B01D53/78 , B01D53/8631 , B01D2257/7027 , B01D2257/708 , B01D2258/0283 , F01N3/04 , F01N3/2066 , F01N5/02 , F01N13/0097 , F01N2610/02 , Y02E20/326 , Y02T10/16 , Y02T10/24
Abstract: A system for reducing emissions includes a gas production source that produces nitrogen oxides, sulfur oxides, hydrogen sulfide, sulfuric acid, nitric acid, formaldehyde, benzene, metal oxides, or volatile organic compound emissions. An exhaust plenum is downstream from the gas production source, and structure for dispersing a solvent is in the exhaust plenum. A collection tank is in fluid communication with the exhaust plenum to receive the solvent from the exhaust plenum, and a heat source is in the exhaust plenum downstream from the structure for dispersing the solvent. A method for reducing emissions from a gas production source includes flowing exhaust gases through an exhaust plenum, dispersing a solvent through a nozzle in the exhaust plenum, collecting the dispersed solvent in a collection tank, and heating the exhaust gases flowing through the exhaust plenum downstream from the nozzle.
Abstract translation: 减排的系统包括产生氮氧化物，硫氧化物，硫化氢，硫酸，硝酸，甲醛，苯，金属氧化物或挥发性有机化合物排放物的气体生产源。 排气增压室位于气体生产源的下游，用于分散溶剂的结构在排气室中。 收集罐与排气室流体连通以从排气室接收溶剂，并且热源位于用于分散溶剂的结构下游的排气室中。 一种用于减少来自气体生产源的排放的方法包括使废气流过排气室，将溶剂分散在排气室中的喷嘴，将分散的溶剂收集在收集罐中，并加热流经排气室的废气下游 从喷嘴。
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公开(公告)号：US20150184859A1
公开(公告)日：2015-07-02
申请号：US14048252
申请日：2013-10-08
Applicant: General Electric Company
Inventor： Sarah Lori Crothers , Gilbert Otto Kraemer
CPC classification number: F23R3/20 , F02C7/22 , F02C7/228 , F02C7/24 , F23D14/02 , F23R3/18 , F23R3/283 , F23R3/286 , F23R3/34 , F23R3/42 , F23R3/46 , F23R2900/00014
Abstract: A system and method for reducing combustion dynamics includes first and second combustors, and each combustor includes a fuel nozzle and a combustion chamber downstream from the fuel nozzle. Each fuel nozzle includes an axially extending center body, a shroud that circumferentially surrounds at least a portion of the axially extending center body, a plurality of vanes that extend radially between the center body and the shroud, a first fuel port through at least one of the plurality of vanes at a first axial distance from the combustion chamber, a second fuel port through the center body at a second axial distance from the combustion chamber, and the plurality of vanes are at a third axial distance from the combustion chamber. The system further includes structure for producing a combustion instability frequency in the first combustor that is different from the combustion instability frequency in the second combustor.
Abstract translation: 用于减少燃烧动力学的系统和方法包括第一和第二燃烧器，并且每个燃烧器包括燃料喷嘴和燃料喷嘴下游的燃烧室。 每个燃料喷嘴包括轴向延伸的中心体，周向围绕轴向延伸的中心体的至少一部分的护罩，在中心体和护罩之间径向延伸的多个叶片，通过下列中的至少一个的第一燃料口： 距离燃烧室第一轴向距离的多个叶片，通过中心体离开燃烧室的第二轴向距离的第二燃料口和多个叶片处于离燃烧室第三轴向距离处。 该系统还包括用于在第一燃烧器中产生与第二燃烧器中的燃烧不稳定频率不同的燃烧不稳定频率的结构。
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Patent Agency Ranking
公开(公告)号：US20140260302A1
公开(公告)日：2014-09-18
申请号：US13804199
申请日：2013-03-14
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Arvind Venugopal Menon , Gilbert Otto Kraemer , Predrag Popovic , Abinash Baruah
Abstract: The present application and the resultant patent provide a diffusion combustor fuel nozzle for a gas turbine engine. The fuel nozzle may include one or more gas fuel passages for one or more flows of gas fuel, a swirler surrounding the one or more gas fuel passages and positioned about a downstream face of the fuel nozzle, a number of swirler gas fuel ports defined in the swirler, and a number of downstream face gas fuel ports defined in the downstream face of the fuel nozzle. The swirler may include a number of swirl vanes and a number of air chambers defined between adjacent swirl vanes. The present application and the resultant patent further provide a method of operating a diffusion combustor fuel nozzle of a gas turbine engine.
Abstract translation: 本申请和所得专利提供了一种用于燃气涡轮发动机的扩散燃烧器燃料喷嘴。 燃料喷嘴可以包括用于一个或多个气体燃料流的一个或多个气体燃料通道，围绕一个或多个气体燃料通道并围绕燃料喷嘴的下游侧定位的旋流器，多个旋流器气体燃料端口限定在 旋流器和限定在燃料喷嘴的下游面中的多个下游面气体燃料端口。 旋流器可以包括多个旋流叶片和限定在相邻旋流叶片之间的多个空气室。 本申请和所得到的专利还提供了一种操作燃气轮机的扩散燃烧器燃料喷嘴的方法。
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公开(公告)号：US20140150402A1
公开(公告)日：2014-06-05
申请号：US13690057
申请日：2012-11-30
Applicant: General Electric Company
Inventor： Ahmed Mostafa ElKady , Sherif Hatem Abdulla Mohamed , Narendra Digamber Joshi , Hasan Karim , Gilbert Otto Kraemer , Samuel David Draper , Ashwin Raman
CPC classification number: F02C3/34 , F02C3/20 , F02C7/00 , F23C9/00 , F23C9/006 , F23C2202/30 , F23J15/02 , F23J15/022 , F23J15/025 , F23R2900/00004
Abstract: In one aspect, a combustion system is configured to facilitate preventing the formation of vanadium pentoxide (V2O5) and decrease a concentration of at least one of vanadium trioxide (V2O3) and vanadium tetroxide (V2O4) particles in an exhaust. The combustion system includes a vanadium-containing fuel supply and a combustor. The combustor is configured to generate a combustor exhaust gas including vanadium trioxide (V2O3) and/or vanadium tetroxide (V2O4) particles and to combust a reduced-oxygen mixture including the vanadium-containing fuel, ambient air, and a portion of the combustor exhaust gas. The combustion system also includes a particle separator configured to remove substantially all of the V2O3 and/or V2O4 particles from the combustor exhaust gas. A method for combusting fuel and a power generation system are also provided.
Abstract translation: 在一个方面，燃烧系统被配置为有助于防止五氧化二钒（V 2 O 5）的形成并且减少排气中的三氧化二钒（V 2 O 3）和四氧化钒（V 2 O 4）颗粒中的至少一种的浓度。 燃烧系统包括含钒燃料供应和燃烧器。 燃烧器被配置为产生包括三氧化二钒（V 2 O 3）和/或四氧化钒（V 2 O 4）颗粒的燃烧器废气，并且燃烧包含含钒燃料，环境空气和燃烧器排气的一部分的还原氧混合物 加油站。 该燃烧系统还包括一个颗粒分离器，其构造成从燃烧器废气中基本上除去所有的V 2 O 3和/或V 2 O 4颗粒。 还提供了燃烧燃料和发电系统的方法。
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公开(公告)号：US20140086810A1
公开(公告)日：2014-03-27
申请号：US13627973
申请日：2012-09-26
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Richard Todd Everhart , Rebecca Evelyn Hefner , Cristina Colindres Kraemer , Gilbert Otto Kraemer , Surinder Singh Pabla , Stephen Gerard Pope
CPC classification number: F01N3/2803 , B01D53/864 , B01D53/8643 , B01D53/88 , B01D2257/502 , B01D2257/702 , B01J33/00 , B01J37/0215 , F01N2510/00 , F01N2510/0684 , F23C13/02 , F23C13/06 , Y10T29/49345 , Y10T29/49885
Abstract: A system includes a catalytic reactor configured to mount to a combustor. The catalytic reactor includes a catalyst configured to reduce emissions associated with combustion in the combustor. The catalytic reactor also includes a first sacrificial coating disposed over the catalyst prior to mounting of the catalytic reactor into the combustor, wherein the first sacrificial coating is removable while the catalytic reactor is mounted to the combustor without damaging the catalyst.
Abstract translation: 一种系统包括配置成安装到燃烧器的催化反应器。 催化反应器包括被配置为减少与燃烧器中的燃烧相关的排放的催化剂。 催化反应器还包括在将催化反应器安装到燃烧器中之前设置在催化剂上的第一牺牲涂层，其中当催化反应器安装到燃烧器而不损坏催化剂时，第一牺牲涂层是可去除的。
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公开(公告)号：US20190178496A1
公开(公告)日：2019-06-13
申请号：US15838193
申请日：2017-12-11
Applicant: General Electric Company
Inventor： Charlie Edmond Jones , James Harper , Matthew Bernard Wilson , Robert Wade Clifford , Yon Han Chong , Gilbert Otto Kraemer
Abstract: A thimble assembly, which directs fluid flow through a combustor liner, includes a thimble boss and a thimble. The thimble boss is mounted an outer surface of the liner and surrounds a liner opening, thus defining a thimble boss passage. The thimble is disposed through the passage and the liner opening. The thimble wall extends from an inlet portion to an outlet of the thimble. The inlet portion has a greater diameter than the outlet and defines an inlet plane and a parallel intermediate plane. A terminal plane, parallel to the intermediate plane, includes an array of points most distant from a corresponding array of points defining the intermediate plane. The thimble wall has a non-uniform length, such that the outlet of the thimble is oriented at an oblique angle relative to the terminal plane. The thimble wall may have an arcuate shape defined as one-fourth of an ellipse.
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公开(公告)号：US09951646B2
公开(公告)日：2018-04-24
申请号：US13932467
申请日：2013-07-01
Applicant: General Electric Company
Inventor： Doug Scott Byrd , Gilbert Otto Kraemer , Hua Zhang , Jianmin Zhang , Valery Ivanovich Ponyavin
CPC classification number: F01D25/002 , B08B7/00 , F05D2270/172
Abstract: An on-line wash system for a compressor including: a nozzle including a flow passage for wash liquid, wherein the flow passage is configured to be coupled to a source of a wash liquid and includes a discharge outlet arranged to project the wash liquid into a stream of working fluid for the turbomachine; an electrode proximate to the flow passage of the nozzle, wherein the electrode is configured to form an electrical field sufficient to charge the wash liquid flowing through the passage and the charge applied to the wash liquid is of a first polarity, and a surface of the compressor charged with the first polarity, wherein the surface is exposed to the stream of working fluid and downstream of the nozzle.
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