公开(公告)号：US20180328588A1

公开(公告)日：2018-11-15

申请号：US15593543

申请日：2017-05-12

Applicant: General Electric Company

Inventor： Donald Timothy Lemon ,  Gilbert Otto Kraemer ,  Wei Chen ,  Marcus Byron Huffman ,  Ronnie Ray Pentecost

IPC: F23R3/36 ,  F23R3/28

CPC classification number: F23R3/36 ,  F23R3/283 ,  F23R3/286

Abstract: A fuel injector is provided for the radial introduction of a liquid fuel/air mixture to a combustor. The fuel injector includes a body having a frame that defines an inlet portion and an outlet member that defines an outlet portion. A fuel plenum is defined within the outlet member, and a fuel injection port, which communicates with the fuel plenum, is defined through the outlet member. A fuel supply conduit, fixed to the body, communicates between a source of liquid fuel and the fuel injection port, via the fuel plenum. Alternately, the fuel injector may include a swirl-inducing device mounted to the outlet member in communication with the fuel injection port, and a fuel supply conduit fixed to the swirl-inducing device. In this embodiment, the fuel supply conduit communicates between the fuel injection port and a source of a liquid fuel and water mixture, via the swirl-inducing device.

公开(公告)号：US09291082B2

公开(公告)日：2016-03-22

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

IPC: F01N3/28 ,  F23C13/02 ,  B01J33/00 ,  B01D53/88 ,  B01D53/86 ,  B01J37/02 ,  F23C13/06

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 and a second sacrificial coating disposed over the catalyst prior to mounting of the catalytic reactor into the combustor, wherein the first and second sacrificial coatings are 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和第二牺牲涂层，其中第一和第二牺牲涂层是可去除的，而催化反应器安装到燃烧器而不损坏催化剂。

公开(公告)号：US09255711B2

公开(公告)日：2016-02-09

申请号：US14048252

申请日：2013-10-08

Applicant: General Electric Company

Inventor： Sarah Lori Crothers ,  Gilbert Otto Kraemer

IPC: F23R3/20 ,  F23R3/46 ,  F23R3/28 ,  F23D14/02 ,  F02C7/22

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: First and second combustors are provided, 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 center body, and vanes that extend radially between the center body and the shroud. A first fuel port through at least one of the vanes is located at a first axial distance from the combustion chamber, a second fuel port through the center body is located at a second axial distance from the combustion chamber, and the vanes are located at a third axial distance from the combustion chamber. The system varies one or more of the first, second, and third axial distances from combustor-to-combustor to produce a combustion instability frequency in the first combustor that is different from the combustion instability frequency in the second combustor.

Abstract translation: 提供第一和第二燃烧器，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，周向围绕中心体的至少一部分的护罩和在中心体和护罩之间径向延伸的叶片。 通过至少一个叶片的第一燃料端口位于离燃烧室的第一轴向距离处，通过中心体的第二燃料端口位于离燃烧室的第二轴向距离处，并且叶片位于 距燃烧室的第三轴向距离。 系统改变从燃烧室到燃烧器的第一，第二和第三轴向距离中的一个或多个，以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。

公开(公告)号：US09151502B2

公开(公告)日：2015-10-06

申请号：US14048272

申请日：2013-10-08

Applicant: General Electric Company

Inventor： Sarah Lori Crothers ,  Gilbert Otto Kraemer

IPC: F23R3/20 ,  F23R3/46 ,  F02C7/24 ,  F02C7/22 ,  F23D14/02 ,  F23R3/28

CPC classification number: F23R3/20 ,  F02C7/22 ,  F02C7/24 ,  F23D14/02 ,  F23R3/286 ,  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, the plurality of vanes being located at a second axial distance from the combustion chamber. A second fuel port is provided through the center body 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，第一燃料口通过至少一个 所述多个叶片处于距燃烧室第一轴向距离处，所述多个叶片位于距燃烧室第二轴向距离处。 第二燃料口通过中心体设置在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。

公开(公告)号：US20150047360A1

公开(公告)日：2015-02-19

申请号：US13965657

申请日：2013-08-13

Applicant: General Electric Company

Inventor： Abinash Baruah ,  Gilbert Otto Kraemer ,  Predrag Popovic ,  William Francis Carnell, JR.

IPC: F23R3/28

CPC classification number: F23R3/34 ,  F23R3/28 ,  F23R3/346

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.

Abstract translation: 用于将液体燃料喷射到燃烧气体流场中的系统包括限定燃烧气体流动路径的环形衬套。 环形衬套包括延伸穿过内壁和外壁的内壁，外壁和燃料喷射器开口。 该系统还包括与燃料喷射器开口同轴对准的气体燃料喷射器。 气体燃料喷射器包括上游端和下游端。 下游端基本上靠近内壁终止。 稀释空气通道至少部分地由气体燃料喷射器限定。 液体燃料喷射器部分地延伸穿过稀释空气通道。 液体燃料喷射器包括从内壁的上游终止的喷射端。

公开(公告)号：US20150000244A1

公开(公告)日：2015-01-01

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: F01N3/20 ,  B01D53/14 ,  B01D53/86

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。

公开(公告)号：US20140298814A1

公开(公告)日：2014-10-09

申请号：US13858192

申请日：2013-04-08

Applicant: GENERAL ELECTRIC COMPANY

Inventor： John Anthony Conchieri ,  Roy Marshall Washam ,  Gilbert Otto Kraemer

IPC: F23R3/00 ,  F02C7/08 ,  F02C7/224 ,  F24H1/00

CPC classification number: F23R3/005 ,  F02C3/205 ,  F02C7/08 ,  F02C7/224 ,  F23L2900/15042 ,  F23R3/40 ,  F24H1/0045

Abstract: A system for pre-heating a working fluid within a combustor includes a compressor for providing the working fluid to the combustor. An outer casing is disposed downstream from the compressor. The outer casing at least partially defines a high pressure plenum that at least partially surrounds the combustor. A combustion chamber is defined within the combustor downstream from the high pressure plenum. A catalytic combustor is disposed within the high pressure plenum upstream from the combustion chamber so as to provide thermal energy to the working fluid upstream from the combustion chamber.

Abstract translation: 用于对燃烧器内的工作流体进行预热的系统包括用于向燃烧器提供工作流体的压缩机。 外壳设置在压缩机的下游。 外壳至少部分地限定至少部分地围绕燃烧器的高压集气室。 燃烧室限定在高压气室下游的燃烧室内。 催化燃烧器设置在燃烧室上游的高压集气室内，以便向燃烧室上游的工作流体提供热能。