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公开(公告)号：US11187415B2
公开(公告)日：2021-11-30
申请号：US15838172
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 , Benjamin Robert Ryan , Gilbert Otto Kraemer
Abstract: An injection assembly for a gas turbine combustor having a liner defining a combustion zone and a secondary combustion zone and a forward casing circumferentially surrounding at least a portion of the liner is provided. The injection assembly includes a thimble assembly and an injector unit. The thimble assembly, which is mounted to the liner, includes a thimble that extends through a thimble aperture in the liner. The injector unit, which is mounted to and extends through the forward casing, includes an injector blade that extends into the thimble. The injection assembly introduces a flow of fuel into a flow of air flowing through the thimble, such that fuel and air are injected into the secondary combustion zone in a direction transverse to a flow of combustion products from the primary combustion zone.
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公开(公告)号：US09360214B2
公开(公告)日：2016-06-07
申请号：US13858192
申请日：2013-04-08
Applicant: General Electric Company
Inventor： John Anthony Conchieri , Roy Marshall Washam , Gilbert Otto Kraemer
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。
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公开(公告)号：US20140238024A1
公开(公告)日：2014-08-28
申请号：US13777179
申请日：2013-02-26
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Gilbert Otto Kraemer
Abstract: A combustor for a gas turbine includes a fuel nozzle having a central swirler that circumferentially surrounds a downstream end of the fuel nozzle. A primary combustion zone is defined within the central swirler. The combustor further includes an outer swirler that circumferentially surrounds at least a portion of the central swirler and a venturi that is disposed downstream from the primary combustion zone. The venturi includes an inner surface. The central swirler imparts angular swirl to a compressed working fluid so as to rapidly mix and react the fuel rich primary zone products with the working fluid. The outer swirler imparts angular swirl to a compressed working fluid so as to provide a cooling boundary layer along the inner surface of the venturi.
Abstract translation: 燃气轮机的燃烧器包括燃料喷嘴，燃料喷嘴具有周向围绕燃料喷嘴的下游端的中心旋流器。 主燃烧区定义在中心旋流器内。 燃烧器还包括外旋流器，其周向地围绕中心旋流器的至少一部分和设置在主燃烧区下游的文丘里管。 文氏管包括内表面。 中心旋流器对压缩的工作流体施加角度涡流，以便使富燃料的初级区域产物与工作流体快速混合和反应。 外旋流器对压缩的工作流体施加角度涡流，以便沿文丘里管的内表面提供冷却边界层。
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14.发明申请公开(公告)号：US20140109587A1
公开(公告)日：2014-04-24
申请号：US14048272
申请日：2013-10-08
Applicant: General Electric Company
Inventor： Sarah Lori Crothers , Gilbert Otto Kraemer
CPC classification number: F23R3/20 , F02C7/22 , F02C7/24 , 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，通过下列中的至少一个的第一燃料口： 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。
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公开(公告)号：US20190178497A1
公开(公告)日：2019-06-13
申请号：US15838172
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 , Benjamin Robert Ryan , Gilbert Otto Kraemer
Abstract: An injection assembly for a gas turbine combustor having a liner defining a combustion zone and a secondary combustion zone and a forward casing circumferentially surrounding at least a portion of the liner is provided. The injection assembly includes a thimble assembly and an injector unit. The thimble assembly, which is mounted to the liner, includes a thimble that extends through a thimble aperture in the liner. The injector unit, which is mounted to and extends through the forward casing, includes an injector blade that extends into the thimble. The injection assembly introduces a flow of fuel into a flow of air flowing through the thimble, such that fuel and air are injected into the secondary combustion zone in a direction transverse to a flow of combustion products from the primary combustion zone.
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Patent Agency Ranking
公开(公告)号：US09310082B2
公开(公告)日：2016-04-12
申请号：US13777179
申请日：2013-02-26
Applicant: General Electric Company
Inventor： Gilbert Otto Kraemer
Abstract: A combustor for a gas turbine includes a fuel nozzle having a central swirler that circumferentially surrounds a downstream end of the fuel nozzle. A primary combustion zone is defined within the central swirler. The combustor further includes an outer swirler that circumferentially surrounds at least a portion of the central swirler and a venturi that is disposed downstream from the primary combustion zone. The venturi includes an inner surface. The central swirler imparts angular swirl to a compressed working fluid so as to rapidly mix and react the fuel rich primary zone products with the working fluid. The outer swirler imparts angular swirl to a compressed working fluid so as to provide a cooling boundary layer along the inner surface of the venturi.
Abstract translation: 燃气轮机的燃烧器包括燃料喷嘴，燃料喷嘴具有周向围绕燃料喷嘴的下游端的中心旋流器。 主燃烧区定义在中心旋流器内。 燃烧器还包括外旋流器，其周向地围绕中心旋流器的至少一部分和设置在主燃烧区下游的文丘里管。 文氏管包括内表面。 中心旋流器对压缩的工作流体施加角度涡流，以便使富燃料的初级区域产物与工作流体快速混合和反应。 外旋流器对压缩的工作流体施加角度涡流，以便沿文丘里管的内表面提供冷却边界层。
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公开(公告)号：US20150000693A1
公开(公告)日：2015-01-01
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
IPC: F01D25/00
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.
Abstract translation: 一种用于压缩机的在线洗涤系统，包括：喷嘴，其包括用于洗涤液体的流动通道，其中所述流动通道被配置为联接到洗涤液体源并且包括排出口，所述排出出口布置成将所述洗涤液体投射到 用于涡轮机的工作液流; 靠近所述喷嘴的流动通道的电极，其中所述电极被配置为形成足以对流过所述通道的洗涤液体充电的电场，并且施加到所述洗涤液体的电荷具有第一极性，并且所述表面 带有第一极性的压缩机，其中表面暴露于工作流体流并且在喷嘴的下游。
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公开(公告)号：US20140287367A1
公开(公告)日：2014-09-25
申请号：US14298538
申请日：2014-06-06
Applicant: General Electric Company
Inventor： Robert Thomas Thatcher , Gilbert Otto Kraemer , Andrew Mitchell Rodwell , Matthew M. Scheid
CPC classification number: F23J3/00 , F02C7/30 , F02C9/28 , F23N1/002 , F23N2041/20 , F23R2900/00004
Abstract: A system for operating a combustor includes a sensor that measures an operating parameter associated with the combustor and generates a signal reflective of the operating parameter. The operating parameter is reflective of an ash deposition rate or an accumulated ash buildup. A controller receives the signal, compares the signal to a predetermined limit, and generates a control signal. A method for operating a combustor includes operating the combustor at a first power level that produces a first temperature that is less than or equal to a first predetermined temperature and creating a layer of ash. The method further includes measuring an operating parameter reflective of an ash deposition rate or an accumulated ash buildup, comparing the operating parameter to a limit, and operating the combustor at a second power level that produces a second temperature that is greater than or equal to the first predetermined temperature.
Abstract translation: 用于操作燃烧器的系统包括测量与燃烧器相关联的操作参数并产生反映操作参数的信号的传感器。 操作参数反映了灰分沉积速率或积聚的灰分积累。 控制器接收信号，将信号与预定极限进行比较，并产生控制信号。 用于操作燃烧器的方法包括以产生小于或等于第一预定温度的第一温度并产生灰分层的第一功率水平操作燃烧器。 该方法还包括测量反映灰分沉积速率或累积的灰分积累的操作参数，将操作参数与极限进行比较，以及在产生第二温度的第二功率水平下操作燃烧器，该第二功率水平大于或等于 第一预定温度。
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公开(公告)号：US20140230447A1
公开(公告)日：2014-08-21
申请号：US13771614
申请日：2013-02-20
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Heena Vinodkumar Panchasara , Gilbert Otto Kraemer
IPC: F23R3/28
CPC classification number: F23R3/286 , F23D2900/14004
Abstract: A fuel nozzle for a gas turbomachine includes an outer nozzle body including an inner surface defining a mixing zone, and an inner nozzle body arranged within the outer nozzle body. The inner nozzle body includes a fluid passage. At least one flow affector extends from the inner nozzle body to the outer nozzle body. The at least one flow affector includes an inner surface that defines an interior chamber having an inlet fluidly connected to the fluid passage and at least two openings fluidically linking the interior chamber and the mixing zone. One or more flow tuning elements are arranged at the interior chamber upstream of the at least two openings. The one or more flow affectors are configured and disposed to condition a fluid passing into the interior chamber to affect a substantially iso-kinetic distribution of the fluid within the interior chamber.
Abstract translation: 用于气体涡轮机的燃料喷嘴包括外喷嘴体，其包括限定混合区的内表面和布置在外喷嘴体内的内喷嘴体。 内部喷嘴体包括流体通道。 至少一个流动体从内部喷嘴体延伸到外部喷嘴体。 至少一个流动检测器包括内表面，该内表面限定具有流体连接到流体通道的入口和至少两个流体连接内室和混合区的开口的内室。 一个或多个流量调节元件布置在至少两个开口的上游的内室。 一个或多个流动构件被构造和设置成调节流入内部室的流体，以影响流体在内部室内的基本上等动力学分布。
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公开(公告)号：US10816203B2
公开(公告)日：2020-10-27
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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