公开(公告)号：US20140366541A1

公开(公告)日：2014-12-18

申请号：US13917964

申请日：2013-06-14

Applicant: General Electric Company

Inventor： Gregory Earl Jensen ,  Bryan Wesley Romig ,  Jason Thurman Stewart ,  Jason Charles Terry

IPC: F02C7/22

CPC classification number: F02C7/22 ,  F23R3/286

Abstract: A gas turbine engine having a combustor that includes: an inner radial wall defining a first interior chamber and a second interior chamber, wherein the first interior chamber extends axially from an end cover to a primary fuel injector, and the second interior chamber extends axially from the primary fuel injector to the turbine; an outer radial wall formed about the inner radial wall so that a flow annulus is formed therebetween; upstream fuel nozzles jutting into the flow annulus from the outer radial wall. The upstream fuel nozzles may include non-uniform circumferential spacing about the inner radial wall.

Abstract translation: 一种具有燃烧器的燃气涡轮发动机，其包括：限定第一内部室和第二内部室的内部径向壁，其中所述第一内部室从端盖轴向延伸到主要燃料喷射器，并且所述第二内部腔室从 主燃料喷射器到涡轮机; 围绕所述内部径向壁形成的外部径向壁，使得在其之间形成流动环空; 上游燃料喷嘴从外部径向壁突出到流动环空中。 上游燃料喷嘴可以包括围绕内部径向壁的不均匀的周向间隔。

公开(公告)号：US20140182297A1

公开(公告)日：2014-07-03

申请号：US13733313

申请日：2013-01-03

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Jason Charles Terry ,  Timothy Andrew Healy ,  Mark William Pinson ,  Gregory Earl Jensen

IPC: F02C9/00

CPC classification number: F02C9/00 ,  F02C9/48

Abstract: A gas turbine includes a compressor section, a combustion section downstream from the compressor section, a turbine section downstream from the combustion section, and a controller. The controller controls the operation of the gas turbine at a reduced load, and is capable of querying a database including multiple sets of operational parameters for the gas turbine correlated with at least one measured output response at each set of operational parameters. One of the sets of operational parameters provides a desired gas turbine load that meets a target level for the output response. Related methods are also disclosed.

Abstract translation: 燃气轮机包括压缩机部分，压缩机部分下游的燃烧部分，燃烧部分下游的涡轮部分和控制器。 控制器以减小的负载控制燃气轮机的操作，并且能够查询数据库，其包括与在每组操作参数下的至少一个测量的输出响应相关的燃气轮机的多组操作参数。 一组操作参数提供满足输出响应的目标水平的期望的燃气轮机负载。 还公开了相关方法。

公开(公告)号：US20140311150A1

公开(公告)日：2014-10-23

申请号：US13864708

申请日：2013-04-17

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Mark William Pinson ,  Gregory Earl Jensen ,  Jason Charles Terry

IPC: F23R3/28 ,  F23R3/14

CPC classification number: F23R3/286 ,  F23D14/24 ,  F23D2900/14004 ,  F23D2900/14021 ,  F23R3/14 ,  F23R3/32

Abstract: A fuel nozzle for use in a gas turbine includes a pre-mix flow passage for directing a flow segment of a flow of a working fluid through the fuel nozzle. A first swirler vane and a second swirler vane extend within the pre-mix flow passage. The first swirler vane provides a first wake region within the flow segment. The second swirler vane provides a second wake region within the flow segment. A fuel injection peg is disposed downstream from the first swirler vane and the second swirler vane. The fuel injection peg is positioned within the flow segment between the first wake region and the second wake region.

Abstract translation: 用于燃气轮机的燃料喷嘴包括用于引导工作流体流的流动段通过燃料喷嘴的预混流动通道。 第一旋流器叶片和第二旋流器叶片在预混合流动通道内延伸。 第一旋流器叶片在流动段内提供第一尾流区域。 第二旋流器叶片在流动段内提供第二尾流区域。 燃料喷射栓设置在第一旋流叶片和第二旋流叶片的下游。 燃料喷射栓定位在第一尾流区域和第二尾流区域之间的流动段内。

公开(公告)号：US20140096526A1

公开(公告)日：2014-04-10

申请号：US13646885

申请日：2012-10-08

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Elias Marquez ,  Gregory Earl Jensen

IPC: F02C1/00

CPC classification number: F23N1/007 ,  F23N2021/10 ,  F23N2035/16 ,  F23N2041/20 ,  F23R3/28

Abstract: An end cover for a gas turbine combustor includes a main body configured to connect to a casing that at least partially surrounds a portion of the gas turbine. A fuel circuit extends within the main body of the end cover. An orifice extends through the main body. The orifice is in fluid communication with the fuel circuit. The end cover further includes a linear actuator. The linear actuator includes a flow control member that extends the fuel circuit and at least partially through the orifice.

Abstract translation: 用于燃气轮机燃烧器的端盖包括构造成连接到至少部分地围绕燃气轮机的一部分的壳体的主体。 燃料电路在端盖的主体内延伸。 孔口延伸穿过主体。 孔与燃料回路流体连通。 端盖还包括线性致动器。 线性致动器包括流动控制构件，其延伸燃料回路并且至少部分地穿过孔口。

公开(公告)号：US09322559B2

公开(公告)日：2016-04-26

申请号：US13864708

申请日：2013-04-17

Applicant: General Electric Company

Inventor： Mark William Pinson ,  Gregory Earl Jensen ,  Jason Charles Terry

IPC: F23R3/28 ,  F23R3/14 ,  F23D14/24 ,  F23R3/32

CPC classification number: F23R3/286 ,  F23D14/24 ,  F23D2900/14004 ,  F23D2900/14021 ,  F23R3/14 ,  F23R3/32

Abstract: A fuel nozzle for use in a gas turbine includes a pre-mix flow passage for directing a flow segment of a flow of a working fluid through the fuel nozzle. A first swirler vane and a second swirler vane extend within the pre-mix flow passage. The first swirler vane provides a first wake region within the flow segment. The second swirler vane provides a second wake region within the flow segment. A fuel injection peg is disposed downstream from the first swirler vane and the second swirler vane. The fuel injection peg is positioned within the flow segment between the first wake region and the second wake region.

Abstract translation: 用于燃气轮机的燃料喷嘴包括用于引导工作流体流的流动段通过燃料喷嘴的预混流动通道。 第一旋流器叶片和第二旋流器叶片在预混合流动通道内延伸。 第一旋流器叶片在流动段内提供第一尾流区域。 第二旋流器叶片在流动段内提供第二尾流区域。 燃料喷射栓设置在第一旋流叶片和第二旋流叶片的下游。 燃料喷射栓定位在第一尾流区域和第二尾流区域之间的流动段内。