公开(公告)号：US20150107255A1

公开(公告)日：2015-04-23

申请号：US14057458

申请日：2013-10-18

Applicant: General Electric Company

Inventor： Jason Thurman Stewart ,  Thomas Edward Johnson ,  Christopher Paul Keener ,  Heath Michael Ostebee

IPC: F23R3/34

CPC classification number: F23R3/346

Abstract: A turbomachine combustor assembly includes a combustor including a combustor body extending from a head end to a second end through a combustion zone. At least one injector is configured and disposed to introduce a first combustible fluid into the combustion zone at the head end of the combustor body. At least one late lean injector (LLI) is configured and disposed to introduce a second combustible fluid downstream of the first combustible fluid. An external fluid delivery system is fluidically connected to the at least one LLI. The external fluid delivery system includes at least one combustible fluid delivery conduit that extends from a first end fluidically connected to the LLI to a second end external to the turbomachine combustor assembly. The second end is configured and disposed to deliver the second combustible mixture to the LLI.

Abstract translation: 涡轮机械燃烧器组件包括燃烧器，该燃烧器包括从头端延伸到第二端并通过燃烧区的燃烧器主体。 至少一个喷射器被构造和设置成将第一可燃流体引入燃烧器主体的头端处的燃烧区域。 至少一个后部稀薄喷射器（LLI）被配置和设置成在第一可燃流体的下游引入第二可燃流体。 外部流体输送系统流体连接到至少一个LLI。 外部流体输送系统包括至少一个可燃流体输送导管，其从流体连接到LLI的第一端延伸到涡轮机燃烧器组件外部的第二端。 第二端被配置和布置成将第二可燃混合物输送到LLI。

公开(公告)号：US20140367495A1

公开(公告)日：2014-12-18

申请号：US13916767

申请日：2013-06-13

Applicant: General Electric Company

Inventor： James Christopher Monaghan ,  Thomas Edward Johnson ,  Heath Michael Ostebee

IPC: F02M55/00 ,  F23R3/28

CPC classification number: F02M55/008 ,  B05B7/04 ,  B05B7/08 ,  F02M2200/80 ,  F23R3/10 ,  F23R3/28 ,  F23R3/286 ,  Y10T29/494

Abstract: A fuel injection head for use in a fuel injection nozzle comprises a monolithic body portion comprising an upstream face, an opposite downstream face, and a peripheral wall extending therebetween. A plurality of pre-mix tubes are integrally formed with and extend axially through the body portion. Each of the pre-mix tubes comprises an inlet adjacent the upstream face, an outlet adjacent the downstream face, and a channel extending between the inlet and the outlet. Each pre-mix tube also includes at least one fuel injector that at least partially extends outward from an exterior surface of the pre-mix tube, wherein the fuel injector is integrally formed with the pre-mix tube and is configured to facilitate fuel flow between the body portion and the channel.

Abstract translation: 一种用于燃料喷射喷嘴的燃料喷射头包括一个整体主体部分，包括一个上游面，一个相对的下游面以及一个在其间延伸的周壁。 多个预混合管一体地形成并且轴向地穿过主体部分。 每个预混合管包括邻近上游面的入口，邻近下游面的出口和在入口和出口之间延伸的通道。 每个预混合管还包括至少一个燃料喷射器，其至少部分地从预混合管的外表面向外延伸，其中燃料喷射器与预混合管一体地形成，并且构造成促进燃料在 身体部分和通道。

公开(公告)号：US20140216054A1

公开(公告)日：2014-08-07

申请号：US13760097

申请日：2013-02-06

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Heath Michael Ostebee ,  Thomas Edward Johnson ,  Jason Thurman Stewart ,  Christopher Paul Keener

IPC: F02C7/20

CPC classification number: F02C7/20 ,  F02C3/14 ,  F23D2900/14004 ,  F23R3/283 ,  F23R3/286 ,  F23R3/46

Abstract: The present application provides a combustor for use with a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles and a fuel injection system for providing a flow of fuel to the micro-mixer fuel nozzles. The fuel injection system may include a number of support struts supporting the fuel nozzles and providing the flow of fuel therethrough. The support struts may include an aerodynamic contoured shape so as to distribute evenly a flow of air to the micro-mixer fuel nozzles.

Abstract translation: 本申请提供了一种与燃气涡轮发动机一起使用的燃烧器。 燃烧器可以包括多个微混合器燃料喷嘴和用于向微混合器燃料喷嘴提供燃料流的燃料喷射系统。 燃料喷射系统可以包括支撑燃料喷嘴的多个支撑支柱，并且通过其提供燃料流。 支撑支柱可以包括空气动力学轮廓形状，以便均匀地分配空气流到微混合器燃料喷嘴。