公开(公告)号：US20160033133A1

公开(公告)日：2016-02-04

申请号：US14448321

申请日：2014-07-31

Applicant: General Electric Company

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

IPC: F23R3/28

CPC classification number: F23R3/286 ,  F23R3/10

Abstract: A micro-mixer nozzle for use in a combustor of a combustion turbine engine, the micro-mixer nozzle including: a fuel plenum defined by a shroud wall connecting a periphery of a forward tube sheet to a periphery of an aft tubesheet; a plurality of mixing tubes extending across the fuel plenum for mixing a supply of compressed air and fuel, each of the mixing tubes forming a passageway between an inlet formed through the forward tubesheet and an outlet formed through the aft tubesheet; and a wall mixing tube formed in the shroud wall.

Abstract translation: 一种用于燃气涡轮发动机的燃烧器的微混合器喷嘴，所述微混合器喷嘴包括：由连接前管板的周边与后管板的周边的护罩壁限定的燃料室; 多个混合管延伸穿过燃料增压室，用于混合供应的压缩空气和燃料，每个混合管在通过前管板形成的入口和通过后管板形成的出口之间形成通道; 以及形成在护罩壁中的壁混合管。

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：US20140338354A1

公开(公告)日：2014-11-20

申请号：US13838107

申请日：2013-03-15

Applicant: General Electric Company

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

IPC: F23R3/28

CPC classification number: F23R3/286

Abstract: A system including a multi-tube fuel nozzle, including a plurality of tubes extending in an axial direction relative to a central axis of the multi-tube fuel nozzle, wherein each tube of the plurality of tubes includes an air inlet, a fuel inlet, and a fuel-air mixture outlet; and an inlet flow conditioner, including a plate extending in a radial direction relative to the central axis of the multi-tube fuel nozzle; an outer wall extending circumferentially about the plate, wherein the outer wall is coupled to the plate; and a plurality of air openings in the plate, the outer wall, or a combination thereof, wherein the plurality of air openings are disposed upstream from the air inlets in the plurality of tubes.

Abstract translation: 一种包括多管燃料喷嘴的系统，包括相对于所述多管燃料喷嘴的中心轴在轴向上延伸的多个管，其中所述多个管中的每个管包括空气入口，燃料入口， 和燃料 - 空气混合物出口; 以及入口流动调节器，包括相对于多管燃料喷嘴的中心轴线在径向方向上延伸的板; 围绕所述板周向延伸的外壁，其中所述外壁联接到所述板; 以及板，外壁或其组合中的多个空气开口，其中多个空气开口设置在多个管中的空气入口的上游。

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。