知搜-全球专利检索

  1. Login
  2. Sign Up

Search Results

100 records (took 0.018 seconds)

    Bundled tube fuel nozzle with internal cooling
    1.
    发明授权
    Bundled tube fuel nozzle with internal cooling 有权

    公开(公告)号：US10309653B2

    公开(公告)日：2019-06-04

    申请号：US15060688

    申请日：2016-03-04

    Applicant: General Electric Company

    Inventor： Patrick Benedict Melton ,  David William Cihlar ,  Timothy James Purcell

    IPC: F23R3/00 ,  F23R3/08 ,  F23R3/28 ,  F23D14/02 ,  F23D14/64

    Abstract: A bundled tube fuel nozzle includes a forward plate, a first intermediate plate and an outer sleeve defining a fuel plenum, a second intermediate plate axially spaced from the first intermediate plate where the first intermediate plate, the second intermediate plate and the outer sleeve define a purge air plenum, an aft plate axially spaced from the second intermediate plate where the second intermediate plate, the aft plate and the outer sleeve define a cooling air plenum and an annular wall that extends from the second intermediate plate to the aft plate. The annular wall defines a cooling flow channel within the bundled tube fuel nozzle. A plurality of apertures is defined proximate to a cool side of the aft plate and provide for fluid communication between the cooling flow channel and the cooling air plenum.

    Wake reducing structure for a turbine system
    4.
    发明授权
    Wake reducing structure for a turbine system 有权
    涡轮机系统的减速结构

    公开(公告)号：US09494321B2

    公开(公告)日：2016-11-15

    申请号：US14102006

    申请日：2013-12-10

    Applicant: General Electric Company

    Inventor： Patrick Benedict Melton ,  Richard Martin DiCintio

    IPC: F23R3/08 ,  F23R3/06 ,  F23R3/16 ,  F23R3/28 ,  F23R3/34

    CPC classification number: F23R3/08 ,  F23R3/06 ,  F23R3/16 ,  F23R3/283 ,  F23R3/346 ,  F23R2900/00018 ,  F23R2900/03043

    Abstract: A wake reducing structure includes a combustor liner having an inner surface and an outer surface, the inner surface defining a combustor chamber. Also included is an airflow path located along the outer surface of the combustor liner. Further included is a wake generating component disposed in the airflow path and proximate the combustor liner, wherein the wake generating component generates a wake region located downstream of the wake generating component. Yet further included is a wake generating component boss operatively coupled to the combustor liner and disposed within a combustor liner aperture. Also included is a cooling channel extending through the wake generating component boss, the cooling channel having an air inlet on an upstream region of the wake generating component boss and an air outlet on a downstream region of the wake generating component boss, the cooling channel configured to supply air to the wake region.

    Abstract translation: 尾流减少结构包括具有内表面和外表面的燃烧器衬套，内表面限定了燃烧室。 还包括沿着燃烧器衬套的外表面设置的气流路径。 进一步包括设置在气流路径中并且靠近燃烧器衬套的尾流产生部件，其中，尾流产生部件产生位于尾流产生部件下游的尾流区域。 另外还包括一个尾灯产生部件凸台，可操作地联接到燃烧器衬套并设置在燃烧器衬套孔内。 还包括延伸穿过尾流产生部件凸台的冷却通道，冷却通道在尾流产生部件凸台的上游区域上具有空气入口，在尾流发生部件凸起的下游区域具有空气出口，冷却通道配置 向尾流区供应空气。

    Combustor cap assembly
    5.
    发明授权
    Combustor cap assembly 有权
    燃烧器盖组件

    公开(公告)号：US09470421B2

    公开(公告)日：2016-10-18

    申请号：US14462646

    申请日：2014-08-19

    Applicant: General Electric Company

    Inventor： Lucas John Stoia ,  Patrick Benedict Melton ,  Carolyn Ashley Antoniono

    IPC: F23R3/28 ,  F23R3/00 ,  F23R3/04 ,  F02C7/18 ,  F23R3/10 ,  F23R3/60

    CPC classification number: F23R3/283 ,  F02C7/18 ,  F05B2260/201 ,  F23R3/002 ,  F23R3/04 ,  F23R3/10 ,  F23R3/60 ,  F23R2900/03041 ,  F23R2900/03044 ,  Y02T50/675

    Abstract: A combustor cap assembly includes an annular shroud and an impingement plate coupled to the shroud. The impingement plate at least partially defines a plurality of impingement cooling holes and a cooling flow return passage. A cap plate is coupled to the impingement plate. The cap plate includes an impingement side which faces a second side portion of the impingement plate where the impingement side is axially spaced from the second side portion to define an impingement air plenum therebetween. The cooling flow return passage is in fluid communication with the impingement air plenum. A fluid conduit extends from a first side portion of the impingement plate towards a first end portion of the shroud. The fluid conduit is in fluid communication with the cooling flow return passage and provides for fluid communication out of the impingement air plenum.

    Abstract translation: 燃烧器盖组件包括环形护罩和联接到护罩的冲击板。 冲击板至少部分地限定多个冲击冷却孔和冷却流回流通道。 盖板联接到冲击板。 盖板包括面对冲击板的第二侧部的冲击侧，其中冲击侧与第二侧部轴向间隔开，以在其间限定冲击空气增压室。 冷却回流通道与冲击空气通风室流体连通。 流体导管从冲击板的第一侧部朝向护罩的第一端部延伸。 流体导管与冷却流回流通道流体连通，并提供流体连通到冲击空气通风室外。

    Systems and methods for late lean injection premixing
    6.
    发明授权
    Systems and methods for late lean injection premixing 有权
    晚期注射预混合的系统和方法

    公开(公告)号：US09404659B2

    公开(公告)日：2016-08-02

    申请号：US13716821

    申请日：2012-12-17

    Applicant: General Electric Company

    Inventor： Patrick Benedict Melton ,  John Vanselow ,  Russell DeForest ,  Lucas Stoia

    IPC: F23R3/06 ,  F23R3/34 ,  F23R3/36 ,  F23R3/28

    CPC classification number: F23R3/36 ,  F23R3/06 ,  F23R3/286 ,  F23R3/34 ,  F23R3/346

    Abstract: A late lean injection combustor assembly may include a first interior in which a first fuel supplied thereto is combustible, a flow sleeve annulus including a second interior in which a second fuel supplied thereto is combustible, at least one fuel injector disposed about the second interior, and at least one elongate premixing conduit disposed about the flow sleeve annulus and in fluid communication with the at least one fuel injector. The at least one elongate premixing conduit may be in fluid communication with a compressor discharge air and the second fuel such that the compressor discharge air and the second fuel are premixed within the elongate premixing conduit before entering the second interior by way of the at least one fuel injector.

    Abstract translation: 后期稀薄注射燃烧器组件可包括其中供应到其中的第一燃料可燃的第一内部，包括第二内部的流动套筒环，其中供应到其中的第二燃料可燃，在第二内部设置的至少一个燃料喷射器， 以及设置在所述流动套筒环周围并与所述至少一个燃料喷射器流体连通的至少一个细长的预混合导管。 所述至少一个细长预混合导管可以与压缩机排放空气和第二燃料流体连通，使得压缩机排出的空气和第二燃料在进入第二内部之前通过至少一个 喷油器。

    Combustor support assembly for mounting a combustion module of a gas turbine
    8.
    发明授权
    Combustor support assembly for mounting a combustion module of a gas turbine 有权
    用于安装燃气轮机的燃烧模块的燃烧器支撑组件

    公开(公告)号：US09400114B2

    公开(公告)日：2016-07-26

    申请号：US13845699

    申请日：2013-03-18

    Applicant: General Electric Company

    Inventor： Patrick Benedict Melton ,  Lucas John Stoia ,  Richard Martin DiCintio ,  Christopher Paul Willis

    IPC: F23R3/60 ,  F23R3/34 ,  F23R3/00

    CPC classification number: F23R3/60 ,  F23R3/005 ,  F23R3/34 ,  F23R2900/00017 ,  F23R2900/00019

    Abstract: A gas turbine comprises a compressor discharge casing that is coupled to an outer turbine shell. The compressor discharge casing includes a combustor opening that extends through the compressor discharge casing and an outer mating surface that circumferentially surrounds the combustor opening. The outer turbine shell defines an inner mating surface. A combustion module extends through the combustor opening. The combustion module includes a forward end that is circumferentially surrounded by a mounting flange and an aft end that is circumferentially surrounded by an aft frame. The mounting flange extends circumferentially around the combustor opening. The mounting flange is coupled to the outer mating surface of the compressor discharge casing and the aft frame is coupled to the inner mating surface of the outer turbine shell.

    Abstract translation: 燃气轮机包括联接到外部涡轮机壳体的压缩机排出壳体。 压缩机排出壳体包括延伸穿过压缩机排出壳体的燃烧器开口和围绕燃烧器开口的外部配合表面。 外涡轮壳体限定内配合表面。 燃烧模块延伸穿过燃烧器开口。 燃烧模块包括由安装凸缘周向地包围的前端和由后框架周向包围的后端。 安装凸缘围绕燃烧器开口周向延伸。 安装凸缘联接到压缩机排出壳体的外配合表面，并且后框架联接到外涡轮机壳体的内配合表面。

    System for controlling a flow rate of a compressed working fluid to a combustor fuel injector
    9.
    发明授权
    System for controlling a flow rate of a compressed working fluid to a combustor fuel injector 有权
    用于控制压缩工作流体到燃烧器燃料喷射器的流量的系统

    公开(公告)号：US09376961B2

    公开(公告)日：2016-06-28

    申请号：US13845397

    申请日：2013-03-18

    Applicant: General Electric Company

    Inventor： Lucas John Stoia ,  Patrick Benedict Melton ,  Richard Martin DiCintio

    IPC: F02C6/08 ,  F02C7/22 ,  F01D9/02 ,  F02C9/52 ,  F23R3/04 ,  F23R3/26

    CPC classification number: F02C7/22 ,  F01D9/02 ,  F02C6/08 ,  F02C9/52 ,  F23R3/045 ,  F23R3/26 ,  F23R3/346

    Abstract: A system for controlling air flow rate of a compressed working fluid to a fuel injector of a combustor includes an outer casing that defines a high pressure plenum around a portion of the combustor, an extraction port in fluid communication with the high pressure plenum and an inlet port. The combustor includes a plurality of fuel injectors arranged around a combustion liner, an inner flow sleeve, an outer air shield that surrounds the plurality of fuel injectors and the inner flow sleeve. The outer air shield defines an injection an air plenum between the outer air shield and the inner flow sleeve and an inlet to the injection air plenum. An external fluid circuit provides fluid communication between the extraction port and the inlet port. A baffle extends between the outer casing and the outer air shield to provide flow separation between the inlet and the high pressure plenum.

    Abstract translation: 用于控制压缩工作流体对燃烧器的燃料喷射器的空气流量的系统包括：外壳，其围绕燃烧器的一部分限定高压增压室;与高压气室流体连通的抽出口和入口 港口。 燃烧器包括围绕燃烧衬套布置的多个燃料喷射器，内部流动套筒，围绕多个燃料喷射器和内部流动套筒的外部空气屏蔽件。 外部空气屏蔽件限定了在外部空气屏蔽和内部流动套筒之间的注入空气增压室和注入空气增压室的入口。 外部流体回路在提取口和入口之间提供流体连通。 挡板在外壳和外部空气屏蔽之间延伸，以提供入口和高压集气室之间的流动分离。

    IGNITER TIP WITH COOLING PASSAGE
    10.
    发明申请
    IGNITER TIP WITH COOLING PASSAGE 审中-公开
    IGNITER TIP与冷却通道

    公开(公告)号：US20160003150A1

    公开(公告)日：2016-01-07

    申请号：US14323144

    申请日：2014-07-03

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Richard Martin DiCintio ,  Patrick Benedict Melton

    IPC: F02C7/18 ,  F02C7/266

    CPC classification number: H01T21/02 ,  B23K26/342 ,  F02C7/18 ,  F02C7/266

    Abstract: An igniter tip for a combustion system is provided. The igniter tip may include a central electrode; an insulator sleeve about the central electrode; and an outer electrode about the insulator sleeve, the outer electrode including a tubular wall having a cooling passage extending within the tubular wall, the cooling passage including an entrance opening and an exit opening to an exterior of the outer electrode. A combustion system may include the igniter tip.

    Abstract translation: 提供了用于燃烧系统的点火器尖端。 点火头可包括中心电极; 围绕中心电极的绝缘体套管; 以及围绕所述绝缘体套筒的外部电极，所述外部电极包括具有在所述管状壁内延伸的冷却通道的管状壁，所述冷却通道包括入口和外部电极外部的出口。 燃烧系统可以包括点火器尖端。

Patent Agency Ranking