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公开(公告)号：US20180128489A1
公开(公告)日：2018-05-10
申请号：US15343601
申请日：2016-11-04
Applicant: General Electric Company
Inventor： Gregory Allen Boardman , Pradeep Naik , Manampathy Gangadharan Giridharan , David Albin Lind , Jeffrey Michael Martini
IPC: F23R3/28
CPC classification number: F23R3/286 , F05D2220/32
Abstract: The present disclosure is directed to a fuel injector for a gas turbine engine including an end wall defining a fluid chamber, a centerbody, and an outer sleeve surrounding the centerbody from the end wall toward a downstream end of the fuel injector. The centerbody includes an axially extended outer wall and inner wall. The outer wall and inner wall extend from the end wall toward the downstream end of the fuel injector. The outer wall, the inner wall, and the end wall together define a fluid conduit extended in a first direction toward the downstream end of the fuel injector and in a second direction toward an upstream end of the fuel injector. The fluid conduit is in fluid communication with the fluid chamber. The outer wall defines at least one radially oriented fluid injection port in fluid communication with the fluid conduit. The outer sleeve and the centerbody define a premix passage radially therebetween and an outlet at the downstream end of the premix passage. The outer sleeve defines a plurality of radially oriented first air inlet ports in circumferential arrangement at a first axial portion of the outer sleeve. The outer sleeve defines a plurality of radially oriented second air inlet ports in circumferential arrangement at a second axial portion of the outer sleeve.
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公开(公告)号：US09765973B2
公开(公告)日：2017-09-19
申请号：US13797986
申请日：2013-03-12
Applicant: General Electric Company
Inventor： Ronald James Chila , Patrick Benedict Melton , Gregory Allen Boardman , James Harold Westmoreland
CPC classification number: F23R3/286 , F23D14/62 , F23R3/10 , Y02T50/675
Abstract: A system includes a multi-tube fuel nozzle. The multi-tube fuel nozzle includes multiple mixing tubes. Each mixing tube includes an annular wall disposed about a central passage and an air inlet region configured to be disposed about a fuel injector extending into the central passage. The central passage extends from an upstream end to a downstream end of the annular wall relative to a direction of flow through the central passage. The air inlet region includes an air entry surface of the annular wall that gradually decreases in diameter in the direction of flow.
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公开(公告)号：US09599343B2
公开(公告)日：2017-03-21
申请号：US13687071
申请日：2012-11-28
Applicant: General Electric Company
CPC classification number: F23R3/286 , F23D11/402 , F23D14/62 , F23D14/64 , F23R3/32 , Y10T29/49229
Abstract: A fuel nozzle for use in a turbine engine is provided. The fuel nozzle includes at least one premixer tube including a tube wall and a plurality of perforations defined therein and extending through the tube wall. The plurality of perforations are configured to channel a flow of air therethrough. The fuel nozzle also includes a liquid fuel plenum positioned upstream from the premixer tube, and at least one fuel injector coupled in flow communication with the liquid fuel plenum and the at least one premixer tube. The at least one fuel injector is configured to channel a flow of liquid fuel from the liquid fuel plenum into the premixer tube.
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公开(公告)号：US09534790B2
公开(公告)日：2017-01-03
申请号：US13735340
申请日：2013-01-07
Applicant: General Electric Company
Inventor： Jun Cai , Gregory Allen Boardman , Hasan Karim , Lucas John Stoia
CPC classification number: F23R3/346 , F23C2900/07001 , F23R3/14 , F23R3/286
Abstract: A fuel injector for a combustor generally includes an annular outer body having an inlet and an outlet. The outer body at least partially defines an outer flow passage. An inner flow passage extends at least partially through the outer flow passage and a radial swirler is disposed at the inlet of the outer body. The radial swirler includes a first radial passage separated from a second radial passage. The first radial passage has a first plurality of swirler vanes and the second radial passage has a second plurality of swirler vanes. The first radial passage is in fluid communication with the outer flow passage and the second radial passage is in fluid communication with the inner flow passage.
Abstract translation: 用于燃烧器的燃料喷射器通常包括具有入口和出口的环形外部主体。 外体至少部分地限定外部流动通道。 内部流动通道至少部分地延伸穿过外部流动通道，并且径向旋流器设置在外部主体的入口处。 径向旋流器包括与第二径向通道分离的第一径向通道。 第一径向通道具有第一多个旋流器叶片，并且第二径向通道具有第二多个旋流器叶片。 第一径向通道与外流道流体连通，第二径向通道与内流道流体连通。
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45.发明授权System having multi-tube fuel nozzle with floating arrangement of mixing tubes 有权具有多管燃料喷嘴的系统，具有混合管的浮动布置公开(公告)号：US09528444B2
公开(公告)日：2016-12-27
申请号：US13797961
申请日：2013-03-12
Applicant: General Electric Company
CPC classification number: F02C7/20 , F02C7/22 , F02C7/2365 , F23R3/286
Abstract: A system includes a multi-tube fuel nozzle. The multi-tube fuel nozzle includes an end cover, a first plate, and multiple tubes. The multiple tubes are disposed and supported in a floating arrangement between the end cover and the first plate. Each tube includes a forward end adjacent the end cover and an aft end adjacent the first plate.
Abstract translation: 系统包括多管燃料喷嘴。 多管燃料喷嘴包括端盖，第一板和多个管。 多个管被布置和支撑在端盖和第一板之间的浮动布置中。 每个管包括邻近端盖的前端和邻近第一板的后端。
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Patent Agency Ranking
公开(公告)号：US20160313007A1
公开(公告)日：2016-10-27
申请号：US14693838
申请日：2015-04-22
Applicant: General Electric Company
Inventor： Jeffrey Michael Martini , Gregory Allen Boardman , Bassam Sabry Mohammad Abd El-Nabi , Gerardo Antonio Salazar-Lois
CPC classification number: F23R3/286 , F23R3/04 , F23R3/14 , F23R3/283 , F23R2900/03044 , F23R2900/03343 , Y02T50/675
Abstract: A gas turbine system include a first body including a central passage extending from a mixing region to a central outlet at a first downstream end portion of the first body, a fuel outlet in the mixing region, an oxidant outlet in the mixing region, and an outer passage including a first passage extending in a downstream direction toward the first downstream end portion and a second passage extending in an upstream direction from the first downstream end portion into the mixing region.
Abstract translation: 一种燃气轮机系统包括：第一主体，包括从第一主体的第一下游端部处的混合区域延伸到中心出口的中心通道，混合区域中的燃料出口，混合区域中的氧化剂出口，以及 外部通道包括沿着下游方向朝向第一下游端部延伸的第一通道和从第一下游端部向上游方向延伸到混合区域的第二通道。
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公开(公告)号：US09383098B2
公开(公告)日：2016-07-05
申请号：US13664705
申请日：2012-10-31
Applicant: General Electric Company
Inventor： Gregory Scott Means , Gregory Allen Boardman , Jonathan Dwight Berry
CPC classification number: F23D11/24 , F23D11/38 , F23D14/00 , F23D2900/00015 , F23R3/283 , F23R3/286 , F23R3/343 , F23R3/46 , F23R2900/00012 , F23R2900/03044
Abstract: A combustor for a gas turbine generally includes a radial flow fuel nozzle having a fuel distribution manifold, and a fuel injection manifold axially separated from the fuel distribution manifold. The fuel injection manifold generally includes an inner side portion, an outer side portion, and a plurality of circumferentially spaced fuel ports that extend through the outer side portion. A plurality of tubes provides axial separation between the fuel distribution manifold and the fuel injection manifold. Each tube defines a fluid communication path between the fuel distribution manifold and the fuel injection manifold.
Abstract translation: 用于燃气轮机的燃烧器通常包括具有燃料分配歧管的径流式燃料喷嘴和与燃料分配歧管轴向分离的燃料喷射歧管。 燃料喷射歧管通常包括延伸穿过外侧部分的内侧部分，外侧部分和多个周向间隔开的燃料端口。 多个管在燃料分配歧管和燃料喷射歧管之间提供轴向间隔。 每个管限定在燃料分配歧管和燃料喷射歧管之间的流体连通路径。
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公开(公告)号：US09222673B2
公开(公告)日：2015-12-29
申请号：US13647636
申请日：2012-10-09
Applicant: General Electric Company
CPC classification number: F23R3/14 , F23D11/103 , F23D11/105 , F23D17/002 , F23R3/286 , F23R3/36 , Y10T29/49826
Abstract: A fuel nozzle is provided. The fuel nozzle includes a nozzle body, a plurality of swirler vanes, and at least one outlet. The nozzle body includes a back plate, a front plate, and a mixing zone defined therebetween. The back plate includes at least one inlet defined therein and the front plate includes at least one discharge defined therein. The plurality of swirler vanes are positioned between the back plate and the front plate and spaced circumferentially about the mixing zone. Each of the plurality of swirler vanes direct air obliquely into the mixing zone. The at least one outlet is defined within at least one of the nozzle body and the plurality of swirler vanes, the at least one outlet configured to inject fuel into said mixing zone.
Abstract translation: 提供燃料喷嘴。 燃料喷嘴包括喷嘴体，多个旋流器叶片和至少一个出口。 喷嘴体包括背板，前板和限定在其间的混合区。 背板包括限定在其中的至少一个入口，并且前板包括限定在其中的至少一个排出口。 多个旋流器叶片位于后板和前板之间并且围绕混合区周向间隔开。 多个旋流器叶片中的每一个将空气倾斜地引导到混合区域中。 所述至少一个出口限定在所述喷嘴主体和所述多个旋流器叶片中的至少一个中，所述至少一个出口构造成将燃料喷射到所述混合区域中。
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公开(公告)号：US20140338340A1
公开(公告)日：2014-11-20
申请号：US13798012
申请日：2013-03-12
Applicant: General Electric Company
Inventor： Patrick Benedict Melton , Ronald James Chila , Gregory Allen Boardman , James Harold Westmoreland
Abstract: A system includes a multi-tube fuel nozzle. The multi-tube fuel nozzle includes multiple tubes. Each tube includes a first end, a second end, and an annular wall disposed about a central passage. The first end is configured to be disposed about a fuel injector. Each tube also includes an air flow conditioner having multiple air ports disposed adjacent the first end. The multiple air ports extend through the wall into the central passage.
Abstract translation: 系统包括多管燃料喷嘴。 多管燃料喷嘴包括多个管。 每个管包括第一端，第二端和围绕中心通道设置的环形壁。 第一端构造成围绕燃料喷射器设置。 每个管还包括具有邻近第一端设置的多个空气端口的空气流调节器。 多个空气端口穿过壁延伸到中心通道中。
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公开(公告)号：US20140260299A1
公开(公告)日：2014-09-18
申请号：US13797848
申请日：2013-03-12
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Gregory Allen Boardman , Patrick Benedict Melton , James Harold Westmoreland , Ronald James Chila , Sarah Lori Crothers
IPC: F02C7/22
CPC classification number: F02C7/22 , F23D14/62 , F23D14/64 , F23R3/10 , F23R3/22 , F23R3/286 , Y02T50/675
Abstract: Embodiments of the present disclosure are directed to systems and methods for premixing fuel and air prior to combustion within a combustion chamber. The system includes a plurality of fuel injectors and a plurality of mixing tubes, wherein each mixing tube has a first portion for receiving one of the plurality of fuel injectors and a second portion having a mixing chamber that is configured to mix fuel and air. The length of the mixing chamber varies among the plurality of mixing tubes to allow for different mixing times.
Abstract translation: 本公开的实施例涉及用于在燃烧室内燃烧之前预混合燃料和空气的系统和方法。 该系统包括多个燃料喷射器和多个混合管，其中每个混合管具有用于容纳多个燃料喷射器中的一个的第一部分和具有配置为混合燃料和空气的混合室的第二部分。 混合室的长度在多个混合管之间变化，以允许不同的混合时间。
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