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1. 发明授权

US10669942B2 Endcover assembly for a combustor 审中-公开
公开(公告)号：US10669942B2
公开(公告)日：2020-06-02
申请号：US15440561
申请日：2017-02-23
申请人： General Electric Company
发明人： Lucas John Stoia , Donald Mark Bailey , Elizabeth Leigh Exley , Heath Michael Ostebee , Timothy James Purcell
IPC分类号： F23R3/28 , F02C7/22 , F23R3/04
摘要： An endcover assembly for a combustor includes an endcover and a fuel nozzle rigidly connected to the endcover. The fuel nozzle includes a plurality of tubes that extends axially through a first plate, a fuel plenum and a second plate where each tube includes an inlet defined upstream of the first plate and an outlet disposed downstream from the second plate. The endcover assembly further includes an inlet flow conditioner having a forward end connected to the endcover and an aft end axially spaced from the forward end. The inlet flow conditioner circumferentially surrounds at least a portion of the fuel nozzle. A support plate is joined to the aft end of the inlet flow conditioner. Each tube of the fuel nozzle extends through a corresponding tube hole defined by the support plate. The fuel nozzle is connected to the support plate.

2. 发明授权

US09574533B2 Fuel injection nozzle and method of manufacturing the same 有权
标题翻译：燃油喷嘴及其制造方法
公开(公告)号：US09574533B2
公开(公告)日：2017-02-21
申请号：US13916767
申请日：2013-06-13
申请人： General Electric Company
发明人： James Christopher Monaghan , Thomas Edward Johnson , Heath Michael Ostebee
IPC分类号： B05B7/04 , B05B7/08 , F02M55/00 , F23R3/28 , F23R3/10
CPC分类号： F02M55/008 , B05B7/04 , B05B7/08 , F02M2200/80 , F23R3/10 , F23R3/28 , F23R3/286 , Y10T29/494
摘要： 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.
摘要翻译：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。

3. 发明授权

US09447975B2 Variable volume combustor with aerodynamic fuel flanges for nozzle mounting 有权
标题翻译：具有用于喷嘴安装的空气动力学燃料法兰的可变容积燃烧器
公开(公告)号：US09447975B2
公开(公告)日：2016-09-20
申请号：US13760094
申请日：2013-02-06
申请人： General Electric Company
发明人： Johnie Franklin McConnaughhay , Christopher Paul Keener , Thomas Edward Johnson , Heath Michael Ostebee
IPC分类号： F23R3/28 , F23R3/10 , F23C5/06
CPC分类号： F23R3/286 , F23C5/06 , F23R3/10 , F23R3/283
摘要： 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 for providing the flow of fuel therethrough. The fuel injection system also may include a number of aerodynamic fuel flanges connecting the micro-mixer fuel nozzles and the support struts.
摘要翻译：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，并且用于提供通过其的燃料流。燃料喷射系统还可以包括连接微混合器燃料喷嘴和支撑支柱的多个空气动力学燃料凸缘。

4. 发明授权

US09435539B2 Variable volume combustor with pre-nozzle fuel injection system 有权
标题翻译：具有预喷嘴燃油喷射系统的可变容积燃烧器
公开(公告)号：US09435539B2
公开(公告)日：2016-09-06
申请号：US13760091
申请日：2013-02-06
申请人： General Electric Company
发明人： Christopher Paul Keener , Thomas Edward Johnson , Johnie Franklin McConnaughhay , Heath Michael Ostebee
IPC分类号： F23R3/28 , F23R3/10 , F23C5/06
CPC分类号： F23R3/286 , F23C5/06 , F23R3/10 , F23R3/283
摘要： The present application provides a combustor for use with a gas turbine engine. The combustor may include a number of fuel nozzles, a pre-nozzle fuel injection system supporting the fuel nozzles, and a linear actuator to maneuver the fuel nozzles and the pre-nozzle fuel injection system.
摘要翻译：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燃料喷嘴，支撑燃料喷嘴的预喷嘴燃料喷射系统，以及用于操纵燃料喷嘴和预喷嘴燃料喷射系统的线性致动器。

5. 发明申请

US20160076578A1 NUT ANTI-ROTATION CAP 审中-公开
标题翻译： NUT防旋转盖
公开(公告)号：US20160076578A1
公开(公告)日：2016-03-17
申请号：US14485296
申请日：2014-09-12
申请人： General Electric Company
发明人： Mark Carmine Bellino , Heath Michael Ostebee , Lucas John Stoia , Christopher Paul Willis
IPC分类号： F16B39/08
CPC分类号： F16B39/08 , F16B39/02
摘要： A nut anti-rotation cap includes an end wall having an inner surface configured to be operatively coupled to an end of a threaded mechanical fastener. Also included is at least one sidewall extending from the end wall, wherein the at least one sidewall is a solid wall configured to be secured to a nut engaged with the threaded mechanical fastener and to enclose an exposed portion of the threaded mechanical fastener.
摘要翻译：螺母防旋转盖包括端壁，所述端壁具有构造成可操作地联接到螺纹机械紧固件的端部的内表面。还包括从端壁延伸的至少一个侧壁，其中至少一个侧壁是实心壁，其构造成固定到与螺纹机械紧固件接合的螺母并且包围螺纹机械紧固件的暴露部分。

6. 发明申请

US20140338356A1 System Having a Multi-Tube Fuel Nozzle with an Aft Plate Assembly 有权
标题翻译：具有具有后板组件的多管燃料喷嘴的系统
公开(公告)号：US20140338356A1
公开(公告)日：2014-11-20
申请号：US13839076
申请日：2013-03-15
申请人： GENERAL ELECTRIC COMPANY
发明人： Christopher Paul Keener , Jason Thurman Stewart , Heath Michael Ostebee
IPC分类号： F23R3/28
CPC分类号： F23R3/286 , F23R3/10 , F23R2900/00012 , Y02T50/675
摘要： A system including a first multi-tube fuel nozzle including a plurality of first tubes extending in an axial direction, wherein each first tube of the plurality of first tubes includes a first air inlet, a first fuel inlet, and a first fuel-air mixture outlet, a second multi-tube fuel nozzle including a plurality of second tubes extending in an axial direction, wherein each second tube of the plurality of second tubes includes a second air inlet, a second fuel inlet, and a second fuel-air mixture outlet, and an aft plate including a plurality of first tube apertures and a plurality of second tube apertures, wherein the plurality of first tubes extend to the plurality of first tube apertures, and the plurality of second tubes extend to the plurality of second tube apertures.
摘要翻译：一种包括第一多管燃料喷嘴的系统，所述第一多管燃料喷嘴包括沿轴向方向延伸的多个第一管，其中所述多个第一管中的每个第一管包括第一空气入口，第一燃料入口和第一燃料 - 空气混合物出口，第二多管燃料喷嘴，其包括在轴向方向上延伸的多个第二管，其中所述多个第二管中的每个第二管包括第二空气入口，第二燃料入口和第二燃料空气混合物出口以及包括多个第一管孔和多个第二管孔的后板，其中所述多个第一管延伸到所述多个第一管孔，并且所述多个第二管延伸到所述多个第二管孔。

7. 发明申请

US20140216050A1 Variable Volume Combustor with Nested Fuel Manifold System 有权
标题翻译：具有嵌套式燃油歧管系统的可变容积燃烧器
公开(公告)号：US20140216050A1
公开(公告)日：2014-08-07
申请号：US13760092
申请日：2013-02-06
申请人： GENERAL ELECTRIC COMPANY
发明人： Johnie Franklin McConnaughhay , Christopher Paul Keener , Thomas Edward Johnson , Heath Michael Ostebee
IPC分类号： F02C7/22
CPC分类号： F02C7/222 , F23R3/26 , F23R3/283 , F23R3/286 , F23R2900/00013
摘要： The present application provides a combustor for use with a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles, a fuel manifold system in communication with the micro-mixer fuel nozzles to deliver a flow of fuel thereto, and a linear actuator to maneuver the micro-mixer fuel nozzles and the fuel manifold system.
摘要翻译：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，与微混合器燃料喷嘴连通以将燃料流传递到其上的燃料歧管系统，以及用于操纵微混合器燃料喷嘴和燃料歧管的线性致动器系统。

8. 发明申请

US20140216048A1 Variable Volume Combustor 有权
标题翻译：可变容积燃烧器
公开(公告)号：US20140216048A1
公开(公告)日：2014-08-07
申请号：US13760090
申请日：2013-02-06
申请人： GENERAL ELECTRIC COMPANY
发明人： Heath Michael Ostebee , Willy Steve Ziminsky , Thomas Edward Johnson , Christopher Paul Keener
IPC分类号： F02C7/22
CPC分类号： F02C7/22 , F23C5/06 , F23R3/10 , F23R3/283 , F23R3/286
摘要： The present application provides a variable volume combustor for use with a gas turbine engine. The variable volume combustor may include a liner, a number of micro-mixer fuel nozzles positioned within the liner, and a linear actuator so as to maneuver the micro-mixer fuel nozzles axially along the liner.
摘要翻译：本申请提供了一种与燃气涡轮发动机一起使用的可变体积燃烧器。可变体积燃烧器可以包括衬套，位于衬套内的多个微混合器燃料喷嘴，以及线性致动器，以便沿着衬套轴向地操纵微混合器燃料喷嘴。

9. 发明申请

US20140216038A1 Variable Volume Combustor with Cantilevered Support Structure 审中-公开
标题翻译：具有悬臂支撑结构的可变容积燃烧器
公开(公告)号：US20140216038A1
公开(公告)日：2014-08-07
申请号：US13760093
申请日：2013-02-06
申请人： GENERAL ELECTRIC COMPANY
发明人： Christopher Paul Keener , Thomas Edward Johnson , Johnie Franklin McConnaughhay , Heath Michael Ostebee
IPC分类号： F02C7/22
CPC分类号： F23R3/283 , F23R3/286 , F23R3/46 , F23R2900/00017
摘要： The present application provides a combustor for use with a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles positioned within an end cover, a common fuel tube extending through the end cover and in communication with the micro-mixer fuel nozzles, a linear actuator to maneuver the common fuel tube and the micro-mixer fuel nozzles, and a sealing support structure positioned between the end cover and the common fuel tube.
摘要翻译：本申请提供了一种与燃气涡轮发动机一起使用的燃烧器。燃烧器可以包括位于端盖内的多个微混合燃料喷嘴，延伸穿过端盖并与微混合燃料喷嘴连通的公共燃料管，用于操纵公共燃料管和微型燃料管的线性致动器混合器燃料喷嘴和位于端盖和公共燃料管之间的密封支撑结构。

10. 发明申请

US20180238239A1 Endcover Assembly for a Combustor 审中-公开
公开(公告)号：US20180238239A1
公开(公告)日：2018-08-23
申请号：US15440561
申请日：2017-02-23
申请人： General Electric Company
发明人： Lucas John Stoia , Donald Mark Bailey , Elizabeth Leigh Exley , Heath Michael Ostebee , Timothy James Purcell
IPC分类号： F02C7/22 , F23R3/28
摘要： An endcover assembly for a combustor includes an endcover and a fuel nozzle rigidly connected to the endcover. The fuel nozzle includes a plurality of tubes that extends axially through a first plate, a fuel plenum and a second plate where each tube includes an inlet defined upstream of the first plate and an outlet disposed downstream from the second plate. The endcover assembly further includes an inlet flow conditioner having a forward end connected to the endcover and an aft end axially spaced from the forward end. The inlet flow conditioner circumferentially surrounds at least a portion of the fuel nozzle. A support plate is joined to the aft end of the inlet flow conditioner. Each tube of the fuel nozzle extends through a corresponding tube hole defined by the support plate. The fuel nozzle is connected to the support plate.

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