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公开(公告)号：US09441835B2
公开(公告)日：2016-09-13
申请号：US13647359
申请日：2012-10-08
Applicant: General Electric Company
Inventor： Brandon Taylor Overby , David Leach
CPC classification number: F23R3/02 , F23L7/00 , F23L2900/07002 , F23L2900/07009 , F23R3/286 , F23R3/36
Abstract: A system includes a gas turbine combustor configured to combust a fuel and an oxidant, such as O2 and O2 mixtures. The system also includes an aerodynamic peg disposed in the gas turbine combustor. The aerodynamic peg includes a first passage configured to convey a first fluid into the gas turbine combustor and a second passage configured to convey a second fluid into the gas turbine combustor. The first fluid and second fluid are different from one another.
Abstract translation: 一种系统包括配置成燃烧燃料和氧化剂如O2和O2混合物的燃气轮机燃烧器。 该系统还包括设置在燃气轮机燃烧器中的空气动力学栓塞。 空气动力学栓塞包括构造成将第一流体输送到燃气涡轮机燃烧器中的第一通道和被构造成将第二流体输送到燃气涡轮机燃烧器中的第二通道。 第一流体和第二流体彼此不同。
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公开(公告)号：US20140338343A1
公开(公告)日：2014-11-20
申请号：US13893721
申请日：2013-05-14
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Dereck Joseph Ouellet , Marcus Byron Huffman , Brandon Taylor Overby , Stephen Wayne Tilley
IPC: F23R3/28
CPC classification number: F23R3/60 , F23M20/005 , F23R3/286 , F23R2900/00014
Abstract: A system for vibration damping a fuel nozzle within a combustor includes a support plate, a fuel nozzle passage that extends through the support plate and a cylindrical damping insert that is coaxially aligned within the fuel nozzle passage and at least partially defines the fuel nozzle passage. The damping insert may include a metallic-mesh liner.
Abstract translation: 用于对燃烧器内的燃料喷嘴进行减振的系统包括支撑板，延伸穿过支撑板的燃料喷嘴通道和在燃料喷嘴通道内同轴对准并且至少部分地限定燃料喷嘴通道的圆柱形阻尼插入件。 阻尼插入件可以包括金属网衬垫。
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公开(公告)号：US09353952B2
公开(公告)日：2016-05-31
申请号：US13688625
申请日：2012-11-29
Applicant: General Electric Company
Inventor： Brandon Taylor Overby , Keith Cletus Belsom , Jonathan Kay Allen , Kyle Eric Benson , Patrick Benedict Melton , Richard Martin DiCintio , Lucas John Stoia , Ronnie Ray Pentecost
IPC: F23R3/48
CPC classification number: F23R3/48
Abstract: A crossfire tube assembly between adjacent combustors includes a first sleeve adapted to provide fluid communication from a first combustor and a second sleeve adapted to connect to provide fluid communication from a second combustor. The second sleeve extends at least partially inside the first sleeve. A bias is between the first and second sleeves.
Abstract translation: 相邻燃烧器之间的交火管组件包括适于提供来自第一燃烧器和适于连接以提供来自第二燃烧器的流体连通的第一燃烧器和第二套管的流体连通的第一套筒。 第二套筒至少部分地在第一套筒内部延伸。 偏置在第一和第二袖之间。
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公开(公告)号：US20140202160A1
公开(公告)日：2014-07-24
申请号：US13749661
申请日：2013-01-24
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Bryan Wesley Romig , Brandon Taylor Overby
IPC: F02C7/00
CPC classification number: F02C7/00 , F02C7/222 , F23R3/045 , F23R3/10 , F23R3/46 , F23R3/60 , F23R2900/00017 , Y02T50/675
Abstract: A system including a gas turbine engine, including a combustor configured to generate products of combustion, a turbine driven by the products of combustion from the combustor, a compressor having a compressor discharge leading into a chamber between the combustor and a compressor discharge casing, an extraction manifold coupled to the combustor, wherein the extraction manifold is fluidly coupled to the chamber.
Abstract translation: 一种包括燃气涡轮发动机的系统，包括构造成产生燃烧产物的燃烧器，由来自燃烧器的燃烧产物驱动的涡轮机，具有通向燃烧器和压缩机排出壳体之间的室中的压缩机排出口的压缩机， 抽吸歧管联接到燃烧器，其中提取歧管流体耦合到腔室。
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公开(公告)号：US20180085869A1
公开(公告)日：2018-03-29
申请号：US15278058
申请日：2016-09-28
Applicant: General Electric Company
Inventor： Todd James Gattermeyer , Stuart Craig Hanson , Brandon Taylor Overby
CPC classification number: F23R3/48 , F01D9/023 , F01D25/285 , F05D2230/64 , F05D2230/70 , F05D2230/72 , F23R2900/00017 , F23R2900/00019
Abstract: A tool kit for decoupling a telescoping tube from a first liner of a gas turbine engine is disclosed. The tool kit includes a base plate coupled to a combustor casing. A post extends outward from the base plate into a combustion chamber defined by the liner. A plunger slidably mounts to the post and is slidable between an extended position and a retracted position. A lever arm pivotably couples to the post and the plunger. Pivoting the lever arm in a first direction slides the plunger to the extended position to decouple the telescoping tube from the liner. A retaining clip couples to the combustor casing and extends into an annular plenum at least partially defined between the liner and the combustor casing. The retaining clip defines a notch that receives the telescoping tube after the plunger assembly decouples the telescoping tube from the liner.
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Patent Agency Ranking
6.发明授权Combustion casing manifold for high pressure air delivery to a fuel nozzle pilot system 有权用于高压空气输送到燃料喷嘴导向系统的燃烧套管歧管公开(公告)号：US09500367B2
公开(公告)日：2016-11-22
申请号：US14076360
申请日：2013-11-11
Applicant: General Electric Company
Inventor： Bryan Wesley Romig , Brandon Taylor Overby
Abstract: The present application provides a pilot manifold system for a combustor of a gas turbine engine. The pilot manifold system may include a casing with a casing manifold, an end cover connected to the casing and having an end cover passage in communication with the casing manifold, and a fuel nozzle mounted about the end cover. The fuel nozzle may include a pilot system in communication with the end cover passage.
Abstract translation: 本申请提供了一种用于燃气涡轮发动机的燃烧器的先导歧管系统。 先导歧管系统可以包括具有套管歧管的壳体，连接到壳体的端盖并且具有与套管歧管连通的端盖通道以及围绕端盖安装的燃料喷嘴。 燃料喷嘴可以包括与端盖通道连通的先导系统。
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公开(公告)号：US20140250981A1
公开(公告)日：2014-09-11
申请号：US13790348
申请日：2013-03-08
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Brandon Taylor Overby , James Carroll Baummer , Mark Carmine Bellino
IPC: G01M3/02
CPC classification number: G01M15/14 , F01D25/285 , F23R3/28 , F23R2900/00012 , G01M3/3281 , G01M13/005
Abstract: A seal test fixture for a gas turbine fuel nozzle including an enclosed container for receiving a body of the gas turbine fuel nozzle including a seal; a test chamber coupled to the enclosed container for sealingly enclosing a flange of the gas turbine fuel nozzle and fluidly communicating with a leak path of the gas turbine fuel nozzle; an air injector opening through which pressurized air is injected into a main fuel chamber of the gas turbine fuel nozzle; and a pressure gauge for measuring an air pressure within the test chamber.
Abstract translation: 一种用于燃气轮机燃料喷嘴的密封测试夹具，包括用于容纳包括密封件的燃气轮机燃料喷嘴的主体的封闭容器; 耦合到所述封闭容器的测试室，用于密封地封闭所述燃气轮机燃料喷嘴的凸缘并与所述燃气轮机燃料喷嘴的泄漏路径流体连通; 空气喷射器开口，加压空气通过该开口喷射到燃气轮机燃料喷嘴的主燃料室中; 以及用于测量测试室内的空气压力的压力计。
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公开(公告)号：US20140144122A1
公开(公告)日：2014-05-29
申请号：US13688625
申请日：2012-11-29
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Brandon Taylor Overby , Keith Cletus Belsom , Jonathan Kay Allen , Kyle Eric Benson , Patrick Benedict Melton , Richard Martin DiCintio , Lucas John Stoia , Ronnie Ray Pentecost
IPC: F23R3/48
CPC classification number: F23R3/48
Abstract: A crossfire tube assembly between adjacent combustors includes a first sleeve adapted to provide fluid communication from a first combustor and a second sleeve adapted to connect to provide fluid communication from a second combustor. The second sleeve extends at least partially inside the first sleeve. A bias is between the first and second sleeves.
Abstract translation: 相邻燃烧器之间的交火管组件包括适于提供来自第一燃烧器和适于连接以提供来自第二燃烧器的流体连通的第一燃烧器和第二套管的流体连通的第一套筒。 第二套筒至少部分地在第一套筒内部延伸。 偏置在第一和第二袖之间。
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9.发明申请Combustion Casing Manifold for High Pressure Air Delivery to a Fuel Nozzle Pilot System 有权用于高压空气输送到燃油喷嘴试验系统的燃烧套管歧管公开(公告)号：US20150128606A1
公开(公告)日：2015-05-14
申请号：US14076360
申请日：2013-11-11
Applicant: General Electric Company
Inventor： Bryan Wesley Romig , Brandon Taylor Overby
IPC: F23R3/28
Abstract: The present application provides a pilot manifold system for a combustor of a gas turbine engine. The pilot manifold system may include a casing with a casing manifold, an end cover connected to the casing and having an end cover passage in communication with the casing manifold, and a fuel nozzle mounted about the end cover. The fuel nozzle may include a pilot system in communication with the end cover passage.
Abstract translation: 本申请提供了一种用于燃气涡轮发动机的燃烧器的先导歧管系统。 先导歧管系统可以包括具有套管歧管的壳体，连接到壳体的端盖并且具有与套管歧管连通的端盖通道以及围绕端盖安装的燃料喷嘴。 燃料喷嘴可以包括与端盖通道连通的先导系统。
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公开(公告)号：US20140096529A1
公开(公告)日：2014-04-10
申请号：US13647359
申请日：2012-10-08
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Brandon Taylor Overby , David Leach
IPC: F23R3/02
CPC classification number: F23R3/02 , F23L7/00 , F23L2900/07002 , F23L2900/07009 , F23R3/286 , F23R3/36
Abstract: A system includes a gas turbine combustor configured to combust a fuel and an oxidant, such as O2 and O2 mixtures. The system also includes an aerodynamic peg disposed in the gas turbine combustor. The aerodynamic peg includes a first passage configured to convey a first fluid into the gas turbine combustor and a second passage configured to convey a second fluid into the gas turbine combustor. The first fluid and second fluid are different from one another.
Abstract translation: 一种系统包括配置成燃烧燃料和氧化剂如O2和O2混合物的燃气轮机燃烧器。 该系统还包括设置在燃气轮机燃烧器中的空气动力学栓塞。 空气动力学栓塞包括构造成将第一流体输送到燃气涡轮机燃烧器中的第一通道和被构造成将第二流体输送到燃气涡轮机燃烧器中的第二通道。 第一流体和第二流体彼此不同。
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