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公开(公告)号：US09869279B2
公开(公告)日：2018-01-16
申请号：US14067559
申请日：2013-10-30
Inventor： Lucas John Stoia , Richard Martin DiCintio , Patrick Benedict Melton , Bryan Wesley Romig , Ilya Aleksandrovich Slobodyanskiy
IPC: F02C3/00 , F02C9/00 , F23R3/46 , F02M25/07 , F02C3/34 , F23C9/00 , F23R3/00 , F23R3/06 , F02M26/19 , F02C3/13
CPC classification number: F02M26/19 , F02C3/13 , F02C3/34 , F23C9/00 , F23R3/005 , F23R3/06 , F23R3/46 , F23R2900/03044 , F23R2900/03045 , Y02E20/16 , Y02T50/675
Abstract: A system includes a turbine combustor, which includes a first wall disposed about a combustion chamber, a second wall disposed about the first wall, and a third wall disposed about the second wall. The third wall is configured to combine an exhaust gas with an oxidant and the combustion chamber is configured to combust a mixture of a fuel, the oxidant, and the exhaust gas.
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公开(公告)号：US20170254540A1
公开(公告)日：2017-09-07
申请号：US15061369
申请日：2016-03-04
Applicant: General Electric Company
Inventor： Richard Martin DiCintio , Seth Reynolds Hoffman
CPC classification number: F23R3/283 , F02C7/222 , F02C7/228 , F05D2220/32 , F05D2240/35 , F05D2260/30 , F23R3/346 , F23R2900/00017
Abstract: A spacer is provided. The spacer includes a substantially ring-shaped frame that defines an opening therein having a radius. The spacer also includes a plurality of fins having an arcuate shape and extending a distance generally radially inward from the frame for tangentially supporting a conduit extending through the opening.
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公开(公告)号：US20170227225A1
公开(公告)日：2017-08-10
申请号：US15019713
申请日：2016-02-09
Applicant: General Electric Company
Abstract: A fuel injector is provided. The fuel injector includes a manifold and a housing coupled to the manifold. The housing defines an interior chamber therein. The fuel injector also includes a nozzle positioned within the interior chamber. The nozzle includes an array of mixing tubes that each have a proximal end, a distal end, and a perforated body extending therebetween. The proximal ends are coupled in flow communication with the manifold such that the perforations of each body are in flow communication with the interior chamber to facilitate discharging a mixture of fuel and compressed gas from the distal ends.
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Patent Agency Ranking
公开(公告)号：US20170226929A1
公开(公告)日：2017-08-10
申请号：US15019459
申请日：2016-02-09
Applicant: General Electric Company
Inventor： Seth Reynolds Hoffman , Richard Martin DiCintio , Jayaprakash Natarajan , Wei Chen
CPC classification number: F02C7/22 , F02C3/14 , F05D2220/32 , F05D2230/00 , F05D2240/35 , F23R3/10 , F23R3/346
Abstract: A fuel injector cover is provided. The fuel injector cover includes a top wall and a plurality of side walls projecting from the top wall and partially defining an open bottom opposite the top wall. The open bottom is sized to receive a fuel injector therein. The fuel injector cover also includes an array of flow apertures formed in at least one of the top wall and the side walls to facilitate gas flow into the cover through the flow apertures.
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公开(公告)号：US09631812B2
公开(公告)日：2017-04-25
申请号：US13845661
申请日：2013-03-18
Applicant: General Electric Company
Inventor： Lucas John Stoia , Richard Martin DiCintio , William Michael Poschel , Patrick Benedict Melton
CPC classification number: F23R3/00 , B25B11/02 , F23R3/60 , F23R2900/00017 , F23R2900/00019 , Y10T29/4932 , Y10T29/53961
Abstract: A support frame for assembling a combustion module for a gas turbine includes a base plate disposed at a bottom end of the support frame and a support plate that is vertically separated from the base plate by one or more vertical support members. The support plate defines an opening that is sized to allow a portion of the combustion module to pass therethrough. A support block extends vertically from the base plate towards the support plate where the support block defines one or more fastener holes for connecting an aft end of a combustion liner of the combustion module to the support block. A central support column extends vertically from the base plate towards the support plate. A horizontal support extends radially outward from the central support column to align the combustion liner with the opening in the support plate.
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66.发明授权公开(公告)号：US09335052B2
公开(公告)日：2016-05-10
申请号：US13672248
申请日：2012-11-08
Applicant: General Electric Company
Inventor： Richard Martin DiCintio
IPC: F23R3/48 , F23R3/60 , F23C6/02 , F16L37/088
CPC classification number: F23R3/48 , F16L37/088 , F23C6/02 , F23R3/60 , Y10T29/49323
Abstract: According to one aspect of the invention, a combustor assembly for a pair of adjacent combustors includes a first passage formed in a liner of a first combustor and a flow sleeve disposed outside the liner of the first combustor, wherein the flow sleeve includes a window and a second passage aligned with the first passage. The assembly also includes a cross-fire tube disposed in the first passage to provide fluid communication between the first combustor and a second combustor and a retention clip disposed through the window to urge the cross-fire tube against an outer surface of the liner to enable the cross-fire tube to receive fluid through the first passage.
Abstract translation: 根据本发明的一个方面，用于一对相邻的燃烧器的燃烧器组件包括形成在第一燃烧器的衬套中的第一通道和设置在第一燃烧器的衬套外部的流动套筒，其中流动套筒包括窗口和 与第一通道对准的第二通道。 组件还包括布置在第一通道中的交叉火管，以在第一燃烧器和第二燃烧器之间提供流体连通，以及通过窗口设置的保持夹，以将交叉火管推压到衬套的外表面上以使得能够 交叉火焰管通过第一通道接收流体。
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67.发明申请SUPPORT FRAME AND METHOD FOR ASSEMBLY OF A COMBUSTION MODULE OF A GAS TURBINE 有权支撑框架和组装燃气涡轮机燃烧模块的方法公开(公告)号：US20140360193A1
公开(公告)日：2014-12-11
申请号：US13845661
申请日：2013-03-18
Applicant: General Electric Company
Inventor： Lucas John Stoia , Richard Martin DiCintio , William Michael Poschel , Patrick Benedict Melton
CPC classification number: F23R3/00 , B25B11/02 , F23R3/60 , F23R2900/00017 , F23R2900/00019 , Y10T29/4932 , Y10T29/53961
Abstract: A support frame for assembling a combustion module for a gas turbine includes a base plate disposed at a bottom end of the support frame and a support plate that is vertically separated from the base plate by one or more vertical support members. The support plate defines an opening that is sized to allow a portion of the combustion module to pass therethrough. A support block extends vertically from the base plate towards the support plate where the support block defines one or more fastener holes for connecting an aft end of a combustion liner of the combustion module to the support block. A central support column extends vertically from the base plate towards the support plate. A horizontal support extends radially outward from the central support column to align the combustion liner with the opening in the support plate.
Abstract translation: 用于组装用于燃气轮机的燃烧模块的支撑框架包括设置在支撑框架的底端处的基板和通过一个或多个垂直支撑构件与基板垂直分离的支撑板。 支撑板限定了一个开口，其尺寸被设计成允许燃烧模块的一部分通过。 支撑块从基板向支撑板垂直延伸，其中支撑块限定一个或多个紧固件孔，用于将燃烧模块的燃烧衬套的后端连接到支撑块。 中心支撑柱从基板向支撑板垂直延伸。 水平支撑件从中心支撑柱径向向外延伸，以将燃烧衬套与支撑板中的开口对准。
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公开(公告)号：US20140123660A1
公开(公告)日：2014-05-08
申请号：US14067559
申请日：2013-10-30
Inventor： Lucas John Stoia , Richard Martin DiCintio , Patrick Benedict Melton , Bryan Wesley Romig , Ilya Aleksandrovich Slobodyanskiy
IPC: F02M25/07
CPC classification number: F02M26/19 , F02C3/13 , F02C3/34 , F23C9/00 , F23R3/005 , F23R3/06 , F23R3/46 , F23R2900/03044 , F23R2900/03045 , Y02E20/16 , Y02T50/675
Abstract: A system includes a turbine combustor, which includes a first wall disposed about a combustion chamber, a second wall disposed about the first wall, and a third wall disposed about the second wall. The third wall is configured to combine an exhaust gas with an oxidant and the combustion chamber is configured to combust a mixture of a fuel, the oxidant, and the exhaust gas.
Abstract translation: 一种系统包括涡轮机燃烧器，其包括围绕燃烧室设置的第一壁，围绕第一壁设置的第二壁和围绕第二壁布置的第三壁。 第三壁构造成将废气与氧化剂组合，并且燃烧室被配置为燃烧燃料，氧化剂和废气的混合物。
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