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91. 发明申请

US20140000265A1 TRANSITION DUCT FOR A GAS TURBINE 有权
标题翻译：用于气体涡轮的过渡式导管
公开(公告)号：US20140000265A1
公开(公告)日：2014-01-02
申请号：US13534744
申请日：2012-06-27
申请人： John Alfred Simo , Patrick Benedict Melton , Richard Martin DiCintio , Christopher Paul Willis
发明人： John Alfred Simo , Patrick Benedict Melton , Richard Martin DiCintio , Christopher Paul Willis
IPC分类号： F23R3/26
CPC分类号： F01D9/023 , F01D25/28 , F23R3/60
摘要： A transition duct for a combustor of a gas turbine generally includes a transition duct having a frame at an aft end of the transition duct. The frame generally includes a downstream end, a radially outer portion, a radially inner portion opposed to the radially outer portion, a first side portion between the radially outer and inner portions, and a second side portion opposed to the first side portion. A slot in the first side portion of the frame may have a downstream surface adjacent to the downstream end of the frame. A heat shield having an inner surface, an outer surface and a plurality of spacers may extend generally outward from the heat shield inner surface such that the inner surface is adjacent to the slot downstream surface and the frame downstream end.
摘要翻译：用于燃气涡轮机的燃烧器的过渡管道通常包括在过渡管道的后端具有框架的过渡管道。框架通常包括下游端，径向外部，与径向外部相对的径向内部，径向外部和内部之间的第一侧部以及与第一侧部相对的第二侧部。框架的第一侧部分中的槽可以具有与框架的下游端相邻的下游表面。具有内表面，外表面和多个间隔件的隔热罩可以从隔热罩内表面大致向外延伸，使得内表面邻近槽下游表面和框架下游端。

92. 发明申请

US20130318976A1 TURBOMACHINE COMBUSTOR NOZZLE AND METHOD OF FORMING THE SAME 审中-公开
标题翻译：涡轮搅拌机喷嘴及其形成方法
公开(公告)号：US20130318976A1
公开(公告)日：2013-12-05
申请号：US13482584
申请日：2012-05-29
申请人： Patrick Benedict Melton , Lucas John Stoia , James Harold Westmoreland
发明人： Patrick Benedict Melton , Lucas John Stoia , James Harold Westmoreland
IPC分类号： F23R3/28 , B23P11/00 , F02C3/04 , F23R3/10
CPC分类号： F23D14/62 , F23R3/283 , F23R3/286 , F23R2900/00018 , Y10T29/49323
摘要： A turbomachine combustor nozzle includes a first plate member having a first plurality of openings, and a second plate member having a second plurality of openings that are configured and disposed to be in alignment with the first plurality of openings. A plurality of nozzle members extends through corresponding ones of the first plurality of openings and the second plurality of openings. Each of the plurality of nozzle members includes a solid core.
摘要翻译：涡轮机燃烧器喷嘴包括具有第一多个开口的第一板构件和具有第二多个开口的第二板构件，第二多个开口被构造和设置成与第一多个开口对准。多个喷嘴构件延伸穿过第一多个开口和第二多个开口中的相应的开口。多个喷嘴构件中的每一个包括实芯。

93. 发明授权

US08567199B2 Method and apparatus of introducing diluent flow into a combustor 有权
标题翻译：将稀释剂流引入燃烧器的方法和装置
公开(公告)号：US08567199B2
公开(公告)日：2013-10-29
申请号：US12250995
申请日：2008-10-14
申请人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Patrick Benedict Melton
发明人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Patrick Benedict Melton
IPC分类号： F02C3/20
CPC分类号： F23R3/28 , F23L7/00 , F23L2900/07002 , F23L2900/07009
摘要： Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. A plurality of injection holes extend through the at least one fuel nozzle and are configured to meter a flow of diluent into the combustor. Further disclosed is a method for providing diluent to a combustor including providing a plurality of openings located at at least one fuel nozzle extending through a through hole in a baffle plate. The diluent is flowed through the plurality of openings toward at least one airflow opening in the at least one fuel nozzle.
摘要翻译：公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。多个喷射孔延伸穿过至少一个燃料喷嘴，并被配置成计量稀释剂流入燃烧器的流量。还公开了一种用于向燃烧器提供稀释剂的方法，包括提供多个位于至少一个延伸穿过挡板中的通孔的燃料喷嘴的开口。稀释剂通过多个开口朝向至少一个燃料喷嘴中的至少一个气流开口流动。

94. 发明申请

US20130272863A1 Transition Piece Cross Sectional Area Convergence Reduction And Selection 审中-公开
标题翻译：过渡段横截面收敛减少和选择
公开(公告)号：US20130272863A1
公开(公告)日：2013-10-17
申请号：US13446718
申请日：2012-04-13
申请人： Richard Martin DiCintio , Patrick Benedict Melton
发明人： Richard Martin DiCintio , Patrick Benedict Melton
IPC分类号： F01D9/02 , B21D53/00
CPC分类号： F01D9/023 , F05D2250/50 , Y10T29/49323
摘要： Disclosed herein are apparatuses, methods, and systems for cross sectional area convergence reduction and selection. In an embodiment, an aft end cross sectional area is determined for a transition piece and a forward end cross sectional area is determined for the transition piece. The transition piece may be fabricated based on a constant slope of cross sectional area change between the aft end and the forward end.
摘要翻译：本文公开了用于横截面积收敛减少和选择的装置，方法和系统。在一个实施例中，对于过渡件确定后端横截面面积，并且为过渡件确定前端横截面面积。可以基于后端和前端之间的横截面积变化的恒定斜率来制造过渡件。

95. 发明申请

US20130241089A1 Micromixer Combustion Head End Assembly 有权
标题翻译：微混合器燃烧头端组件
公开(公告)号：US20130241089A1
公开(公告)日：2013-09-19
申请号：US13423894
申请日：2012-03-19
申请人： James Harold Westmoreland , Patrick Benedict Melton
发明人： James Harold Westmoreland , Patrick Benedict Melton
IPC分类号： B01F5/04 , B01F3/04
CPC分类号： F23R3/286
摘要： Embodiments of the present application can provide systems and methods for a micromixer combustion head end assembly. The micromixer may include one or more base nozzle structures. The base nozzle structures may include coaxial tubes. The coaxial tubes may include an inner tube and an outer tube. The micromixer may also include one or more segmented mixing tube bundles at least partially supported by a respective base nozzle structure. Moreover, the micromixer may include an end cap assembly disposed about the one or more segmented mixing tube bundles.
摘要翻译：本申请的实施例可以提供用于微混合器燃烧头端组件的系统和方法。微混合器可以包括一个或多个基本喷嘴结构。基座喷嘴结构可以包括同轴管。同轴管可包括内管和外管。微混合器还可以包括至少部分由相应的基座喷嘴结构支撑的一个或多个分段的混合管束。此外，微混合器可以包括围绕一个或多个分段的混合管束设置的端盖组件。

96. 发明申请

US20130234396A1 Transition Piece Aft-Frame Seals 审中-公开
标题翻译：过渡件后框密封件
公开(公告)号：US20130234396A1
公开(公告)日：2013-09-12
申请号：US13416496
申请日：2012-03-09
申请人： Christopher Paul Willis , Patrick Benedict Melton , John Alfred Simo
发明人： Christopher Paul Willis , Patrick Benedict Melton , John Alfred Simo
IPC分类号： F02C7/28 , F16J15/02 , F02C7/12
CPC分类号： F01D9/023 , F05D2240/55
摘要： A transition piece aft-frame seal assembly may include an elongate body including a first side and a second side. The seal assembly may also include at least one feed hole disposed on the first side of the body. The seal assembly may also include at least one passageway extending through the body from the first side to the second side and in communication with the at least one feed hole. Moreover, the seal assembly may include at least one cooling hole disposed at the second side of the body and in communication with the at least one passageway. A flow of cooling fluid may enter the at least one feed hole, the at least one passageway, and the at least one cooling hole, wherein the at least one cooling hole directs the flow of cooling fluid to a recirculation zone about adjacent transition piece aft-frame assemblies.
摘要翻译：过渡件后框架密封组件可以包括包括第一侧和第二侧的细长主体。密封组件还可以包括设置在主体的第一侧上的至少一个进给孔。密封组件还可以包括至少一个从第一侧延伸穿过主体到第二侧并与至少一个进给孔连通的通道。此外，密封组件可以包括设置在主体的第二侧并与至少一个通道连通的至少一个冷却孔。冷却流体流可以进入至少一个进料孔，至少一个通道和至少一个冷却孔，其中至少一个冷却孔将冷却流体的流引导到相邻过渡件后部的再循环区域框架装配。

97. 发明授权

US08528839B2 Combustor nozzle and method for fabricating the combustor nozzle 有权
标题翻译：燃烧器喷嘴及其制造方法
公开(公告)号：US08528839B2
公开(公告)日：2013-09-10
申请号：US13009108
申请日：2011-01-19
申请人： Donald Mark Bailey , William Lawrence Byrne , Patrick Benedict Melton
发明人： Donald Mark Bailey , William Lawrence Byrne , Patrick Benedict Melton
IPC分类号： F02C7/22
CPC分类号： B22D25/00 , F23C2900/07001 , F23D2900/00008 , F23R3/14 , F23R3/286 , F23R2900/00018 , Y02T50/675
摘要： A combustor nozzle includes a single-piece swirler. The single-piece swirler includes a center body extending axially along the single-piece swirler, a first fuel passage inside the center body, and a plurality of vanes extending radially from the center body. A method for fabricating a combustor nozzle includes casting a single-piece swirler having a center body and a plurality of vanes extending radially from the center body.
摘要翻译：燃烧器喷嘴包括单件旋流器。单件旋流器包括沿着单件旋流器轴向延伸的中心体，中心体内的第一燃料通道和从中心体径向延伸的多个叶片。一种用于制造燃烧器喷嘴的方法包括浇铸具有中心体的单件旋流器和从中心体径向延伸的多个叶片。

98. 发明申请

US20130180253A1 SYSTEM AND METHOD FOR SUPPLYING A WORKING FLUID TO A COMBUSTOR 审中-公开
标题翻译：向工作人员提供工作流体的系统和方法
公开(公告)号：US20130180253A1
公开(公告)日：2013-07-18
申请号：US13349886
申请日：2012-01-13
申请人： Lucas John Stoia , Patrick Benedict Melton , Roy Marshall Washam
发明人： Lucas John Stoia , Patrick Benedict Melton , Roy Marshall Washam
IPC分类号： F23R3/28
CPC分类号： F23R3/04 , F23R3/346
摘要： A system for supplying a working fluid to a combustor includes a fuel nozzle, a combustion chamber, and fuel injectors circumferentially arranged around the combustion chamber. A combustor casing surrounds the combustion chamber. A distribution manifold encloses the fuel injectors, and a plenum passes through the combustor casing. A method for supplying a working fluid to a combustor includes flowing a working fluid from a compressor through a combustion chamber, diverting a portion of the working fluid into a plenum, and flowing the diverted portion of the working fluid outside of the compressor and the combustor. The method further includes flowing the diverted portion of the working fluid through a combustor casing and through a distribution manifold that encloses fuel injectors circumferentially arranged around the combustion chamber.
摘要翻译：用于向燃烧器供应工作流体的系统包括燃料喷嘴，燃烧室和围绕燃烧室周向布置的燃料喷射器。燃烧器壳体围绕燃烧室。分配歧管围绕燃料喷射器，并且气室通过燃烧器壳体。将工作流体供给到燃烧器的方法包括使来自压缩机的工作流体流过燃烧室，将工作流体的一部分转移到集气室中，并使工作流体的转向部分流出压缩机和燃烧器外部。该方法还包括使工作流体的转向部分流过燃烧器壳体并且通过围绕燃烧室周向布置的围绕燃料喷射器的分配歧管流动。

99. 发明申请

US20130174561A1 Late Lean Injection System Transition Piece 有权
标题翻译：后精益注射系统过渡件
公开(公告)号：US20130174561A1
公开(公告)日：2013-07-11
申请号：US13346054
申请日：2012-01-09
申请人： Lucas John Stoia , Patrick Benedict Melton
发明人： Lucas John Stoia , Patrick Benedict Melton
IPC分类号： F23R3/28 , F23R3/42
CPC分类号： F01D9/023 , F02C7/222 , F23R3/283 , F23R3/286 , F23R3/346 , F23R2900/03044
摘要： A late lean injection system transition piece includes a flowsleeve interface extending circumferentially around a transition interior. Also included is an impingement sleeve mounting surface extending circumferentially around the transition interior. Further included is a plurality of fuel injectors integrated substantially within the transition piece and disposed between the flowsleeve interface and the impingement sleeve mounting surface. Yet further included is an inner surface extending circumferentially around the transition interior, wherein the inner surface is spaced radially inward of the flowsleeve interface and the impingement sleeve mounting surface.
摘要翻译：后期的稀薄注射系统过渡件包括围绕过渡内部周向延伸的流动界面。还包括围绕过渡内部周向延伸的冲击套筒安装表面。还包括多个基本上集成在过渡件内并且设置在流动接口和冲击套筒安装表面之间的燃料喷射器。还包括一个围绕过渡内部周向延伸的内表面，其中内表面沿流动界面和冲击套筒安装表面径向向内间隔开。

100. 发明申请

US20130167542A1 FLOWSLEEVE OF A TURBOMACHINE COMPONENT 有权
标题翻译：涡轮机组件的流量
公开(公告)号：US20130167542A1
公开(公告)日：2013-07-04
申请号：US13343200
申请日：2012-01-04
申请人： Lucas John Stoia , Russell Pierson DeForest , Patrick Benedict Melton
发明人： Lucas John Stoia , Russell Pierson DeForest , Patrick Benedict Melton
IPC分类号： F02C7/22
CPC分类号： F23R3/286 , F23R3/346 , F23R3/54
摘要： A flowsleeve of a turbomachine component is provided. The flowsleeve includes an annular body including an upstream casing and a downstream casing. The upstream casing defines a fuel feed, and the downstream casing defines an airway opening, and a premixing passage. The premixing passage is fluidly coupled to the fuel feed and the airway opening and has a passage interior in which fuel and air receivable from the fuel feed and the airway opening, respectively, are combinable to form a fuel and air mixture.
摘要翻译：提供涡轮机组件的流动。流水线包括包括上游壳体和下游壳体的环形体。上游壳体限定燃料供给，并且下游壳体限定气道开口和预混合通道。预混合通道流体地联接到燃料进料和气道开口并且具有通道内部，分别从燃料进料和气道开口接收的燃料和空气可组合以形成燃料和空气混合物。

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