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1.发明申请公开(公告)号：US20120304648A1
公开(公告)日：2012-12-06
申请号：US13153944
申请日：2011-06-06
IPC分类号： F02C7/22
摘要： A late lean injection sleeve assembly allows the injection of fuel at the aft end of a gas turbine liner, before the transition piece, into the combustion gases downstream of a turbine combustor's fuel nozzles. The late lean injection enables fuel injection downstream of the fuel nozzles to create a secondary/tertiary (with quaternary injection upstream of the fuel nozzles) combustion zone while reducing/eliminating the risk of fuel leaking into the combustion discharge case. The fuel is delivered by the flow sleeve into one or more nozzles that mix the fuel with CDC air before injecting it into the combustor's liner.
摘要翻译： 后期的稀薄注射套筒组件允许将燃料涡轮机衬套的后端处的燃料喷射到涡轮机燃烧器的燃料喷嘴下游的燃烧气体中。 后期的稀薄喷射使得燃料喷嘴下游的燃料喷射能够在减少/消除燃料泄漏到燃烧排放情况下的风险中产生二次/三次（在燃料喷嘴的上游具有四次注入）燃烧区域。 燃料由流动套管输送到一个或多个喷嘴中，该喷嘴将燃料与CDC空气混合，然后将其注入到燃烧器的衬套内。
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2.发明授权Integrated late lean injection on a combustion liner and late lean injection sleeve assembly 有权在燃烧衬套和后期精密注射套筒组件上集成后期精馏公开(公告)号：US08601820B2
公开(公告)日：2013-12-10
申请号：US13153944
申请日：2011-06-06
摘要： A late lean injection sleeve assembly allows the injection of fuel at the aft end of a gas turbine liner, before the transition piece, into the combustion gases downstream of a turbine combustor's fuel nozzles. The late lean injection enables fuel injection downstream of the fuel nozzles to create a secondary/tertiary (with quaternary injection upstream of the fuel nozzles) combustion zone while reducing/eliminating the risk of fuel leaking into the combustor discharge case. The fuel is delivered by the flow sleeve into one or more nozzles that mix the fuel with CDC air before injecting it into the combustor's liner.
摘要翻译： 后期的稀薄注射套筒组件允许将燃料涡轮机衬套的后端处的燃料喷射到涡轮机燃烧器的燃料喷嘴下游的燃烧气体中。 后期的稀薄喷射使得燃料喷嘴下游的燃料喷射能够在减少/消除燃料泄漏到燃烧器排出壳体中的风险的同时产生二级/三级（在燃料喷嘴的上游具有四级注入）燃烧区域。 燃料由流动套管输送到一个或多个喷嘴中，该喷嘴将燃料与CDC空气混合，然后将其注入到燃烧器的衬套内。
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公开(公告)号：US09010127B2
公开(公告)日：2015-04-21
申请号：US13410417
申请日：2012-03-02
申请人： Christopher Paul Willis , William Lawrence Byrne , David William Cihlar , Donald Timothy Lemon , Patrick Benedict Melton
发明人： Christopher Paul Willis , William Lawrence Byrne , David William Cihlar , Donald Timothy Lemon , Patrick Benedict Melton
CPC分类号： F01D9/023
摘要： A transition piece aft frame assembly is provided, and includes a transition piece aft frame and a heat shield. The transition piece aft frame has an aft face. At least a portion of the aft face is exposed to an exhaust gas stream. The heat shield is connected to the transition piece aft frame. The heat shield is oriented to generally deflect the exhaust gas stream away from the aft face of the transition piece aft frame.
摘要翻译： 提供过渡件后框架组件，并且包括过渡件后框架和隔热罩。 过渡件后框架有一个后面。 后表面的至少一部分暴露于排气流。 隔热罩与过渡件后框架连接。 隔热罩被定向成使废气流大致偏离过渡件后框架的后表面。
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公开(公告)号：US08826667B2
公开(公告)日：2014-09-09
申请号：US13115018
申请日：2011-05-24
申请人： Patrick Benedict Melton , Bradley Donald Crawley , David William Cihlar , Robert Joseph Rohrssen , Ronald James Chila
发明人： Patrick Benedict Melton , Bradley Donald Crawley , David William Cihlar , Robert Joseph Rohrssen , Ronald James Chila
CPC分类号： F23R3/002 , F23R3/045 , F23R2900/03043 , Y02T50/675
摘要： A system includes a gas turbine combustor, which includes a combustion liner disposed about a combustion region, a flow sleeve disposed about the combustion liner, an air passage between the combustion liner and the flow sleeve, and a structure extending between the combustion liner and the flow sleeve. The structure obstructs an airflow path through the air passage. The gas turbine combustor also includes an aerodynamic wake reducer configured to redirect an airflow around the structure to reduce a wake region downstream of the structure.
摘要翻译： 一种系统包括燃气轮机燃烧器，其包括围绕燃烧区域设置的燃烧衬套，围绕燃烧衬套设置的流动套筒，在燃烧衬套和流动套筒之间的空气通道，以及在燃烧衬套和燃烧衬套之间延伸的结构 流动套管 该结构妨碍通过空气通道的气流路径。 燃气轮机燃烧器还包括空气动力尾流减速器，其被配置成重新定向结构周围的气流以减少结构下游的尾流区域。
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公开(公告)号：US20120210729A1
公开(公告)日：2012-08-23
申请号：US13030340
申请日：2011-02-18
CPC分类号： F23R3/002 , F01D9/023 , F05D2230/60 , F05D2260/201 , F23R3/60 , F23R2900/03044 , Y10T29/49229
摘要： A bracket for a combustor, and a method for mounting a transition piece in a combustor, are disclosed. The combustor has an impingement sleeve at least partially surrounding a transition piece and an outer casing at least partially surrounding the impingement sleeve. The bracket is mounted to the transition piece and connected to the outer casing. The method includes mounting a bracket to the transition piece, extending the bracket through an impingement sleeve, the impingement sleeve at least partially surrounding the transition piece, and connecting the bracket to an outer casing, the outer casing at least partially surrounding the impingement sleeve.
摘要翻译： 公开了一种用于燃烧器的支架，以及用于将过渡件安装在燃烧器中的方法。 燃烧器具有至少部分地围绕过渡件的冲击套管和至少部分地围绕冲击套筒的外壳。 支架安装在过渡件上并连接到外壳。 该方法包括将支架安装到过渡件上，通过冲击套筒延伸支架，冲击套筒至少部分地围绕过渡件，并将支架连接到外壳上，外壳至少部分地围绕冲击套筒。
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6.发明申请IMPINGEMENT SLEEVE AND METHODS FOR DESIGNING AND FORMING IMPINGEMENT SLEEVE 有权IMPINGEMENT SLEEVE AND METHODS FOR DESIGN AND FORMING IMPINGEMENT SLEEVE公开(公告)号：US20120234012A1
公开(公告)日：2012-09-20
申请号：US13048394
申请日：2011-03-15
申请人： Jerome David Brown , Ronald James Chila , Patrick Benedict Melton , Russell DeForest , David William Cihlar
发明人： Jerome David Brown , Ronald James Chila , Patrick Benedict Melton , Russell DeForest , David William Cihlar
CPC分类号： F01D9/023 , F05D2260/201 , F23R2900/03044 , Y10T29/49229
摘要： An impingement sleeve and methods for designing and forming an impingement sleeve are disclosed. In one embodiment, a method for designing an impingement sleeve is disclosed. The method includes determining a desired operational value for a transition piece, inputting a combustor characteristic into a processor, and utilizing the combustor characteristic in the processor to determine a cooling hole pattern for the impingement sleeve, the cooling hole pattern comprising a plurality of cooling holes, at least a portion of the plurality of cooling holes being generally longitudinally asymmetric, the cooling hole pattern providing the desired operational value.
摘要翻译： 公开了一种冲击套筒和用于设计和形成冲击套筒的方法。 在一个实施例中，公开了一种用于设计冲击套筒的方法。 该方法包括确定过渡件的期望操作值，将燃烧器特性输入到处理器中，以及利用处理器中的燃烧器特性来确定冲击套筒的冷却孔图案，冷却孔图案包括多个冷却孔 所述多个冷却孔的至少一部分大致纵向不对称，所述冷却孔图案提供期望的操作值。
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公开(公告)号：US09255484B2
公开(公告)日：2016-02-09
申请号：US13049237
申请日：2011-03-16
CPC分类号： F01D9/023 , F01D25/12 , F02C7/20 , F05D2260/201 , F05D2260/202 , F05D2260/2322 , F23R3/60 , F23R2900/00012 , F23R2900/03041 , F23R2900/03042 , F23R2900/03043 , F23R2900/03044
摘要： An aft frame and a method for cooling an aft frame are disclosed. In one embodiment, an aft frame for a transition piece in a combustor is disclosed. The combustor includes the transition piece and an impingement sleeve at least partially defining a flow path therebetween. The aft frame includes a body and a generally radially extending cooling passage defined in the body, the cooling passage comprising a first end configured to accept a coolant. The aft frame further includes an exhaust passage defined in the body, the exhaust passage including a first end in communication with the cooling passage and a second end configured for communication with the flow path for flowing the coolant therethrough.
摘要翻译： 公开了一种后框架和用于冷却后框架的方法。 在一个实施例中，公开了一种用于燃烧室中的过渡件的后框架。 该燃烧器包括过渡件和至少部分地限定其间的流动路径的冲击套筒。 后框架包括主体和限定在主体中的大致径向延伸的冷却通道，冷却通道包括构造成接受冷却剂的第一端。 后框架还包括限定在主体中的排气通道，排气通道包括与冷却通道连通的第一端和构造成与用于使冷却剂流过的流路连通的第二端。
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公开(公告)号：US20130086915A1
公开(公告)日：2013-04-11
申请号：US13267994
申请日：2011-10-07
IPC分类号： F02C7/18
CPC分类号： F23R3/002 , F01D9/023 , F05D2240/55 , F23R3/06 , F23R3/46 , F23R2900/00012 , F23R2900/03042 , F23R2900/03044
摘要： A combustion liner assembly is provided and includes a combustion liner and a transition piece. A portion of the transition piece is circumferentially disposed around a portion of the combustion liner. A seal is attached to the transition piece, and the seal is configured to apply a compressive force to an aft end of the combustion liner.
摘要翻译： 提供燃烧衬套组件并且包括燃烧衬套和过渡件。 过渡件的一部分周向地布置在燃烧衬套的一部分周围。 密封件附接到过渡件，并且密封件构造成对燃烧衬套的后端施加压缩力。
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公开(公告)号：US20120304656A1
公开(公告)日：2012-12-06
申请号：US13153836
申请日：2011-06-06
CPC分类号： F01D9/023
摘要： An apparatus is disclosed. The apparatus may include a body configured to flow hot gases of combustion between a forward end and an aft end. Additionally, the body may include a plurality of raised sections spaced apart circumferentially around an outer perimeter of the body. The raised sections may generally extend lengthwise between the forward and aft ends.
摘要翻译： 公开了一种装置。 该装置可以包括构造成在前端和后端之间流动燃烧的热气体的主体。 另外，主体可以包括围绕主体的外周缘周向间隔开的多个凸起部分。 凸起部分通常可以在前端和后端之间纵向延伸。
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公开(公告)号：US20120304652A1
公开(公告)日：2012-12-06
申请号：US13149044
申请日：2011-05-31
申请人： Bradley Donald Crawley , David William Cihlar , Patrick Benedict Melton , Frederick Millard Setzer, JR.
发明人： Bradley Donald Crawley , David William Cihlar , Patrick Benedict Melton , Frederick Millard Setzer, JR.
IPC分类号： F02C7/22
摘要： An injector apparatus is provided and includes an annular inlet in which a first fluid traveling in a first direction is mixable with a second fluid to form a mixture, an annular outlet disposed downstream from the inlet from which the mixture is injectable into a main flow in a third direction and an annular intermediate section fluidly interposed between the inlet and the outlet and along which the mixture is re-directable from the inlet to the outlet.
摘要翻译： 提供了一种注射器装置，其包括环形入口，其中在第一方向上行进的第一流体可与第二流体混合以形成混合物，设置在入口下游的环形出口，混合物从该入口可注入主流体 第三方向和流体介于入口和出口之间的环形中间部分，并且混合物可从该入口和出口重新定向。
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