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1.发明授权Methods relating to integrating late lean injection into combustion turbine engines 有权将后期精益注入集成到燃气涡轮发动机中的方法公开(公告)号：US08407892B2
公开(公告)日：2013-04-02
申请号：US13204306
申请日：2011-08-05
CPC分类号： F23R3/346 , F23R3/06 , F23R3/283 , F23R3/60 , F23R2900/00012 , F23R2900/00017 , F23R2900/00018 , F23R2900/03044 , Y10T29/49316 , Y10T29/4932 , Y10T29/49323 , Y10T29/49348
摘要： The present application thus describes a method of manufacture for a late lean injection system in a combustor of a combustion turbine engine. The method may include the steps of: a) identifying a desired position within the flow assembly for a late lean injector, wherein the late lean injector comprises a late lean nozzle and a transfer tube; b) corresponding to the desired position for the late lean injector, identifying an injection point on the inner radial wall and a late lean nozzle position on the outer radial wall; c) positioning the inner radial wall and the outer radial wall in an unassembled position; d) while in the unassembled position, forming a hole through the inner radial wall at the injection point and slideably engaging the transfer tube within the hole; e) installing the late lean nozzle in the outer radial wall at the late lean nozzle position; f) positioning the inner radial wall and the outer radial wall in an assembled position; and g) connecting the transfer tube to the late lean nozzle.
摘要翻译： 因此，本申请描述了在燃气轮机的燃烧器中用于后期稀薄喷射系统的制造方法。 该方法可以包括以下步骤：a）识别用于后期稀薄注射器的流动组件内的期望位置，其中后期稀释注射器包括后倾斜喷嘴和传送管; b）对应于后期稀薄注射器的期望位置，识别内部径向壁上的注射点和外部径向壁上的后倾斜喷嘴位置; c）将内部径向壁和外部径向壁定位在未组装位置; d）在未组装位置时，在注射点处通过内部径向壁形成孔并且可滑动地接合孔内的传送管; e）在后部稀薄喷嘴位置将后部稀薄喷嘴安装在外径向壁上; f）将内径向壁和外径向壁定位在组装位置; 并且g）将传送管连接到后倾的喷嘴。
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2.发明申请METHODS RELATING TO INTEGRATING LATE LEAN INJECTION INTO COMBUSTION TURBINE ENGINES 有权将高分子注入整合到燃油涡轮发动机中的方法公开(公告)号：US20130031783A1
公开(公告)日：2013-02-07
申请号：US13204306
申请日：2011-08-05
IPC分类号： B21D53/00
CPC分类号： F23R3/346 , F23R3/06 , F23R3/283 , F23R3/60 , F23R2900/00012 , F23R2900/00017 , F23R2900/00018 , F23R2900/03044 , Y10T29/49316 , Y10T29/4932 , Y10T29/49323 , Y10T29/49348
摘要： The present application thus describes a method of manufacture for a late lean injection system in a combustor of a combustion turbine engine. The method may include the steps of: a) identifying a desired position within the flow assembly for a late lean injector, wherein the late lean injector comprises a late lean nozzle and a transfer tube; b) corresponding to the desired position for the late lean injector, identifying an injection point on the inner radial wall and a late lean nozzle position on the outer radial wall; c) positioning the inner radial wall and the outer radial wall in an unassembled position; d) while in the unassembled position, forming a hole through the inner radial wall at the injection point and slideably engaging the transfer tube within the hole; e) installing the late lean nozzle in the outer radial wall at the late lean nozzle position; f) positioning the inner radial wall and the outer radial wall in an assembled position; and g) connecting the transfer tube to the late lean nozzle.
摘要翻译： 因此，本申请描述了在燃气轮机的燃烧器中用于后期稀薄喷射系统的制造方法。 该方法可以包括以下步骤：a）识别用于后期稀薄注射器的流动组件内的期望位置，其中后期稀释注射器包括后倾斜喷嘴和传送管; b）对应于后期稀薄注射器的期望位置，识别内部径向壁上的注射点和外部径向壁上的后倾斜喷嘴位置; c）将内部径向壁和外部径向壁定位在未组装位置; d）在未组装位置时，在注射点处通过内部径向壁形成孔并且可滑动地接合孔内的传送管; e）在后部稀薄喷嘴位置将后部稀薄喷嘴安装在外径向壁上; f）将内径向壁和外径向壁定位在组装位置; 并且g）将传送管连接到后倾的喷嘴。
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3.发明授权Assemblies and apparatus related to integrating late lean injection into combustion turbine engines 有权与后期精馏注入燃气涡轮发动机相关的装置和装置公开(公告)号：US09010120B2
公开(公告)日：2015-04-21
申请号：US13204369
申请日：2011-08-05
CPC分类号： F23R3/06 , F23R3/283 , F23R3/346 , F23R3/60 , F23R2900/00012 , F23R2900/00017 , F23R2900/03044
摘要： A transfer tube for use in a late lean injection system of a combustor, wherein the combustor includes an inner radial wall, which defines a primary combustion chamber downstream of a primary fuel nozzle, and an outer radial wall, which surrounds the inner radial wall forming a flow annulus therebetween, the outer radial wall including a late lean nozzle, the transfer tube including flow directing structure that defines a fluid passageway. At a first end, the flow directing structure may include an inlet and attachment means that attach the transfer tube to the late lean nozzle. The flow directing structure may have a configuration such that the fluid passageway spans the flow annulus and positions the outlet at a desirable injection point in the inner radial wall.
摘要翻译： 一种用于燃烧器的后期稀薄注射系统的转移管，其中所述燃烧器包括限定主燃料喷嘴下游的初级燃烧室的内部径向壁和围绕形成的内部径向壁的外部径向壁 其间的流动环空，所述外部径向壁包括后倾斜的喷嘴，所述输送管包括限定流体通道的流动引导结构。 在第一端，流动引导结构可以包括将传送管附接到后部稀薄喷嘴的入口和附接装置。 流动引导结构可以具有这样的构造，使得流体通道跨越流动环空并将出口定位在内部径向壁中期望的注入点。
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4.发明授权Assemblies and apparatus related to integrating late lean injection into combustion turbine engines 有权与后期精馏注入燃气涡轮发动机相关的装置和装置公开(公告)号：US08919137B2
公开(公告)日：2014-12-30
申请号：US13204340
申请日：2011-08-05
摘要： An assembly for use in a late lean injection system of a combustor of a combustion turbine engine, wherein the combustor includes an inner radial wall, which defines a primary combustion chamber downstream of a primary fuel nozzle, and an outer radial wall, which surrounds the inner radial wall forming a flow annulus therebetween, the assembly comprising: a boss rigidly secured to the inner radial wall, the boss being configured to define a hollow passageway through the inner radial wall; a transfer tube slideably engaged within the boss; a stop formed on the transfer tube; and damping means positioned between the boss and the stop.
摘要翻译： 一种用于燃气涡轮发动机的燃烧器的后期稀注射系统的组件，其中所述燃烧器包括限定主燃料喷嘴下游的主燃烧室的内径向壁，以及外径向壁围绕 所述内部径向壁在其间形成流动环空，所述组件包括：刚性地固定到所述内部径向壁的凸台，所述凸起构造成限定通过所述内部径向壁的中空通道; 转移管可滑动地接合在所述凸台内; 形成在转移管上的止动件; 以及位于凸台和止挡件之间的阻尼装置。
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公开(公告)号：US20130269820A1
公开(公告)日：2013-10-17
申请号：US13446751
申请日：2012-04-13
CPC分类号： F01D9/023 , F05D2230/00 , F05D2250/70 , G06F17/5009 , G06F17/5086 , G06F2217/80 , Y10T29/49234
摘要： Disclosed herein are apparatuses, methods, and systems for transition piece contouring. In an embodiment, a high thermal stress section of a transition piece and a low thermal stress section of a transition piece is a determined The low thermal stress section of the transition piece may be contoured to intercept hot gas flow.
摘要翻译： 本文公开了用于过渡件轮廓加工的装置，方法和系统。 在一个实施例中，确定过渡件的高热应力部分和过渡件的低热应力部分。过渡件的低热应力部分可以被轮廓化以截取热气流。
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6.发明申请公开(公告)号：US20130232986A1
公开(公告)日：2013-09-12
申请号：US13417409
申请日：2012-03-12
CPC分类号： F23R3/28 , F02C7/222 , F05D2260/231 , F05D2260/941 , F23R2900/00005
摘要： A combustor includes a combustion chamber and a casing that circumferentially surrounds the combustion chamber to at least partially define an annular passage between the casing and the combustion chamber. A fuel plenum extends radially through the casing to provide fluid communication through the casing to the annular passage, and a liner extends inside at least a portion of the fuel plenum to prevent fuel from directly impinging upon at least a portion of the fuel plenum. A method of reducing thermal stresses in a combustor includes flowing a fuel inside a fuel plenum that extends radially through a casing, shielding at least a portion of the fuel plenum from direct impingement by the fuel radially inward of the casing, and flowing the fuel from the fuel plenum into an annular passage between the casing and a combustion chamber.
摘要翻译： 燃烧器包括燃烧室和围绕燃烧室的壳体，以至少部分地限定壳体和燃烧室之间的环形通道。 燃料增压室径向地延伸穿过壳体以提供通过壳体到环形通道的流体连通，并且衬套在燃料增压室的至少一部分内部延伸，以防止燃料直接撞击在燃料增压室的至少一部分上。 一种降低燃烧器中的热应力的方法包括将燃料通过一个径向延伸穿过壳体的燃料增压室流动，从而屏蔽至少一部分燃料压力室不受壳体径向向内的燃料的直接冲击，并使燃料从 燃料增压室进入壳体和燃烧室之间的环形通道。
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公开(公告)号：US09127553B2
公开(公告)日：2015-09-08
申请号：US13446751
申请日：2012-04-13
IPC分类号： F01D9/02
CPC分类号： F01D9/023 , F05D2230/00 , F05D2250/70 , G06F17/5009 , G06F17/5086 , G06F2217/80 , Y10T29/49234
摘要： Disclosed herein are apparatuses, methods, and systems for transition piece contouring. In an embodiment, a high thermal stress section of a transition piece and a low thermal stress section of a transition piece is a determined. The low thermal stress section of the transition piece may be contoured to intercept hot gas flow.
摘要翻译： 本文公开了用于过渡件轮廓加工的装置，方法和系统。 在一个实施例中，确定过渡件的高热应力部分和过渡件的低热应力部分。 过渡件的低热应力部分可以是轮廓以拦截热气流。
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8.发明申请ASSEMBLIES AND APPARATUS RELATED TO INTEGRATING LATE LEAN INJECTION INTO COMBUSTION TURBINE ENGINES 有权集成和装置相关的整体升级注入燃油涡轮发动机公开(公告)号：US20130031906A1
公开(公告)日：2013-02-07
申请号：US13204340
申请日：2011-08-05
IPC分类号： F23R3/42
摘要： An assembly for use in a late lean injection system of a combustor of a combustion turbine engine, wherein the combustor includes an inner radial wall, which defines a primary combustion chamber downstream of a primary fuel nozzle, and an outer radial wall, which surrounds the inner radial wall forming a flow annulus therebetween, the assembly comprising: a boss rigidly secured to the inner radial wall, the boss being configured to define a hollow passageway through the inner radial wall; a transfer tube slideably engaged within the boss; a stop formed on the transfer tube; and damping means positioned between the boss and the stop.
摘要翻译： 一种用于燃气涡轮发动机的燃烧器的后期稀注射系统的组件，其中所述燃烧器包括限定主燃料喷嘴下游的主燃烧室的内径向壁，以及外径向壁围绕 所述内部径向壁在其间形成流动环空，所述组件包括：刚性地固定到所述内部径向壁的凸台，所述凸起构造成限定通过所述内部径向壁的中空通道; 转移管可滑动地接合在所述凸台内; 形成在转移管上的止动件; 以及位于凸台和止挡件之间的阻尼装置。
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9.发明授权System for supplying a fuel and a working fluid through a liner to a combustion chamber 有权用于将燃料和工作流体通过衬套供应到燃烧室的系统公开(公告)号：US09151500B2
公开(公告)日：2015-10-06
申请号：US13420715
申请日：2012-03-15
申请人： Wei Chen , Patrick Benedict Melton , Russell DeForest , Lucas John Stoia , Richard Martin DiCintio
发明人： Wei Chen , Patrick Benedict Melton , Russell DeForest , Lucas John Stoia , Richard Martin DiCintio
摘要： A system for supplying a working fluid to a combustor includes a combustion chamber and a flow sleeve that circumferentially surrounds at least a portion of the combustion chamber. A tube provides fluid communication for the working fluid to flow through the flow sleeve and into the combustion chamber, wherein the tube comprises an axial centerline. A first set of injectors are circumferentially arranged around the tube and angled radially with respect to the axial centerline of the tube, wherein the first set of injectors provide fluid communication for the working fluid to flow through a wall of the tube.
摘要翻译： 用于向燃烧器供应工作流体的系统包括燃烧室和周向围绕燃烧室的至少一部分的流动套管。 管提供流体连通以使工作流体流过流动套筒并进入燃烧室，其中管包括轴向中心线。 第一组喷射器围绕管周向布置并且相对于管的轴向中心线径向成角度，其中第一组喷射器为工作流体提供流体连通以流过管的壁。
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公开(公告)号：US20140014792A1
公开(公告)日：2014-01-16
申请号：US13548263
申请日：2012-07-13
申请人： Christopher Paul Willis , Patrick Benedict Melton , Lucas John Stoia , Richard Martin DiCintio , David William Cihlar
发明人： Christopher Paul Willis , Patrick Benedict Melton , Lucas John Stoia , Richard Martin DiCintio , David William Cihlar
CPC分类号： F16B41/002 , F16B43/005
摘要： A fastener assembly configured for use within an opening defined in a transition piece bracket is disclosed. The fastener assembly may generally include a fastener having a head configured to be positioned proximal to a first end of the opening and a body. The body may include a shank portion, a threaded portion opposite the shank portion and a recessed portion defined between the shank portion and the threaded portion. The fastener assembly may also include a retention member configured to be positioned within the opening adjacent the recessed portion such that the retention member engages at least one of the shank portion or the threaded portion as the fastener is moved within the opening. In addition, the fastener assembly may include a biasing member engaged against the retention member. The biasing member may be configured to bias the head of the fastener away from the first end of the opening.
摘要翻译： 公开了一种构造用于在过渡件支架中限定的开口内使用的紧固件组件。 紧固件组件通常可以包括紧固件，该紧固件具有被配置成邻近开口的第一端定位的头部和主体。 主体可以包括柄部分，与柄部分相对的螺纹部分和限定在柄部分和螺纹部分之间的凹部。 紧固件组件还可以包括保持构件，该保持构件构造成邻近凹部部分定位在开口内，使得当紧固件在开口内移动时，保持构件接合柄部分或螺纹部分中的至少一个。 另外，紧固件组件可以包括抵靠保持构件接合的偏置构件。 偏置构件可以构造成将紧固件的头部偏离开口的第一端。
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