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31.发明授权Premixing burner with impingement cooled centerbody and method of cooling centerbody 失效具有冲击冷却中心体的预混合燃烧器和冷却中心体的方法公开(公告)号：US07007477B2
公开(公告)日：2006-03-07
申请号：US10859232
申请日：2004-06-03
IPC分类号： F23R3/32
摘要： A gas-air premixing burner for gas turbines includes an air swirler and an annular burner tube surrounding a bluff centerbody. The bluff body serves to stabilize the flame by defining a recirculating vortex. Cooling air is directed to impinge against the bluff face of the centerbody and the spent impingement cooling air flows in a reverse direction towards the air swirler within the centerbody and is discharged through holes at the outer diameter of the centerbody, where it mixes with the fuel/air mixture prior to reaching the flame zone.
摘要翻译： 用于燃气轮机的气体 - 空气预混合燃烧器包括一个空气旋流器和一个围绕着虚张声势中心体的环形燃烧器管。 非流线形体用于通过限定再循环涡流来稳定火焰。 冷却空气被引导以撞击中心体的虚张声光的表面，而消耗的冲击冷却空气朝向中心体内的空气旋流器的相反方向流动，并且通过中心体的外径处的孔排出，其中与燃料混合 /空气混合物到达火焰区域。
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公开(公告)号：US08365535B2
公开(公告)日：2013-02-05
申请号：US12368011
申请日：2009-02-09
IPC分类号： F02C1/00
摘要： A fuel nozzle manifold comprising a flange, a stem and a swirler is provided. The flange has a first fluid inlet fluidly connected to a radially extending first flow passage, the stem includes at least a first axially extending and only partially circumferentially extending flow channel, and the swirler has at least a first radially extending premix passage. The flange and the stem can comprise a homogeneous component, or two separate components fluidly connecting the first axially extending flow channel to the first flow passage, to form a fluid connection between the flange and the stem, the swirler comprises another component fitted together with the flange and stem component and fluidly connecting the first premix passage and the first flow channel.
摘要翻译： 提供了一种包括凸缘，杆和旋流器的燃料喷嘴歧管。 所述凸缘具有流体连接到径向延伸的第一流动通道的第一流体入口，所述杆包括至少第一轴向延伸且仅部分周向延伸的流动通道，并且所述旋流器具有至少第一径向延伸的预混合通道。 凸缘和杆可以包括均匀的部件或两个分开的部件，其将第一轴向延伸的流动通道流体地连接到第一流动通道，以在凸缘和阀杆之间形成流体连接，旋流器包括与 法兰和阀杆部件，并且流体地连接第一预混合通道和第一流动通道。
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公开(公告)号：US08353150B2
公开(公告)日：2013-01-15
申请号：US13491291
申请日：2012-06-07
IPC分类号： F02C1/00
CPC分类号： F23R3/286 , F23D14/82 , F23D2209/10 , F23D2900/14004
摘要： A nozzle is provided and includes an outer annulus defined by an exterior wall and an interior wall and including air inlets through which air flows to a fuel mixing zone and a combustion zone, an inner annulus disposed within the interior wall and including a fuel volume into which fuel is fed to a distal end thereof, which is adjacent to and isolated from the combustion zone and an airflow line, disposed between the fuel volume and the interior wall, through which air flows to the combustion zone with the airflow line and the combustion zone isolated from the fuel volume, and a fuse configured to melt during a flameholding incident and to form a breach through which fuel flows from the fuel volume, bypassing the fuel mixing zone, to a fuel burning zone downstream from the fuel mixing zone.
摘要翻译： 提供喷嘴并且包括由外壁和内壁限定的外环，并且包括空气入口，空气通过空气入口流入燃料混合区和燃烧区，设置在内壁内的内环，并且包括燃料体积 该燃料被供给到其远端，其远离燃烧区域并且与燃料区隔开并且设置在燃料体积和内壁之间的气流管线，空气通过气流线路和燃烧物流向燃烧区域 隔离燃料体积的区域;以及熔断器，其构造成在火焰保持入射期间熔化并形成泄漏，燃料通过燃料从旁通燃料混合区域的燃料体积流到燃料混合区下游的燃料燃烧区域。
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34.发明授权公开(公告)号：US08079218B2
公开(公告)日：2011-12-20
申请号：US12469910
申请日：2009-05-21
CPC分类号： F23R3/045 , F23C2900/07022 , F23D14/48 , F23D14/76 , F23D14/82 , F23D2900/00018 , F23R3/283 , F23R2900/00005
摘要： The structure and operation of a fuel nozzle for a gas turbine combustor is disclosed where the fuel nozzle provides for flameholding protection and, more specifically, to such a nozzle that provides for nondestructive protection from flameholding. The nozzle provides for differential thermal expansion between tubes forming fuel passages to allowing for the nondestructive venting of fuel during a flameholding condition. Upon extinguishing the flameholding condition, the nozzle returns to normal operating condition.
摘要翻译： 公开了一种用于燃气轮机燃烧器的燃料喷嘴的结构和操作，其中燃料喷嘴提供阻燃保护，更具体地，涉及这样的喷嘴，其提供无损保护的非破坏性保护。 喷嘴提供形成燃料通道的管之间的差分热膨胀，以允许在保持静止状态期间燃料的非破坏性排气。 熄灭保护条件后，喷嘴返回正常工作状态。
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公开(公告)号：US07908841B2
公开(公告)日：2011-03-22
申请号：US12247706
申请日：2008-10-08
IPC分类号： F02B43/00
CPC分类号： F02C3/28 , F02C3/26 , F05D2220/722 , F23C2900/03002 , F23K5/007 , F23K2401/10 , F23R3/28 , F23R5/00 , F23R2900/00002 , Y02E20/16 , Y02E20/18
摘要： A direct-fired coal combustion system includes a swirl chamber having an input configured to receive a coal-water slurry and causing the coal-water slurry to mix with discharge air from a compressor to gasify the coal-water slurry and create a synthesis gas. The system also includes a cyclone separator directly coupled to the second end of the swirl chamber and a second stage combustion input coupled to an output of the cyclone separator.
摘要翻译： 直燃煤燃烧系统包括涡流室，其具有被配置为接收煤水浆料并使煤水浆料与来自压缩机的排出空气混合以将煤水浆料气化并产生合成气的输入。 该系统还包括直接联接到涡流室的第二端的旋风分离器和耦合到旋风分离器的输出的第二级燃烧输入。
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公开(公告)号：US20100199674A1
公开(公告)日：2010-08-12
申请号：US12368011
申请日：2009-02-09
IPC分类号： F02C1/00
摘要： A fuel nozzle manifold comprising a flange, a stem and a swirler is provided. The flange has a first fluid inlet fluidly connected to a radially extending first flow passage, the stem includes at least a first axially extending and only partially circumferentially extending flow channel, and the swirler has at least a first radially extending premix passage. The flange and the stem can comprise a homogeneous component, or two separate components fluidly connecting the first axially extending flow channel to the first flow passage, to form a fluid connection between the flange and the stem, the swirler comprises another component fitted together with the flange and stem component and fluidly connecting the first premix passage and the first flow channel.
摘要翻译： 提供了一种包括凸缘，杆和旋流器的燃料喷嘴歧管。 所述凸缘具有流体连接到径向延伸的第一流动通道的第一流体入口，所述杆包括至少第一轴向延伸且仅部分周向延伸的流动通道，并且所述旋流器具有至少第一径向延伸的预混合通道。 凸缘和杆可以包括均匀的部件或两个分开的部件，其将第一轴向延伸的流动通道流体地连接到第一流动通道，以在凸缘和阀杆之间形成流体连接，旋流器包括与 法兰和阀杆部件，并且流体地连接第一预混合通道和第一流动通道。
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公开(公告)号：US20100083882A1
公开(公告)日：2010-04-08
申请号：US12247706
申请日：2008-10-08
IPC分类号： F23K1/00
CPC分类号： F02C3/28 , F02C3/26 , F05D2220/722 , F23C2900/03002 , F23K5/007 , F23K2401/10 , F23R3/28 , F23R5/00 , F23R2900/00002 , Y02E20/16 , Y02E20/18
摘要： A direct-fired coal combustion system includes a swirl chamber having an input configured to receive a coal-water slurry and causing the coal-water slurry to mix with discharge air from a compressor to gasify the coal-water slurry and create a synthesis gas. The system also includes a cyclone separator directly coupled to the second end of the swirl chamber and a second stage combustion input coupled to an output of the cyclone separator.
摘要翻译： 直燃煤燃烧系统包括涡流室，其具有被配置为接收煤水浆料并使煤水浆料与来自压缩机的排出空气混合以将煤水浆料气化并产生合成气的输入。 该系统还包括直接联接到涡流室的第二端的旋风分离器和耦合到旋风分离器的输出的第二级燃烧输入。
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38.发明申请公开(公告)号：US20090293482A1
公开(公告)日：2009-12-03
申请号：US12128231
申请日：2008-05-28
CPC分类号： F23R3/286 , F23D14/82 , F23D2900/00015 , F23R3/343
摘要： A fuel nozzle assembly for a combustor of a gas turbine including: a nozzle body having a front and an inner tube defining a fuel passage extending through the nozzle body, wherein the front proximate to a combustion section of the combustor; an outer casing around the inner tube, wherein an air passage is defined between the outer casing and the inner tube; a gas conduit arranged in the air passage and having an outlet proximate to the front of the nozzle body, wherein fuel starts flowing through the expandable conduit only after a flashback condition occurs in the combustor, and a premix fuel passage and port discharging fuel to a premix section of the combustor, wherein the gas conduit has an inlet open to the premix fuel passage.
摘要翻译： 一种用于燃气轮机的燃烧器的燃料喷嘴组件，包括：喷嘴体，其具有限定通过所述喷嘴主体延伸的燃料通道的前部管和内部管，其中所述前部靠近所述燃烧器的燃烧部分; 围绕所述内管的外壳，其中在所述外壳和所述内管之间限定空气通道; 布置在所述空气通道中并且具有靠近所述喷嘴主体的前部的出口的气体导管，其中仅在所述燃烧器中发生回火状态之后燃料开始流过所述可膨胀导管，以及预燃燃料通道和将燃料喷射到 燃烧器的预混合部分，其中气体管道具有通向预混合燃料通道的入口。
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公开(公告)号：US07546735B2
公开(公告)日：2009-06-16
申请号：US10963724
申请日：2004-10-14
CPC分类号： F23L7/00 , F02C3/20 , F23C2900/07001 , F23D17/002 , F23D2209/30 , F23D2900/00008 , F23L2900/07008 , F23R3/286
摘要： A combustor for a gas turbine includes a combustion chamber and a plurality of radially outer nozzles surrounding a single, center nozzle, the radially outer nozzles configured to supply only gas fuel to the combustion chamber and the center nozzle configured to supply both gas and liquid fuel to the combustion chamber.
摘要翻译： 燃气轮机的燃烧器包括燃烧室和围绕单个中心喷嘴的多个径向外部喷嘴，所述径向外部喷嘴构造成仅向燃烧室供应气体燃料，并且中心喷嘴构造成供应气体和液体燃料 到燃烧室。
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