-
公开(公告)号：US20130047619A1
公开(公告)日：2013-02-28
申请号：US13221027
申请日：2011-08-30
摘要： An injection nozzle assembly includes a nozzle body having an outer surface and an inner surface that defines a flow passage, and a center body arranged within the nozzle body and extending along the flow passage. The center body includes a first end that extends to a tip portion through an intermediate portion that defines a fluid passage. The intermediate portion includes a first outer dimension and the tip portion includes a second outer dimension that is distinct from the first outer dimension. The center body includes a plurality of grooves that extend axially along the tip portion.
摘要翻译： 喷嘴组件包括具有外表面和限定流动通道的内表面的喷嘴体，以及布置在喷嘴体内并沿着流动通道延伸的中心体。 中心体包括通过限定流体通道的中间部分延伸到尖端部分的第一端。 中间部分包括第一外部尺寸，并且尖端部分包括与第一外部尺寸不同的第二外部尺寸。 中心体包括沿尖端部分轴向延伸的多个凹槽。
-
公开(公告)号：US20120291447A1
公开(公告)日：2012-11-22
申请号：US13110256
申请日：2011-05-18
IPC分类号： F02C7/22
CPC分类号： F23D11/16 , F23C2900/07021 , F23L7/005 , F23L2900/07008 , F23R3/343
摘要： A combustor nozzle includes a first and second liquid fuel passages that terminate at first and second fuel ports. A first diluent passage terminates at a first diluent outlet radially surrounding the second fuel ports. A second diluent passage terminates at a second diluent outlet between the first diluent outlet and the second fuel ports. A third diluent passage surrounds at least a portion of the first and second diluent passages. A method for supplying fuel to a combustor includes flowing a liquid fuel through a first fuel passage and flowing an emulsified liquid fuel through a second fuel passage. The method further includes flowing a first diluent through a shroud surrounding the second fuel passage to a first diluent passage surrounding at least a portion of the second fuel passage and flowing a second diluent through a second diluent passage radially disposed between the first diluent passage and the second fuel passage.
摘要翻译： 燃烧器喷嘴包括在第一和第二燃料端口处终止的第一和第二液体燃料通道。 第一稀释剂通道终止于径向围绕第二燃料端口的第一稀释剂出口。 第二稀释剂通道在第一稀释剂出口和第二燃料端口之间终止于第二稀释剂出口。 第三稀释剂通道围绕第一和第二稀释剂通道的至少一部分。 用于向燃烧器供应燃料的方法包括使液体燃料流过第一燃料通道并使乳化液体燃料流过第二燃料通道。 该方法还包括使第一稀释剂流过围绕第二燃料通道的护罩到围绕第二燃料通道的至少一部分的第一稀释剂通道，并使第二稀释剂流过放射状设置在第一稀释剂通道和第二稀释剂通道 第二燃料通道。
-
公开(公告)号：US08205452B2
公开(公告)日：2012-06-26
申请号：US12364488
申请日：2009-02-02
CPC分类号： F23R3/286 , F02C7/22 , F05D2240/36 , F23R3/12 , F23R3/283 , F23R3/34 , F23R3/36 , F23R3/46 , Y02T50/675
摘要： In one embodiment, a system includes a fuel nozzle that includes a fuel injector configured to output a fuel flow and a premixer tube disposed about the fuel flow output from the fuel injector. The premixer tube includes a perforated portion and a non-perforated portion, and the non-perforated portion is downstream of the perforated portion.
摘要翻译： 在一个实施例中，系统包括燃料喷嘴，其包括配置成输出燃料流的燃料喷射器和围绕燃料喷射器输出的燃料流布置的预混合管。 预混合管包括穿孔部分和非穿孔部分，并且非穿孔部分在穿孔部分的下游。
-
公开(公告)号：US20120073302A1
公开(公告)日：2012-03-29
申请号：US12890903
申请日：2010-09-27
CPC分类号： F23R3/14 , F23D11/402 , F23D14/64 , F23D2900/00008 , F23D2900/14701 , F23R3/286 , F23R3/343 , F23R3/36
摘要： A fuel nozzle assembly is disclosed. The fuel nozzle assembly comprises an outer burner tube and an inner burner tube defining a pre-mixing annulus therebetween. The fuel nozzle assembly further comprises a swirler assembly, the swirler assembly comprising a plurality of swirler vanes disposed in an annular array about the inner burner tube and configured to interact with primary air upstream of the pre-mixing annulus. The fuel nozzle assembly further comprises an air injection feature configured to flow secondary air into the pre-mixing annulus downstream of the swirler assembly such that the secondary air flows in a generally linear path longitudinally with respect to the pre-mixing annulus and adjacent at least one of the outer burner tube and the inner burner tube.
摘要翻译： 公开了一种燃料喷嘴组件。 燃料喷嘴组件包括外部燃烧器管和在其间限定预混合环的内部燃烧器管。 所述燃料喷嘴组件还包括旋流器组件，所述旋流器组件包括围绕所述内部燃烧器管设置成环形阵列并被配置为与所述预混合环空上游的一次空气相互作用的多个旋流器叶片。 燃料喷嘴组件还包括空气喷射特征，该空气喷射特征构造成将二次空气流入旋流器组件下游的预混合环空，使得二次空气相对于预混气环纵向流动，并且至少相邻 外部燃烧器管和内部燃烧器管之一。
-
公开(公告)号：US09719681B2
公开(公告)日：2017-08-01
申请号：US13153585
申请日：2011-06-06
申请人： Hua Zhang , Douglas Frank Beadie , Gregory Allen Boardman , Geoffrey David Myers , William Thomas Ross
发明人： Hua Zhang , Douglas Frank Beadie , Gregory Allen Boardman , Geoffrey David Myers , William Thomas Ross
CPC分类号： F23K5/12 , F02C3/30 , F02C7/222 , F05D2240/126 , F05D2240/127 , Y10T137/0318 , Y10T137/85978
摘要： A system for supplying fuel includes a fuel manifold, a water manifold, and a fluid junction between the fuel manifold and the water manifold. A turbulator downstream from the fluid junction receives a fluid flow from the fluid junction. A method for supplying fuel includes flowing fuel through a fuel manifold, flowing water through a water manifold, and combining a portion of the water from the water manifold with the fuel from the fuel manifold to create emulsion fuel. The method further includes flowing the emulsion fuel through a turbulator.
-
26.发明授权Systems and methods for suppressing combustion driven pressure fluctuations with a premix combustor having multiple premix times 有权用具有多个预混时间的预混合燃烧器抑制燃烧驱动的压力波动的系统和方法公开(公告)号：US09212823B2
公开(公告)日：2015-12-15
申请号：US13604952
申请日：2012-09-06
申请人： Gregory Allen Boardman , Ronald James Chila , Mark Allan Hadley , Johnie Franklin McConnaughhay , Sarah Lori Crothers
发明人： Gregory Allen Boardman , Ronald James Chila , Mark Allan Hadley , Johnie Franklin McConnaughhay , Sarah Lori Crothers
IPC分类号： F23R3/28
CPC分类号： F23R3/286 , F23R2900/00014 , F23R2900/03043 , F23R2900/03045
摘要： A combustor having a combustion chamber is provided with an external flow sleeve and a combustor liner surrounding the combustion chamber. A plurality of flow channels are provided on the combustor liner and a plurality of nozzles are disposed at predetermined locations on the flow channels. The locations of the nozzles are selected to provide different mixing times for fuel injected through the nozzles.
摘要翻译： 具有燃烧室的燃烧器设置有外部流动套筒和围绕燃烧室的燃烧室衬套。 多个流动通道设置在燃烧器衬套上，并且多个喷嘴设置在流动通道上的预定位置处。 选择喷嘴的位置以为通过喷嘴喷射的燃料提供不同的混合时间。
-
公开(公告)号：US09074773B2
公开(公告)日：2015-07-07
申请号：US13367686
申请日：2012-02-07
CPC分类号： F23R3/286 , F23R2900/00015
摘要： A combustor assembly is disclosed. The combustor assembly may include an annular trapped vortex cavity located adjacent to a downstream end of a bundle of air/fuel premixing injection tubes. The annular trapped vortex cavity may include an opening at a radially inner portion of the annular trapped vortex cavity adjacent to the head end of the bundle of premixing tubes. The annular trapped vortex cavity may also include one or more air injection holes and one or more fuel sources disposed about the annular trapped vortex cavity such that the one or more air injection holes and the one or more fuel sources are configured to drive a vortex within the annular trapped vortex cavity.
摘要翻译： 公开了一种燃烧器组件。 燃烧器组件可以包括邻近空气/燃料预混合注射管束的下游端定位的环形捕获涡流腔。 环形捕获的涡流空腔可以包括在与预混合管束的头端相邻的环形捕获涡流腔的径向内部的开口。 环形捕获的涡流空腔还可以包括一个或多个空气喷射孔和围绕环形捕获的涡流腔设置的一个或多个燃料源，使得一个或多个空气喷射孔和一个或多个燃料源被配置成驱动内部的涡流 环形捕获涡流腔。
-
28.发明申请Systems and Methods For Suppressing Combustion Driven Pressure Fluctuations With a Premix Combustor Having Multiple Premix Times 有权用具有多个预混时间的预混合燃烧器抑制燃烧驱动的压力波动的系统和方法公开(公告)号：US20140060063A1
公开(公告)日：2014-03-06
申请号：US13604952
申请日：2012-09-06
申请人： Gregory Allen Boardman , Ronald James Chila , Mark Allan Hadley , Johnie Franklin McConnaughhay , Sarah Lori Crothers
发明人： Gregory Allen Boardman , Ronald James Chila , Mark Allan Hadley , Johnie Franklin McConnaughhay , Sarah Lori Crothers
CPC分类号： F23R3/286 , F23R2900/00014 , F23R2900/03043 , F23R2900/03045
摘要： A combustor having a combustion chamber is provided with an external flow sleeve and a combustor liner surrounding the combustion chamber. A plurality of flow channels are provided on the combustor liner and a plurality of nozzles are disposed at predetermined locations on the flow channels. The locations of the nozzles are selected to provide different mixing times for fuel injected through the nozzles.
摘要翻译： 具有燃烧室的燃烧器设置有外部流动套筒和围绕燃烧室的燃烧室衬套。 多个流动通道设置在燃烧器衬套上，并且多个喷嘴设置在流动通道上的预定位置处。 选择喷嘴的位置以为通过喷嘴喷射的燃料提供不同的混合时间。
-
29.发明申请Liquid Cartridge with Passively Fueled Premixed Air Blast Circuit for Gas Operation 有权用于气体操作的带有被动燃料预混气爆炸电路的液体盒公开(公告)号：US20130312422A1
公开(公告)日：2013-11-28
申请号：US13480896
申请日：2012-05-25
摘要： A gas/liquid fuel nozzle assembly includes a premixing tube bundle having an array of mixing tubes, a fuel plenum delivering fuel to the mixing tubes, a cartridge tube disposed within the fuel plenum, and a liquid fuel cartridge disposed in the cartridge tube. The liquid fuel cartridge is spaced from the cartridge tube to define an annulus. The cartridge tube and the fuel plenum are constructed in fluid communication such that gas fuel in the plenum is injected into the annulus.
摘要翻译： 气体/液体燃料喷嘴组件包括具有混合管阵列的预混合管束，将燃料输送到混合管的燃料增压室，设置在燃料增压室内的筒管和设置在筒管中的液体燃料盒。 液体燃料盒与筒管间隔开以限定环形空间。 筒管和燃料增压室被构造成流体连通，使得气室中的气体燃料被注入到环空中。
-
公开(公告)号：US08590311B2
公开(公告)日：2013-11-26
申请号：US12768758
申请日：2010-04-28
CPC分类号： F23R3/286
摘要： An improved mixing tube design and fuel nozzle that allows for a more uniform and thorough mixing of fuel and air being fed to the combustor of a gas turbine engine, wherein each of a plurality of mixing tubes comprises a pair of concentric hollow cylinders that define a ring-like, annular path for the flow of fuel between the two hollow cylinders in each mixing tube, a plurality of air injection slots formed in the concentric hollow cylinders defining corresponding air flow paths from the outside into the interior of each mixing tube, and one or more fuel injection ports formed in selected ones of the plurality of air injection slots that allow for the flow of fuel from the annular path formed by the hollow cylinders into the air flow path, resulting in significantly better mixing and improved thermodynamic behavior of the fuel and air mixture downstream of the nozzle and upstream of the combustor.
摘要翻译： 一种改进的混合管设计和燃料喷嘴，其允许将燃料和空气进一步均匀且充分地混合到燃气涡轮发动机的燃烧器中，其中多个混合管中的每一个包括一对同心的中空圆筒， 在每个混合管中的两个中空圆柱体之间的用于燃料流动的环形环形路径，形成在同心中空圆柱体中的多个空气注入槽限定从外部到每个混合管的内部的相应空气流动路径，以及 一个或多个燃料喷射口形成在多个空气喷射槽中的选定的空气喷射槽中，允许燃料从由中空圆筒形成的环形路径流入空气流动路径，导致显着更好的混合和改进的热力学行为 燃料和空气混合物在喷嘴下游和燃烧器的上游。
-
-
-
-
-
-
-
-
-
搜索结果
51 条记录 (耗时 0.034 秒)
