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11.发明授权Flame holding tolerant fuel and air premixer for a gas turbine combustor 失效用于燃气轮机燃烧器的火焰保持容忍燃料和空气预混合器公开(公告)号：US08312722B2
公开(公告)日：2012-11-20
申请号：US12256901
申请日：2008-10-23
CPC分类号： F23R3/286 , F23D14/62 , F23D2214/00 , F23R3/283
摘要： A fuel nozzle with active cooling is provided. It includes an outer peripheral wall, a nozzle center body concentrically disposed within the outer wall in a fuel and air pre-mixture. The fuel and air pre-mixture includes an air inlet, a fuel inlet and a premixing passage defined between the outer wall in the center body. A gas fuel flow passage is provided. A first cooling passage is included within the center body in a second cooling passage is defined between the center body and the outer wall.
摘要翻译： 提供具有主动冷却的燃料喷嘴。 它包括外周壁，在燃料和空气预混合物中同心地设置在外壁内的喷嘴中心体。 燃料和空气预混合物包括空气入口，燃料入口和限定在中心体的外壁之间的预混合通道。 提供了一种气体燃料流动通道。 第一冷却通道包括在中心体内，第二冷却通道限定在中心体和外壁之间。
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公开(公告)号：US20120255310A1
公开(公告)日：2012-10-11
申请号：US13083769
申请日：2011-04-11
IPC分类号： F02C7/22
CPC分类号： F23C7/006 , F23D14/70 , F23D2208/10 , F23D2209/20 , F23D2900/00003 , F23D2900/11402 , F23R3/14 , F23R3/286
摘要： A combustor nozzle includes a center body and a shroud circumferentially surrounding at least a portion of the center body to define a passage between the center body and the shroud. A guide between the center body and the shroud can pivot with respect to the center body. A method for supplying fuel to a combustor includes flowing a working fluid through a nozzle at a mass flow rate and flowing a fuel through the nozzle. The method further includes sensing a flame holding event inside the nozzle and pivoting a guide inside the nozzle to increase the mass flow rate of the working fluid flowing through the nozzle.
摘要翻译： 燃烧器喷嘴包括中心体和护罩，周向地围绕中心体的至少一部分以限定中心体和护罩之间的通道。 中心体和护罩之间的引导件可相对于中心体枢转。 向燃烧器供给燃料的方法包括使工作流体以质量流量流过喷嘴并使燃料流过喷嘴。 该方法还包括感测喷嘴内的火焰保持事件并使喷嘴内部的引导件枢转以增加流过喷嘴的工作流体的质量流量。
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公开(公告)号：US08181891B2
公开(公告)日：2012-05-22
申请号：US12555129
申请日：2009-09-08
申请人： Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Lacy , William David York , Christian Xavier Stevenson
发明人： Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Lacy , William David York , Christian Xavier Stevenson
CPC分类号： B05B1/14 , B33Y80/00 , F23C2900/9901 , F23D14/48 , F23D14/62 , F23D2213/00 , F23R3/286 , F23R2900/00002 , F23R2900/00018
摘要： A monolithic fuel injection head for a fuel nozzle includes a substantially hollow vesicle body formed with an upstream end face, a downstream end face and a peripheral wall extending therebetween, an internal baffle plate extending radially outwardly from a downstream end of the bore, terminating short of the peripheral wall, thereby defining upstream and downstream fuel plenums in the vesicle body, in fluid communication by way of a radial gap between the baffle plate and the peripheral wall. A plurality of integral pre-mix tubes extend axially through the upstream and downstream fuel plenums in the vesicle body and through the baffle plate, with at least one fuel injection hole extending between each of the pre-mix tubes and the upstream fuel plenum, thereby enabling fuel in the upstream plenum to be injected into the plurality of pre-mix tubes. The fuel injection head is formed by direct metal laser sintering.
摘要翻译： 用于燃料喷嘴的单片燃料喷射头包括基本上中空的囊泡体，其形成有上游端面，下游端面和在其间延伸的周壁，内部挡板从孔的下游端径向向外延伸，终止短路 从而限定囊泡体中的上游和下游燃料增压室，通过挡板和周壁之间的径向间隙流体连通。 多个整体式预混合管轴向地延伸穿过囊泡主体中的上游和下游燃料增压室并通过挡板，在每个预混合管和上游燃料增压室之间延伸有至少一个燃料喷射孔，由此 使上游气室中的燃料能够喷射到多个预混合管中。 燃料喷射头由直接金属激光烧结形成。
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公开(公告)号：US08157189B2
公开(公告)日：2012-04-17
申请号：US12417896
申请日：2009-04-03
IPC分类号： B05B15/00
CPC分类号： F23D14/62 , F23R3/10 , F23R3/286 , F23R2900/00002
摘要： A fuel injection nozzle comprises a body member having an upstream wall opposing a downstream wall, a baffle member having an upstream surface and a downstream surface, a first chamber, a second chamber, a fuel inlet communicative with the first chamber operative to emit a first gas into the first chamber, and a plurality of mixing tubes, each of the mixing tubes having a tube inner surface, a tube outer surface, a first inlet communicative with an aperture in the upstream wall operative to receive a second gas, a second inlet communicative with the tube outer surface and the tube inner surface operative to translate the first gas into the mixing tube, a mixing portion operative to mix the first gas and the second gas, and an outlet communicative with an aperture in the downstream wall operative to emit the mixed first and second gasses.
摘要翻译： 燃料喷射喷嘴包括主体构件，其具有与下游壁相对的上游壁，具有上游表面和下游表面的挡板构件，第一腔室，第二腔室，与第一腔室连通的燃料入口，其操作以发射第一 气体进入第一室，以及多个混合管，每个混合管具有管内表面，管外表面，与上游壁中的孔连通的第一入口，用于接收第二气体，第二入口 与管外表面和管内表面通信，其可操作以将第一气体平移到混合管中，混合部分可操作以混合第一气体和第二气体，以及与下游壁中的孔连通的出口，其可操作地发射 混合的第一和第二气体。
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公开(公告)号：US20120006030A1
公开(公告)日：2012-01-12
申请号：US12832330
申请日：2010-07-08
申请人： Jong Ho Uhm , Thomas Edward Johnson , Kwanwoo Kim
发明人： Jong Ho Uhm , Thomas Edward Johnson , Kwanwoo Kim
IPC分类号： F02C7/22
CPC分类号： F23R3/28 , F23D14/62 , F23D14/82 , F23G2900/54402 , F23R2900/00002
摘要： A turbomachine includes a compressor, a combustor operatively connected to the compressor, an end cover mounted to the combustor, and an injection nozzle assembly operatively connected to the combustor. The injection nozzle assembly includes a first end portion that extends to a second end portion, and a plurality of tube elements provided at the second end portion. Each of the plurality of tube elements defining a fluid passage includes a body having a first end section that extends to a second end section. The second end section projects beyond the second end portion of the injection nozzle assembly.
摘要翻译： 涡轮机包括压缩机，可操作地连接到压缩机的燃烧器，安装到燃烧器的端盖和可操作地连接到燃烧器的喷嘴组件。 注射喷嘴组件包括延伸到第二端部的第一端部和设置在第二端部处的多个管状元件。 限定流体通道的多个管元件中的每一个包括具有延伸到第二端部的第一端部的主体。 第二端部突出超过喷嘴组件的第二端部。
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公开(公告)号：US20110197587A1
公开(公告)日：2011-08-18
申请号：US12707754
申请日：2010-02-18
IPC分类号： F02C7/22
摘要： A fuel injection nozzle includes at least one tube disposed in the nozzle having a venturi shaped profile defining a gas flow path including an inlet operative to receive a first gas, at least one port operative to emit a second gas into the gas flow path, and an outlet operative to emit a mixture of the first gas and the second gas into a combustor.
摘要翻译： 燃料喷射喷嘴包括设置在喷嘴中的至少一个管，其具有文氏管形轮廓，其限定气体流动路径，其包括可操作以接收第一气体的入口，至少一个端口，其可操作以将第二气体发射到气体流动路径中;以及 可操作地将第一气体和第二气体的混合物发射到燃烧器中的出口。
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公开(公告)号：US20110072824A1
公开(公告)日：2011-03-31
申请号：US12570678
申请日：2009-09-30
申请人： BAIFANG ZUO , WILLY STEVE ZIMINSKY , THOMAS EDWARD JOHNSON , JOHN CHARLES INTILE , BENJAMIN PAUL LACY
发明人： BAIFANG ZUO , WILLY STEVE ZIMINSKY , THOMAS EDWARD JOHNSON , JOHN CHARLES INTILE , BENJAMIN PAUL LACY
IPC分类号： F02C7/22
CPC分类号： F23D14/62 , F23C2900/07001 , F23D2900/14004 , F23D2900/14701 , F23R3/14 , F23R3/286
摘要： A nozzle includes an inlet, an outlet, and an axial centerline. A shroud surrounding the axial centerline extends from the inlet to the outlet and defines a circumference. The circumference proximate the inlet is greater than the circumference at a first point downstream of the inlet, and the circumference at the first point downstream of the inlet is less than the circumference at a second point downstream of the first point. A method for supplying a fuel through a nozzle directs a first airflow along a first path and a second airflow along a second path separate from the first path. The method further includes injecting the fuel into at least one of the first path or the second path and accelerating at least one of the first airflow or the second airflow.
摘要翻译： 喷嘴包括入口，出口和轴向中心线。 围绕轴向中心线的护罩从入口延伸到出口并限定圆周。 入口周围的圆周大于入口下游第一点处的圆周，入口下游第一点处的圆周小于第一点下游第二点处的圆周。 用于通过喷嘴供应燃料的方法沿着第一路径引导第一气流和沿着与第一路径分离的第二路径的第二气流。 该方法还包括将燃料喷射到第一路径或第二路径中的至少一个中并且加速第一气流或第二气流中的至少一个。
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18.发明申请公开(公告)号：US20110000214A1
公开(公告)日：2011-01-06
申请号：US12495918
申请日：2009-07-01
CPC分类号： F23D14/76 , F23D2900/00018 , F23R3/14 , F23R3/283 , F23R3/286 , Y10T29/49229
摘要： A method of assembling a gas turbine engine is provided. The method includes coupling a combustor in flow communication with a compressor such that the combustor receives at least some of the air discharged by the compressor. A fuel nozzle assembly is coupled to the combustor and includes at least one fuel nozzle that includes a plurality of interior surfaces, wherein a thermal barrier coating is applied across at least one of the plurality of interior surfaces to facilitate shielding the interior surfaces from combustion gases.
摘要翻译： 提供一种组装燃气涡轮发动机的方法。 该方法包括将与压缩机流动连通的燃烧器联接，使得燃烧器接收由压缩机排出的至少一些空气。 燃料喷嘴组件联接到燃烧器并且包括至少一个燃料喷嘴，其包括多个内表面，其中热屏障涂层跨越多个内表面中的至少一个施加，以便于内表面与燃烧气体的屏蔽 。
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公开(公告)号：US20100180602A1
公开(公告)日：2010-07-22
申请号：US12355047
申请日：2009-01-16
IPC分类号： F02C7/22
摘要： A combustor assembly for a turbine engine includes a cap assembly which gradually increases the volume of compressed air provided to the combustor assembly, and which slows the compressed air in a controlled manner before delivering the compressed air into a combustor area. The cap assembly includes inner and outer sleeves which are mounted in a concentric fashion. The annular space formed between the inner and outer sleeves gradually increases from an aft end to a forward end. A stepped portion is formed on the inner sleeve of the cap assembly, and this stepped portion is joined to a corresponding combustor liner.
摘要翻译： 用于涡轮发动机的燃烧器组件包括帽组件，其逐渐增加设置到燃烧器组件的压缩空气的体积，并且在将压缩空气输送到燃烧器区域之前以受控的方式减慢压缩空气。 盖组件包括以同心方式安装的内套筒和外套筒。 形成在内套筒和外套筒之间的环形空间从后端逐渐增加到前端。 在盖组件的内套上形成阶梯部，该阶梯部与相应的燃烧器衬套接合。
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公开(公告)号：US20100089367A1
公开(公告)日：2010-04-15
申请号：US12249158
申请日：2008-10-10
申请人： Thomas Edward Johnson , Willy Steve Ziminsky , Benjamin Paul Lacy , William David York , Christian Xavier Stevenson
发明人： Thomas Edward Johnson , Willy Steve Ziminsky , Benjamin Paul Lacy , William David York , Christian Xavier Stevenson
IPC分类号： F02M61/14
CPC分类号： F23D14/82
摘要： A fuel nozzle assembly is provided. The assembly includes an outer nozzle body having a first end and a second end and at least one inner nozzle tube having a first end and a second end. One of the nozzle body or nozzle tube includes a fuel plenum and a fuel passage extending therefrom, while the other of the nozzle body or nozzle tube includes a fuel injection hole slidably aligned with the fuel passage to form a fuel flow path therebetween at an interface between the body and the tube. The nozzle body and the nozzle tube are fixed against relative movement at the first ends of the nozzle body and nozzle tube, enabling the fuel flow path to close at the interface due to thermal growth after a flame enters the nozzle tube.
摘要翻译： 提供燃料喷嘴组件。 组件包括具有第一端和第二端的外部喷嘴本体和具有第一端和第二端的至少一个内部喷嘴管。 喷嘴主体或喷嘴管中的一个包括燃料增压室和从其延伸的燃料通道，而喷嘴体或喷嘴管中的另一个包括与燃料通道可滑动地对准的燃料喷射孔，以在界面处形成燃料流动路径 在身体和管之间。 喷嘴体和喷嘴管相对于喷嘴体和喷嘴管的第一端处的相对运动被固定，使得燃料流路在火焰进入喷嘴管之后由于热生长而在界面处闭合。
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