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1. 发明授权

US08511086B1 System and method for reducing combustion dynamics in a combustor 失效
标题翻译：用于减少燃烧器中的燃烧动力学的系统和方法
公开(公告)号：US08511086B1
公开(公告)日：2013-08-20
申请号：US13409326
申请日：2012-03-01
申请人： Jong Ho Uhm , Thomas Edward Johnson , Baifang Zuo , William David York
发明人： Jong Ho Uhm , Thomas Edward Johnson , Baifang Zuo , William David York
IPC分类号： F02C1/00
CPC分类号： F23R3/286 , F23L2900/07002 , F23L2900/07008 , F23L2900/07009 , F23R2900/00013 , F23R2900/00014
摘要： A system for reducing combustion dynamics in a combustor includes an end cap having an upstream surface axially separated from a downstream surface, and tube bundles extend through the end cap. A diluent supply in fluid communication with the end cap provides diluent flow to the end cap. Diluent distributors circumferentially arranged inside at least one tube bundle extend downstream from the downstream surface and provide fluid communication for the diluent flow through the end cap. A method for reducing combustion dynamics in a combustor includes flowing fuel through tube bundles that extend axially through an end cap, flowing a diluent through diluent distributors into a combustion chamber, wherein the diluent distributors are circumferentially arranged inside at least one tube bundle and each diluent distributor extends downstream from the end cap, and forming a diluent barrier in the combustion chamber between at least one pair of adjacent tube bundles.
摘要翻译：用于减少燃烧器中的燃烧动力学的系统包括具有从下游表面轴向分离的上游表面的端盖，并且管束延伸穿过端盖。与端盖流体连通的稀释剂供应器提供了向端盖的稀释剂流。周向布置在至少一个管束内的稀释剂分配器延伸到下游表面的下游，并且提供流过端盖的稀释剂流的流体连通。一种用于减少燃烧动力学的方法，包括使燃料通过管束流动，所述管束轴向延伸穿过端盖，使稀释剂流经稀释剂分配器进入燃烧室，其中稀释剂分配器周向地布置在至少一个管束内，每个稀释剂分配器从端盖延伸到下游，并且在燃烧室中在至少一对相邻的管束之间形成稀释剂阻挡层。

2. 发明授权

US09121612B2 System and method for reducing combustion dynamics in a combustor 有权
标题翻译：用于减少燃烧器中的燃烧动力学的系统和方法
公开(公告)号：US09121612B2
公开(公告)日：2015-09-01
申请号：US13409309
申请日：2012-03-01
申请人： Jong Ho Uhm , Thomas Edward Johnson , Baifang Zuo , William David York
发明人： Jong Ho Uhm , Thomas Edward Johnson , Baifang Zuo , William David York
IPC分类号： F23R3/28 , F23R3/00 , F02C3/30 , F23R3/54 , F23R3/32 , F23D14/62
CPC分类号： F23R3/286 , F02C3/30 , F23C2900/07022 , F23D14/62 , F23R3/002 , F23R3/32 , F23R3/54 , F23R2900/00013
摘要： A system for reducing combustion dynamics in a combustor includes an end cap having an upstream surface axially separated from a downstream surface, and tube bundles extend from the upstream surface through the downstream surface. A divider inside a tube bundle defines a diluent passage that extends axially through the downstream surface, and a diluent supply in fluid communication with the divider provides diluent flow to the diluent passage. A method for reducing combustion dynamics in a combustor includes flowing a fuel through tube bundles, flowing a diluent through a diluent passage inside a tube bundle, wherein the diluent passage extends axially through at least a portion of the end cap into a combustion chamber, and forming a diluent barrier in the combustion chamber between the tube bundle and at least one other adjacent tube bundle.
摘要翻译：用于减少燃烧器中的燃烧动力学的系统包括具有从下游表面轴向分离的上游表面的端盖，并且管束从上游表面延伸穿过下游表面。管束内的分隔器限定了一个沿轴向延伸穿过下游表面的稀释剂通道，与分隔器流体连通的稀释剂供应器提供稀释剂流向稀释剂通道。一种用于减少燃烧动力学的方法，包括使燃料通过管束流动，使稀释剂流过管束内的稀释剂通道，其中稀释剂通道轴向延伸通过端盖的至少一部分进入燃烧室，以及在管束与至少一个其它相邻管束之间的燃烧室中形成稀释剂阻挡层。

3. 发明授权

US09140454B2 Bundled multi-tube nozzle for a turbomachine 有权
标题翻译：捆绑的多管喷嘴用于涡轮机
公开(公告)号：US09140454B2
公开(公告)日：2015-09-22
申请号：US12358805
申请日：2009-01-23
申请人： Benjamin Paul Lacy , Willy Steve Ziminsky , Thomas Edward Johnson , Baifang Zuo , William David York , Jong Ho Uhm
发明人： Benjamin Paul Lacy , Willy Steve Ziminsky , Thomas Edward Johnson , Baifang Zuo , William David York , Jong Ho Uhm
IPC分类号： F23R3/34 , F23R3/28 , F23R3/10
CPC分类号： F23R3/286 , F23D2900/00008 , F23D2900/00012 , F23R3/10 , F23R3/34
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 cap member having a first surface that extends to a second surface. The cap member further includes a plurality of openings. A plurality of bundled mini-tube assemblies are detachably mounted in the plurality of openings in the cap member. Each of the plurality of bundled mini-tube assemblies includes a main body section having a first end section and a second end section. A fluid plenum is arranged within the main body section. A plurality of tubes extend between the first and second end sections. Each of the plurality of tubes is fluidly connected to the fluid plenum.
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。注射喷嘴组件包括具有延伸到第二表面的第一表面的盖构件。盖构件还包括多个开口。多个捆扎的微型管组件可拆卸地安装在盖构件中的多个开口中。多个捆扎的微型管组件中的每一个包括具有第一端部部分和第二端部部分的主体部分。主体部分内设有流体通风室。多个管在第一和第二端部之间延伸。多个管中的每一个流体连接到流体通风室。

4. 发明申请

US20130227953A1 SYSTEM AND METHOD FOR REDUCING COMBUSTION DYNAMICS IN A COMBUSTOR 有权
标题翻译：用于减少燃烧器燃烧动力学的系统和方法
公开(公告)号：US20130227953A1
公开(公告)日：2013-09-05
申请号：US13409309
申请日：2012-03-01
申请人： Jong Ho Uhm , Thomas Edward Johnson , Baifang Zuo , William David York
发明人： Jong Ho Uhm , Thomas Edward Johnson , Baifang Zuo , William David York
IPC分类号： F23R3/28
CPC分类号： F23R3/286 , F02C3/30 , F23C2900/07022 , F23D14/62 , F23R3/002 , F23R3/32 , F23R3/54 , F23R2900/00013
摘要： A system for reducing combustion dynamics in a combustor includes an end cap having an upstream surface axially separated from a downstream surface, and tube bundles extend from the upstream surface through the downstream surface. A divider inside a tube bundle defines a diluent passage that extends axially through the downstream surface, and a diluent supply in fluid communication with the divider provides diluent flow to the diluent passage. A method for reducing combustion dynamics in a combustor includes flowing a fuel through tube bundles, flowing a diluent through a diluent passage inside a tube bundle, wherein the diluent passage extends axially through at least a portion of the end cap into a combustion chamber, and forming a diluent barrier in the combustion chamber between the tube bundle and at least one other adjacent tube bundle.
摘要翻译：用于减少燃烧器中的燃烧动力学的系统包括具有从下游表面轴向分离的上游表面的端盖，并且管束从上游表面延伸穿过下游表面。管束内的分隔器限定了一个沿轴向延伸穿过下游表面的稀释剂通道，与分隔器流体连通的稀释剂供应器提供稀释剂流向稀释剂通道。一种用于减少燃烧动力学的方法，包括使燃料通过管束流动，使稀释剂流过管束内的稀释剂通道，其中稀释剂通道轴向延伸通过端盖的至少一部分进入燃烧室，以及在管束与至少一个其它相邻管束之间的燃烧室中形成稀释剂阻挡层。

5. 发明授权

US08424311B2 Premixed direct injection disk 有权
标题翻译：预混直接注射盘
公开(公告)号：US08424311B2
公开(公告)日：2013-04-23
申请号：US12394544
申请日：2009-02-27
申请人： William David York , Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Lacy , Baifang Zuo , Jong Ho Uhm
发明人： William David York , Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Lacy , Baifang Zuo , Jong Ho Uhm
IPC分类号： F23R3/286
CPC分类号： F23R3/286 , F23D14/02 , F23D14/82 , F23D2209/10 , F23R2900/03282
摘要： A fuel/air mixing disk for use in a fuel/air mixing combustor assembly is provided. The disk includes a first face, a second face, and at least one fuel plenum disposed therebetween. A plurality of fuel/air mixing tubes extend through the pre-mixing disk, each mixing tube including an outer tube wall extending axially along a tube axis and in fluid communication with the at least one fuel plenum. At least a portion of the plurality of fuel/air mixing tubes further includes at least one fuel injection hole have a fuel injection hole diameter extending through said outer tube wall, the fuel injection hole having an injection angle relative to the tube axis. The invention provides good fuel air mixing with low combustion generated NOx and low flow pressure loss translating to a high gas turbine efficiency, that is durable, and resistant to flame holding and flash back.
摘要翻译：提供了一种用于燃料/空气混合燃烧器组件的燃料/空气混合盘。盘包括第一面，第二面和设置在它们之间的至少一个燃料增压室。多个燃料/空气混合管延伸穿过预混合盘，每个混合管包括沿管轴线轴向延伸并与至少一个燃料增压室流体连通的外管壁。多个燃料/空气混合管的至少一部分还包括至少一个燃料喷射孔，其具有延伸穿过所述外管壁的燃料喷射孔直径，燃料喷射孔相对于管轴具有喷射角。本发明提供了具有低燃烧产生的NOx和低流量压力损失的良好的燃料空气混合，转化为高燃气轮机效率，耐久性，并且耐火焰保持和回闪。

6. 发明申请

US20130227955A1 SYSTEM AND METHOD FOR REDUCING COMBUSTION DYNAMICS IN A COMBUSTOR 失效
标题翻译：用于减少燃烧器燃烧动力学的系统和方法
公开(公告)号：US20130227955A1
公开(公告)日：2013-09-05
申请号：US13409326
申请日：2012-03-01
申请人： Jong Ho Uhm , Thomas Edward Johnson , Baifang Zuo , William David York
发明人： Jong Ho Uhm , Thomas Edward Johnson , Baifang Zuo , William David York
IPC分类号： F02C3/30
CPC分类号： F23R3/286 , F23L2900/07002 , F23L2900/07008 , F23L2900/07009 , F23R2900/00013 , F23R2900/00014
摘要： A system for reducing combustion dynamics in a combustor includes an end cap having an upstream surface axially separated from a downstream surface, and tube bundles extend through the end cap. A diluent supply in fluid communication with the end cap provides diluent flow to the end cap. Diluent distributors circumferentially arranged inside at least one tube bundle extend downstream from the downstream surface and provide fluid communication for the diluent flow through the end cap. A method for reducing combustion dynamics in a combustor includes flowing fuel through tube bundles that extend axially through an end cap, flowing a diluent through diluent distributors into a combustion chamber, wherein the diluent distributors are circumferentially arranged inside at least one tube bundle and each diluent distributor extends downstream from the end cap, and forming a diluent barrier in the combustion chamber between at least one pair of adjacent tube bundles.
摘要翻译：用于减少燃烧器中的燃烧动力学的系统包括具有从下游表面轴向分离的上游表面的端盖，并且管束延伸穿过端盖。与端盖流体连通的稀释剂供应器提供了向端盖的稀释剂流。周向布置在至少一个管束内的稀释剂分配器延伸到下游表面的下游，并且提供流过端盖的稀释剂流的流体连通。一种用于减少燃烧动力学的方法，包括使燃料通过管束流动，所述管束轴向延伸穿过端盖，使稀释剂流经稀释剂分配器进入燃烧室，其中稀释剂分配器周向地布置在至少一个管束内，每个稀释剂分配器从端盖延伸到下游，并且在燃烧室中在至少一对相邻的管束之间形成稀释剂阻挡层。

7. 发明申请

US20100218501A1 PREMIXED DIRECT INJECTION DISK 有权
标题翻译：优先直接注射盘
公开(公告)号：US20100218501A1
公开(公告)日：2010-09-02
申请号：US12394544
申请日：2009-02-27
申请人： William David York , Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Lacy , Baifang Zuo , Jong Ho Uhm
发明人： William David York , Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Lacy , Baifang Zuo , Jong Ho Uhm
IPC分类号： F02C7/22
CPC分类号： F23R3/286 , F23D14/02 , F23D14/82 , F23D2209/10 , F23R2900/03282
摘要： A fuel/air mixing disk for use in a fuel/air mixing combustor assembly is provided. The disk includes a first face, a second face, and at least one fuel plenum disposed therebetween. A plurality of fuel/air mixing tubes extend through the pre-mixing disk, each mixing tube including an outer tube wall extending axially along a tube axis and in fluid communication with the at least one fuel plenum. At least a portion of the plurality of fuel/air mixing tubes further includes at least one fuel injection hole have a fuel injection hole diameter extending through said outer tube wall, the fuel injection hole having an injection angle relative to the tube axis. The invention provides good fuel air mixing with low combustion generated NOx and low flow pressure loss translating to a high gas turbine efficiency, that is durable, and resistant to flame holding and flash back.
摘要翻译：提供了一种用于燃料/空气混合燃烧器组件的燃料/空气混合盘。盘包括第一面，第二面和设置在它们之间的至少一个燃料增压室。多个燃料/空气混合管延伸穿过预混合盘，每个混合管包括沿管轴线轴向延伸并与至少一个燃料增压室流体连通的外管壁。多个燃料/空气混合管的至少一部分还包括至少一个燃料喷射孔，其具有延伸穿过所述外管壁的燃料喷射孔直径，燃料喷射孔相对于管轴具有喷射角。本发明提供了具有低燃烧产生的NOx和低流量压力损失的良好的燃料空气混合，转化为高燃气轮机效率，耐久性，并且耐火焰保持和回闪。

8. 发明授权

US08539773B2 Premixed direct injection nozzle for highly reactive fuels 有权
标题翻译：用于高反应性燃料的预混合直喷喷嘴
公开(公告)号：US08539773B2
公开(公告)日：2013-09-24
申请号：US12365382
申请日：2009-02-04
申请人： Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Paul Lacy , William David York , Jong Ho Uhm , Baifang Zuo
发明人： Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Paul Lacy , William David York , Jong Ho Uhm , Baifang Zuo
IPC分类号： F23R3/30 , F23R3/32
CPC分类号： F23R3/286 , F23D2900/00008 , F23D2900/00012 , F23R3/10 , F23R3/34
摘要： A fuel/air mixing tube for use in a fuel/air mixing tube bundle is provided. The fuel/air mixing tube includes an outer tube wall extending axially along a tube axis between an inlet end and an exit end, the outer tube wall having a thickness extending between an inner tube surface having a inner diameter and an outer tube surface having an outer tube diameter. The tube further includes at least one fuel injection hole having a fuel injection hole diameter extending through the outer tube wall, the fuel injection hole having an injection angle relative to the tube axis. The invention provides good fuel air mixing with low combustion generated NOx and low flow pressure loss translating to a high gas turbine efficiency, that is durable, and resistant to flame holding and flash back.
摘要翻译：提供了一种用于燃料/空气混合管束的燃料/空气混合管。燃料/空气混合管包括沿入口端和出口端之间的管轴线轴向延伸的外管壁，外管壁具有在具有内径的内管表面和外管表面之间延伸的厚度，外管直径。该管还包括至少一个具有延伸穿过外管壁的燃料喷射孔直径的燃料喷射孔，燃料喷射孔相对于管轴具有喷射角。本发明提供了具有低燃烧产生的NOx和低流量压力损失的良好的燃料空气混合，转化为高燃气轮机效率，耐久性，并且耐火焰保持和回闪。

9. 发明申请

US20100192581A1 PREMIXED DIRECT INJECTION NOZZLE 有权
标题翻译：预先注射喷嘴
公开(公告)号：US20100192581A1
公开(公告)日：2010-08-05
申请号：US12365382
申请日：2009-02-04
申请人： Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Paul Lacy , William David York , Jong Ho Uhm , Baifang Zuo
发明人： Willy Steve Ziminsky , Thomas Edward Johnson , Benjamin Paul Lacy , William David York , Jong Ho Uhm , Baifang Zuo
IPC分类号： F02C1/00
CPC分类号： F23R3/286 , F23D2900/00008 , F23D2900/00012 , F23R3/10 , F23R3/34
摘要： A fuel/air mixing tube for use in a fuel/air mixing tube bundle is provided. The fuel/air mixing tube includes an outer tube wall extending axially along a tube axis between an inlet end and an exit end, the outer tube wall having a thickness extending between an inner tube surface having a inner diameter and an outer tube surface having an outer tube diameter. The tube further includes at least one fuel injection hole having a fuel injection hole diameter extending through the outer tube wall, the fuel injection hole having an injection angle relative to the tube axis. The invention provides good fuel air mixing with low combustion generated NOx and low flow pressure loss translating to a high gas turbine efficiency, that is durable, and resistant to flame holding and flash back.
摘要翻译：提供了一种用于燃料/空气混合管束的燃料/空气混合管。燃料/空气混合管包括沿入口端和出口端之间的管轴线轴向延伸的外管壁，外管壁具有在具有内径的内管表面和外管表面之间延伸的厚度，外管直径。该管还包括至少一个具有延伸穿过外管壁的燃料喷射孔直径的燃料喷射孔，燃料喷射孔相对于管轴具有喷射角。本发明提供了具有低燃烧产生的NOx和低流量压力损失的良好的燃料空气混合，转化为高燃气轮机效率，耐久性，并且耐火焰保持和回闪。

10. 发明申请

US20100186413A1 BUNDLED MULTI-TUBE NOZZLE FOR A TURBOMACHINE 有权
标题翻译：完整的多管喷嘴用于涡轮发动机
公开(公告)号：US20100186413A1
公开(公告)日：2010-07-29
申请号：US12358805
申请日：2009-01-23
申请人： Benjamin Paul Lacy , Willy Steve Ziminsky , Thomas Edward Johnson , Baifang Zuo , William David York , Jong Ho Uhm
发明人： Benjamin Paul Lacy , Willy Steve Ziminsky , Thomas Edward Johnson , Baifang Zuo , William David York , Jong Ho Uhm
IPC分类号： F02C7/22 , B05B1/14 , B05B7/04
CPC分类号： F23R3/286 , F23D2900/00008 , F23D2900/00012 , F23R3/10 , F23R3/34
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 cap member having a first surface that extends to a second surface. The cap member further includes a plurality of openings. A plurality of bundled mini-tube assemblies are detachably mounted in the plurality of openings in the cap member. Each of the plurality of bundled mini-tube assemblies includes a main body section having a first end section and a second end section. A fluid plenum is arranged within the main body section. A plurality of tubes extend between the first and second end sections. Each of the plurality of tubes is fluidly connected to the fluid plenum.
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。注射喷嘴组件包括具有延伸到第二表面的第一表面的盖构件。盖构件还包括多个开口。多个捆扎的微型管组件可拆卸地安装在盖构件中的多个开口中。多个捆扎的微型管组件中的每一个包括具有第一端部部分和第二端部部分的主体部分。主体部分内设有流体通风室。多个管在第一和第二端部之间延伸。多个管中的每一个流体连接到流体通风室。

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