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1. 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。

2. 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。

3. 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。

4. 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。

5. 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。

6. 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。

7. 发明申请

US20100008179A1 PRE-MIXING APPARATUS FOR A TURBINE ENGINE 有权
标题翻译：涡轮发动机预混装置
公开(公告)号：US20100008179A1
公开(公告)日：2010-01-14
申请号：US12169865
申请日：2008-07-09
申请人： Benjamin Paul Lacy , Balachandar Varatharajan , Willy Steve Ziminsky , Gilbert Otto Kraemer , Ertan Yilmaz , Patrick Benedict Melton , Baifang Zuo , Christian Xavier Stevenson , David Kenton Felling , Jong Ho Uhm
发明人： Benjamin Paul Lacy , Balachandar Varatharajan , Willy Steve Ziminsky , Gilbert Otto Kraemer , Ertan Yilmaz , Patrick Benedict Melton , Baifang Zuo , Christian Xavier Stevenson , David Kenton Felling , Jong Ho Uhm
IPC分类号： B01F15/02
CPC分类号： F23R3/286 , F23R3/34
摘要： A pre-mixing apparatus for a turbine engine includes a main body having an inlet portion, an outlet portion and an exterior wall that collectively establish at least one fluid delivery plenum, and a plurality of fluid delivery tubes extending through at least a portion of the at least one fluid delivery plenum. Each of the plurality of fluid delivery tubes includes at least one fluid delivery opening fluidly connected to the at least one fluid delivery plenum. With this arrangement, a first fluid is selectively delivered to the at least one fluid delivery plenum, passed through the at least one fluid delivery opening and mixed with a second fluid flowing through the plurality of fluid delivery tubes prior to being combusted in a combustion chamber of a turbine engine.
摘要翻译：用于涡轮发动机的预混合装置包括主体，其具有共同建立至少一个流体输送气室的入口部分，出口部分和外壁，以及延伸穿过至少一部分流体输送管道的多个流体输送管至少一个流体输送室。多个流体输送管中的每一个包括流体连接到至少一个流体输送室的至少一个流体输送开口。通过这种布置，第一流体被选择性地输送到至少一个流体输送气室，通过至少一个流体输送口，并且在燃烧在燃烧室中之前与流过多个流体输送管的第二流体混合的涡轮发动机。

8. 发明授权

US08147121B2 Pre-mixing apparatus for a turbine engine 有权
标题翻译：一种用于涡轮发动机的预混合装置
公开(公告)号：US08147121B2
公开(公告)日：2012-04-03
申请号：US12169865
申请日：2008-07-09
申请人： Benjamin Paul Lacy , Balachandar Varatharajan , Willy Steve Ziminsky , Gilbert Otto Kraemer , Ertan Yilmaz , Patrick Benedict Melton , Baifang Zuo , Christian Xavier Stevenson , David Kenton Felling , Jong Ho Uhm
发明人： Benjamin Paul Lacy , Balachandar Varatharajan , Willy Steve Ziminsky , Gilbert Otto Kraemer , Ertan Yilmaz , Patrick Benedict Melton , Baifang Zuo , Christian Xavier Stevenson , David Kenton Felling , Jong Ho Uhm
IPC分类号： B01F15/02 , B01F5/06 , B01F15/00
CPC分类号： F23R3/286 , F23R3/34
摘要： A pre-mixing apparatus for a turbine engine includes a main body having an inlet portion, an outlet portion and an exterior wall that collectively establish at least one fluid delivery plenum, and a plurality of fluid delivery tubes extending through at least a portion of the at least one fluid delivery plenum. Each of the plurality of fluid delivery tubes includes at least one fluid delivery opening fluidly connected to the at least one fluid delivery plenum. With this arrangement, a first fluid is selectively delivered to the at least one fluid delivery plenum, passed through the at least one fluid delivery opening and mixed with a second fluid flowing through the plurality of fluid delivery tubes prior to being combusted in a combustion chamber of a turbine engine.
摘要翻译：用于涡轮发动机的预混合装置包括主体，其具有共同建立至少一个流体输送气室的入口部分，出口部分和外壁，以及延伸穿过至少一部分流体输送管道的多个流体输送管至少一个流体输送室。多个流体输送管中的每一个包括流体连接到至少一个流体输送室的至少一个流体输送开口。通过这种布置，第一流体被选择性地输送到至少一个流体输送气室，通过至少一个流体输送口，并且在燃烧在燃烧室中之前与流过多个流体输送管的第二流体混合的涡轮发动机。

9. 发明授权

US07886991B2 Premixed direct injection nozzle 有权
标题翻译：预混直喷喷嘴
公开(公告)号：US07886991B2
公开(公告)日：2011-02-15
申请号：US12245266
申请日：2008-10-03
申请人： Baifang Zuo , Thomas Edward Johnson , Benjamin Paul Lacy , Willy Steve Ziminsky
发明人： Baifang Zuo , Thomas Edward Johnson , Benjamin Paul Lacy , Willy Steve Ziminsky
IPC分类号： B05B1/24
CPC分类号： F23R3/286 , F23R3/283
摘要： An injection nozzle having a main body portion with an outer peripheral wall is disclosed. The nozzle includes a plurality of fuel/air mixing tubes disposed within the main body portion and a fuel flow passage fluidly connected to the plurality of fuel/air mixing tubes. Fuel and air are partially premixed inside the plurality of the tubes. A second body portion, having an outer peripheral wall extending between a first end and an opposite second end, is connected to the main body portion. The partially premixed fuel and air mixture from the first body portion gets further mixed inside the second body portion. The second body portion converges from the first end toward said second end. The second body portion also includes cooling passages that extend along all the walls around the second body to provide thermal damage resistance for occasional flame flash back into the second body.
摘要翻译：公开了一种具有外周壁的主体部分的喷嘴。喷嘴包括设置在主体部分内的多个燃料/空气混合管和流体连接到多个燃料/空气混合管的燃料流动通道。燃料和空气在多个管内部分地预混合。具有在第一端和相对的第二端之间延伸的外周壁的第二主体部分连接到主体部分。来自第一主体部分的部分预混合的燃料和空气混合物在第二主体部分内被进一步混合。第二主体部分从第一端朝向所述第二端收敛。第二主体部分还包括沿着围绕第二主体的所有壁延伸的冷却通道，以提供对偶尔的火焰闪回第二主体的热损伤性。

10. 发明申请

US20110197587A1 MULTI-TUBE PREMIXING INJECTOR 审中-公开
标题翻译：多管预注射器
公开(公告)号：US20110197587A1
公开(公告)日：2011-08-18
申请号：US12707754
申请日：2010-02-18
申请人： Baifang Zuo , Thomas Edward Johnson , Benjamin Paul Lacy , Ertan Yilmaz , Willy Steve Ziminsky
发明人： Baifang Zuo , Thomas Edward Johnson , Benjamin Paul Lacy , Ertan Yilmaz , Willy Steve Ziminsky
IPC分类号： F02C7/22
CPC分类号： F23R3/286 , F23D14/02 , F23D14/62
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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