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51. 发明授权

US08984887B2 Combustor and method for supplying fuel to a combustor 有权
标题翻译：用于向燃烧器供应燃料的燃烧器和方法
公开(公告)号：US08984887B2
公开(公告)日：2015-03-24
申请号：US13244526
申请日：2011-09-25
申请人： Jonathan Dwight Berry
发明人： Jonathan Dwight Berry
IPC分类号： F23R3/28 , F23R3/36
CPC分类号： F23R3/286 , F23R3/36
摘要： A combustor includes an end cap having an upstream surface axially separated from a downstream surface and a cap shield circumferentially surrounding the upstream and downstream surfaces. A first circuit of tubes extends from the upstream surface through the downstream surface. A first fuel plenum is in fluid communication with the first circuit of tubes. A second circuit of tubes extends from the upstream surface through the downstream surface. A second fuel plenum downstream from the first fuel plenum is in fluid communication with the second circuit of tubes. A method for supplying fuel to a combustor includes flowing a working fluid through tubes, flowing fuel or diluent from a first fuel plenum through a first circuit of tubes, and flowing fuel or diluent from a second fuel plenum through a second circuit of tubes, wherein the second fuel plenum is downstream from the first fuel plenum.
摘要翻译：燃烧器包括具有从下游表面轴向分离的上游表面的端盖和周向围绕上游表面和下游表面的盖屏蔽。管的第一回路从上游表面延伸穿过下游表面。第一燃料增压室与管的第一回路流体连通。管的第二回路从上游表面延伸穿过下游表面。从第一燃料增压室下游的第二燃料增压室与管的第二回路流体连通。用于向燃烧器供应燃料的方法包括使工作流体通过管流动，使来自第一燃料增压室的燃料或稀释剂流经管的第一回路，以及将来自第二燃料增压室的燃料或稀释剂流经管的第二回路，第二燃料增压室位于第一燃料增压室的下游。

52. 发明授权

US08904797B2 Sector nozzle mounting systems 有权
标题翻译：扇形喷嘴安装系统
公开(公告)号：US08904797B2
公开(公告)日：2014-12-09
申请号：US13194178
申请日：2011-07-29
申请人： Jonathan Dwight Berry , Derrick Walter Simons , Jason Thurman Stewart
发明人： Jonathan Dwight Berry , Derrick Walter Simons , Jason Thurman Stewart
IPC分类号： F02C1/00 , F23R3/28
CPC分类号： F23R3/283 , F23M20/005 , F23R3/286 , F23R2900/00005 , F23R2900/00014
摘要： Systems are provided for mounting sector nozzles within gas turbine combustors. In one embodiment, a sector nozzle includes a nozzle portion configured to mix fuel and air to produce a fuel-air mixture and a shell coupled to the nozzle portion. The sector nozzle also includes a first longitudinal strut and a second longitudinal strut coupled to a first surface of the shell on opposite sides of a window within the first surface. A third longitudinal strut is coupled to a second surface of the shell, and the second surface is disposed opposite of the first surface.
摘要翻译：提供了用于在燃气轮机燃烧器中安装扇形喷嘴的系统。在一个实施例中，扇形喷嘴包括配置成混合燃料和空气以产生燃料 - 空气混合物的喷嘴部分和联接到喷嘴部分的壳体。扇形喷嘴还包括第一纵向支柱和第二纵向支柱，该第二纵向支柱在第一表面内的窗口的相对侧上联接到壳体的第一表面。第三纵向支柱联接到壳体的第二表面，并且第二表面设置成与第一表面相对。

53. 发明申请

US20130305739A1 FUEL NOZZLE CAP 审中-公开
标题翻译：燃油喷嘴盖
公开(公告)号：US20130305739A1
公开(公告)日：2013-11-21
申请号：US13475887
申请日：2012-05-18
申请人： Jonathan Dwight Berry
发明人： Jonathan Dwight Berry
IPC分类号： F02C7/20 , F02C6/08 , F23R3/54 , F23R3/28 , F02C7/18
CPC分类号： F23R3/283 , F23R3/286
摘要： Certain embodiments include a first individual sector configured to fit together with a plurality of individual sectors to form a combustor cap assembly of a turbine combustor, wherein the first individual sector is configured to fixedly attach to a first fuel nozzle of a plurality of fuel nozzles, the first individual sector comprises a first substantially enclosed cavity configured to surround the first fuel nozzle, and the first substantially enclosed cavity is configured to receive a cooling air flow.
摘要翻译：某些实施例包括被配置成与多个单独的扇区配合在一起以形成涡轮机燃烧器的燃烧器盖组件的第一单独扇区，其中第一单独扇区被构造成固定地连接到多个燃料喷嘴的第一燃料喷嘴，第一单独扇区包括构造成围绕第一燃料喷嘴的第一基本上封闭的空腔，并且第一基本上封闭的空腔构造成接收冷却空气流。

54. 发明授权

US08567199B2 Method and apparatus of introducing diluent flow into a combustor 有权
标题翻译：将稀释剂流引入燃烧器的方法和装置
公开(公告)号：US08567199B2
公开(公告)日：2013-10-29
申请号：US12250995
申请日：2008-10-14
申请人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Patrick Benedict Melton
发明人： Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Patrick Benedict Melton
IPC分类号： F02C3/20
CPC分类号： F23R3/28 , F23L7/00 , F23L2900/07002 , F23L2900/07009
摘要： Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. A plurality of injection holes extend through the at least one fuel nozzle and are configured to meter a flow of diluent into the combustor. Further disclosed is a method for providing diluent to a combustor including providing a plurality of openings located at at least one fuel nozzle extending through a through hole in a baffle plate. The diluent is flowed through the plurality of openings toward at least one airflow opening in the at least one fuel nozzle.
摘要翻译：公开了一种燃烧器，其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。多个喷射孔延伸穿过至少一个燃料喷嘴，并被配置成计量稀释剂流入燃烧器的流量。还公开了一种用于向燃烧器提供稀释剂的方法，包括提供多个位于至少一个延伸穿过挡板中的通孔的燃料喷嘴的开口。稀释剂通过多个开口朝向至少一个燃料喷嘴中的至少一个气流开口流动。

55. 发明授权

US08550809B2 Combustor and method for conditioning flow through a combustor 有权
标题翻译：用于调节通过燃烧器的流动的燃烧器和方法
公开(公告)号：US08550809B2
公开(公告)日：2013-10-08
申请号：US13277516
申请日：2011-10-20
申请人： Jong Ho Uhm , Chunyang Wu , Jonathan Dwight Berry , Jason Thurman Stewart
发明人： Jong Ho Uhm , Chunyang Wu , Jonathan Dwight Berry , Jason Thurman Stewart
IPC分类号： F23D14/62
CPC分类号： F23R3/10 , F23R3/286 , F23R3/343
摘要： A combustor includes an end cap that extends radially across a portion of the combustor and includes an upstream surface axially separated from a downstream surface. A combustion chamber is downstream of the end cap. Premixer tubes extend from a premixer tube inlet proximate to the upstream surface through the downstream surface to provide fluid communication through the end cap and include means for conditioning flow through the plurality of premixer tubes. A method for conditioning flow through a combustor includes flowing a working fluid through a first and second set of premixer tubes that extend axially through an end cap, wherein the second set of premixer tubes includes means for conditioning flow through the second set of premixer tubes, and flowing a fuel through the first or second set of premixer tubes.
摘要翻译：燃烧器包括端盖，其径向延伸穿过燃烧器的一部分并且包括与下游表面轴向分离的上游表面。燃烧室位于端盖的下游。预混合器管从靠近上游表面的预混合器入口通过下游表面延伸以提供通过端盖的流体连通，并且包括用于调节通过多个预混合器管的流动的装置。用于调节通过燃烧器的流动的方法包括使工作流体流过轴向延伸通过端盖的第一组和第二组预混合管，其中第二组预混合管包括用于调节通过第二组预混合管的流动的装置，并使燃料流过第一组或第二组预混合器管。

56. 发明申请

US20130192234A1 BUNDLED MULTI-TUBE NOZZLE ASSEMBLY 审中-公开
标题翻译：整套多管喷头组件
公开(公告)号：US20130192234A1
公开(公告)日：2013-08-01
申请号：US13359033
申请日：2012-01-26
申请人： Jason Thurman Stewart , Christopher Paul Keener , Jonathan Dwight Berry , Michael John Hughes
发明人： Jason Thurman Stewart , Christopher Paul Keener , Jonathan Dwight Berry , Michael John Hughes
IPC分类号： F02M63/00 , F02M51/00 , F15D1/00
CPC分类号： F23D14/08 , F23D14/64 , F23D14/66 , F23D14/70 , F23D2900/14481 , F23R3/286 , Y02E20/348 , Y10T137/0318
摘要： A method for reducing emissions in a turbo machine is disclosed. The method includes providing fuel to a multi-tube nozzle and reducing the differences in the mass flow rate of fuel into each tube. An improved multi-tube nozzle is also disclosed. The nozzle includes an assembly that reduces the difference in the mass flow rate of fuel into each tube.
摘要翻译：公开了一种减少涡轮机排放的方法。该方法包括向多管喷嘴提供燃料并且减少燃料进入每个管的质量流率的差异。还公开了一种改进的多管喷嘴。喷嘴包括减少燃料进入每个管的质量流量差的组件。

57. 发明申请

US20130101943A1 COMBUSTOR AND METHOD FOR CONDITIONING FLOW THROUGH A COMBUSTOR 有权
标题翻译：用于通过燃烧器调节流量的COMBUSTOR和方法
公开(公告)号：US20130101943A1
公开(公告)日：2013-04-25
申请号：US13277516
申请日：2011-10-20
申请人： Jong Ho Uhm , Chunyang Wu , Jonathan Dwight Berry , Jason Thurman Stewart
发明人： Jong Ho Uhm , Chunyang Wu , Jonathan Dwight Berry , Jason Thurman Stewart
IPC分类号： F23D14/62
CPC分类号： F23R3/10 , F23R3/286 , F23R3/343
摘要： A combustor includes an end cap that extends radially across a portion of the combustor and includes an upstream surface axially separated from a downstream surface. A combustion chamber is downstream of the end cap. Premixer tubes extend from a premixer tube inlet proximate to the upstream surface through the downstream surface to provide fluid communication through the end cap and include means for conditioning flow through the plurality of premixer tubes. A method for conditioning flow through a combustor includes flowing a working fluid through a first and second set of premixer tubes that extend axially through an end cap, wherein the second set of premixer tubes includes means for conditioning flow through the second set of premixer tubes, and flowing a fuel through the first or second set of premixer tubes.
摘要翻译：燃烧器包括端盖，其径向延伸穿过燃烧器的一部分并且包括与下游表面轴向分离的上游表面。燃烧室位于端盖的下游。预混合器管从靠近上游表面的预混合管入口延伸穿过下游表面以提供通过端盖的流体连通，并且包括用于调节通过多个预混合器管的流动的装置。用于调节通过燃烧器的流动的方法包括使工作流体流过轴向延伸通过端盖的第一组和第二组预混合管，其中第二组预混合管包括用于调节通过第二组预混合管的流动的装置，并使燃料流过第一组或第二组预混合器管。

58. 发明授权

US08397482B2 Dry 3-way catalytic reduction of gas turbine NOx 有权
标题翻译：燃气轮机NOx的干式三元催化还原
公开(公告)号：US08397482B2
公开(公告)日：2013-03-19
申请号：US12153231
申请日：2008-05-15
申请人： Gilbert Otto Kraemer , Ashok Kumar Anand , James Anthony West , Hasan Ul Karim , Sam David Draper , Jonathan Dwight Berry
发明人： Gilbert Otto Kraemer , Ashok Kumar Anand , James Anthony West , Hasan Ul Karim , Sam David Draper , Jonathan Dwight Berry
IPC分类号： F02C7/08 , F02G1/00 , F02G3/00
CPC分类号： F02C3/34 , B01D53/8625 , B01D53/8643 , B01D2255/1021 , B01D2255/204 , B01D2255/206 , B01D2255/20715 , B01D2255/2092 , F02C6/18 , Y02E20/16 , Y02T10/22
摘要： A power generation system capable of eliminating NOx components in the exhaust gas by using a 3-way catalyst, comprising a gas compressor to increase the pressure of ambient air fed to the system; a combustor capable of oxidizing a mixture of fuel and compressed air to generate an expanded, high temperature exhaust gas; a gas turbine engine that uses the force of the high temperature gas; an exhaust gas recycle (EGR) stream back to the combustor; a 3-way catalytic reactor downstream of the gas turbine engine outlet which treats the exhaust gas stream to remove substantially all of the NOx components; a heat recovery steam generator (HRSG); an EGR compressor; and an electrical generator.
摘要翻译：一种能够通过使用三元催化剂消除废气中的NOx成分的发电系统，其包括气体压缩机，以增加供给到系统的环境空气的压力; 能够氧化燃料和压缩空气的混合物以产生膨胀的高温废气的燃烧器; 使用高温气体的力的燃气轮机; 废气再循环（EGR）流回燃烧器; 在燃气涡轮发动机出口下游的三元催化反应器，其处理排气流以去除基本上所有的NOx组分; 热回收蒸汽发生器（HRSG）; 一个EGR压缩机; 和发电机。

59. 发明授权

US08266912B2 Reusable weld joint for syngas fuel nozzles 有权
标题翻译：合成气燃料喷嘴可重复使用的焊缝
公开(公告)号：US08266912B2
公开(公告)日：2012-09-18
申请号：US12211791
申请日：2008-09-16
申请人： Jonathan Dwight Berry , James T. Brown
发明人： Jonathan Dwight Berry , James T. Brown
IPC分类号： F02C1/00 , F02C7/20 , F02G3/00 , F16J15/02
CPC分类号： F02C7/28 , F23R3/12 , F23R3/283 , F23R2900/00002 , F23R2900/00012 , F23R2900/00017 , Y02T50/675 , Y02T50/678
摘要： A system, one embodiment, includes an annular seal configured to seal a turbine fuel nozzle to a turbine combustor, wherein the annular seal includes a first annular seal portion having an inner annular surface, a first base portion, and a first peripheral portion opposite from the first base portion. The embodiment also includes the first annular seal portion configured to couple to a second annular seal portion having an outer annular surface, a second base portion, and a second peripheral portion opposite from the second base portion. Further, the embodiment includes the first and second peripheral portions sealable by a weld.
摘要翻译：一个实施例的系统包括环形密封件，其构造成将涡轮燃料喷嘴密封到涡轮机燃烧器，其中环形密封件包括具有内环形表面的第一环形密封部分，第一基部部分和与第一周边部分相对的第一周边部分第一基部。该实施例还包括第一环形密封部分，其构造成联接到具有外环形表面的第二环形密封部分，第二基部部分和与第二基部部分相对的第二周边部分。此外，该实施例包括可通过焊接密封的第一和第二周边部分。

60. 发明申请

US20120204571A1 COMBUSTOR AND METHOD FOR INTRODUCING A SECONDARY FLUID INTO A FUEL NOZZLE 审中-公开
标题翻译：用于将二次流体引入燃料喷嘴的燃烧器和方法
公开(公告)号：US20120204571A1
公开(公告)日：2012-08-16
申请号：US13027815
申请日：2011-02-15
申请人： Gilbert Otto Kraemer , Jonathan Dwight Berry , Predrag Popovic
发明人： Gilbert Otto Kraemer , Jonathan Dwight Berry , Predrag Popovic
IPC分类号： F02C7/22 , F23R3/00
CPC分类号： F23R3/286 , F23D14/48 , F23L7/007 , F23L2900/07002 , F23L2900/07005 , Y02E20/344
摘要： A combustor is disclosed that includes a baffle plate and a fuel nozzle extending through the baffle plate. The combustor may also include a shroud extending from the baffle plate and surrounding at least a portion of the fuel nozzle. A passage may be defined between the shroud and an outer surface of the fuel nozzle for receiving a first fluid. Additionally, the passage may be sealed from a second fluid flowing adjacent to the shroud.
摘要翻译：公开了一种燃烧器，其包括挡板和延伸穿过挡板的燃料喷嘴。燃烧器还可以包括从挡板延伸并围绕燃料喷嘴的至少一部分的护罩。可以在护罩和用于接收第一流体的燃料喷嘴的外表面之间限定通道。此外，通道可以与邻近护罩流动的第二流体密封。

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