公开(公告)号：US20130192234A1

公开(公告)日：2013-08-01

申请号：US13359033

申请日：2012-01-26

Applicant: Jason Thurman Stewart ,  Christopher Paul Keener ,  Jonathan Dwight Berry ,  Michael John Hughes

Inventor： Jason Thurman Stewart ,  Christopher Paul Keener ,  Jonathan Dwight Berry ,  Michael John Hughes

IPC: F02M63/00 ,  F02M51/00 ,  F15D1/00

CPC classification number: F23D14/08 ,  F23D14/64 ,  F23D14/66 ,  F23D14/70 ,  F23D2900/14481 ,  F23R3/286 ,  Y02E20/348 ,  Y10T137/0318

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20130101943A1

公开(公告)日：2013-04-25

申请号：US13277516

申请日：2011-10-20

Applicant: Jong Ho Uhm ,  Chunyang Wu ,  Jonathan Dwight Berry ,  Jason Thurman Stewart

Inventor： Jong Ho Uhm ,  Chunyang Wu ,  Jonathan Dwight Berry ,  Jason Thurman Stewart

IPC: F23D14/62

CPC classification number: F23R3/10 ,  F23R3/286 ,  F23R3/343

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US08397482B2

公开(公告)日：2013-03-19

申请号：US12153231

申请日：2008-05-15

Applicant: Gilbert Otto Kraemer ,  Ashok Kumar Anand ,  James Anthony West ,  Hasan Ul Karim ,  Sam David Draper ,  Jonathan Dwight Berry

Inventor： Gilbert Otto Kraemer ,  Ashok Kumar Anand ,  James Anthony West ,  Hasan Ul Karim ,  Sam David Draper ,  Jonathan Dwight Berry

IPC: F02C7/08 ,  F02G1/00 ,  F02G3/00

CPC classification number: F02C3/34 ,  B01D53/8625 ,  B01D53/8643 ,  B01D2255/1021 ,  B01D2255/204 ,  B01D2255/206 ,  B01D2255/20715 ,  B01D2255/2092 ,  F02C6/18 ,  Y02E20/16 ,  Y02T10/22

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20120291352A1

公开(公告)日：2012-11-22

申请号：US13566545

申请日：2012-08-03

Applicant: Jonathan Dwight Berry ,  Hasan Karim ,  Abdul Rafey Khan

Inventor： Jonathan Dwight Berry ,  Hasan Karim ,  Abdul Rafey Khan

IPC: C10L3/00

CPC classification number: C01B3/386 ,  B01J8/0278 ,  B01J2208/00176 ,  B01J2208/00221 ,  B01J2208/00371 ,  B01J2208/0053 ,  B01J2208/00849 ,  C01B2203/0261 ,  C01B2203/0877 ,  C01B2203/0883 ,  C01B2203/84 ,  C10J3/466 ,  C10J2200/09 ,  C10J2300/0959 ,  C10J2300/0989 ,  C10J2300/1861 ,  C10J2300/1884 ,  F23C2900/03002

Abstract: The present subject matter discloses a fluid cooled reformer for gas turbine systems and a method for cooling both a fuel reformer and a heated reformate stream produced by such fuel reformer. The fluid cooled reformer may include a pressure vessel and a reactor assembly disposed within the pressure vessel, The reactor assembly may include a reactor and may be configured to receive and reform an oxygen/fuel mixture to produce a heated reformate stream. Additionally, the fluid cooled reformer may include an inlet configured to direct a fluid stream into the pressure vessel. At least a portion of the fluid stream may be used to cool the reactor assembly. A reformate cooling section may be disposed downstream of the reactor of the reactor assembly and may be configured to cool the heated reformate stream.

Abstract translation: 本发明公开了一种用于燃气轮机系统的流体冷却重整器和用于冷却由这种燃料重整器生产的燃料重整器和加热的重整产品流的方法。 流体冷却的重整器可以包括压力容器和设置在压力容器内的反应器组件。反应器组件可以包括反应器，并且可以被配置为接收和改造氧/燃料混合物以产生加热的重整产物流。 此外，流体冷却的重整器可以包括构造成将流体流引导到压力容器中的入口。 流体流的至少一部分可用于冷却反应器组件。 重整物冷却段可以设置在反应器组件的反应器的下游，并且可以被配置为冷却加热的重整产物流。

公开(公告)号：US08266912B2

公开(公告)日：2012-09-18

申请号：US12211791

申请日：2008-09-16

Applicant: Jonathan Dwight Berry ,  James T. Brown

Inventor： Jonathan Dwight Berry ,  James T. Brown

IPC: F02C1/00 ,  F02C7/20 ,  F02G3/00 ,  F16J15/02

CPC classification number: F02C7/28 ,  F23R3/12 ,  F23R3/283 ,  F23R2900/00002 ,  F23R2900/00012 ,  F23R2900/00017 ,  Y02T50/675 ,  Y02T50/678

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20120204571A1

公开(公告)日：2012-08-16

申请号：US13027815

申请日：2011-02-15

Applicant: Gilbert Otto Kraemer ,  Jonathan Dwight Berry ,  Predrag Popovic

Inventor： Gilbert Otto Kraemer ,  Jonathan Dwight Berry ,  Predrag Popovic

IPC: F02C7/22 ,  F23R3/00

CPC classification number: F23R3/286 ,  F23D14/48 ,  F23L7/007 ,  F23L2900/07002 ,  F23L2900/07005 ,  Y02E20/344

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20120186266A1

公开(公告)日：2012-07-26

申请号：US13010828

申请日：2011-01-21

Applicant: Abdul Rafey Khan ,  Hasan Karim ,  Jonathan Dwight Berry

Inventor： Abdul Rafey Khan ,  Hasan Karim ,  Jonathan Dwight Berry

IPC: F02C6/18 ,  F02G3/00

CPC classification number: F02C3/20 ,  F02C7/22 ,  F23C2900/03002 ,  F23R3/28 ,  Y02T50/678

Abstract: A reformer for use in a gas turbine engine specially configured to treat a supplemental fuel feed to the combustor that includes a reformer core containing a catalyst composition and an inlet flow channel for transporting the reformer fuel mixture, air and steam (either saturated or superheated) into a reformer core. An outlet flow channel transports the resulting reformate stream containing reformed and thermally cracked hydrocarbons and substantial amounts of hydrogen out of the reformer core for later combination with the main combustor feed. Because the catalytic partial oxidation reaction in the reformer is highly exothermic, the additional heat is transferred (and thermally integrated) using one or more heat exchange units for a first and/or second auxiliary gas turbine fuel stream that undergo thermal cracking and vaporization before combining with the reformate. The combined, hydrogen-enriched feed significantly improves combustor performance.

Abstract translation: 一种用于燃气涡轮发动机的改质器，其特别构造为处理燃烧器的补充燃料，其包括含有催化剂组合物的重整器芯和用于输送重整器燃料混合物的入口流动通道，空气和蒸汽（饱和或过热） 进入重组核心。 出口流动通道将得到的重整产物流输送到重整器芯中，以便与主燃烧器进料混合。 因为重整器中的催化部分氧化反应是高度放热的，所以使用一个或多个用于在组合之前经受热裂解和蒸发的第一和/或第二辅助燃气轮机燃料流的热交换单元转移（并热集成）附加的热量 与重组。 组合的富氢进料显着提高了燃烧室性能。

公开(公告)号：US08191373B2

公开(公告)日：2012-06-05

申请号：US12366913

申请日：2009-02-06

Applicant: Jonathan Dwight Berry ,  Timur Rustemovich Repikov ,  Heath Michael Ostebee

Inventor： Jonathan Dwight Berry ,  Timur Rustemovich Repikov ,  Heath Michael Ostebee

IPC: F02C1/00 ,  F02C7/20

CPC classification number: F23R3/60 ,  F23M5/04 ,  F23R3/002 ,  F23R2900/00017 ,  F23R2900/03044

Abstract: An impingement shield assembly for a turbine includes a first impingement shield portion and a second impingement shield joined to the first impingement shield portion. The assembly also includes a first connection portion formed on the first impingement shield portion, a second connection portion formed on the first impingement shield portion and first and second wedge weld portions that mate with and hold the first and a second connection portions in a fixed relationship to one another.

Abstract translation: 用于涡轮机的冲击屏蔽组件包括第一冲击屏蔽部分和与第一冲击屏蔽部分接合的第二冲击屏蔽。 组件还包括形成在第一冲击屏蔽部分上的第一连接部分，形成在第一冲击屏蔽部分上的第二连接部分和第一和第二楔形焊接部分，第一和第二楔形焊接部分以固定关系与第一和第二连接部分配合 彼此。

公开(公告)号：US20120079829A1

公开(公告)日：2012-04-05

申请号：US12898267

申请日：2010-10-05

Applicant: Jonathan Dwight Berry ,  Chunyang Wu ,  Baifang Zuo

Inventor： Jonathan Dwight Berry ,  Chunyang Wu ,  Baifang Zuo

IPC: F02C1/00 ,  F02C7/22

CPC classification number: F23R3/286 ,  F23D2900/00003 ,  F23R3/12

Abstract: A turbomachine includes a compressor section, a combustor operatively connected to the compressor section, an end cover mounted to the combustor, and an injection nozzle assembly operatively connected to the combustor. The injection nozzle assembly includes a plurality of mixing tube elements. Each of the plurality of mixing tube elements includes a conduit having a first fluid inlet, a second fluid inlet arranged downstream from the first fluid inlet, a discharge end arranged downstream from the first and second fluid inlets, and a vortex generator arranged between the first and second fluid inlets. The vortex generator is configured and disposed to create multiple vortices within the conduit to mix first and second fluids passing through each of the plurality of mixing tube elements.

Abstract translation: 涡轮机包括压缩机部分，可操作地连接到压缩机部分的燃烧器，安装到燃烧器的端盖以及可操作地连接到燃烧器的喷嘴组件。 注射喷嘴组件包括多个混合管元件。 多个混合管元件中的每一个包括具有第一流体入口，布置在第一流体入口下游的第二流体入口，布置在第一和第二流体入口下游的排放端，以及设置在第一流体入口之间的涡流发生器 和第二个流体入口。 涡流发生器被配置和设置成在管道内产生多个涡流以混合通过多个混合管元件中的每一个的第一和第二流体。

公开(公告)号：US20120055167A1

公开(公告)日：2012-03-08

申请号：US12877385

申请日：2010-09-08

Applicant: Thomas Edward Johnson ,  Willy Steve Ziminsky ,  Jonathan Dwight Berry

Inventor： Thomas Edward Johnson ,  Willy Steve Ziminsky ,  Jonathan Dwight Berry

IPC: F02C7/22

CPC classification number: F23R3/286 ,  F01D9/023 ,  F23R3/005 ,  F23R3/54 ,  F23R2900/00002

Abstract: A nozzle includes a fuel plenum and an air plenum downstream of the fuel plenum. A primary fuel channel includes an inlet in fluid communication with the fuel plenum and a primary air port in fluid communication with the air plenum. Secondary fuel channels radially outward of the primary fuel channel include a secondary fuel port in fluid communication with the fuel plenum. A shroud circumferentially surrounds the secondary fuel channels. A method for mixing fuel and air in a nozzle prior to combustion includes flowing fuel to a fuel plenum and flowing air to an air plenum downstream of the fuel plenum. The method further includes injecting fuel from the fuel plenum through a primary fuel passage, injecting fuel from the fuel plenum through secondary fuel passages, and injecting air from the air plenum through the primary fuel passage.

Abstract translation: 喷嘴包括燃料增压室和在燃料增压室下游的空气增压室。 主要燃料通道包括与燃料增压室流体连通的入口和与空气压力室流体连通的主空气端口。 主要燃料通道径向向外的次级燃料通道包括与燃料增压室流体连通的次级燃料口。 护罩周向地包围二次燃料通道。 在燃烧之前将燃料和空气混合在喷嘴中的方法包括将燃料流入燃料增压室并将空气流到燃料增压室下游的空气压力室。 该方法还包括从燃料通风室喷射燃料通过主燃料通道，从燃料通风室喷射燃料通过二次燃料通道，以及从空气通风室喷射空气通过主燃料通道。