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    Fluid Cooled Reformer and Method for Cooling a Reformer
    82.
    发明申请
    Fluid Cooled Reformer and Method for Cooling a Reformer 有权
    流体冷却重整器和冷却重整器的方法

    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。

    Reusable weld joint for syngas fuel nozzles
    83.
    发明授权
    Reusable weld joint for syngas fuel nozzles 有权
    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

    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。

    REFORMED MULTI-FUEL PREMIXED LOW EMISSION COMBUSTOR AND RELATED METHOD
    85.
    发明申请
    REFORMED MULTI-FUEL PREMIXED LOW EMISSION COMBUSTOR AND RELATED METHOD 有权
    改进的多燃料低排放COMBUSTOR及相关方法

    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。

    Interlocking retention strip
    86.
    发明授权
    Interlocking retention strip 有权
    联锁保持条

    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。

    TURBOMACHINE INCLUDING A MIXING TUBE ELEMENT HAVING A VORTEX GENERATOR
    87.
    发明申请
    TURBOMACHINE INCLUDING A MIXING TUBE ELEMENT HAVING A VORTEX GENERATOR 有权
    涡轮发动机包括具有VORTEX发电机的混合管元件

    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。

    APPARATUS AND METHOD FOR MIXING FUEL IN A GAS TURBINE NOZZLE
    88.
    发明申请
    APPARATUS AND METHOD FOR MIXING FUEL IN A GAS TURBINE NOZZLE 有权
    燃气涡轮喷嘴混合燃料的装置和方法

    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。

    METHOD AND FLOW SLEEVE PROFILE REDUCTION TO EXTEND COMBUSTOR LINER LIFE
    90.
    发明申请
    METHOD AND FLOW SLEEVE PROFILE REDUCTION TO EXTEND COMBUSTOR LINER LIFE 审中-公开
    方法和流程套件减少扩展COMBUSTOR LINER LIFE

    公开(公告)号：US20100300107A1

    公开(公告)日：2010-12-02

    申请号：US12474371

    申请日：2009-05-29

    Applicant: Jesse Ellis Barton ,  Jonathan Dwight Berry ,  James Thomas Brown ,  Mark Allan Hadley ,  Patrick Benedict Melton ,  Svetlana Yakubova

    Inventor： Jesse Ellis Barton ,  Jonathan Dwight Berry ,  James Thomas Brown ,  Mark Allan Hadley ,  Patrick Benedict Melton ,  Svetlana Yakubova

    IPC: F02C7/12 ,  F23R3/42

    CPC classification number: F23R3/002 ,  F23R3/005

    Abstract: A gas turbine includes a combustor liner having at least one hole formed therein. The gas turbine also includes a flow sleeve that at least partially surrounds the liner thereby forming a plenum between the flow sleeve and the liner, the plenum having an airflow therethrough, a portion of the airflow passing through the at least one hole in the liner and into the liner thereby reducing the mass of the airflow in the plenum. The flow sleeve has an axial profile that is reduced in cross section dimension at a predetermined axial location of the flow sleeve, thereby reducing a width of the plenum at the predetermined axial location. The reduction at the cross section dimension in the flow sleeve increases a velocity of the airflow in the plenum at the predetermined axial location, the increased velocity airflow increasing transfer of heat away from the liner.

    Abstract translation: 燃气轮机包括其中形成有至少一个孔的燃烧器衬套。 燃气轮机还包括至少部分地围绕衬套的流动套管，从而在流动套筒和衬套之间形成一个气室，气室具有穿过其中的气流，一部分气流穿过衬套中的至少一个孔， 进入衬里，从而减小了气室中气流的质量。 流动套筒具有在流动套筒的预定轴向位置处的横截面尺寸减小的轴向轮廓，从而减小了在预定轴向位置处的增压室的宽度。 流动套管中的横截面尺寸的减小增加了在预定轴向位置处的增压室中的气流的速度，增加的速度气流增加了热量从衬套的转移。

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