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公开(公告)号：US20130086912A1
公开(公告)日：2013-04-11
申请号：US13267828
申请日：2011-10-06
Applicant: Jonathan Dwight Berry
Inventor： Jonathan Dwight Berry
CPC classification number: F23R3/283 , F23D2214/00 , F23R3/286 , F23R2900/03043 , F23R2900/03044 , Y02T50/675
Abstract: A system includes a multi-tube fuel nozzle including a fuel nozzle head that includes an outer wall surrounding a chamber. The outer wall includes a downstream wall portion configured to face a combustion region. The multi-tube fuel nozzle also includes multiple tubes extending through the chamber to the downstream wall portion. Each tube of the multiple tubes includes an upstream portion, a downstream portion, and at least one fuel inlet disposed at the upstream portion, and is configured to receive air and mix the air with fuel from the at least one fuel inlet. The multi-tube fuel nozzle includes a fuel conduit extending through the chamber crosswise to and around the multiple tubes. The fuel conduit includes multiple impingement cooling orifices. A fuel flow path extends through the fuel conduit, through the impingement cooling orifices, through the chamber, and into the at least one fuel inlet of each tube.
Abstract translation: 一种系统包括多管燃料喷嘴，其包括燃料喷嘴头，燃料喷嘴头包括围绕室的外壁。 外壁包括构造成面对燃烧区域的下游壁部分。 多管燃料喷嘴还包括多个管，其延伸穿过室至下游壁部分。 多个管的每个管包括上游部分，下游部分和设置在上游部分处的至少一个燃料入口，并且构造成接收空气并将空气与来自至少一个燃料入口的燃料混合。 该多管燃料喷嘴包括一个燃料管道，该燃料管道横跨多个管道并围绕多个管道延伸穿过该腔室。 燃料管道包括多个冲击冷却孔。 燃料流动路径延伸穿过燃料管道，穿过冲击冷却孔通过室，并且进入每个管的至少一个燃料入口。
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公开(公告)号：US20120279223A1
公开(公告)日：2012-11-08
申请号：US13099853
申请日：2011-05-03
Applicant: Carl Robert Barker , Thomas Edward Johnson , Jonathan Dwight Berry
Inventor： Carl Robert Barker , Thomas Edward Johnson , Jonathan Dwight Berry
CPC classification number: F23R3/283 , F23R3/286 , F23R3/34 , F23R3/46 , F23R2900/00014 , F23R2900/00017
Abstract: An integrated plate is provided for use with a combustor including a casing, a fuel plenum extending circumferentially about the casing, and a fuel nozzle extending axially through the casing. The integrated plate includes a plurality of fuel injection pegs that extend radially between the fuel plenum and the fuel nozzle.
Abstract translation: 提供了一种集成板，其用于燃烧器，所述燃烧器包括壳体，围绕壳体周向延伸的燃料增压室和沿轴向延伸穿过壳体的燃料喷嘴。 集成板包括在燃料室和燃料喷嘴之间径向延伸的多个燃料喷射栓。
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63.发明授权公开(公告)号：US08276391B2
公开(公告)日：2012-10-02
申请号：US12762842
申请日：2010-04-19
Applicant: Jonathan Dwight Berry , Kara Johnston Edwards , Heath Michael Ostebee
Inventor： Jonathan Dwight Berry , Kara Johnston Edwards , Heath Michael Ostebee
Abstract: A resilient annular seal structure is disposed radially between an aft end portion of a combustor liner and a forward end portion of a transition piece, the resilient annular seal structure configured to form a first annular cavity radially between the forward end portion of the transition piece and the aft end portion of said combustor. At least one transfer tube radially extends from the second flow sleeve through the second flow annulus to the transition piece, and is arranged to supply compressor discharge cooling air radially from an area outside the first and second substantially axially extending flow annuli directly to the resilient annular seal structure and to the aft end of the combustor liner.
Abstract translation: 弹性环形密封结构径向设置在燃烧器衬套的后端部分与过渡件的前端部分之间，该弹性环形密封结构构造成在过渡件的前端部分和 所述燃烧器的后端部分。 至少一个传送管从第二流动套管径向地延伸穿过第二流动环到过渡件，并且被布置成将压缩机排出冷却空气从第一和第二大致轴向延伸的流动环的外部径向径向地供应到弹性环 密封结构和燃烧器衬套的后端。
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公开(公告)号：US20120055168A1
公开(公告)日：2012-03-08
申请号：US12877363
申请日：2010-09-08
Applicant: Jonathan Dwight Berry , Michael John Hughes
Inventor： Jonathan Dwight Berry , Michael John Hughes
Abstract: A system for providing hydrogen enriched fuel includes first and second gas turbines. The second gas turbine receives a portion of compressed working fluid from the first gas turbine and produces a reformed fuel, and a fuel skid provides fluid communication between a turbine in the second gas turbine and a combustor in the first gas turbine. A method for providing hydrogen enriched fuel includes diverting a portion of a first compressed working fluid from a first compressor to a second compressor and providing a second compressed working fluid from the second compressor. The method further includes mixing a fuel with the second compressed working fluid in a reformer to produce a reformed fuel, flowing the reformed fuel through a second turbine to cool the reformed fuel, and connecting the second turbine to the second compressor so that the second turbine drives the second compressor.
Abstract translation: 一种用于提供富氢燃料的系统包括第一和第二燃气轮机。 第二燃气轮机从第一燃气轮机接收压缩的工作流体的一部分并产生重整的燃料，并且燃料滑道提供第二燃气轮机中的涡轮与第一燃气轮机中的燃烧器之间的流体连通。 提供富氢燃料的方法包括将第一压缩工作流体的一部分从第一压缩机转向第二压缩机，并从第二压缩机提供第二压缩工作流体。 该方法还包括在重整器中将燃料与第二压缩工作流体混合以产生重整燃料，使重整燃料流过第二涡轮以冷却重整燃料，并将第二涡轮连接到第二压缩机，使得第二涡轮 驱动第二压缩机。
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公开(公告)号：US20110243805A1
公开(公告)日：2011-10-06
申请号：US12749985
申请日：2010-03-30
Applicant: Jonathan Dwight Berry , Hasan Karim , Abdul Rafey Khan
Inventor： Jonathan Dwight Berry , Hasan Karim , Abdul Rafey Khan
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产生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。
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Patent Agency Ranking
66.发明申请公开(公告)号：US20110179803A1
公开(公告)日：2011-07-28
申请号：US12694544
申请日：2010-01-27
Applicant: JONATHAN DWIGHT BERRY , MICHAEL JOHN HUGHES
Inventor： JONATHAN DWIGHT BERRY , MICHAEL JOHN HUGHES
Abstract: The present subject matter provides a system for modifying static pressure recoveries and emissions formation within a gas turbine. The system includes a bled diffuser positioned downstream from a compressor section of the gas turbine and a bleed duct extending from the bled diffuser. The bleed duct may be configured to direct bleed air from the pressurized airflow exiting the compressor section to a secondary combustion system located downstream from the main combustion system in a combustor. The bleed air flowing into the secondary combustion system may be mixed with fuel to form an air/fuel mixture.
Abstract translation: 本主题提供了一种用于改变燃气轮机内静压回收率和排放物形成的系统。 该系统包括位于燃气涡轮机的压缩机部分下游的排放扩散器和从流血扩散器延伸的排放管道。 排放管道可以被配置为将排出压缩机部分的加压气流的排出空气引导到位于燃烧器中的主燃烧系统下游的二次燃烧系统。 流入二次燃烧系统的排出空气可与燃料混合以形成空气/燃料混合物。
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公开(公告)号：US20110048030A1
公开(公告)日：2011-03-03
申请号：US12553153
申请日：2009-09-03
Applicant: Jonathan Dwight Berry , Kevin Weston McMahan
Inventor： Jonathan Dwight Berry , Kevin Weston McMahan
IPC: F02C7/12
CPC classification number: F23R3/002 , F01D9/023 , F23R2900/03043 , F23R2900/03044
Abstract: An aft frame of a turbine engine transition piece body is provided and includes an annular body disposed within a first annular space defined between an impingement sleeve and a compressor discharge casing and aft of a second annular space defined between the transition piece body and the impingement sleeve and including a main portion with a first surface facing the first annular space and a second surface facing the forward annular space. The main portion has an impingement hole extending therethrough from an inlet at the first surface of the annular body to an outlet at the second surface of the annular body to define a fluid path along which the first and second annular spaces communicate with one another.
Abstract translation: 提供了一种涡轮发动机过渡件本体的后框架，并且包括设置在限定在冲击套筒和压缩机排出壳体之间的第一环形空间内的环形体，以及限定在过渡件主体和冲击套筒之间的第二环形空间的后部 并且包括具有面向第一环形空间的第一表面的主要部分和面向前部环形空间的第二表面。 主要部分具有从环形体的第一表面处的入口延伸到环形体的第二表面处的出口的冲击孔，以限定第一和第二环形空间彼此连通的流体路径。
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公开(公告)号：US20100089021A1
公开(公告)日：2010-04-15
申请号：US12250995
申请日：2008-10-14
Applicant: Jesse Ellis Barton , Jonathan Dwight Berry , Mark Allan Hadley , Patrick Benedict Melton
CPC classification number: F23R3/28 , F23L7/00 , F23L2900/07002 , F23L2900/07009
Abstract: 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.
Abstract translation: 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。
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公开(公告)号：US20090223227A1
公开(公告)日：2009-09-10
申请号：US12073407
申请日：2008-03-05
Applicant: John Lipinski , Girard Simons , Jonathan Dwight Berry , Abhijit Som
Inventor： John Lipinski , Girard Simons , Jonathan Dwight Berry , Abhijit Som
IPC: F02C7/22
CPC classification number: F23R3/346 , F23C2900/06042 , F23R3/10 , F23R3/28 , F23R2900/00002
Abstract: A combustor liner cap including a cap center body portion and a fuel nozzle portion defined peripherally of the cap center body portion. A plurality of fuel nozzle ports are defined through the fuel nozzle portion and a plurality of air jet holes are defined through the cap center body portion, and each air jet hole is aligned along a radius of the liner cap with a respective fuel nozzle port.
Abstract translation: 一种燃烧器衬套，其包括盖中心体部分和在帽中心体部分周围限定的燃料喷嘴部分。 通过燃料喷嘴部分限定多个燃料喷嘴口，并且通过盖中心体部分限定多个空气喷射孔，并且每个空气喷射孔沿着衬套帽的半径与相应的燃料喷嘴口对齐。
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70.发明授权公开(公告)号：US09534781B2
公开(公告)日：2017-01-03
申请号：US13468988
申请日：2012-05-10
Applicant: Michael John Hughes , Thomas Edward Johnson , Jonathan Dwight Berry , William David York
Abstract: A system includes a multi-tube fuel nozzle with a fuel nozzle body and a plurality of tubes. The fuel nozzle body includes a nozzle wall surrounding a chamber. The plurality of tubes extend through the chamber, wherein each tube of the plurality of tubes includes an air intake portion, a fuel intake portion, and an air-fuel mixture outlet portion. The multi-tube fuel nozzle also includes a differential configuration of the air intake portions among the plurality of tubes.
Abstract translation: 一种系统包括具有燃料喷嘴体和多个管的多管燃料喷嘴。 燃料喷嘴体包括围绕室的喷嘴壁。 多个管延伸穿过室，其中多个管中的每个管包括进气部分，燃料进入部分和空气 - 燃料混合物出口部分。 多管燃料喷嘴还包括多个管中的进气部分的差动构造。
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