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    SYSTEM AND METHOD FOR PRODUCING HYDROGEN RICH FUEL
    41.
    发明申请
    SYSTEM AND METHOD FOR PRODUCING HYDROGEN RICH FUEL 审中-公开
    用于生产氢燃料的系统和方法

    公开(公告)号：US20130305738A1

    公开(公告)日：2013-11-21

    申请号：US13473990

    申请日：2012-05-17

    Applicant: Michael John Hughes ,  Jonathan Dwight Berry

    Inventor： Michael John Hughes ,  Jonathan Dwight Berry

    IPC: F02C7/22 ,  F02C6/06

    CPC classification number: F02C3/20 ,  C01B3/38 ,  C01B2203/0227 ,  C01B2203/84 ,  F02C3/04 ,  F02C3/22 ,  F02C6/10 ,  F02C7/22 ,  F05D2210/20

    Abstract: A system for providing hydrogen enriched fuel includes first and second gas turbines. The second gas turbine receives a fuel from a fuel supply and 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. Mixing a first portion of a compressed fuel with the second compressed working fluid in a reformer to produce a reformed fuel, flowing a second portion of the compressed fuel to a second turbine for cooling, and flowing the reformed fuel through the second turbine to cool the reformed fuel.

    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。 第二燃气轮机从燃料供应源和来自第一燃气轮机的压缩工作流体的一部分接收燃料并产生重整的燃料，并且燃料滑板提供第二燃气轮机中的涡轮与第一气体中的燃烧器之间的流体连通 涡轮。 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。 在重整器中将压缩燃料的第一部分与第二压缩工作流体混合以产生重整燃料，将第二部分的压缩燃料流动到第二涡轮机进行冷却，并使重整燃料流过第二涡轮以冷却 改装燃油

    Diluent shroud for combustor
    44.
    发明授权
    Diluent shroud for combustor 有权
    用于燃烧器的稀释罩

    公开(公告)号：US08454350B2

    公开(公告)日：2013-06-04

    申请号：US12260545

    申请日：2008-10-29

    Applicant: Jonathan Dwight Berry ,  John Joseph Lipinski ,  Girard Albert Simons ,  Abhijit Som

    Inventor： Jonathan Dwight Berry ,  John Joseph Lipinski ,  Girard Albert Simons ,  Abhijit Som

    IPC: F23C5/00

    CPC classification number: F23R3/10 ,  F23R3/28

    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 through baffle hole. At least one diluent shroud is affixed to the at least one baffle plate and is configured to guide a diluent flow toward a mixing chamber of the at least one fuel nozzle. Further disclosed is a method for introducing a diluent flow into a mixing chamber of a fuel nozzle including urging the diluent flow from a plenum through a baffle plate gap between a baffle plate and an outer surface of the fuel nozzle. The diluent flow is directed via at least one diluent shroud extending from the baffle plate toward a plurality of air swirler holes extending through a fuel nozzle tip. The diluent flow is flowed through the plurality of air swirler holes into the mixing chamber.

    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通过挡板孔的燃料喷嘴。 至少一个稀释剂护罩固定在所述至少一个挡板上，并被构造成将稀释剂流引向所述至少一个燃料喷嘴的混合室。 进一步公开的是一种将稀释剂流引入燃料喷嘴的混合室中的方法，包括将稀释剂流从气室推压通过挡板和燃料喷嘴的外表面之间的挡板间隙。 稀释剂流经由从挡板延伸的至少一个稀释剂护罩朝向延伸穿过燃料喷嘴尖端的多个空气旋流器引导。 稀释剂流通过多个空气旋流器孔流入混合室。

    COMBUSTOR AND METHOD FOR SUPPLYING FUEL TO A COMBUSTOR
    45.
    发明申请
    COMBUSTOR AND METHOD FOR SUPPLYING FUEL TO A COMBUSTOR 有权
    用于向燃烧器供应燃料的燃烧器和方法

    公开(公告)号：US20130074510A1

    公开(公告)日：2013-03-28

    申请号：US13244526

    申请日：2011-09-25

    Applicant: Jonathan Dwight Berry

    Inventor： Jonathan Dwight Berry

    IPC: F23R3/28

    CPC classification number: F23R3/286 ,  F23R3/36

    Abstract: 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.

    Abstract translation: 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。

    SECTOR NOZZLE MOUNTING SYSTEMS
    47.
    发明申请
    SECTOR NOZZLE MOUNTING SYSTEMS 有权
    部门喷嘴安装系统

    公开(公告)号：US20130025283A1

    公开(公告)日：2013-01-31

    申请号：US13194178

    申请日：2011-07-29

    Applicant: Jonathan Dwight Berry ,  Derrick Walter Simons ,  Jason Thurman Stewart

    Inventor： Jonathan Dwight Berry ,  Derrick Walter Simons ,  Jason Thurman Stewart

    IPC: F23R3/28

    CPC classification number: F23R3/283 ,  F23M20/005 ,  F23R3/286 ,  F23R2900/00005 ,  F23R2900/00014

    Abstract: 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.

    Abstract translation: 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。

    COMBUSTOR NOZZLE AND METHOD FOR SUPPLYING FUEL TO A COMBUSTOR
    48.
    发明申请
    COMBUSTOR NOZZLE AND METHOD FOR SUPPLYING FUEL TO A COMBUSTOR 审中-公开
    燃烧器喷嘴和向燃烧器供应燃料的方法

    公开(公告)号：US20120282558A1

    公开(公告)日：2012-11-08

    申请号：US13101530

    申请日：2011-05-05

    Applicant: Gilbert Otto Kraemer ,  Jonathan Dwight Berry ,  Jason Randolph Marshall

    Inventor： Gilbert Otto Kraemer ,  Jonathan Dwight Berry ,  Jason Randolph Marshall

    IPC: F23M3/00 ,  B05B1/34 ,  B05B1/26

    CPC classification number: F23D11/107 ,  F23C2900/07022 ,  F23D14/24 ,  F23R3/00

    Abstract: A combustor nozzle includes a fuel supply in fluid communication with a fuel passage that terminates at a fuel outlet. An oxidant supply is in fluid communication with an oxidant passage radially displaced from the fuel passage and that terminates at an oxidant outlet radially displaced from the fuel outlet. A diluent passage radially displaced from the fuel passage and the oxidant passage terminates at a diluent outlet disposed between the fuel outlet and the oxidant outlet. A method for supplying fuel to a combustor includes flowing the fuel through a fuel outlet and flowing an oxidant through an oxidant outlet radially displaced from the fuel outlet. The method further includes flowing a diluent through a diluent outlet radially disposed between the fuel outlet and the oxidant outlet.

    Abstract translation: 燃烧器喷嘴包括与终止于燃料出口处的燃料通道流体连通的燃料供应。 氧化剂供应源与从燃料通道径向偏移的氧化剂通道流体连通，并且终止于从燃料出口径向偏移的氧化剂出口。 从燃料通道和氧化剂通道径向偏移的稀释剂通道终止于设置在燃料出口和氧化剂出口之间的稀释剂出口。 向燃烧器供应燃料的方法包括使燃料流过燃料出口并使氧化剂流过从燃料出口径向偏移的氧化剂出口。 该方法还包括使稀释剂流过径向设置在燃料出口和氧化剂出口之间的稀释剂出口。

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