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公开(公告)号：US20130032643A1
公开(公告)日：2013-02-07
申请号：US13195394
申请日：2011-08-01
Applicant: Jonathan Dwight BERRY , Heath Michael OSTEBEE
Inventor： Jonathan Dwight BERRY , Heath Michael OSTEBEE
CPC classification number: F23R3/283 , F23R3/286 , F23R2900/00012
Abstract: A substantially wedge-shaped sector nozzle includes a nozzle body having inner and outer arcuate segments connected by diverging radial side plates and a nozzle plate at an aft end of the nozzle body formed with an array of fuel orifices. One of the diverging radial side plates supports a radially-oriented leaf seal assembly adapted to seal against a flat plate of an adjacent similarly-shaped sector nozzle.
Abstract translation: 基本上楔形的扇形喷嘴包括喷嘴体，其具有通过发散的径向侧板连接的内部和外部弓形段，以及在形成有燃料孔阵列的喷嘴体的后端处的喷嘴板。 发散的径向侧板中的一个支撑径向取向的叶片密封组件，其适于密封邻近的类似形状的扇形喷嘴的平板。
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公开(公告)号：US20130025284A1
公开(公告)日：2013-01-31
申请号：US13194385
申请日：2011-07-29
Applicant: Chunyang WU , Derrick Walter SIMONS , Jonathan Dwight BERRY , Michael John HUGHES
Inventor： Chunyang WU , Derrick Walter SIMONS , Jonathan Dwight BERRY , Michael John HUGHES
IPC: F23R3/58
CPC classification number: F23R3/14 , F05B2260/96 , F23R3/286 , F23R3/34 , F23R2900/00014
Abstract: A premixing apparatus for a gas turbine system includes non-swirl elements around a periphery of a face of a premixing apparatus and a swirl assembly located substantially at a center of the face. The non-swirl elements premix a premixture prior to the premixture being delivered to a combustor of the gas turbine system. The swirl assembly disturbs a flow of fluid prior to the fluid being delivered to the combustor. The premixture includes fuel and oxidant, and the fluid disturbed by the swirl assembly includes the oxidant or the premixture.
Abstract translation: 用于燃气涡轮机系统的预混合装置包括围绕预混合装置的表面的周边的非旋转元件和基本上位于该表面中心的旋转组件。 非旋流元件在将预混合物输送到燃气轮机系统的燃烧器之前将混合物预混合。 涡流组件在流体被输送到燃烧器之前会扰乱流体流动。 预混合物包括燃料和氧化剂，并且由涡旋组件扰动的流体包括氧化剂或预混合物。
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公开(公告)号：US20120305677A1
公开(公告)日：2012-12-06
申请号：US13153506
申请日：2011-06-06
Applicant: Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Jonathan Dwight Berry
Inventor： Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Jonathan Dwight Berry
IPC: F23D11/38
Abstract: A system for conditioning flow through a plurality of nozzles arranged in a combustor includes a shield circumferentially surrounding at least a portion of the plurality of nozzles and a plurality of baffles disposed circumferentially around the shield. Each baffle is circumferentially disposed between adjacent nozzles.
Abstract translation: 用于调节流过布置在燃烧器中的多个喷嘴的流动系统包括周向围绕多个喷嘴的至少一部分的屏蔽件和围绕屏蔽件周向设置的多个挡板。 每个挡板周向地设置在相邻喷嘴之间。
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公开(公告)号：US08252251B2
公开(公告)日：2012-08-28
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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15.发明申请Systems and Methods of Providing High Pressure Air to a Head End of a Combustor 有权向燃烧器头端提供高压空气的系统和方法公开(公告)号：US20110197586A1
公开(公告)日：2011-08-18
申请号：US12705737
申请日：2010-02-15
Applicant: Jonathan Dwight Berry , Constantin Dinu , Carl Robert Barker , Krishna Kumar Venkataraman
IPC: F02C3/14
CPC classification number: F23R3/02
Abstract: A combustor includes a first flow path and a second flow path. The first flow path places a diffuser in indirect fluid communication with a combustor cap assembly by way of an intervening lower combustor annular passageway. The second flow path places the diffuser in direct fluid communication with the combustor cap assembly.
Abstract translation: 燃烧器包括第一流路和第二流路。 第一流路通过中间的下部燃烧器环形通道将扩散器与燃烧器盖组件间接流体连通。 第二流路将扩散器与燃烧器盖组件直接流体连通。
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Patent Agency Ranking
公开(公告)号：US20110162375A1
公开(公告)日：2011-07-07
申请号：US12652181
申请日：2010-01-05
Applicant: Jonathan Dwight Berry
Inventor： Jonathan Dwight Berry
IPC: F02C7/22
Abstract: Systems are provided for supplying fuel to secondary combustion zones within gas turbine engines. In one embodiment, a system includes a transition piece support structure extending from a compressor casing and configured to support a combustor transition piece of a gas turbine engine. A fuel passageway is integrated with the support structure.
Abstract translation: 提供用于向燃气涡轮发动机内的二级燃烧区供应燃料的系统。 在一个实施例中，系统包括从压缩机壳体延伸并且构造成支撑燃气涡轮发动机的燃烧器过渡件的过渡件支撑结构。 燃料通道与支撑结构集成。
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17.发明授权公开(公告)号：US07921653B2
公开(公告)日：2011-04-12
申请号：US11984925
申请日：2007-11-26
Applicant: Abhijit Som , Jonathan Dwight Berry
Inventor： Abhijit Som , Jonathan Dwight Berry
CPC classification number: F01D9/023
Abstract: A combustor for a turbine including a combustor liner; a first flow sleeve surrounding the combustor liner with a first flow annulus therebetween, the first flow sleeve having at least one cooling aperture formed about a circumference thereof for directing compressor discharge air as cooling air into the first flow annulus; a casing surrounding first flow sleeve with a second flow annulus therebetween, the first flow sleeve having at least one air extraction opening formed about a circumference thereof for directing compressor discharge air from the first flow annulus as extraction air into the second flow annulus; and an extraction port operatively coupled to the casing for extracting the extraction air from the second flow annulus.
Abstract translation: 一种用于涡轮机的燃烧器，包括燃烧器衬套; 围绕所述燃烧器衬套的第一流动套筒，其间具有第一流动环空，所述第一流动套筒具有围绕其圆周形成的至少一个冷却孔，用于将压缩机排出的空气作为冷却空气引导到所述第一流动环空中; 围绕其间具有第二流动环的第一流动套管的壳体，所述第一流动套筒具有围绕其周边形成的至少一个空气抽取开口，用于将来自所述第一流动环空间的压缩机排出的空气作为抽出空气引导到所述第二流动环空中; 以及可操作地联接到所述壳体以从所述第二流动环空提取抽取空气的抽出端口。
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公开(公告)号：US20110016878A1
公开(公告)日：2011-01-27
申请号：US12508918
申请日：2009-07-24
Applicant: Jonathan Dwight Berry , Geoffrey David Myers
Inventor： Jonathan Dwight Berry , Geoffrey David Myers
CPC classification number: F02C9/52 , F02C7/222 , F02C9/54 , F23R3/005 , F23R3/10 , F23R3/26 , F23R2900/03044
Abstract: A gas turbine system comprising, a diffuser operative to diffuse an airstream output from a compressor, a fuel nozzle operative to receive fuel and emit the fuel in a combustor, and at least one bleed duct operative to direct bleed air from down stream of the combustor to the fuel nozzle.
Abstract translation: 一种燃气轮机系统，包括：扩散器，其用于扩散从压缩机输出的气流;燃料喷嘴，其可操作地接收燃料并在燃烧器中发射燃料;以及至少一个排放管，其可操作以从所述燃烧器的下游引导排放空气 到燃料喷嘴。
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公开(公告)号：US20100205972A1
公开(公告)日：2010-08-19
申请号：US12372246
申请日：2009-02-17
Applicant: Ronald James Chila , Ronald Scott Bunker , Kevin Weston McMahan , Jonathan Dwight Berry
IPC: F02C7/12
Abstract: A method, system, and apparatus is provided for transferring heat from a can combustor associated with a gas turbine by providing a one-piece can combustor body having surface features that facilitate the transfer of heat away from the can combustor body, and by directing air flow to the surface features so that heat from the can combustor body is transferred from the surface features to the air flow.
Abstract translation: 提供了一种方法，系统和装置，用于通过提供具有便于将热量从罐式燃烧器主体传递的表面特征的一体式罐式燃烧器主体，以及通过引导空气 流到表面特征，使得来自罐式燃烧器主体的热量从表面特征传递到气流。
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公开(公告)号：US20100066035A1
公开(公告)日：2010-03-18
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: 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。
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