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41. 发明授权

US08276391B2 Combustor liner cooling at transition duct interface and related method 有权
标题翻译：过渡管道界面的燃烧器衬管冷却及相关方法
公开(公告)号：US08276391B2
公开(公告)日：2012-10-02
申请号：US12762842
申请日：2010-04-19
申请人： Jonathan Dwight Berry , Kara Johnston Edwards , Heath Michael Ostebee
发明人： Jonathan Dwight Berry , Kara Johnston Edwards , Heath Michael Ostebee
IPC分类号： F02C7/18 , F23R3/46
CPC分类号： F23R3/002 , F23R3/04
摘要： 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.
摘要翻译：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。

42. 发明申请

US20120055168A1 SYSTEM AND METHOD FOR PRODUCING HYDROGEN RICH FUEL 审中-公开
标题翻译：用于生产氢燃料的系统和方法
公开(公告)号：US20120055168A1
公开(公告)日：2012-03-08
申请号：US12877363
申请日：2010-09-08
申请人： Jonathan Dwight Berry , Michael John Hughes
发明人： Jonathan Dwight Berry , Michael John Hughes
IPC分类号： F02C3/20 , F02C3/28
CPC分类号： F02C6/00 , F02C3/28 , F02C3/34
摘要： 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.
摘要翻译：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。

43. 发明申请

US20110243805A1 FLUID COOLED REFORMER AND METHOD FOR COOLING A REFORMER 有权
标题翻译：流体冷却改性剂和冷却改性剂的方法
公开(公告)号：US20110243805A1
公开(公告)日：2011-10-06
申请号：US12749985
申请日：2010-03-30
申请人： Jonathan Dwight Berry , Hasan Karim , Abdul Rafey Khan
发明人： Jonathan Dwight Berry , Hasan Karim , Abdul Rafey Khan
IPC分类号： F25B29/00 , F28D21/00
CPC分类号： 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
摘要： 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.
摘要翻译：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。

44. 发明申请

US20110048030A1 IMPINGEMENT COOLED TRANSITION PIECE AFT FRAME 有权
公开(公告)号：US20110048030A1
公开(公告)日：2011-03-03
申请号：US12553153
申请日：2009-09-03
申请人： Jonathan Dwight Berry , Kevin Weston McMahan
发明人： Jonathan Dwight Berry , Kevin Weston McMahan
IPC分类号： F02C7/12
CPC分类号： F23R3/002 , F01D9/023 , F23R2900/03043 , F23R2900/03044
摘要： 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.
摘要翻译：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。

45. 发明申请

US20090223227A1 Combustion cap with crown mixing holes 审中-公开
标题翻译：燃烧盖与冠混合孔
公开(公告)号：US20090223227A1
公开(公告)日：2009-09-10
申请号：US12073407
申请日：2008-03-05
申请人： John Lipinski , Girard Simons , Jonathan Dwight Berry , Abhijit Som
发明人： John Lipinski , Girard Simons , Jonathan Dwight Berry , Abhijit Som
IPC分类号： F02C7/22
CPC分类号： F23R3/346 , F23C2900/06042 , F23R3/10 , F23R3/28 , F23R2900/00002
摘要： 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.
摘要翻译：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。

46. 发明授权

US09534781B2 System and method having multi-tube fuel nozzle with differential flow 有权
标题翻译：具有差动流量的多管燃料喷嘴的系统和方法
公开(公告)号：US09534781B2
公开(公告)日：2017-01-03
申请号：US13468988
申请日：2012-05-10
申请人： Michael John Hughes , Thomas Edward Johnson , Jonathan Dwight Berry , William David York
发明人： Michael John Hughes , Thomas Edward Johnson , Jonathan Dwight Berry , William David York
IPC分类号： F23R3/04 , F23N3/08 , F23R3/26 , F23R3/28
CPC分类号： F23N3/082 , F23R3/045 , F23R3/26 , F23R3/286
摘要： 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.
摘要翻译：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。

47. 发明授权

US09388985B2 Premixing apparatus for gas turbine system 有权
标题翻译：燃气轮机系统预混装置
公开(公告)号：US09388985B2
公开(公告)日：2016-07-12
申请号：US13194385
申请日：2011-07-29
申请人： Chunyang Wu , Derrick Walter Simons , Jonathan Dwight Berry , Michael John Hughes
发明人： Chunyang Wu , Derrick Walter Simons , Jonathan Dwight Berry , Michael John Hughes
IPC分类号： F23R3/14 , F23R3/28 , F23R3/34
CPC分类号： F23R3/14 , F05B2260/96 , F23R3/286 , F23R3/34 , F23R2900/00014
摘要： 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.
摘要翻译：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。

48. 发明授权

US09243803B2 System for cooling a multi-tube fuel nozzle 有权
标题翻译：多管燃油喷嘴冷却系统
公开(公告)号：US09243803B2
公开(公告)日：2016-01-26
申请号：US13267828
申请日：2011-10-06
申请人： Jonathan Dwight Berry
发明人： Jonathan Dwight Berry
IPC分类号： F23R3/28
CPC分类号： F23R3/283 , F23D2214/00 , F23R3/286 , F23R2900/03043 , F23R2900/03044 , Y02T50/675
摘要： 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.
摘要翻译：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。

49. 发明授权

US09103551B2 Combustor leaf seal arrangement 有权
标题翻译：燃烧器叶密封装置
公开(公告)号：US09103551B2
公开(公告)日：2015-08-11
申请号：US13195394
申请日：2011-08-01
申请人： Jonathan Dwight Berry , Heath Michael Ostebee
发明人： Jonathan Dwight Berry , Heath Michael Ostebee
IPC分类号： F23R3/28
CPC分类号： F23R3/283 , F23R3/286 , F23R2900/00012
摘要： 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.
摘要翻译：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。

50. 发明授权

US08984887B2 Combustor and method for supplying fuel to a combustor 有权
标题翻译：用于向燃烧器供应燃料的燃烧器和方法
公开(公告)号：US08984887B2
公开(公告)日：2015-03-24
申请号：US13244526
申请日：2011-09-25
申请人： Jonathan Dwight Berry
发明人： Jonathan Dwight Berry
IPC分类号： F23R3/28 , F23R3/36
CPC分类号： F23R3/286 , F23R3/36
摘要： 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.
摘要翻译：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。

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