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1. 发明授权

US06179608B2 Swirling flashback arrestor 失效
标题翻译：旋流闪回避雷器
公开(公告)号：US06179608B2
公开(公告)日：2001-01-30
申请号：US09322867
申请日：1999-05-28
申请人： Gilbert O. Kraemer , Jonathan Dwight Berry
发明人： Gilbert O. Kraemer , Jonathan Dwight Berry
IPC分类号： F02G300
CPC分类号： F23D14/82 , F23D2209/10 , F23R3/18 , F23R3/286 , F23R3/40
摘要： A structure is disclosed that will quench a flame front during a flashback event in a gas turbine while simultaneously providing a mixing function during normal operations. The device disclosed consists of two monoliths one upstream of the other. In the basic embodiment of the invention the downstream monolith acts as a mixer while the combination of the upstream monolith and the downstream monolith act as the flashback arrestor. Other embodiments of the device also allow the downstream monolith to be a flameholder.
摘要翻译：公开了一种在燃气轮机中的闪回事件期间熄灭火焰前沿的结构，同时在正常操作期间提供混合功能。所公开的装置由另一个上游的两个整料组成。在本发明的基本实施例中，下游整体件充当混合器，而上游整料和下游整料的组合用作回流保护器。该装置的其它实施例还允许下游整料作为火焰稳定器。

2. 发明授权

US08991149B2 Dry 3-way catalytic reduction of gas turbine NOX 有权
标题翻译：燃气轮机NOX的干式三元催化还原
公开(公告)号：US08991149B2
公开(公告)日：2015-03-31
申请号：US13332723
申请日：2011-12-21
申请人： Ashok Kumar Anand , James Anthony West , Gilbert Otto Kraemer , Hasan Ui Karim , Sam David Draper , Jonathan Dwight Berry
发明人： Ashok Kumar Anand , James Anthony West , Gilbert Otto Kraemer , Hasan Ui Karim , Sam David Draper , Jonathan Dwight Berry
IPC分类号： F02C7/08 , F02G1/00 , F02G3/00 , F02C3/34 , B01D53/86 , F02C6/18
CPC分类号： F02C3/34 , B01D53/8625 , B01D53/8643 , B01D2255/1021 , B01D2255/204 , B01D2255/206 , B01D2255/20715 , B01D2255/2092 , F02C6/18 , Y02E20/16 , Y02T10/22
摘要： A power generation system capable of eliminating NOxcomponents in the exhaust gas by using a 3-way catalyst, comprising a gas compressor to increase the pressure of ambient air fed to the system; a combustor capable of oxidizing a mixture of fuel and compressed air to generate an expanded, high temperature exhaust gas; a turbine that uses the force of the high temperature gas; an exhaust gas recycle (EGR) stream back to the combustor; a 3-way catalytic reactor downstream of the gas turbine engine outlet which treats the exhaust gas stream to remove substantially all of the NOx components; a heat recovery steam generator (HRSG); an EGR compressor feeding gas to the combustor and turbine; and an electrical generator.
摘要翻译：一种发电系统，其能够通过使用三元催化剂来除去废气中的NOx组分，所述三元催化剂包括气体压缩机，以增加供给到所述系统的环境空气的压力; 能够氧化燃料和压缩空气的混合物以产生膨胀的高温废气的燃烧器; 使用高温气体的力的涡轮机; 废气再循环（EGR）流回燃烧器; 在燃气涡轮发动机出口下游的三元催化反应器，其处理排气流以去除基本上所有的NOx组分; 热回收蒸汽发生器（HRSG）; EGR压缩机将气体输送到燃烧器和涡轮机; 和发电机。

3. 发明授权

US08733106B2 Fuel injector and support plate 有权
标题翻译：燃油喷射器和支撑板
公开(公告)号：US08733106B2
公开(公告)日：2014-05-27
申请号：US13099853
申请日：2011-05-03
申请人： Carl Robert Barker , Thomas Edward Johnson , Jonathan Dwight Berry
发明人： Carl Robert Barker , Thomas Edward Johnson , Jonathan Dwight Berry
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/283 , F23R3/286 , F23R3/34 , F23R3/46 , F23R2900/00014 , F23R2900/00017
摘要： 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.
摘要翻译：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。

4. 发明授权

US08707705B2 Impingement cooled transition piece aft frame 有权
标题翻译：冲击冷却过渡件后框架
公开(公告)号：US08707705B2
公开(公告)日：2014-04-29
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。

5. 发明申请

US20130219912A1 COMBUSTOR AND METHOD FOR PURGING A COMBUSTOR 有权
标题翻译：燃烧器和燃烧器的方法
公开(公告)号：US20130219912A1
公开(公告)日：2013-08-29
申请号：US13405564
申请日：2012-02-27
申请人： Jonathan Dwight Berry , Michael John Hughes
发明人： Jonathan Dwight Berry , Michael John Hughes
IPC分类号： F02C7/00
CPC分类号： F23R3/10 , F23D2209/30 , F23R3/286
摘要： A combustor includes an end cap. The end cap includes a first surface and a second surface downstream from the first surface, a shroud that circumferentially surrounds at least a portion of the first and second surfaces, a plate that extends radially within the shroud, a plurality of tubes that extend through the plate and the first and second surfaces, and a first purge port that extends through one or more of the plurality of tubes, wherein the purge port is axially aligned with the plate.
摘要翻译：燃烧器包括端盖。端盖包括第一表面和第二表面，在第一表面的下游，围绕第一和第二表面的至少一部分的护罩，在护罩内径向延伸的板，延伸穿过该护罩的多个管板和第一和第二表面，以及延伸穿过多个管中的一个或多个的第一吹扫口，其中吹扫口与板轴向对准。

6. 发明授权

US08495881B2 System and method for thermal control in a cap of a gas turbine combustor 有权
标题翻译：在燃气轮机燃烧器的盖中进行热控制的系统和方法
公开(公告)号：US08495881B2
公开(公告)日：2013-07-30
申请号：US12476926
申请日：2009-06-02
申请人： Kara Johnston Edwards , Kevin Weston McMahan , Thomas Edward Johnson , Jonathan Dwight Berry
发明人： Kara Johnston Edwards , Kevin Weston McMahan , Thomas Edward Johnson , Jonathan Dwight Berry
IPC分类号： F02C1/00
CPC分类号： F23R3/10 , F23R2900/03041
摘要： A system comprises a turbine combustor cap. The turbine combustor cap includes a plurality of segments. Each segment of the plurality of segments has edges abutting at least two fuel nozzle receptacles. Moreover, each segment of the plurality of segments does not completely surrounding any one fuel nozzle receptacle.
摘要翻译：一种系统包括涡轮机燃烧器盖。涡轮机燃烧器盖包括多个段。多个段的每个段具有邻接至少两个燃料喷嘴容器的边缘。此外，多个段的每个段都不完全围绕任何一个燃料喷嘴容器。

7. 发明授权

US08371123B2 Apparatus for conditioning airflow through a nozzle 有权
标题翻译：用于调节通过喷嘴的气流的装置
公开(公告)号：US08371123B2
公开(公告)日：2013-02-12
申请号：US12607386
申请日：2009-10-28
申请人： Jason Thurman Stewart , Jonathan Dwight Berry , Michael John Hughes
发明人： Jason Thurman Stewart , Jonathan Dwight Berry , Michael John Hughes
IPC分类号： F02C1/00
CPC分类号： F23R3/14 , F23R3/10 , F23R3/54
摘要： A nozzle includes a center body and a shroud surrounding the center body to define an annular passage. An arcuate annular guide extending from a point radially inward of the shroud to a point radially outward of the shroud defines a first airflow between the arcuate annular guide and the shroud and a second airflow between the arcuate annular guide and the center body.
摘要翻译：喷嘴包括中心体和围绕中心体的护罩以限定环形通道。从护罩的径向向内的点延伸到护罩的径向外侧的弧形环形引导件限定了弓形环形引导件和护罩之间的第一气流以及弧形环形引导件和中心体之间的第二气流。

8. 发明申请

US20130025285A1 SYSTEM FOR CONDITIONING AIR FLOW INTO A MULTI-NOZZLE ASSEMBLY 审中-公开
标题翻译：将空气流量调节到多个喷嘴组件的系统
公开(公告)号：US20130025285A1
公开(公告)日：2013-01-31
申请号：US13194465
申请日：2011-07-29
申请人： Jason Thurman Stewart , Jonathan Dwight Berry
发明人： Jason Thurman Stewart , Jonathan Dwight Berry
IPC分类号： F02C1/00
CPC分类号： F02C7/2365 , F05D2240/36 , F23R3/10 , F23R3/286
摘要： A system includes a turbine fuel nozzle assembly. The turbine fuel nozzle assembly includes a first fuel nozzle including a first air inlet and a second fuel nozzle including a second air inlet. The turbine fuel nozzle assembly also includes a first inlet flow conditioner disposed adjacent the first air inlet of the first fuel nozzle, wherein the first air inlet flow conditioner extends only partially around the first fuel nozzle. The turbine fuel nozzle further includes a second inlet flow conditioner disposed adjacent the second air inlet of the second fuel nozzle, wherein the second air inlet flow conditioner extends only partially around the second fuel nozzle, and the second inlet flow conditioner is separate from the first inlet flow conditioner.
摘要翻译：一种系统包括涡轮燃料喷嘴组件。涡轮燃料喷嘴组件包括包括第一空气入口的第一燃料喷嘴和包括第二空气入口的第二燃料喷嘴。涡轮燃料喷嘴组件还包括邻近第一燃料喷嘴的第一空气入口设置的第一入口流动调节器，其中第一空气入口流动调节器仅部分地围绕第一燃料喷嘴延伸。涡轮燃料喷嘴还包括与第二燃料喷嘴的第二空气入口相邻设置的第二入口流动调节器，其中第二进气流量调节器仅部分地围绕第二燃料喷嘴延伸，并且第二入口流动调节器与第一进气流量调节器分离入口流量调节器。

9. 发明申请

US20120279224A1 GAS TURBINE ENGINE COMBUSTOR 有权
标题翻译：燃气轮机发动机
公开(公告)号：US20120279224A1
公开(公告)日：2012-11-08
申请号：US13099938
申请日：2011-05-03
申请人： Donald Mark Bailey , Jonathan Dwight Berry , Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Robert Joseph Rohrssen , John Drake Vanselow
发明人： Donald Mark Bailey , Jonathan Dwight Berry , Luis Manuel Flamand , Kwanwoo Kim , Patrick Benedict Melton , Robert Joseph Rohrssen , John Drake Vanselow
IPC分类号： F23C3/00
CPC分类号： F23R3/283 , F23D2900/00003 , F23R3/286 , F23R3/46 , F23R3/54 , F23R2900/00017 , F23R2900/00018
摘要： A gas turbine engine combustor is provided and includes an array of fuel nozzles, a combustion casing assembly disposed about the array of fuel nozzles and an end cap assembly disposed within the combustion casing assembly to define with the combustion casing assembly an axis-symmetric annulus through which fluid travels into each of the fuel nozzles, at least one of the combustion casing assembly and the end cap assembly being formed with lobed, three-dimensional contouring.
摘要翻译：提供了一种燃气涡轮发动机燃烧器，其包括燃料喷嘴阵列，围绕燃料喷嘴阵列设置的燃烧壳体组件和设置在燃烧壳体组件内的端盖组件，以便与燃烧壳体组件形成轴对称的环通过所述流体行进到每个燃料喷嘴中，燃烧壳体组件和端盖组件中的至少一个形成有叶状的三维轮廓。

10. 发明授权

US08234872B2 Turbine air flow conditioner 失效
标题翻译：涡轮空气流量调节器
公开(公告)号：US08234872B2
公开(公告)日：2012-08-07
申请号：US12434505
申请日：2009-05-01
申请人： Jonathan Dwight Berry , Jason Thurman Stewart
发明人： Jonathan Dwight Berry , Jason Thurman Stewart
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/04 , F23M9/02
摘要： A system includes an air flow conditioner configured to mount in an air chamber separated from a combustion chamber of a turbine combustor. The air flow conditioner comprises a perforated annular wall configured to direct an air flow in both an axial direction and a radial direction relative to an axis of the turbine combustor. In addition, the air flow conditioner is configured to uniformly supply the air flow into air inlets of one or more fuel nozzles.
摘要翻译：一种系统包括：空气流调节器，其构造成安装在与涡轮机燃烧器的燃烧室分离的空气室中。空气流调节器包括穿孔环形壁，其构造成相对于涡轮机燃烧器的轴线在轴向方向和径向方向上引导空气流。此外，气流调节器构造成将空气流均匀地供应到一个或多个燃料喷嘴的空气入口中。

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