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1. 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。

2. 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。

3. 发明授权

US08191373B2 Interlocking retention strip 有权
标题翻译：联锁保持条
公开(公告)号：US08191373B2
公开(公告)日：2012-06-05
申请号：US12366913
申请日：2009-02-06
申请人： Jonathan Dwight Berry , Timur Rustemovich Repikov , Heath Michael Ostebee
发明人： Jonathan Dwight Berry , Timur Rustemovich Repikov , Heath Michael Ostebee
IPC分类号： F02C1/00 , F02C7/20
CPC分类号： F23R3/60 , F23M5/04 , F23R3/002 , F23R2900/00017 , F23R2900/03044
摘要： An impingement shield assembly for a turbine includes a first impingement shield portion and a second impingement shield joined to the first impingement shield portion. The assembly also includes a first connection portion formed on the first impingement shield portion, a second connection portion formed on the first impingement shield portion and first and second wedge weld portions that mate with and hold the first and a second connection portions in a fixed relationship to one another.
摘要翻译：用于涡轮机的冲击屏蔽组件包括第一冲击屏蔽部分和与第一冲击屏蔽部分接合的第二冲击屏蔽。组件还包括形成在第一冲击屏蔽部分上的第一连接部分，形成在第一冲击屏蔽部分上的第二连接部分和第一和第二楔形焊接部分，第一和第二楔形焊接部分以固定关系与第一和第二连接部分配合彼此。

4. 发明申请

US20100199628A1 Interlocking Retention Strip 有权
标题翻译：联锁固定带
公开(公告)号：US20100199628A1
公开(公告)日：2010-08-12
申请号：US12366913
申请日：2009-02-06
申请人： Jonathan Dwight Berry , Timur Rustemovich Repikov , Heath Michael Ostebee
发明人： Jonathan Dwight Berry , Timur Rustemovich Repikov , Heath Michael Ostebee
IPC分类号： F02C7/00 , F23R3/42 , B23K9/00
CPC分类号： F23R3/60 , F23M5/04 , F23R3/002 , F23R2900/00017 , F23R2900/03044
摘要： An impingement shield assembly for a turbine includes a first impingement shield portion and a second impingement shield joined to the first impingement shield portion. The assembly also includes a first connection portion formed on the first impingement shield portion, a second connection portion formed on the first impingement shield portion and first and second wedge weld portions that mate with and hold the first and a second connection portions in a fixed relationship to one another.
摘要翻译：用于涡轮机的冲击屏蔽组件包括第一冲击屏蔽部分和与第一冲击屏蔽部分接合的第二冲击屏蔽。组件还包括形成在第一冲击屏蔽部分上的第一连接部分，形成在第一冲击屏蔽部分上的第二连接部分和第一和第二楔形焊接部分，第一和第二楔形焊接部分以固定关系与第一和第二连接部分配合彼此。

5. 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。

6. 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。

7. 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。

8. 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。

9. 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。

10. 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。

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