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。

公开(公告)号：US20120098276A1

公开(公告)日：2012-04-26

申请号：US13332723

申请日：2011-12-21

Applicant: Gilbert Otto Kraemer ,  Ashok Kumar Anand ,  James Anthony West ,  Hasan Ui Karim ,  Sam David Draper ,  Jonathan Dwight Berry

Inventor： Gilbert Otto Kraemer ,  Ashok Kumar Anand ,  James Anthony West ,  Hasan Ui Karim ,  Sam David Draper ,  Jonathan Dwight Berry

IPC: F02C7/08 ,  H02K7/18

CPC classification number: F02C3/34 ,  B01D53/8625 ,  B01D53/8643 ,  B01D2255/1021 ,  B01D2255/204 ,  B01D2255/206 ,  B01D2255/20715 ,  B01D2255/2092 ,  F02C6/18 ,  Y02E20/16 ,  Y02T10/22

Abstract: A power generation system capable of eliminating NO components 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.

Abstract translation: 一种能够通过使用三元催化剂消除废气中的NO成分的发电系统，其包括气体压缩机以增加供给到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。

公开(公告)号：US20120085100A1

公开(公告)日：2012-04-12

申请号：US12901648

申请日：2010-10-11

Applicant: Michael John Hughes ,  Jonathan Dwight Berry ,  Jason Thurman Stewart ,  Almaz Valeev ,  Chunyang Wu

Inventor： Michael John Hughes ,  Jonathan Dwight Berry ,  Jason Thurman Stewart ,  Almaz Valeev ,  Chunyang Wu

IPC: F02C7/22

CPC classification number: F23R3/286 ,  F23C2900/07001 ,  F23C2900/9901 ,  F23R3/36

Abstract: The present application provides for a combustor for combusting a flow of fuel and a flow of air. The combustor may include a number of fuel nozzles, a lean pre-nozzle fuel injection system positioned upstream of the fuel nozzles, and a premixing annulus positioned between the fuel nozzles and the lean pre-nozzle fuel injection system to premix the flow of fuel and the flow of air.

Abstract translation: 本申请提供了一种用于燃烧燃料流和空气流的燃烧器。 燃烧器可以包括多个燃料喷嘴，位于燃料喷嘴上游的稀薄预喷嘴燃料喷射系统以及位于燃料喷嘴和稀薄预喷嘴燃料喷射系统之间的预混合环，以预混合燃料流和 空气流动。

公开(公告)号：US20100300106A1

公开(公告)日：2010-12-02

申请号：US12476926

申请日：2009-06-02

Applicant: Kara Johnston Edwards ,  Kevin Weston McMahan ,  Thomas Edward Johnson ,  Jonathan Dwight Berry

Inventor： Kara Johnston Edwards ,  Kevin Weston McMahan ,  Thomas Edward Johnson ,  Jonathan Dwight Berry

IPC: F02C1/00

CPC classification number: F23R3/10 ,  F23R2900/03041

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20100089022A1

公开(公告)日：2010-04-15

申请号：US12251050

申请日：2008-10-14

Applicant: Jesse Ellis Barton ,  Jonathan Dwight Berry ,  Mark Allan Hadley

Inventor： Jesse Ellis Barton ,  Jonathan Dwight Berry ,  Mark Allan Hadley

IPC: F02C3/30

CPC classification number: F23R3/04 ,  F23L7/005 ,  F23L2900/07002 ,  F23R3/10 ,  F23R3/283 ,  F23R2900/00012

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 baffle hole. A shroud is disposed between the baffle plate and the at least one fuel nozzle and is affixed to the baffle plate. A plurality of openings in the shroud are configured to meter a flow of diluent between the baffle hole and the at least one fuel nozzle. Further disclosed is a method for providing diluent to a combustor including providing a plurality of openings disposed in a shroud affixed to a baffle plate and disposed between the baffle plate and at least one fuel nozzle extending through a through hole in the baffle plate. The diluent is flowed through the plurality of openings toward at least one airflow opening in the at least one fuel nozzle.

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挡板孔的燃料喷嘴。 挡板布置在挡板和至少一个燃料喷嘴之间并且固定到挡板上。 护罩中的多个开口构造成测量在挡板孔和至少一个燃料喷嘴之间的稀释剂流。 还公开了一种用于向燃烧器提供稀释剂的方法，包括提供设置在固定到挡板上的护罩中的多个开口，并设置在挡板和延伸穿过挡板中的通孔的至少一个燃料喷嘴之间。 稀释剂通过多个开口朝向至少一个燃料喷嘴中的至少一个气流开口流动。

公开(公告)号：US20090184181A1

公开(公告)日：2009-07-23

申请号：US12017364

申请日：2008-01-22

Applicant: Jonathan Dwight Berry ,  Gilbert Otto Kraemer

Inventor： Jonathan Dwight Berry ,  Gilbert Otto Kraemer

IPC: B05B1/14

CPC classification number: F23R3/286 ,  F23C2900/07001 ,  F23D14/62

Abstract: An injection system for fuel and air that includes a number of lobes positioned adjacent to each other. Each of the lobes has a trailing end. A number of jets may be positioned adjacent to the trailing end.

Abstract translation: 一种用于燃料和空气的喷射系统，其包括彼此相邻定位的多个叶片。 每个裂片具有尾端。 可以将多个喷嘴定位成与尾端相邻。

公开(公告)号：US20090133403A1

公开(公告)日：2009-05-28

申请号：US11984925

申请日：2007-11-26

Applicant: Abhijit Som ,  Jonathan Dwight Berry

Inventor： Abhijit Som ,  Jonathan Dwight Berry

IPC: F23R3/02

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。

公开(公告)号：US06179608B2

公开(公告)日：2001-01-30

申请号：US09322867

申请日：1999-05-28

Applicant: Gilbert O. Kraemer ,  Jonathan Dwight Berry

Inventor： Gilbert O. Kraemer ,  Jonathan Dwight Berry

IPC: F02G300

CPC classification number: F23D14/82 ,  F23D2209/10 ,  F23R3/18 ,  F23R3/286 ,  F23R3/40

Abstract: 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.

Abstract translation: 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。