公开(公告)号：WO2013147632A1

公开(公告)日：2013-10-03

申请号：PCT/RU2012/000231

申请日：2012-03-29

Applicant: GENERAL ELECTRIC COMPANY ,  SLOBODYANSKIY, Ilya Aleksandrovich ,  KRAEMER, Gilbert Otto ,  GINESSIN, Leonid Yulievich ,  SUBBOTA, Andrey Pavlovich

Inventor： SLOBODYANSKIY, Ilya Aleksandrovich ,  KRAEMER, Gilbert Otto ,  GINESSIN, Leonid Yulievich ,  SUBBOTA, Andrey Pavlovich

IPC: F23R3/28 ,  F23L7/00 ,  F23K5/00

CPC classification number: F23R3/283 ,  F23K5/007 ,  F23L7/00 ,  F23L2900/07002 ,  F23L2900/07009

Abstract: A bi-directional end cover assembly (14) for a gas turbine combustor comprising an end cover plate provided with plural nozzle supports (34), at least one fuel inlet, and at least one diluent manifold (36; 38) communicating with an annular internal passage (40) provided with plural outlet apertures (42) which open to a combustion chamber of the combustor; one or more conduits adapted, in use, to supply a diluent to the at least one diluent manifold (36; 38) and to the annular internal passage (40) in a diluent-injection mode; one or more conduits adapted, in use, to extract working fluid from the combustion chamber via the annular internal passage (40) and the at least one diluent manifold in a working-fluid-extraction mode; and control valves (46; 54) for selectively controlling flow of the diluent in the diluent-injection mode and flow of working fluid in the working-fluid-extraction mode.

Abstract translation: 一种用于燃气轮机燃烧器的双向端盖组件（14），其包括设有多个喷嘴支撑（34）的端盖板，至少一个燃料入口和至少一个与环形 内部通道（40）设置有多个出口孔（42），其通向燃烧器的燃烧室; 一种或多种在使用中适于以稀释剂注射模式将稀释剂供应至至少一种稀释剂歧管（36; 38）和环形内部通道（40）的管道; 一种或多种管道，其在使用中适应于通过所述环形内部通道（40）和所述至少一个稀释剂歧管以工作流体提取模式从所述燃烧室中提取工作流体; 以及用于选择性地控制稀释剂注入模式中的稀释剂流动和工作流体提取模式中的工作流体流的控制阀（46; 54）。

公开(公告)号：WO2016109725A1

公开(公告)日：2016-07-07

申请号：PCT/US2015/068151

申请日：2015-12-30

Applicant: EXXONMOBIL UPSTREAM RESEARCH COMPANY ,  THATCHER, Jonathan, Carl ,  SLOBODYANSKIY, Ilya, Aleksandrovich ,  VOREL, Aaron, Lavene

Inventor： THATCHER, Jonathan, Carl ,  SLOBODYANSKIY, Ilya, Aleksandrovich ,  VOREL, Aaron, Lavene

IPC: H02P9/04 ,  F02C9/38 ,  F01D15/10

CPC classification number: H02P9/04 ,  F01D15/10 ,  F02C3/14 ,  F02C3/34 ,  F02C6/00 ,  F02C9/26 ,  F02C9/38 ,  F02C9/48 ,  F05D2220/32 ,  F05D2220/76 ,  F05D2270/05 ,  H02K7/1823 ,  Y02E20/16

Abstract: A method includes combusting a fuel and an oxidant in a combustor of an exhaust gas recirculation (EGR) gas turbine system that produces electrical power and provides a portion of the electrical power to an electrical grid. The method further includes controlling, via one or more processors, one or more parameters of the EGR gas turbine system to decrease the portion of the electrical power provided to the electrical grid in response to an over-frequency event associated with the electrical grid, wherein controlling the one or more parameters comprises decreasing a flow rate of fuel to the combustor in response to the over-frequency event.

Abstract translation: 一种方法包括在排气再循环（EGR）燃气轮机系统的燃烧器中燃烧燃料和氧化剂，其产生电力并将一部分电力提供给电网。 该方法还包括经由一个或多个处理器控制EGR燃气涡轮机系统的一个或多个参数，以响应于与电网相关联的过频事件来减小提供给电网的电力的部分，其中 控制一个或多个参数包括响应于过频事件降低燃烧器对燃烧器的流量。

公开(公告)号：WO2013147633A8

公开(公告)日：2014-10-16

申请号：PCT/RU2012000232

申请日：2012-03-29

Applicant: EXXONMOBIL UPSTREAM RES CO ,  GEN ELECTRIC ,  SOKOLOV ALEXANDER NIKOLAY ,  TRETYAKOV DMITRY VLADLENOVICH ,  SLOBODYANSKIY ILYA ALEKSANDROVICH

Inventor： SOKOLOV ALEXANDER NIKOLAY ,  TRETYAKOV DMITRY VLADLENOVICH ,  SLOBODYANSKIY ILYA ALEKSANDROVICH

IPC: F23R3/04 ,  F23C7/02 ,  F23C9/08 ,  F23R3/28

CPC classification number: F23R3/04 ,  F02C3/04 ,  F02C7/18 ,  F05D2240/35 ,  F23C7/02 ,  F23C9/08 ,  F23C2900/06041 ,  F23R3/002 ,  F23R3/283 ,  F23R3/286 ,  F23R2900/03041

Abstract: A turbomachine combustor assembly includes a combustor body (20), and a combustor liner (24) arranged within the combustor body (20). The combustor liner (24) defines a combustion chamber (30) having a head end (32) and a discharge end (37). A plurality of combustor nozzles (44-49) are arranged in an annular array at the head end (32) of the combustion chamber (30), and a fluid delivery nozzle (90) is arranged substantially centrally within the annular array at the head end (32) of the combustion chamber (30). The fluid delivery nozzle (90) includes a first end portion (98) that extends to a second end portion (99) through a wall portion (100). The wall portion (100) includes at least one combustion chamber outlet (113). The fluid delivery nozzle (90) is configured to deliver a non-combustible fluid into the at least one of the plurality of combustor nozzles (44-49) and the combustion chamber (30).

Abstract translation: 涡轮机械燃烧器组件包括燃烧器主体（20）和布置在燃烧器主体（20）内的燃烧器衬套（24）。 燃烧器衬套（24）限定具有头端（32）和排出端（37）的燃烧室（30）。 多个燃烧器喷嘴（44-49）在燃烧室（30）的头端（32）处以环形阵列布置，并且流体输送喷嘴（90）基本上设置在头部的环形阵列内的中心 燃烧室（30）的端部（32）。 流体输送喷嘴（90）包括通过壁部（100）延伸到第二端部（99）的第一端部（98）。 壁部分（100）包括至少一个燃烧室出口（113）。 流体输送喷嘴（90）构造成将不可燃流体输送到多个燃烧器喷嘴（44-49）和燃烧室（30）中的至少一个。

公开(公告)号：WO2016115152A1

公开(公告)日：2016-07-21

申请号：PCT/US2016/013071

申请日：2016-01-12

Applicant: EXXONMOBIL UPSTREAM RESEARCH COMPANY ,  ALLEN, Jonathan Kay ,  TROUT, Jesse Edwin ,  SLOBODYANSKIY, Ilya Aleksandrovich ,  BORCHERT, Bradford David ,  KAZAKIS, Michael V. ,  SIDKO, Igor Petrovich

Inventor： ALLEN, Jonathan Kay ,  TROUT, Jesse Edwin ,  SLOBODYANSKIY, Ilya Aleksandrovich ,  BORCHERT, Bradford David ,  KAZAKIS, Michael V. ,  SIDKO, Igor Petrovich

IPC: F23R3/06 ,  F23R3/04

CPC classification number: F23R3/16 ,  F02C3/04 ,  F02C3/34 ,  F23R3/045 ,  F23R3/06 ,  F23R3/28 ,  Y02E20/16 ,  Y02T50/675

Abstract: A system includes a turbine combustor. The turbine combustor has a combustor liner disposed about a combustion chamber, a flow sleeve, and a radial passageway. The flow sleeve disposed at an offset about the combustor liner to define a passage, wherein the passage is configured to direct an exhaust gas flow toward a head end of the turbine combustor. The radial passageway extends between the flow sleeve and the combustor liner, and the radial passageway is configured to isolate an oxidant flow through the radial passageway from the exhaust gas flow through the passage for a first operating condition and a second operating condition of the turbine combustor. The offset between the combustor liner and the flow sleeve at the first operating condition is greater than the offset between the combustor liner and the flow sleeve at the second operating condition.

Abstract translation: 一种系统包括涡轮机燃烧器。 涡轮机燃烧器具有围绕燃烧室，流动套筒和径向通道设置的燃烧器衬套。 流动套管布置在围绕燃烧器衬套的偏移处以限定通道，其中通道构造成引导废气流朝向涡轮机燃烧器的头端。 径向通道在流动套管和燃烧器衬套之间延伸，并且径向通道构造成将通过径向通道的氧化剂流与通过通道的排气流隔离，用于涡轮机燃烧器的第一操作状态和第二操作状态 。 在第一操作条件下，燃烧器衬套和流动套管之间的偏移量大于在第二操作条件下燃烧器衬套和流动套筒之间的偏移。

公开(公告)号：WO2013147633A1

公开(公告)日：2013-10-03

申请号：PCT/RU2012/000232

申请日：2012-03-29

Applicant: GENERAL ELECTRIC COMPANY ,  SOKOLOV, Alexander Nikolay ,  TRETYAKOV, Dmitry Vladimirovich ,  SLOBODYANSKIY, Ilya Aleksandrovich

Inventor： SOKOLOV, Alexander Nikolay ,  TRETYAKOV, Dmitry Vladimirovich ,  SLOBODYANSKIY, Ilya Aleksandrovich

IPC: F23R3/04 ,  F23R3/28 ,  F23C7/02 ,  F23C9/08

CPC classification number: F23R3/04 ,  F02C3/04 ,  F02C7/18 ,  F05D2240/35 ,  F23C7/02 ,  F23C9/08 ,  F23C2900/06041 ,  F23R3/002 ,  F23R3/283 ,  F23R3/286 ,  F23R2900/03041

Abstract: A turbomachine combustor assembly includes a combustor body (20), and a combustor liner (24) arranged within the combustor body (20). The combustor liner (24) defines a combustion chamber (30) having a head end (32) and a discharge end (37). A plurality of combustor nozzles (44-49) are arranged in an annular array at the head end (32) of the combustion chamber (30), and a fluid delivery nozzle (90) is arranged substantially centrally within the annular array at the head end (32) of the combustion chamber (30). The fluid delivery nozzle (90) includes a first end portion (98) that extends to a second end portion (99) through a wall portion (100). The wall portion (100) includes at least one combustion chamber outlet (113). The fluid delivery nozzle (90) is configured to deliver a non-combustible fluid into the at least one of the plurality of combustor nozzles (44-49) and the combustion chamber (30).

Abstract translation: 涡轮机械燃烧器组件包括燃烧器主体（20）和布置在燃烧器主体（20）内的燃烧器衬套（24）。 燃烧器衬套（24）限定具有头端（32）和排出端（37）的燃烧室（30）。 多个燃烧器喷嘴（44-49）在燃烧室（30）的头端（32）处以环形阵列布置，并且流体输送喷嘴（90）基本上设置在头部的环形阵列内的中心 燃烧室（30）的端部（32）。 流体输送喷嘴（90）包括通过壁部（100）延伸到第二端部（99）的第一端部（98）。 壁部分（100）包括至少一个燃烧室出口（113）。 流体输送喷嘴（90）构造成将不可燃流体输送到多个燃烧器喷嘴（44-49）和燃烧室（30）中的至少一个。