JP2012522922A5 - - Google Patents

Download PDF

Info

Publication number
JP2012522922A5
JP2012522922A5 JP2012502550A JP2012502550A JP2012522922A5 JP 2012522922 A5 JP2012522922 A5 JP 2012522922A5 JP 2012502550 A JP2012502550 A JP 2012502550A JP 2012502550 A JP2012502550 A JP 2012502550A JP 2012522922 A5 JP2012522922 A5 JP 2012522922A5
Authority
JP
Japan
Prior art keywords
turbine
combustor
fuel
load
compressor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2012502550A
Other languages
English (en)
Japanese (ja)
Other versions
JP5680053B2 (ja
JP2012522922A (ja
Filing date
Publication date
Priority claimed from CH00536/09A external-priority patent/CH700796A1/de
Application filed filed Critical
Publication of JP2012522922A publication Critical patent/JP2012522922A/ja
Publication of JP2012522922A5 publication Critical patent/JP2012522922A5/ja
Application granted granted Critical
Publication of JP5680053B2 publication Critical patent/JP5680053B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2012502550A 2009-04-01 2010-03-12 改善された部分負荷エミッション特性を備えたガスタービン Expired - Fee Related JP5680053B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH00536/09A CH700796A1 (de) 2009-04-01 2009-04-01 Verfahren zum CO-emissionsarmen Betrieb einer Gasturbine mit sequentieller Verbrennung und Gasturbine mit verbessertem Teillast- Emissionsverhalten.
CH00536/09 2009-04-01
PCT/EP2010/053171 WO2010112318A1 (de) 2009-04-01 2010-03-12 Gasturbine mit verbessertem teillast-emissionsverhalten

Publications (3)

Publication Number Publication Date
JP2012522922A JP2012522922A (ja) 2012-09-27
JP2012522922A5 true JP2012522922A5 (enExample) 2013-05-02
JP5680053B2 JP5680053B2 (ja) 2015-03-04

Family

ID=40848719

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012502550A Expired - Fee Related JP5680053B2 (ja) 2009-04-01 2010-03-12 改善された部分負荷エミッション特性を備えたガスタービン

Country Status (7)

Country Link
US (2) US8434312B2 (enExample)
EP (1) EP2414653B1 (enExample)
JP (1) JP5680053B2 (enExample)
CH (1) CH700796A1 (enExample)
ES (1) ES2627679T3 (enExample)
RU (1) RU2562681C2 (enExample)
WO (1) WO2010112318A1 (enExample)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH700796A1 (de) 2009-04-01 2010-10-15 Alstom Technology Ltd Verfahren zum CO-emissionsarmen Betrieb einer Gasturbine mit sequentieller Verbrennung und Gasturbine mit verbessertem Teillast- Emissionsverhalten.
EP2630341B1 (en) * 2010-10-19 2016-08-24 General Electric Technology GmbH Method for operating a combined-cycle power plant with cogeneration and a combined-cycle power plant for carrying out the method
DK2630342T3 (en) * 2010-10-19 2014-12-15 Alstom Technology Ltd Method for operation of a gas / steam-combi power plant with cogeneration and a gas / steam-combi power plant for carrying out the process
CH704829A2 (de) * 2011-04-08 2012-11-15 Alstom Technology Ltd Gasturbogruppe und zugehöriges Betriebsverfahren.
WO2014001230A1 (en) 2012-06-29 2014-01-03 Alstom Technology Ltd Method for a part load co reduction operation for a sequential gas turbine
RU2561956C2 (ru) 2012-07-09 2015-09-10 Альстом Текнолоджи Лтд Газотурбинная система сгорания
RU2563445C2 (ru) * 2012-07-13 2015-09-20 Альстом Текнолоджи Лтд Способ и устройство для регулирования помпажа газотурбинного двигателя
AU2013219140B2 (en) 2012-08-24 2015-10-08 Ansaldo Energia Switzerland AG Method for mixing a dilution air in a sequential combustion system of a gas turbine
EP2700879B1 (en) 2012-08-24 2019-03-27 Ansaldo Energia Switzerland AG Method for mixing a dilution air in a sequential combustion system of a gas turbine, and sequential combustion system for a gas turbine comprising dilution air injector
CA2829613C (en) 2012-10-22 2016-02-23 Alstom Technology Ltd. Method for operating a gas turbine with sequential combustion and gas turbine for conducting said method
JP5899133B2 (ja) * 2013-02-01 2016-04-06 株式会社日立製作所 2軸ガスタービン
EP2600063A3 (en) 2013-02-19 2014-05-07 Alstom Technology Ltd Method of operating a gas turbine with staged and/or sequential combustion
US9624829B2 (en) 2013-03-05 2017-04-18 Industrial Turbine Company (Uk) Limited Cogen heat load matching through reheat and capacity match
US10036317B2 (en) * 2013-03-05 2018-07-31 Industrial Turbine Company (Uk) Limited Capacity control of turbine by the use of a reheat combustor in multi shaft engine
EP2789915A1 (en) * 2013-04-10 2014-10-15 Alstom Technology Ltd Method for operating a combustion chamber and combustion chamber
EP2829705A1 (en) * 2013-07-24 2015-01-28 Alstom Technology Ltd Gas turbine and method of controlling gas turbine
EP2835516A1 (en) * 2013-08-08 2015-02-11 Alstom Technology Ltd Gas turbine with improved part load emissions behavior
JP6190670B2 (ja) * 2013-08-30 2017-08-30 三菱日立パワーシステムズ株式会社 ガスタービン燃焼システム
EP2857658A1 (en) * 2013-10-01 2015-04-08 Alstom Technology Ltd Gas turbine with sequential combustion arrangement
RU2561754C1 (ru) * 2014-02-12 2015-09-10 Открытое акционерное общество "Газпром" Кольцевая камера сгорания газотурбинного двигателя и способ её эксплуатации
US20160237904A1 (en) * 2015-02-13 2016-08-18 General Electric Company Systems and methods for controlling an inlet air temperature of an intercooled gas turbine engine
EP3061944A1 (en) 2015-02-26 2016-08-31 General Electric Technology GmbH Method for controlling the operation of a gas turbine with sequential combustion
US10316696B2 (en) 2015-05-08 2019-06-11 General Electric Company System and method for improving exhaust energy recovery
US9957900B2 (en) 2015-05-11 2018-05-01 General Electric Company System and method for flow control in turbine
US10330015B2 (en) * 2015-09-25 2019-06-25 General Electric Company Transient emission temperature control of turbine systems
US10920676B2 (en) * 2016-11-17 2021-02-16 General Electric Company Low partial load emission control for gas turbine system
HUE050483T2 (hu) * 2017-03-14 2020-12-28 Gen Electric Módszer és rendszer egy szekvenciális gázturbinamotor vezérlésére
US11092085B2 (en) * 2017-03-14 2021-08-17 General Electric Company Method and system for controlling a sequential gas turbine engine
EP3421761B1 (en) * 2017-06-30 2020-11-25 Ansaldo Energia IP UK Limited Second-stage combustor for a sequential combustor of a gas turbine
RU2685802C1 (ru) * 2017-12-28 2019-04-23 Игорь Анатольевич Мнушкин Газоперекачивающий агрегат
EP3524799A1 (de) 2018-02-13 2019-08-14 Siemens Aktiengesellschaft Verfahren zum betreiben einer brenneranordnung einer gasturbine
EP3578762A1 (en) * 2018-06-08 2019-12-11 General Electric Technology GmbH Method for determining an outlet temperature of an upstream combustion stage in a gas turbine engine having at least two serially arranged combustion stages
EP3683426B1 (en) * 2019-01-15 2023-05-03 Ansaldo Energia Switzerland AG Method for operating a gas turbine power plant and gas turbine power plant
JP7231493B2 (ja) * 2019-06-12 2023-03-01 三菱重工業株式会社 制御装置、ガスタービン、制御方法及びプログラム
EP3772616B1 (en) * 2019-08-08 2024-02-07 Ansaldo Energia Switzerland AG Method for operating a gas turbine assembly comprising a sequential combustor
EP3822468B1 (en) * 2019-11-18 2024-04-03 Ansaldo Energia Switzerland AG Gas turbine engine operable at very low partial load and method of controlling a gas turbine engine
US11203986B1 (en) * 2020-06-08 2021-12-21 General Electric Company Systems and methods for extended emissions compliant operation of a gas turbine engine
CN112627989A (zh) * 2021-01-08 2021-04-09 大连欧谱纳透平动力科技有限公司 控制小型燃气轮机排气温度和氮氧化物浓度的系统及方法
CN114001374B (zh) * 2021-11-12 2024-12-03 西安热工研究院有限公司 一种适用于气液两相双燃料旋转爆震燃烧室
EP4206452A1 (en) * 2021-12-30 2023-07-05 Ansaldo Energia Switzerland AG Method for operating a gas turbine assembly for a power plant and gas turbine assembly for a power plant

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5226287A (en) * 1991-07-19 1993-07-13 General Electric Company Compressor stall recovery apparatus
JP3131805B2 (ja) * 1992-06-16 2001-02-05 三井造船株式会社 ガスタービン用燃焼器における燃料分配制御装置
JPH06213456A (ja) * 1993-01-13 1994-08-02 Mitsui Eng & Shipbuild Co Ltd ガスタービン用燃焼器とその燃料制御装置
EP0646705B1 (de) * 1993-09-06 1999-06-09 Asea Brown Boveri Ag Verfahren zur Erstellung eines Teillastbetriebes bei einer Gasturbogruppe
DE59307747D1 (de) * 1993-09-06 1998-01-08 Asea Brown Boveri Verfahren zur Regelung einer mit zwei Brennkammern bestückten Gasturbogruppe
DE4446610A1 (de) * 1994-12-24 1996-06-27 Abb Management Ag Verfahren zum Betrieb einer Gasturbogruppe
RU2186232C2 (ru) * 1997-05-06 2002-07-27 Особов Виктор Исаакович Способ работы газотурбинной установки
EP0921292B1 (de) * 1997-12-08 2003-09-10 ALSTOM (Switzerland) Ltd Verfahren zur Regelung einer Gasturbogruppe
DE59811336D1 (de) * 1998-07-22 2004-06-09 Alstom Technology Ltd Baden Verfahren zum Betrieb einer Gasturbinenbrennkammer mit flüssigem Brennstoff
JP2002295831A (ja) * 2001-03-30 2002-10-09 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器の燃焼制御システム
DE10160997A1 (de) * 2001-12-12 2003-07-03 Rolls Royce Deutschland Magervormischbrenner für eine Gasturbine sowie Verfahren zum Betrieb eines Magervormischbrenners
EP1531305A1 (en) * 2003-11-12 2005-05-18 United Technologies Corporation Multi-point fuel injector
JP4015656B2 (ja) * 2004-11-17 2007-11-28 三菱重工業株式会社 ガスタービン燃焼器
JP4486549B2 (ja) * 2005-06-06 2010-06-23 三菱重工業株式会社 ガスタービンの燃焼器
US7565805B2 (en) 2005-11-22 2009-07-28 General Electric Company Method for operating gas turbine engine systems
WO2010000020A1 (en) 2008-06-30 2010-01-07 Cathrx Ltd A catheter
CH700796A1 (de) 2009-04-01 2010-10-15 Alstom Technology Ltd Verfahren zum CO-emissionsarmen Betrieb einer Gasturbine mit sequentieller Verbrennung und Gasturbine mit verbessertem Teillast- Emissionsverhalten.

Similar Documents

Publication Publication Date Title
JP2012522922A5 (enExample)
RU2015139836A (ru) Способ работы газотурбинной установкой со ступенчатым и/или последовательным сгоранием
RU2011144106A (ru) Газовая турбина с уменьшенными выбросами при частичной нагрузке
CN103133147B (zh) 用于改变燃气涡轮系统中的功率输出的方法和设备
CN105492752B (zh) 直接废气再循环系统
US9470145B2 (en) System and method for heating fuel in a combined cycle gas turbine
CN104160131B (zh) 构造为调整电力输出的燃气涡轮机发动机
CN104373219B (zh) 具有改进部分负载排放性能的燃气涡轮
RU2017141162A (ru) Система и способ для системы двигателя с разветвленной выпускной системой
US9435258B2 (en) System and method for heating combustor fuel
RU2017140837A (ru) Система и способ для системы двигателя с разветвленной выпускной системой
WO2008090445A3 (en) Exhaust gas control system for internal combustion engine and method for controlling the same
JP2012092842A5 (ja) ピストン往復内燃機関のための給気制御装置、ピストン往復内燃機関のための給気制御装置に用いられる弁、および、ピストン往復内燃機関の運動を制御するための方法
CN102482989A (zh) 用于空气节流式发动机的涡轮增压器系统
CN103104345A (zh) 用于吹扫燃气涡轮发动机的气体燃料线路的系统
US10174639B2 (en) Steam turbine preheating system
JP2017106444A (ja) 入口抽気加熱制御システム
CA2987412A1 (en) Method for operating an internal combustion engine
CN104832221B (zh) 涡轮增压防喘振系统
CN101799370B (zh) 多功能相继增压热动力试验台
EP3181859A1 (en) System and method for controlling gas turbine exhaust energy via exhaust gas damper and compressed gas supply
KR101098662B1 (ko) 엔진 시스템
Li et al. Research on a closed-loop control strategy of boost pressure in diesel engines with regulated two-stage turbocharging system
US12454919B2 (en) Exhaust cooling injection for improved turndown
US9638098B2 (en) Bypass mechanism for an exhaust system