CN103216339B - 燃烧器熄火恢复方法和系统 - Google Patents

燃烧器熄火恢复方法和系统 Download PDF

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Publication number
CN103216339B
CN103216339B CN201310027202.0A CN201310027202A CN103216339B CN 103216339 B CN103216339 B CN 103216339B CN 201310027202 A CN201310027202 A CN 201310027202A CN 103216339 B CN103216339 B CN 103216339B
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CN
China
Prior art keywords
combustion
fuel
turbine
controller
gas turbine
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CN201310027202.0A
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English (en)
Chinese (zh)
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CN103216339A (zh
Inventor
B.W.罗米格
D.W.西蒙斯
V.纳拉
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The General Electric Company PLC
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General Electric Co
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Publication of CN103216339A publication Critical patent/CN103216339A/zh
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Publication of CN103216339B publication Critical patent/CN103216339B/zh
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/262—Restarting after flame-out
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Regulation And Control Of Combustion (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Control Of Turbines (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
CN201310027202.0A 2012-01-18 2013-01-18 燃烧器熄火恢复方法和系统 Active CN103216339B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/352496 2012-01-18
US13/352,496 US8959925B2 (en) 2012-01-18 2012-01-18 Combustor recovery method and system

Publications (2)

Publication Number Publication Date
CN103216339A CN103216339A (zh) 2013-07-24
CN103216339B true CN103216339B (zh) 2016-07-06

Family

ID=47559318

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310027202.0A Active CN103216339B (zh) 2012-01-18 2013-01-18 燃烧器熄火恢复方法和系统

Country Status (5)

Country Link
US (1) US8959925B2 (cg-RX-API-DMAC7.html)
EP (1) EP2617964B1 (cg-RX-API-DMAC7.html)
JP (1) JP6154612B2 (cg-RX-API-DMAC7.html)
CN (1) CN103216339B (cg-RX-API-DMAC7.html)
RU (1) RU2614471C2 (cg-RX-API-DMAC7.html)

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EP2762687A1 (en) * 2013-02-01 2014-08-06 Siemens Aktiengesellschaft Method for starting a combustion system
US9500367B2 (en) 2013-11-11 2016-11-22 General Electric Company Combustion casing manifold for high pressure air delivery to a fuel nozzle pilot system
US9790834B2 (en) 2014-03-20 2017-10-17 General Electric Company Method of monitoring for combustion anomalies in a gas turbomachine and a gas turbomachine including a combustion anomaly detection system
US10161635B2 (en) * 2014-06-13 2018-12-25 Rolls-Royce Corporation Combustor with spring-loaded crossover tubes
US9791351B2 (en) 2015-02-06 2017-10-17 General Electric Company Gas turbine combustion profile monitoring
CN105840318A (zh) * 2016-04-18 2016-08-10 姚军 引擎快速重启方法及装置
JP6590771B2 (ja) * 2016-08-09 2019-10-16 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器
US10641179B2 (en) * 2016-11-07 2020-05-05 General Electric Company System and method for starting gas turbine engines
US10731568B2 (en) * 2016-11-23 2020-08-04 General Electric Company Systems and methods for reducing airflow imbalances in turbines
EP3456946A1 (en) 2017-09-18 2019-03-20 Siemens Aktiengesellschaft Controller & method
JP6965108B2 (ja) * 2017-11-08 2021-11-10 三菱パワー株式会社 ガスタービン燃焼器
US11519292B2 (en) 2021-03-24 2022-12-06 General Electric Company Non-optical flame detector and method for a combustor of a turbine engine
KR20240165768A (ko) 2023-05-16 2024-11-25 두산에너빌리티 주식회사 가스터빈 연소기 자동제어 시스템 및 방법

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US4249372A (en) * 1979-07-16 1981-02-10 General Electric Company Cross-ignition assembly for combustion apparatus
US5404709A (en) * 1993-09-20 1995-04-11 General Electric Company Method for supplying fuel to a gas turbine engine
US5722230A (en) * 1995-08-08 1998-03-03 General Electric Co. Center burner in a multi-burner combustor
US6334294B1 (en) * 2000-05-16 2002-01-01 General Electric Company Combustion crossfire tube with integral soft chamber
CN1702306A (zh) * 2004-05-28 2005-11-30 通用电气公司 用来预测和/或避免稀油熄火的方法和装置
CN1743651A (zh) * 2004-08-31 2006-03-08 通用电气公司 避免燃气涡轮发动机贫燃料熄火的方法和设备

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US4625510A (en) * 1981-04-24 1986-12-02 Bendix Avelex Inc. Stress limiter apparatus for a gas turbine engine
JPH11148370A (ja) * 1997-11-17 1999-06-02 Hitachi Ltd ガスタービン
US6274945B1 (en) * 1999-12-13 2001-08-14 Capstone Turbine Corporation Combustion control method and system
US6772583B2 (en) * 2002-09-11 2004-08-10 Siemens Westinghouse Power Corporation Can combustor for a gas turbine engine
BRPI0406806A (pt) * 2003-01-17 2005-12-27 Catalytica Energy Sys Inc Sistema e método de controle dinâmico para multicombustor catalìtico para motor de turbina a gás
US7246002B2 (en) 2003-11-20 2007-07-17 General Electric Company Method for controlling fuel splits to gas turbine combustor
US7389643B2 (en) 2005-01-31 2008-06-24 General Electric Company Inboard radial dump venturi for combustion chamber of a gas turbine
US7614238B2 (en) 2005-11-22 2009-11-10 Honeywell International Inc. Method for lean blowout protection in turbine engines
US7457688B2 (en) * 2006-09-19 2008-11-25 General Electric Company Method and system for detection and transfer to electrical island operation
US7802434B2 (en) * 2006-12-18 2010-09-28 General Electric Company Systems and processes for reducing NOx emissions
US8707704B2 (en) 2007-05-31 2014-04-29 General Electric Company Method and apparatus for assembling turbine engines
US7997083B2 (en) * 2007-08-28 2011-08-16 General Electric Company Method and system for detection of gas turbine combustion blowouts utilizing fuel normalized power response
JP4959523B2 (ja) * 2007-11-29 2012-06-27 株式会社日立製作所 燃焼装置，燃焼装置の改造方法及び燃焼装置の燃料噴射方法
US8997499B2 (en) 2009-03-04 2015-04-07 Alstom Technology Ltd Load rejection and recovery using a secondary fuel nozzle
US20110083440A1 (en) * 2009-10-14 2011-04-14 General Electric Company High strength crossover manifold and method of joining
US20120006032A1 (en) * 2010-07-06 2012-01-12 General Electric Company Systems, methods, and apparatus for confirming ignition in a gas turbine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4249372A (en) * 1979-07-16 1981-02-10 General Electric Company Cross-ignition assembly for combustion apparatus
US5404709A (en) * 1993-09-20 1995-04-11 General Electric Company Method for supplying fuel to a gas turbine engine
US5722230A (en) * 1995-08-08 1998-03-03 General Electric Co. Center burner in a multi-burner combustor
US6334294B1 (en) * 2000-05-16 2002-01-01 General Electric Company Combustion crossfire tube with integral soft chamber
CN1702306A (zh) * 2004-05-28 2005-11-30 通用电气公司 用来预测和/或避免稀油熄火的方法和装置
CN1743651A (zh) * 2004-08-31 2006-03-08 通用电气公司 避免燃气涡轮发动机贫燃料熄火的方法和设备

Also Published As

Publication number Publication date
EP2617964B1 (en) 2019-03-13
US8959925B2 (en) 2015-02-24
CN103216339A (zh) 2013-07-24
RU2614471C2 (ru) 2017-03-28
JP2013148090A (ja) 2013-08-01
RU2013102017A (ru) 2014-07-27
EP2617964A2 (en) 2013-07-24
EP2617964A3 (en) 2017-08-02
JP6154612B2 (ja) 2017-06-28
US20130180260A1 (en) 2013-07-18

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Effective date of registration: 20231226

Address after: Swiss Baden

Patentee after: GENERAL ELECTRIC CO. LTD.

Address before: New York State, USA

Patentee before: General Electric Co.

TR01 Transfer of patent right