CN103629670A - 用于降低燃烧动态的系统和方法 - Google Patents

用于降低燃烧动态的系统和方法 Download PDF

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Publication number
CN103629670A
CN103629670A CN201310365409.9A CN201310365409A CN103629670A CN 103629670 A CN103629670 A CN 103629670A CN 201310365409 A CN201310365409 A CN 201310365409A CN 103629670 A CN103629670 A CN 103629670A
Authority
CN
China
Prior art keywords
axial distance
combustor
burner
fuel
combustion
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.)
Pending
Application number
CN201310365409.9A
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English (en)
Chinese (zh)
Inventor
S.L.克罗瑟斯
G.O.克雷默
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN103629670A publication Critical patent/CN103629670A/zh
Pending legal-status Critical Current

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Classifications

    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • 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
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03343—Pilot burners operating in premixed mode

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
CN201310365409.9A 2012-08-21 2013-08-21 用于降低燃烧动态的系统和方法 Pending CN103629670A (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/590,309 US9032704B2 (en) 2012-08-21 2012-08-21 System for reducing combustion dynamics
US13/590,309 2012-08-21

Publications (1)

Publication Number Publication Date
CN103629670A true CN103629670A (zh) 2014-03-12

Family

ID=50069702

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310365409.9A Pending CN103629670A (zh) 2012-08-21 2013-08-21 用于降低燃烧动态的系统和方法

Country Status (5)

Country Link
US (1) US9032704B2 (enExample)
JP (1) JP6169920B2 (enExample)
CN (1) CN103629670A (enExample)
CH (1) CH706861B1 (enExample)
DE (1) DE102013108725B4 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106196173A (zh) * 2015-04-15 2016-12-07 通用电气公司 用于控制燃烧系统中的燃烧动态的系统和方法

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US8966909B2 (en) * 2012-08-21 2015-03-03 General Electric Company System for reducing combustion dynamics
US9151502B2 (en) * 2012-08-21 2015-10-06 General Electric Company System and method for reducing modal coupling of combustion dynamics
US10088165B2 (en) 2015-04-07 2018-10-02 General Electric Company System and method for tuning resonators
US9534787B2 (en) 2013-03-12 2017-01-03 General Electric Company Micromixing cap assembly
US9765973B2 (en) 2013-03-12 2017-09-19 General Electric Company System and method for tube level air flow conditioning
US9347668B2 (en) 2013-03-12 2016-05-24 General Electric Company End cover configuration and assembly
US9528444B2 (en) 2013-03-12 2016-12-27 General Electric Company System having multi-tube fuel nozzle with floating arrangement of mixing tubes
US9671112B2 (en) 2013-03-12 2017-06-06 General Electric Company Air diffuser for a head end of a combustor
US9650959B2 (en) * 2013-03-12 2017-05-16 General Electric Company Fuel-air mixing system with mixing chambers of various lengths for gas turbine system
US9366439B2 (en) 2013-03-12 2016-06-14 General Electric Company Combustor end cover with fuel plenums
US9759425B2 (en) 2013-03-12 2017-09-12 General Electric Company System and method having multi-tube fuel nozzle with multiple fuel injectors
US9651259B2 (en) 2013-03-12 2017-05-16 General Electric Company Multi-injector micromixing system
JP5984770B2 (ja) * 2013-09-27 2016-09-06 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およびこれを備えたガスタービン機関
US9964045B2 (en) 2014-02-03 2018-05-08 General Electric Company Methods and systems for detecting lean blowout in gas turbine systems
US9709279B2 (en) * 2014-02-27 2017-07-18 General Electric Company System and method for control of combustion dynamics in combustion system
US9709278B2 (en) 2014-03-12 2017-07-18 General Electric Company System and method for control of combustion dynamics in combustion system
US9644846B2 (en) 2014-04-08 2017-05-09 General Electric Company Systems and methods for control of combustion dynamics and modal coupling in gas turbine engine
US9845956B2 (en) * 2014-04-09 2017-12-19 General Electric Company System and method for control of combustion dynamics in combustion system
US9845732B2 (en) 2014-05-28 2017-12-19 General Electric Company Systems and methods for variation of injectors for coherence reduction in combustion system
US9551283B2 (en) 2014-06-26 2017-01-24 General Electric Company Systems and methods for a fuel pressure oscillation device for reduction of coherence
US10094568B2 (en) * 2014-08-28 2018-10-09 General Electric Company Combustor dynamics mitigation
WO2016057009A1 (en) * 2014-10-06 2016-04-14 Siemens Aktiengesellschaft Combustor and method for damping vibrational modes under high-frequency combustion dynamics
US10344982B2 (en) 2016-12-30 2019-07-09 General Electric Company Compact multi-residence time bundled tube fuel nozzle having transition portions of different lengths
KR102572047B1 (ko) * 2018-10-05 2023-08-30 파이브즈 필라드 버너 및 버너 연소 방법
KR102460672B1 (ko) 2021-01-06 2022-10-27 두산에너빌리티 주식회사 연료 노즐, 연료 노즐 모듈 및 이를 포함하는 연소기
DE102021110616A1 (de) 2021-04-26 2022-10-27 Rolls-Royce Deutschland Ltd & Co Kg Kraftstoffdüse mit unterschiedlichen ersten und zweiten Ausströmöffnungen für die Bereitstellung eines Wasserstoff-Luft-Gemisches
KR102667812B1 (ko) 2022-02-07 2024-05-20 두산에너빌리티 주식회사 연소기용 노즐 및 이를 포함하는 가스 터빈
US12281795B1 (en) * 2024-03-11 2025-04-22 Rtx Corporation Cluster of swirled mini-mixers for fuel-staged, axially staged combustion
US20250362020A1 (en) * 2024-05-22 2025-11-27 General Electric Company Gas turbine engine and fuel nozzle assembly therefor

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US5943866A (en) * 1994-10-03 1999-08-31 General Electric Company Dynamically uncoupled low NOx combustor having multiple premixers with axial staging
JP2003090535A (ja) * 2001-09-17 2003-03-28 Ishikawajima Harima Heavy Ind Co Ltd ガスタービンの燃焼器
US7827797B2 (en) 2006-09-05 2010-11-09 General Electric Company Injection assembly for a combustor
US7578130B1 (en) 2008-05-20 2009-08-25 General Electric Company Methods and systems for combustion dynamics reduction
US8408004B2 (en) 2009-06-16 2013-04-02 General Electric Company Resonator assembly for mitigating dynamics in gas turbines
US20120180487A1 (en) * 2011-01-19 2012-07-19 General Electric Company System for flow control in multi-tube fuel nozzle
US8875516B2 (en) * 2011-02-04 2014-11-04 General Electric Company Turbine combustor configured for high-frequency dynamics mitigation and related method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106196173A (zh) * 2015-04-15 2016-12-07 通用电气公司 用于控制燃烧系统中的燃烧动态的系统和方法
CN106196173B (zh) * 2015-04-15 2020-03-24 通用电气公司 用于控制燃烧系统中的燃烧动态的系统和方法

Also Published As

Publication number Publication date
JP2014040999A (ja) 2014-03-06
CH706861A8 (de) 2014-07-31
CH706861A2 (de) 2014-02-28
CH706861B1 (en) 2017-03-31
DE102013108725B4 (de) 2025-01-23
JP6169920B2 (ja) 2017-07-26
US9032704B2 (en) 2015-05-19
US20140053528A1 (en) 2014-02-27
DE102013108725A1 (de) 2014-02-27

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Application publication date: 20140312