FR2954968B1 - Dispositif acoustique pour circuit de carburant - Google Patents

Dispositif acoustique pour circuit de carburant Download PDF

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Publication number
FR2954968B1
FR2954968B1 FR1150009A FR1150009A FR2954968B1 FR 2954968 B1 FR2954968 B1 FR 2954968B1 FR 1150009 A FR1150009 A FR 1150009A FR 1150009 A FR1150009 A FR 1150009A FR 2954968 B1 FR2954968 B1 FR 2954968B1
Authority
FR
France
Prior art keywords
fluid
upstream
fuel
fuel circuit
define
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.)
Expired - Fee Related
Application number
FR1150009A
Other languages
English (en)
French (fr)
Other versions
FR2954968A1 (fr
Inventor
Kwanwoo Kim
Kapil Kumar Singh
Fei Han
Shiva Srinivasan
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 FR2954968A1 publication Critical patent/FR2954968A1/fr
Application granted granted Critical
Publication of FR2954968B1 publication Critical patent/FR2954968B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F02C7/22—Fuel supply systems
    • F02C7/228—Dividing fuel between various burners
    • 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
    • F02C7/22—Fuel supply systems
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/128—Nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/08—Purpose of the control system to produce clean exhaust gases
    • F05D2270/082—Purpose of the control system to produce clean exhaust gases with as little NOx as possible
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
FR1150009A 2010-01-04 2011-01-03 Dispositif acoustique pour circuit de carburant Expired - Fee Related FR2954968B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/651,600 US8322140B2 (en) 2010-01-04 2010-01-04 Fuel system acoustic feature to mitigate combustion dynamics for multi-nozzle dry low NOx combustion system and method

Publications (2)

Publication Number Publication Date
FR2954968A1 FR2954968A1 (fr) 2011-07-08
FR2954968B1 true FR2954968B1 (fr) 2021-07-23

Family

ID=44203224

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1150009A Expired - Fee Related FR2954968B1 (fr) 2010-01-04 2011-01-03 Dispositif acoustique pour circuit de carburant

Country Status (4)

Country Link
US (1) US8322140B2 (enExample)
JP (1) JP5487095B2 (enExample)
CN (1) CN102116478B (enExample)
FR (1) FR2954968B1 (enExample)

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* Cited by examiner, † Cited by third party
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US10088165B2 (en) 2015-04-07 2018-10-02 General Electric Company System and method for tuning resonators
US9303564B2 (en) 2013-02-27 2016-04-05 General Electric Company Combustor can temperature control system
JP6021705B2 (ja) 2013-03-22 2016-11-09 三菱重工業株式会社 燃焼器、および、ガスタービン
EP3004743B1 (de) * 2013-09-23 2017-05-17 Siemens Aktiengesellschaft Brenner für eine gasturbine und verfahren zur reduzierung von thermoakustischen schwingungen in einer gasturbine
US9644845B2 (en) 2014-02-03 2017-05-09 General Electric Company System and method for reducing modal coupling of combustion dynamics
US9964045B2 (en) 2014-02-03 2018-05-08 General Electric Company Methods and systems for detecting lean blowout in gas turbine systems
US9689574B2 (en) 2014-02-03 2017-06-27 General Electric Company System and method for reducing modal coupling of combustion dynamics
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
JP6452298B2 (ja) * 2014-03-25 2019-01-16 三菱日立パワーシステムズ株式会社 噴射ノズル、ガスタービン燃焼器及びガスタービン
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
US10113747B2 (en) * 2015-04-15 2018-10-30 General Electric Company Systems and methods for control of combustion dynamics in combustion system
US20180363905A1 (en) * 2016-01-13 2018-12-20 General Electric Company Fuel nozzle assembly for reducing multiple tone combustion dynamics
DE102017212616A1 (de) * 2017-07-21 2019-01-24 Rolls-Royce Deutschland Ltd & Co Kg Düsenbaugruppe für eine Brennkammer eines Triebwerks
US11506125B2 (en) 2018-08-01 2022-11-22 General Electric Company Fluid manifold assembly for gas turbine engine
WO2026034272A1 (ja) * 2024-08-05 2026-02-12 三菱重工業株式会社 ガスタービン燃焼器、及びガスタービン

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US5321949A (en) * 1991-07-12 1994-06-21 General Electric Company Staged fuel delivery system with secondary distribution valve
JP2759722B2 (ja) * 1992-05-20 1998-05-28 川崎重工業株式会社 ガスタ−ビンの燃焼制御装置
EP0686812B1 (en) * 1994-06-10 2000-03-29 General Electric Company Operating a combustor of a gas turbine
US5943866A (en) * 1994-10-03 1999-08-31 General Electric Company Dynamically uncoupled low NOx combustor having multiple premixers with axial staging
JP3578852B2 (ja) * 1995-12-05 2004-10-20 東京瓦斯株式会社 マルチバーナ式燃焼器の燃料供給システム及び該燃料供給システムを持つガスタービン
SE9802707L (sv) * 1998-08-11 2000-02-12 Abb Ab Brännkammaranordning och förfarande för att reducera inverkan av akustiska trycksvängningar i en brännkammaranordning
WO2000034714A1 (de) * 1998-12-08 2000-06-15 Siemens Aktiengesellschaft Verbrennungsvorrichtung und verfahren zur verbrennung eines brennstoffs
EP1010939B1 (de) * 1998-12-15 2004-02-11 ALSTOM (Switzerland) Ltd Brennkammer mit akustisch gedämpftem Brennstoffversorgungssystem
JP3962554B2 (ja) * 2001-04-19 2007-08-22 三菱重工業株式会社 ガスタービン燃焼器及びガスタービン
US6820431B2 (en) * 2002-10-31 2004-11-23 General Electric Company Acoustic impedance-matched fuel nozzle device and tunable fuel injection resonator assembly
US7464552B2 (en) * 2004-07-02 2008-12-16 Siemens Energy, Inc. Acoustically stiffened gas-turbine fuel nozzle
RU2300702C1 (ru) * 2006-04-04 2007-06-10 Общество с ограниченной ответственностью "Научно-производственное предприятие "ЭСТ" Способ сжигания топлива и устройство для его осуществления
US7827797B2 (en) * 2006-09-05 2010-11-09 General Electric Company Injection assembly for a combustor
US20090077945A1 (en) * 2007-08-24 2009-03-26 Delavan Inc Variable amplitude double binary valve system for active fuel control
US20090111063A1 (en) * 2007-10-29 2009-04-30 General Electric Company Lean premixed, radial inflow, multi-annular staged nozzle, can-annular, dual-fuel combustor
EP2110602A1 (de) * 2008-04-16 2009-10-21 Siemens Aktiengesellschaft Akustiche Teilentkopplung zur Verringerung von selbstinduzierten Flammenschwingungen
US7578130B1 (en) * 2008-05-20 2009-08-25 General Electric Company Methods and systems for combustion dynamics reduction
US8087228B2 (en) * 2008-09-11 2012-01-03 General Electric Company Segmented combustor cap
US8707707B2 (en) * 2009-01-07 2014-04-29 General Electric Company Late lean injection fuel staging configurations

Also Published As

Publication number Publication date
US20110162370A1 (en) 2011-07-07
CN102116478B (zh) 2014-12-31
JP2011137629A (ja) 2011-07-14
FR2954968A1 (fr) 2011-07-08
CN102116478A (zh) 2011-07-06
JP5487095B2 (ja) 2014-05-07
US8322140B2 (en) 2012-12-04

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