KR101576720B1 - 가스 터빈 연소기 - Google Patents

가스 터빈 연소기 Download PDF

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Publication number
KR101576720B1
KR101576720B1 KR1020137033961A KR20137033961A KR101576720B1 KR 101576720 B1 KR101576720 B1 KR 101576720B1 KR 1020137033961 A KR1020137033961 A KR 1020137033961A KR 20137033961 A KR20137033961 A KR 20137033961A KR 101576720 B1 KR101576720 B1 KR 101576720B1
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South Korea
Prior art keywords
resonance device
resonance
inner cylinder
inner tube
combustion
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Korean (ko)
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KR20140012183A (ko
Inventor
신지 아카마츠
히로아키 기시다
겐지 사토
겐타로 도쿠야마
게이스케 마츠야마
다카요시 다카시마
Original Assignee
미츠비시 히타치 파워 시스템즈 가부시키가이샤
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Publication of KR20140012183A publication Critical patent/KR20140012183A/ko
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/24Heat or noise insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23MCASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M20/00Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
    • F23M20/005Noise absorbing means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00014Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
KR1020137033961A 2011-07-07 2012-06-28 가스 터빈 연소기 Active KR101576720B1 (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2011151310A JP5804808B2 (ja) 2011-07-07 2011-07-07 ガスタービン燃焼器及びその燃焼振動減衰方法
JPJP-P-2011-151310 2011-07-07
PCT/JP2012/066596 WO2013005651A1 (ja) 2011-07-07 2012-06-28 ガスタービン燃焼器

Publications (2)

Publication Number Publication Date
KR20140012183A KR20140012183A (ko) 2014-01-29
KR101576720B1 true KR101576720B1 (ko) 2015-12-10

Family

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KR1020137033961A Active KR101576720B1 (ko) 2011-07-07 2012-06-28 가스 터빈 연소기

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Country Link
US (2) US9003800B2 (cg-RX-API-DMAC7.html)
EP (1) EP2730845B1 (cg-RX-API-DMAC7.html)
JP (1) JP5804808B2 (cg-RX-API-DMAC7.html)
KR (1) KR101576720B1 (cg-RX-API-DMAC7.html)
CN (1) CN103620307B (cg-RX-API-DMAC7.html)
WO (1) WO2013005651A1 (cg-RX-API-DMAC7.html)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5804808B2 (ja) * 2011-07-07 2015-11-04 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及びその燃焼振動減衰方法
US10088165B2 (en) * 2015-04-07 2018-10-02 General Electric Company System and method for tuning resonators
US20160003162A1 (en) * 2013-02-28 2016-01-07 Siemens Aktiengesellschaft Damping device for a gas turbine, gas turbine and method for damping thermoacoustic oscillations
US9410484B2 (en) 2013-07-19 2016-08-09 Siemens Aktiengesellschaft Cooling chamber for upstream weld of damping resonator on turbine component
CN107076416B (zh) 2014-08-26 2020-05-19 西门子能源公司 用于燃气涡轮发动机中的声共振器的薄膜冷却孔装置
US20170268777A1 (en) * 2014-09-05 2017-09-21 Siemens Aktiengesellschaft Acoustic damping system for a combustor of a gas turbine engine
JP6623485B2 (ja) * 2014-09-25 2019-12-25 三菱日立パワーシステムズ株式会社 燃焼器、及びこれを備えるガスタービン
WO2016057009A1 (en) * 2014-10-06 2016-04-14 Siemens Aktiengesellschaft Combustor and method for damping vibrational modes under high-frequency combustion dynamics
CN104566477B (zh) * 2014-12-31 2019-02-01 北京华清燃气轮机与煤气化联合循环工程技术有限公司 用于燃气轮机火焰筒的调频装置及燃气轮机火焰筒
KR101853456B1 (ko) * 2015-06-16 2018-04-30 두산중공업 주식회사 가스터빈용 연소 덕트 조립체
WO2016209222A1 (en) * 2015-06-24 2016-12-29 Siemens Aktiengesellschaft Combustor basket cooling ring
US10513984B2 (en) 2015-08-25 2019-12-24 General Electric Company System for suppressing acoustic noise within a gas turbine combustor
DE112016005084B4 (de) * 2015-11-05 2022-09-22 Mitsubishi Heavy Industries, Ltd. Verbrennungszylinder, Gasturbinenbrennkammer und Gasturbine
US10344978B2 (en) * 2016-03-15 2019-07-09 General Electric Company Combustion liner cooling
US10197275B2 (en) 2016-05-03 2019-02-05 General Electric Company High frequency acoustic damper for combustor liners
US10876732B2 (en) * 2016-10-19 2020-12-29 Gloyer-Taylor Laboratories Llc Scalable acoustically-stable combustion chamber and design methods
JP6797728B2 (ja) * 2017-03-24 2020-12-09 三菱パワー株式会社 ガスタービン燃焼器の共鳴吸音装置並びにこれを備えたガスタービン燃焼器及びガスタービン
KR102044668B1 (ko) 2018-11-30 2019-11-20 한국기계연구원 연소진동 저감용 노즐 가이드를 구비한 가스터빈 연소기
DE102019205540A1 (de) * 2019-04-17 2020-10-22 Siemens Aktiengesellschaft Resonator, Verfahren zur Herstellung eines solchen sowie mit einem solchen versehene Brenneranordnung
JP2021063464A (ja) * 2019-10-15 2021-04-22 三菱パワー株式会社 ガスタービン燃焼器
KR102117531B1 (ko) * 2019-11-07 2020-06-10 한국기계연구원 연소진동 저감을 위한 음향 감쇠 구조를 갖는 가스터빈 연소기용 버너
US20240027069A1 (en) * 2020-03-31 2024-01-25 Mitsubishi Heavy Industries, Ltd. Combustor for gas turbine and gas turbine
DE102020213836A1 (de) * 2020-11-04 2022-05-05 Siemens Energy Global GmbH & Co. KG Resonatorring, Verfahren und Brennkorb

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110138812A1 (en) 2009-12-15 2011-06-16 Johnson Clifford E Resonator System for Turbine Engines

Family Cites Families (50)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3819009A (en) * 1973-02-01 1974-06-25 Gen Electric Duct wall acoustic treatment
DE3766807D1 (de) * 1986-11-25 1991-01-31 Gen Electric Kombinierter diffusions- und vormischpilotbrenner.
US4944362A (en) 1988-11-25 1990-07-31 General Electric Company Closed cavity noise suppressor
EP0576717A1 (de) * 1992-07-03 1994-01-05 Abb Research Ltd. Gasturbinen-Brennkammer
US5410884A (en) * 1992-10-19 1995-05-02 Mitsubishi Jukogyo Kabushiki Kaisha Combustor for gas turbines with diverging pilot nozzle cone
JPH06159033A (ja) 1992-11-20 1994-06-07 Ishikawajima Harima Heavy Ind Co Ltd 音響ライナー
JP3930252B2 (ja) * 2000-01-07 2007-06-13 三菱重工業株式会社 ガスタービン燃焼器
US6530221B1 (en) * 2000-09-21 2003-03-11 Siemens Westinghouse Power Corporation Modular resonators for suppressing combustion instabilities in gas turbine power plants
US6973790B2 (en) * 2000-12-06 2005-12-13 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor, gas turbine, and jet engine
JP3676228B2 (ja) 2000-12-06 2005-07-27 三菱重工業株式会社 ガスタービン燃焼器およびガスタービン並びにジェットエンジン
DE60135436D1 (de) * 2001-01-09 2008-10-02 Mitsubishi Heavy Ind Ltd Gasturbinenbrennkammer
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
JP2003065536A (ja) 2001-08-21 2003-03-05 Mitsubishi Heavy Ind Ltd 低noxガスタービン燃焼器
EP1423645B1 (de) * 2001-09-07 2008-10-08 Alstom Technology Ltd Dämpfungsanordnung zur reduzierung von brennkammerpulsationen in einer gasturbinenanlage
JP3993484B2 (ja) 2002-07-15 2007-10-17 三菱重工業株式会社 燃焼器冷却構造
JP2005076982A (ja) * 2003-08-29 2005-03-24 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
US6920958B2 (en) 2003-10-17 2005-07-26 The Boeing Company Annular acoustic panel
JP2005264729A (ja) 2004-03-16 2005-09-29 Mitsubishi Heavy Ind Ltd 遮音構造及びこの遮音構造を備えたタービン
JP4274996B2 (ja) 2004-04-27 2009-06-10 三菱重工業株式会社 ガスタービン燃焼器
US7337875B2 (en) 2004-06-28 2008-03-04 United Technologies Corporation High admittance acoustic liner
JP2006097983A (ja) 2004-09-29 2006-04-13 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
JP2006097981A (ja) 2004-09-29 2006-04-13 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
JP2006132505A (ja) 2004-11-09 2006-05-25 Mitsubishi Heavy Ind Ltd 音響装置、燃焼器及びガスタービン
US20060169533A1 (en) 2005-02-03 2006-08-03 Patrick William P Acoustic liner with a nonuniform depth backwall
US20060169532A1 (en) 2005-02-03 2006-08-03 Patrick William P Acoustic liner with nonuniform impedance
JP4754987B2 (ja) 2005-02-22 2011-08-24 三菱重工業株式会社 減衰装置、燃焼器及びガスタービン
US7296655B2 (en) 2005-04-22 2007-11-20 United Technologies Corporation Duct liner acoustic splice
GB0510538D0 (en) 2005-05-24 2005-06-29 Rolls Royce Plc A rotor blade containment assembly for a gas turbine engine
US7311175B2 (en) 2005-08-10 2007-12-25 United Technologies Corporation Acoustic liner with bypass cooling
US7401682B2 (en) 2005-08-10 2008-07-22 United Technologies Corporation Architecture for an acoustic liner
US7861823B2 (en) 2005-11-04 2011-01-04 United Technologies Corporation Duct for reducing shock related noise
JP2007132640A (ja) 2005-11-14 2007-05-31 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
US8602156B2 (en) 2006-05-19 2013-12-10 United Technologies Corporation Multi-splice acoustic liner
US7469770B2 (en) 2006-06-29 2008-12-30 United Technologies Corporation Anechoic visco-thermal liner
JP4773904B2 (ja) 2006-07-11 2011-09-14 三菱重工業株式会社 ガスタービン燃焼器
US7788926B2 (en) * 2006-08-18 2010-09-07 Siemens Energy, Inc. Resonator device at junction of combustor and combustion chamber
JP2008121961A (ja) 2006-11-10 2008-05-29 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器用の音響ライナー
US8769963B2 (en) * 2007-01-30 2014-07-08 Siemens Energy, Inc. Low leakage spring clip/ring combinations for gas turbine engine
JP4146492B2 (ja) 2007-01-31 2008-09-10 三菱重工業株式会社 燃焼器尾筒の冷却構造
JP2008304125A (ja) 2007-06-07 2008-12-18 Mitsubishi Heavy Ind Ltd 音響ダンパの振動低減構造
JP2009062977A (ja) 2007-08-15 2009-03-26 Rohr Inc 線形音響ライナー
JP2008114838A (ja) 2007-10-26 2008-05-22 General Electric Co <Ge> 補助動力装置組立体
GB0813821D0 (en) 2008-07-29 2008-09-03 Rolls Royce Plc A fan casing for a gas turbine engine
US8408004B2 (en) * 2009-06-16 2013-04-02 General Electric Company Resonator assembly for mitigating dynamics in gas turbines
US8789372B2 (en) * 2009-07-08 2014-07-29 General Electric Company Injector with integrated resonator
RU2508506C2 (ru) * 2009-09-01 2014-02-27 Дженерал Электрик Компани Способ и установка для ввода текучей среды в камеру сгорания газотурбинного двигателя
EP2302302A1 (en) * 2009-09-23 2011-03-30 Siemens Aktiengesellschaft Helmholtz resonator for a gas turbine combustion chamber
JP5804808B2 (ja) * 2011-07-07 2015-11-04 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及びその燃焼振動減衰方法
US9395082B2 (en) * 2011-09-23 2016-07-19 Siemens Aktiengesellschaft Combustor resonator section with an internal thermal barrier coating and method of fabricating the same
US9163837B2 (en) * 2013-02-27 2015-10-20 Siemens Aktiengesellschaft Flow conditioner in a combustor of a gas turbine engine

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110138812A1 (en) 2009-12-15 2011-06-16 Johnson Clifford E Resonator System for Turbine Engines

Also Published As

Publication number Publication date
JP5804808B2 (ja) 2015-11-04
EP2730845A4 (en) 2015-02-25
US10197284B2 (en) 2019-02-05
JP2013019567A (ja) 2013-01-31
EP2730845A1 (en) 2014-05-14
EP2730845B1 (en) 2020-02-12
CN103620307B (zh) 2015-08-12
CN103620307A (zh) 2014-03-05
US20130008167A1 (en) 2013-01-10
US9003800B2 (en) 2015-04-14
KR20140012183A (ko) 2014-01-29
WO2013005651A1 (ja) 2013-01-10
US20150101343A1 (en) 2015-04-16

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