CN103620307B - 燃气轮机燃烧器 - Google Patents
燃气轮机燃烧器 Download PDFInfo
- Publication number
- CN103620307B CN103620307B CN201280030030.6A CN201280030030A CN103620307B CN 103620307 B CN103620307 B CN 103620307B CN 201280030030 A CN201280030030 A CN 201280030030A CN 103620307 B CN103620307 B CN 103620307B
- Authority
- CN
- China
- Prior art keywords
- resonance device
- inner core
- described inner
- gas turbine
- resonance
- 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.)
- Active
Links
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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
-
- 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
-
- 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
- F02C7/24—Heat or noise insulation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, 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
- F23M20/00—Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
- F23M20/005—Noise absorbing means
-
- 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
- F23R3/002—Wall structures
-
- 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
Landscapes
- 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)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2011-151310 | 2011-07-07 | ||
| 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 |
| 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 |
|---|---|
| CN103620307A CN103620307A (zh) | 2014-03-05 |
| CN103620307B true CN103620307B (zh) | 2015-08-12 |
Family
ID=47437006
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201280030030.6A Active CN103620307B (zh) | 2011-07-07 | 2012-06-28 | 燃气轮机燃烧器 |
Country Status (6)
| Country | Link |
|---|---|
| US (2) | US9003800B2 (enExample) |
| EP (1) | EP2730845B1 (enExample) |
| JP (1) | JP5804808B2 (enExample) |
| KR (1) | KR101576720B1 (enExample) |
| CN (1) | CN103620307B (enExample) |
| WO (1) | WO2013005651A1 (enExample) |
Families Citing this family (23)
| 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 |
| JP6456481B2 (ja) * | 2014-08-26 | 2019-01-23 | シーメンス エナジー インコーポレイテッド | ガスタービンエンジン内の音響共鳴器用のフィルム冷却孔配列 |
| CN106605102B (zh) * | 2014-09-05 | 2019-10-22 | 西门子公司 | 用于燃气涡轮发动机的燃烧器的声学阻尼系统 |
| 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 |
| JP6522747B2 (ja) * | 2014-10-06 | 2019-05-29 | シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft | 高周波数燃焼ダイナミックスのもとで振動モードを減衰するための燃焼器及び方法 |
| 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 |
| WO2017077955A1 (ja) * | 2015-11-05 | 2017-05-11 | 三菱日立パワーシステムズ株式会社 | 燃焼用筒、ガスタービン燃焼器及びガスタービン |
| 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 |
| DE112021002128T5 (de) * | 2020-03-31 | 2023-03-09 | Mitsubishi Heavy Industries, Ltd. | Brennkammer für Gasturbine und Gasturbine |
| DE102020213836A1 (de) * | 2020-11-04 | 2022-05-05 | Siemens Energy Global GmbH & Co. KG | Resonatorring, Verfahren und Brennkorb |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0576717A1 (de) * | 1992-07-03 | 1994-01-05 | Abb Research Ltd. | Gasturbinen-Brennkammer |
| CN1551965A (zh) * | 2001-09-07 | 2004-12-01 | ��ķ�Ƽ���������˾ | 减小燃气轮机装置中的燃烧室脉动的减振装置 |
| 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 |
Family Cites Families (48)
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| 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 |
| 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 |
| US6530221B1 (en) * | 2000-09-21 | 2003-03-11 | Siemens Westinghouse Power Corporation | Modular resonators for suppressing combustion instabilities in gas turbine power plants |
| 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 |
| US6973790B2 (en) * | 2000-12-06 | 2005-12-13 | Mitsubishi Heavy Industries, Ltd. | Gas turbine combustor, gas turbine, and jet engine |
| 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 |
| 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 |
| JP2006097981A (ja) | 2004-09-29 | 2006-04-13 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器 |
| JP2006097983A (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 |
| US20060169532A1 (en) | 2005-02-03 | 2006-08-03 | Patrick William P | Acoustic liner with nonuniform impedance |
| US20060169533A1 (en) | 2005-02-03 | 2006-08-03 | Patrick William P | Acoustic liner with a nonuniform depth backwall |
| 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 |
| US7401682B2 (en) | 2005-08-10 | 2008-07-22 | United Technologies Corporation | Architecture for an acoustic liner |
| US7311175B2 (en) | 2005-08-10 | 2007-12-25 | United Technologies Corporation | Acoustic liner with bypass cooling |
| 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 |
| US8413443B2 (en) * | 2009-12-15 | 2013-04-09 | Siemens Energy, Inc. | Flow control through a resonator system of gas turbine combustor |
| 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 |
-
2011
- 2011-07-07 JP JP2011151310A patent/JP5804808B2/ja active Active
-
2012
- 2012-06-28 CN CN201280030030.6A patent/CN103620307B/zh active Active
- 2012-06-28 EP EP12807850.8A patent/EP2730845B1/en active Active
- 2012-06-28 KR KR1020137033961A patent/KR101576720B1/ko active Active
- 2012-06-28 WO PCT/JP2012/066596 patent/WO2013005651A1/ja not_active Ceased
- 2012-07-02 US US13/539,559 patent/US9003800B2/en active Active
-
2014
- 2014-12-19 US US14/577,719 patent/US10197284B2/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0576717A1 (de) * | 1992-07-03 | 1994-01-05 | Abb Research Ltd. | Gasturbinen-Brennkammer |
| 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 |
| CN1551965A (zh) * | 2001-09-07 | 2004-12-01 | ��ķ�Ƽ���������˾ | 减小燃气轮机装置中的燃烧室脉动的减振装置 |
Also Published As
| Publication number | Publication date |
|---|---|
| US20150101343A1 (en) | 2015-04-16 |
| CN103620307A (zh) | 2014-03-05 |
| US9003800B2 (en) | 2015-04-14 |
| US20130008167A1 (en) | 2013-01-10 |
| WO2013005651A1 (ja) | 2013-01-10 |
| JP5804808B2 (ja) | 2015-11-04 |
| EP2730845B1 (en) | 2020-02-12 |
| JP2013019567A (ja) | 2013-01-31 |
| US10197284B2 (en) | 2019-02-05 |
| EP2730845A1 (en) | 2014-05-14 |
| KR20140012183A (ko) | 2014-01-29 |
| EP2730845A4 (en) | 2015-02-25 |
| KR101576720B1 (ko) | 2015-12-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| ASS | Succession or assignment of patent right |
Owner name: MITSUBISHI HITACHI POWER SYSTEM LTD. Free format text: FORMER OWNER: MITSUBISHI JUKOGIO KK Effective date: 20150303 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20150303 Address after: Kanagawa Applicant after: Mitsubishi Hitachi Power System Ltd. Address before: Tokyo, Japan, Japan Applicant before: Mit-subishi Heavy Industries Ltd. |
|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: Kanagawa Prefecture, Japan Patentee after: Mitsubishi Power Co., Ltd Address before: Kanagawa Prefecture, Japan Patentee before: MITSUBISHI HITACHI POWER SYSTEMS, Ltd. |