DE60135280D1 - Vorrichtung zur Verminderung von Schwingungen einer Turbinenbrennkammer - Google Patents
Vorrichtung zur Verminderung von Schwingungen einer TurbinenbrennkammerInfo
- Publication number
- DE60135280D1 DE60135280D1 DE60135280T DE60135280T DE60135280D1 DE 60135280 D1 DE60135280 D1 DE 60135280D1 DE 60135280 T DE60135280 T DE 60135280T DE 60135280 T DE60135280 T DE 60135280T DE 60135280 D1 DE60135280 D1 DE 60135280D1
- Authority
- DE
- Germany
- Prior art keywords
- combustion chamber
- turbine combustion
- reducing vibrations
- vibrations
- reducing
- 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 - Lifetime
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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/26—Controlling the air flow
-
- 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
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
-
- 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
- F23R3/54—Reverse-flow combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2210/00—Noise abatement
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
- F23D2900/00008—Burner assemblies with diffusion and premix modes, i.e. dual mode burners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
- F23D2900/14—Special features of gas burners
- F23D2900/14004—Special features of gas burners with radially extending gas distribution spokes
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2000220832A JP2002039533A (ja) | 2000-07-21 | 2000-07-21 | 燃焼器、ガスタービン及びジェットエンジン |
Publications (1)
Publication Number | Publication Date |
---|---|
DE60135280D1 true DE60135280D1 (de) | 2008-09-25 |
Family
ID=18715365
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60135280T Expired - Lifetime DE60135280D1 (de) | 2000-07-21 | 2001-04-26 | Vorrichtung zur Verminderung von Schwingungen einer Turbinenbrennkammer |
Country Status (5)
Country | Link |
---|---|
US (1) | US6594999B2 (de) |
EP (1) | EP1174662B1 (de) |
JP (1) | JP2002039533A (de) |
CA (1) | CA2353514C (de) |
DE (1) | DE60135280D1 (de) |
Families Citing this family (74)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2913822B2 (ja) * | 1990-11-14 | 1999-06-28 | トヨタ自動車株式会社 | 加速スリップ制御装置 |
GB2375601A (en) * | 2001-05-18 | 2002-11-20 | Siemens Ag | Burner apparatus for reducing combustion vibrations |
JP3986348B2 (ja) * | 2001-06-29 | 2007-10-03 | 三菱重工業株式会社 | ガスタービン燃焼器の燃料供給ノズルおよびガスタービン燃焼器並びにガスタービン |
JP2003028425A (ja) * | 2001-07-17 | 2003-01-29 | Mitsubishi Heavy Ind Ltd | 予混合燃焼器のパイロットバーナー、予混合燃焼器、およびガスタービン |
CA2399534C (en) * | 2001-08-31 | 2007-01-02 | Mitsubishi Heavy Industries, Ltd. | Gasturbine and the combustor thereof |
ITMI20012780A1 (it) * | 2001-12-21 | 2003-06-21 | Nuovo Pignone Spa | Dispositivo di iniezione principale di combustibile liquido per camera di combustione singola dotata di camera di pre-miscelamento di una tu |
PL372916A1 (en) | 2002-04-11 | 2005-08-08 | Richard A. Haase | Water combustion technology-methods, processes, systems and apparatus for the combustion of hydrogen and oxygen |
US6786047B2 (en) * | 2002-09-17 | 2004-09-07 | Siemens Westinghouse Power Corporation | Flashback resistant pre-mix burner for a gas turbine combustor |
US6832481B2 (en) | 2002-09-26 | 2004-12-21 | Siemens Westinghouse Power Corporation | Turbine engine fuel nozzle |
US20050003316A1 (en) * | 2003-05-31 | 2005-01-06 | Eugene Showers | Counterflow fuel injection nozzle in a burner-boiler system |
US7302802B2 (en) * | 2003-10-14 | 2007-12-04 | Pratt & Whitney Canada Corp. | Aerodynamic trip for a combustion system |
US7086235B2 (en) * | 2003-11-26 | 2006-08-08 | United Technologies Corporation | Cascade ignition of catalytic combustors |
US7425127B2 (en) * | 2004-06-10 | 2008-09-16 | Georgia Tech Research Corporation | Stagnation point reverse flow combustor |
EP1614963A1 (de) * | 2004-07-09 | 2006-01-11 | Siemens Aktiengesellschaft | Verfahren und Vormischverbrennungssystem |
JP4070758B2 (ja) * | 2004-09-10 | 2008-04-02 | 三菱重工業株式会社 | ガスタービン燃焼器 |
EP1703208B1 (de) * | 2005-02-04 | 2007-07-11 | Enel Produzione S.p.A. | Dämpfung von thermoakustischen Schwingungen in einer Gasturbinenbrennkammer mit ringförmiger Kammer |
US7624578B2 (en) * | 2005-09-30 | 2009-12-01 | General Electric Company | Method and apparatus for generating combustion products within a gas turbine engine |
US7540153B2 (en) * | 2006-02-27 | 2009-06-02 | Mitsubishi Heavy Industries Ltd. | Combustor |
US7540152B2 (en) * | 2006-02-27 | 2009-06-02 | Mitsubishi Heavy Industries, Ltd. | Combustor |
US7770395B2 (en) * | 2006-02-27 | 2010-08-10 | Mitsubishi Heavy Industries, Ltd. | Combustor |
US7523614B2 (en) * | 2006-02-27 | 2009-04-28 | Mitsubishi Heavy Industries, Ltd. | Combustor |
US7762074B2 (en) * | 2006-04-04 | 2010-07-27 | Siemens Energy, Inc. | Air flow conditioner for a combustor can of a gas turbine engine |
US7571611B2 (en) * | 2006-04-24 | 2009-08-11 | General Electric Company | Methods and system for reducing pressure losses in gas turbine engines |
US8197249B1 (en) | 2006-04-28 | 2012-06-12 | The United States Of America, As Represented By The Administrator Of The National Aeronautics And Space Administration | Fully premixed low emission, high pressure multi-fuel burner |
US20070277530A1 (en) * | 2006-05-31 | 2007-12-06 | Constantin Alexandru Dinu | Inlet flow conditioner for gas turbine engine fuel nozzle |
US7788926B2 (en) * | 2006-08-18 | 2010-09-07 | Siemens Energy, Inc. | Resonator device at junction of combustor and combustion chamber |
JP5054988B2 (ja) * | 2007-01-24 | 2012-10-24 | 三菱重工業株式会社 | 燃焼器 |
US20090145132A1 (en) * | 2007-12-07 | 2009-06-11 | General Electric Company | Methods and system for reducing pressure losses in gas turbine engines |
JP4997645B2 (ja) * | 2008-10-14 | 2012-08-08 | 独立行政法人 宇宙航空研究開発機構 | 流体素子による空気流量配分制御機構を備えた燃焼器 |
US20110000215A1 (en) * | 2009-07-01 | 2011-01-06 | General Electric Company | Combustor Can Flow Conditioner |
US8402763B2 (en) * | 2009-10-26 | 2013-03-26 | General Electric Company | Combustor headend guide vanes to reduce flow maldistribution into multi-nozzle arrangement |
US20110173983A1 (en) * | 2010-01-15 | 2011-07-21 | General Electric Company | Premix fuel nozzle internal flow path enhancement |
EP2397762A1 (de) * | 2010-06-17 | 2011-12-21 | Siemens Aktiengesellschaft | Dämpfvorrichtung zum Dämpfen von Druckschwingungen in einer Brennkammer einer Turbine |
US20120111013A1 (en) * | 2010-11-08 | 2012-05-10 | General Electric Company | System for directing air flow in a fuel nozzle assembly |
US9719419B2 (en) * | 2011-03-16 | 2017-08-01 | Mitsubishi Heavy Industries, Ltd. | Gas turbine combustor with top hat nozzle arrangements |
CN102323374A (zh) * | 2011-06-09 | 2012-01-18 | 中国科学技术大学 | 开放空间粉尘连续吹喷预混燃烧实验系统 |
US9182122B2 (en) | 2011-10-05 | 2015-11-10 | General Electric Company | Combustor and method for supplying flow to a combustor |
US20130086913A1 (en) * | 2011-10-07 | 2013-04-11 | General Electric Company | Turbomachine combustor assembly including a combustion dynamics mitigation system |
CN103134078B (zh) * | 2011-11-25 | 2015-03-25 | 中国科学院工程热物理研究所 | 一种阵列驻涡燃料-空气预混器 |
US9134030B2 (en) * | 2012-01-23 | 2015-09-15 | General Electric Company | Micromixer of turbine system |
US20130199190A1 (en) * | 2012-02-08 | 2013-08-08 | Jong Ho Uhm | Fuel injection assembly for use in turbine engines and method of assembling same |
WO2013128572A1 (ja) * | 2012-02-28 | 2013-09-06 | 三菱重工業株式会社 | 燃焼器及びガスタービン |
US20130219897A1 (en) * | 2012-02-28 | 2013-08-29 | Mitsubishi Heavy Industries, Ltd. | Combustor and gas turbine |
US9353949B2 (en) | 2012-04-17 | 2016-05-31 | Siemens Energy, Inc. | Device for improved air and fuel distribution to a combustor |
US9395084B2 (en) * | 2012-06-06 | 2016-07-19 | General Electric Company | Fuel pre-mixer with planar and swirler vanes |
US9335050B2 (en) * | 2012-09-26 | 2016-05-10 | United Technologies Corporation | Gas turbine engine combustor |
US20140123649A1 (en) * | 2012-11-07 | 2014-05-08 | Juan E. Portillo Bilbao | Acoustic damping system for a combustor of a gas turbine engine |
US9366438B2 (en) * | 2013-02-14 | 2016-06-14 | Siemens Aktiengesellschaft | Flow sleeve inlet assembly in a gas turbine engine |
JP6239247B2 (ja) * | 2013-03-15 | 2017-11-29 | 三菱重工業株式会社 | ガスタービン燃焼器 |
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 |
US9400108B2 (en) | 2013-05-14 | 2016-07-26 | Siemens Aktiengesellschaft | Acoustic damping system for a combustor of a gas turbine engine |
EP2933560B1 (de) * | 2014-04-17 | 2017-12-06 | Ansaldo Energia Switzerland AG | Verfahren zur Vormischung von Luft mit gasförmigem Brennstoff und Brenneranordnung zur Durchführung des Verfahrens |
US20160047316A1 (en) * | 2014-08-14 | 2016-02-18 | General Electric Company | Systems and apparatus relating to gas turbine combustors |
US10101032B2 (en) | 2015-04-01 | 2018-10-16 | General Electric Company | Micromixer system for a turbine system and an associated method thereof |
JP6484126B2 (ja) * | 2015-06-26 | 2019-03-13 | 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 |
US10393020B2 (en) * | 2015-08-26 | 2019-08-27 | Rohr, Inc. | Injector nozzle configuration for swirl anti-icing system |
US10295190B2 (en) | 2016-11-04 | 2019-05-21 | General Electric Company | Centerbody injector mini mixer fuel nozzle assembly |
US10465909B2 (en) | 2016-11-04 | 2019-11-05 | General Electric Company | Mini mixing fuel nozzle assembly with mixing sleeve |
US10724740B2 (en) | 2016-11-04 | 2020-07-28 | General Electric Company | Fuel nozzle assembly with impingement purge |
US10393382B2 (en) | 2016-11-04 | 2019-08-27 | General Electric Company | Multi-point injection mini mixing fuel nozzle assembly |
US10352569B2 (en) | 2016-11-04 | 2019-07-16 | General Electric Company | Multi-point centerbody injector mini mixing fuel nozzle assembly |
US10634353B2 (en) | 2017-01-12 | 2020-04-28 | General Electric Company | Fuel nozzle assembly with micro channel cooling |
CN107676815B (zh) * | 2017-09-05 | 2020-03-10 | 中国联合重型燃气轮机技术有限公司 | 燃烧器和具有该燃烧器的燃气轮机 |
CN107702144B (zh) * | 2017-09-05 | 2020-03-10 | 中国联合重型燃气轮机技术有限公司 | 燃烧器和具有该燃烧器的燃气轮机 |
JP6895867B2 (ja) * | 2017-10-27 | 2021-06-30 | 三菱パワー株式会社 | ガスタービン燃焼器、ガスタービン |
KR102046455B1 (ko) * | 2017-10-30 | 2019-11-19 | 두산중공업 주식회사 | 연료 노즐, 이를 포함하는 연소기 및 가스 터빈 |
US10890329B2 (en) | 2018-03-01 | 2021-01-12 | General Electric Company | Fuel injector assembly for gas turbine engine |
US10935245B2 (en) | 2018-11-20 | 2021-03-02 | General Electric Company | Annular concentric fuel nozzle assembly with annular depression and radial inlet ports |
US11073114B2 (en) | 2018-12-12 | 2021-07-27 | General Electric Company | Fuel injector assembly for a heat engine |
US11286884B2 (en) | 2018-12-12 | 2022-03-29 | General Electric Company | Combustion section and fuel injector assembly for a heat engine |
US11156360B2 (en) | 2019-02-18 | 2021-10-26 | General Electric Company | Fuel nozzle assembly |
KR102363091B1 (ko) * | 2020-07-06 | 2022-02-14 | 두산중공업 주식회사 | 연소기용 노즐, 이를 포함하는 연소기, 및 가스 터빈 |
US11686474B2 (en) | 2021-03-04 | 2023-06-27 | General Electric Company | Damper for swirl-cup combustors |
US11506388B1 (en) | 2021-05-07 | 2022-11-22 | General Electric Company | Furcating pilot pre-mixer for main mini-mixer array in a gas turbine engine |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
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BE482256A (de) * | 1947-05-23 | |||
US3169369A (en) * | 1963-06-19 | 1965-02-16 | Gen Electric | Combustion system |
US3169367A (en) * | 1963-07-18 | 1965-02-16 | Westinghouse Electric Corp | Combustion apparatus |
US3765824A (en) * | 1972-08-02 | 1973-10-16 | Foster Wheeler Corp | Apparatus for determining air flow to a gas burner |
CH586375A5 (de) * | 1975-06-25 | 1977-03-31 | Bbc Brown Boveri & Cie | |
US4199936A (en) * | 1975-12-24 | 1980-04-29 | The Boeing Company | Gas turbine engine combustion noise suppressor |
JPS59229114A (ja) * | 1983-06-08 | 1984-12-22 | Hitachi Ltd | ガスタ−ビン用燃焼器 |
US4504217A (en) * | 1983-10-14 | 1985-03-12 | Zurn Industries, Inc. | Low excess air burner having a movable venturi |
US5259184A (en) | 1992-03-30 | 1993-11-09 | General Electric Company | Dry low NOx single stage dual mode combustor construction for a gas turbine |
US5237813A (en) * | 1992-08-21 | 1993-08-24 | Allied-Signal Inc. | Annular combustor with outer transition liner cooling |
JP3174638B2 (ja) * | 1992-09-18 | 2001-06-11 | 株式会社日立製作所 | ガスタービン燃焼器の予混合構造 |
US5461865A (en) * | 1994-02-24 | 1995-10-31 | United Technologies Corporation | Tangential entry fuel nozzle |
US5644918A (en) * | 1994-11-14 | 1997-07-08 | General Electric Company | Dynamics free low emissions gas turbine combustor |
US5685157A (en) * | 1995-05-26 | 1997-11-11 | General Electric Company | Acoustic damper for a gas turbine engine combustor |
US5813232A (en) * | 1995-06-05 | 1998-09-29 | Allison Engine Company, Inc. | Dry low emission combustor for gas turbine engines |
JPH09170716A (ja) * | 1995-12-19 | 1997-06-30 | Hitachi Ltd | 燃料予混合装置及びガスタービン燃焼装置 |
US5778676A (en) * | 1996-01-02 | 1998-07-14 | General Electric Company | Dual fuel mixer for gas turbine combustor |
DE19737998A1 (de) * | 1997-08-30 | 1999-03-04 | Abb Research Ltd | Brennervorrichtung |
JP3592912B2 (ja) * | 1997-11-13 | 2004-11-24 | 三菱重工業株式会社 | ガスタービン燃焼器 |
DE59809097D1 (de) * | 1998-09-30 | 2003-08-28 | Alstom Switzerland Ltd | Brennkammer für eine Gasturbine |
US6530221B1 (en) * | 2000-09-21 | 2003-03-11 | Siemens Westinghouse Power Corporation | Modular resonators for suppressing combustion instabilities in gas turbine power plants |
-
2000
- 2000-07-21 JP JP2000220832A patent/JP2002039533A/ja active Pending
-
2001
- 2001-04-26 EP EP01401068A patent/EP1174662B1/de not_active Expired - Lifetime
- 2001-04-26 DE DE60135280T patent/DE60135280D1/de not_active Expired - Lifetime
- 2001-07-16 CA CA002353514A patent/CA2353514C/en not_active Expired - Lifetime
- 2001-07-20 US US09/908,637 patent/US6594999B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CA2353514A1 (en) | 2002-01-21 |
US6594999B2 (en) | 2003-07-22 |
CA2353514C (en) | 2006-10-31 |
EP1174662B1 (de) | 2008-08-13 |
US20020011070A1 (en) | 2002-01-31 |
EP1174662A1 (de) | 2002-01-23 |
JP2002039533A (ja) | 2002-02-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |