DE60021296D1 - Abstimmung einer Brennkammer - Google Patents
Abstimmung einer BrennkammerInfo
- Publication number
- DE60021296D1 DE60021296D1 DE60021296T DE60021296T DE60021296D1 DE 60021296 D1 DE60021296 D1 DE 60021296D1 DE 60021296 T DE60021296 T DE 60021296T DE 60021296 T DE60021296 T DE 60021296T DE 60021296 D1 DE60021296 D1 DE 60021296D1
- Authority
- DE
- Germany
- Prior art keywords
- tuning
- combustion chamber
- combustion
- chamber
- 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
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
- F23R3/28—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
- F23R3/02—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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00013—Reducing thermo-acoustic vibrations by active means
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US250912 | 1981-04-03 | ||
US09/250,912 US6272842B1 (en) | 1999-02-16 | 1999-02-16 | Combustor tuning |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60021296D1 true DE60021296D1 (de) | 2005-08-25 |
DE60021296T2 DE60021296T2 (de) | 2006-04-20 |
Family
ID=22949675
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60021296T Expired - Fee Related DE60021296T2 (de) | 1999-02-16 | 2000-02-16 | Abstimmung einer Brennkammer |
Country Status (4)
Country | Link |
---|---|
US (1) | US6272842B1 (de) |
EP (1) | EP1030112B1 (de) |
JP (1) | JP2000240944A (de) |
DE (1) | DE60021296T2 (de) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6735949B1 (en) | 2002-06-11 | 2004-05-18 | General Electric Company | Gas turbine engine combustor can with trapped vortex cavity |
US6820431B2 (en) * | 2002-10-31 | 2004-11-23 | General Electric Company | Acoustic impedance-matched fuel nozzle device and tunable fuel injection resonator assembly |
US7302802B2 (en) * | 2003-10-14 | 2007-12-04 | Pratt & Whitney Canada Corp. | Aerodynamic trip for a combustion system |
US20070089427A1 (en) * | 2005-10-24 | 2007-04-26 | Thomas Scarinci | Two-branch mixing passage and method to control combustor pulsations |
US7665305B2 (en) * | 2005-12-29 | 2010-02-23 | Delavan Inc | Valve assembly for modulating fuel flow to a gas turbine engine |
WO2007113130A1 (de) * | 2006-03-30 | 2007-10-11 | Alstom Technology Ltd | Brenneranordnung, vorzugsweise in einer brennkammer für eine gasturbine |
US8028512B2 (en) | 2007-11-28 | 2011-10-04 | Solar Turbines Inc. | Active combustion control for a turbine engine |
US20100175380A1 (en) * | 2009-01-13 | 2010-07-15 | General Electric Company | Traversing fuel nozzles in cap-less combustor assembly |
US8308076B2 (en) | 2009-02-20 | 2012-11-13 | Pratt & Whitney Canada Corp. | Nozzle design to reduce fretting |
US8042752B2 (en) * | 2009-02-20 | 2011-10-25 | Pratt & Whitney Canada Corp. | Nozzle repair to reduce fretting |
US8720206B2 (en) * | 2009-05-14 | 2014-05-13 | General Electric Company | Methods and systems for inducing combustion dynamics |
US9200571B2 (en) * | 2009-07-07 | 2015-12-01 | General Electric Company | Fuel nozzle assembly for a gas turbine engine |
RU2508506C2 (ru) * | 2009-09-01 | 2014-02-27 | Дженерал Электрик Компани | Способ и установка для ввода текучей среды в камеру сгорания газотурбинного двигателя |
US8272224B2 (en) * | 2009-11-02 | 2012-09-25 | General Electric Company | Apparatus and methods for fuel nozzle frequency adjustment |
US9003761B2 (en) | 2010-05-28 | 2015-04-14 | General Electric Company | System and method for exhaust gas use in gas turbine engines |
FR2961292B1 (fr) * | 2010-06-14 | 2014-01-31 | Snecma | Procede pour reduire les instabilites de combustion dans une chambre de combustion ; chambre de combustion de moteur a turbine a gaz selon ce procede |
US8365534B2 (en) | 2011-03-15 | 2013-02-05 | General Electric Company | Gas turbine combustor having a fuel nozzle for flame anchoring |
RU2011115528A (ru) | 2011-04-21 | 2012-10-27 | Дженерал Электрик Компани (US) | Топливная форсунка, камера сгорания и способ работы камеры сгорания |
FR2976649B1 (fr) * | 2011-06-20 | 2015-01-23 | Turbomeca | Procede d'injection de carburant dans une chambre de combustion d'une turbine a gaz et systeme d'injection pour sa mise en oeuvre |
US9745896B2 (en) * | 2013-02-26 | 2017-08-29 | General Electric Company | Systems and methods to control combustion dynamic frequencies based on a compressor discharge temperature |
EP3062019B1 (de) * | 2015-02-27 | 2018-11-21 | Ansaldo Energia Switzerland AG | Verfahren und vorrichtung zur flammenstabilisation in einem brennersystem einer stationären brennkraftmaschine |
WO2022079523A1 (en) * | 2020-10-14 | 2022-04-21 | King Abdullah University Of Science And Technology | Adjustable fuel injector for flame dynamics control |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3905192A (en) * | 1974-08-29 | 1975-09-16 | United Aircraft Corp | Combustor having staged premixing tubes |
US4532762A (en) * | 1982-07-22 | 1985-08-06 | The Garrett Corporation | Gas turbine engine variable geometry combustor apparatus |
US5082421A (en) | 1986-04-28 | 1992-01-21 | Rolls-Royce Plc | Active control of unsteady motion phenomena in turbomachinery |
US4967550A (en) | 1987-04-28 | 1990-11-06 | Rolls-Royce Plc | Active control of unsteady motion phenomena in turbomachinery |
US5211004A (en) | 1992-05-27 | 1993-05-18 | General Electric Company | Apparatus for reducing fuel/air concentration oscillations in gas turbine combustors |
DE4228817C2 (de) * | 1992-08-29 | 1998-07-30 | Mtu Muenchen Gmbh | Brennkammer für Gasturbinentriebwerke |
DE4228816C2 (de) | 1992-08-29 | 1998-08-06 | Mtu Muenchen Gmbh | Brenner für Gasturbinentriebwerke |
US5428951A (en) * | 1993-08-16 | 1995-07-04 | Wilson; Kenneth | Method and apparatus for active control of combustion devices |
US5943866A (en) * | 1994-10-03 | 1999-08-31 | General Electric Company | Dynamically uncoupled low NOx combustor having multiple premixers with axial staging |
GB2299399A (en) * | 1995-03-25 | 1996-10-02 | Rolls Royce Plc | Variable geometry air-fuel injector |
US5685157A (en) | 1995-05-26 | 1997-11-11 | General Electric Company | Acoustic damper for a gas turbine engine combustor |
US5822992A (en) * | 1995-10-19 | 1998-10-20 | General Electric Company | Low emissions combustor premixer |
JP3706443B2 (ja) * | 1996-09-24 | 2005-10-12 | 三菱重工業株式会社 | アニュラ型ガスタービン燃焼器 |
US5809769A (en) * | 1996-11-06 | 1998-09-22 | The United States Of America As Represented By The United States Department Of Energy | Combustor oscillation attenuation via the control of fuel-supply line dynamics |
-
1999
- 1999-02-16 US US09/250,912 patent/US6272842B1/en not_active Expired - Fee Related
-
2000
- 2000-02-15 JP JP2000036604A patent/JP2000240944A/ja active Pending
- 2000-02-16 DE DE60021296T patent/DE60021296T2/de not_active Expired - Fee Related
- 2000-02-16 EP EP00301198A patent/EP1030112B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE60021296T2 (de) | 2006-04-20 |
EP1030112B1 (de) | 2005-07-20 |
US6272842B1 (en) | 2001-08-14 |
JP2000240944A (ja) | 2000-09-08 |
EP1030112A1 (de) | 2000-08-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |