EP1319895A3 - Brûleur à prémélange à combustion pauvre pour turbine à gaz et son procédé de fonctionnement - Google Patents
Brûleur à prémélange à combustion pauvre pour turbine à gaz et son procédé de fonctionnement Download PDFInfo
- Publication number
- EP1319895A3 EP1319895A3 EP02023428A EP02023428A EP1319895A3 EP 1319895 A3 EP1319895 A3 EP 1319895A3 EP 02023428 A EP02023428 A EP 02023428A EP 02023428 A EP02023428 A EP 02023428A EP 1319895 A3 EP1319895 A3 EP 1319895A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- premix burner
- gas turbine
- lean
- burn
- fuel
- 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.)
- Granted
Links
- 239000000446 fuel Substances 0.000 abstract 4
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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
- F23R3/346—Feeding into different combustion zones for staged combustion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2201/00—Staged combustion
- F23C2201/20—Burner staging
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10160997A DE10160997A1 (de) | 2001-12-12 | 2001-12-12 | Magervormischbrenner für eine Gasturbine sowie Verfahren zum Betrieb eines Magervormischbrenners |
| DE10160997 | 2001-12-12 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP1319895A2 EP1319895A2 (fr) | 2003-06-18 |
| EP1319895A3 true EP1319895A3 (fr) | 2004-01-07 |
| EP1319895B1 EP1319895B1 (fr) | 2007-11-07 |
Family
ID=7708919
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP02023428A Expired - Lifetime EP1319895B1 (fr) | 2001-12-12 | 2002-10-19 | Brûleur à prémélange à combustion pauvre pour turbine à gaz et son procédé de fonctionnement |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US6945053B2 (fr) |
| EP (1) | EP1319895B1 (fr) |
| DE (2) | DE10160997A1 (fr) |
Families Citing this family (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0302721D0 (en) * | 2003-02-05 | 2003-03-12 | Rolls Royce Plc | Fuel nozzles |
| US20090217669A1 (en) * | 2003-02-05 | 2009-09-03 | Young Kenneth J | Fuel nozzles |
| US7506511B2 (en) * | 2003-12-23 | 2009-03-24 | Honeywell International Inc. | Reduced exhaust emissions gas turbine engine combustor |
| US7303388B2 (en) * | 2004-07-01 | 2007-12-04 | Air Products And Chemicals, Inc. | Staged combustion system with ignition-assisted fuel lances |
| US7137256B1 (en) * | 2005-02-28 | 2006-11-21 | Peter Stuttaford | Method of operating a combustion system for increased turndown capability |
| JP4476176B2 (ja) * | 2005-06-06 | 2010-06-09 | 三菱重工業株式会社 | ガスタービンの予混合燃焼バーナー |
| JP4486549B2 (ja) * | 2005-06-06 | 2010-06-23 | 三菱重工業株式会社 | ガスタービンの燃焼器 |
| US7836677B2 (en) * | 2006-04-07 | 2010-11-23 | Siemens Energy, Inc. | At least one combustion apparatus and duct structure for a gas turbine engine |
| US7631499B2 (en) * | 2006-08-03 | 2009-12-15 | Siemens Energy, Inc. | Axially staged combustion system for a gas turbine engine |
| FR2906868B1 (fr) * | 2006-10-06 | 2011-11-18 | Snecma | Injecteur de carburant pour chambre de combustion de moteur a turbine a gaz |
| JP5147938B2 (ja) * | 2007-07-02 | 2013-02-20 | シーメンス アクチエンゲゼルシヤフト | バーナおよびバーナの運転方法 |
| FR2922995B1 (fr) * | 2007-10-31 | 2009-12-04 | Snecma | Chambre de combustion annulaire de moteur a turbine a gaz. |
| EP2107301B1 (fr) | 2008-04-01 | 2016-01-06 | Siemens Aktiengesellschaft | Injection de gaz dans un brûleur |
| US20100192578A1 (en) * | 2009-01-30 | 2010-08-05 | General Electric Company | System and method for suppressing combustion instability in a turbomachine |
| US20100192582A1 (en) | 2009-02-04 | 2010-08-05 | Robert Bland | Combustor nozzle |
| CH700796A1 (de) * | 2009-04-01 | 2010-10-15 | Alstom Technology Ltd | Verfahren zum CO-emissionsarmen Betrieb einer Gasturbine mit sequentieller Verbrennung und Gasturbine mit verbessertem Teillast- Emissionsverhalten. |
| US9068751B2 (en) * | 2010-01-29 | 2015-06-30 | United Technologies Corporation | Gas turbine combustor with staged combustion |
| US9746185B2 (en) * | 2010-02-25 | 2017-08-29 | Siemens Energy, Inc. | Circumferential biasing and profiling of fuel injection in distribution ring |
| US9631560B2 (en) * | 2011-11-22 | 2017-04-25 | United Technologies Corporation | Fuel-air mixture distribution for gas turbine engine combustors |
| US10240533B2 (en) | 2011-11-22 | 2019-03-26 | United Technologies Corporation | Fuel distribution within a gas turbine engine combustor |
| US9310072B2 (en) | 2012-07-06 | 2016-04-12 | Hamilton Sundstrand Corporation | Non-symmetric arrangement of fuel nozzles in a combustor |
| US20140083111A1 (en) * | 2012-09-25 | 2014-03-27 | United Technologies Corporation | Gas turbine asymmetric fuel nozzle combustor |
| EP3067536A1 (fr) * | 2015-03-09 | 2016-09-14 | General Electric Technology GmbH | Procédé d'exploitation d'une turbine à gaz |
| JP6634658B2 (ja) * | 2016-12-20 | 2020-01-22 | 三菱重工業株式会社 | メインノズル、燃焼器及びメインノズルの製造方法 |
| DE102017201771A1 (de) * | 2017-02-03 | 2018-08-09 | Siemens Aktiengesellschaft | Umfangsstufungskonzept für eine Brenneranordnung |
| US11181274B2 (en) * | 2017-08-21 | 2021-11-23 | General Electric Company | Combustion system and method for attenuation of combustion dynamics in a gas turbine engine |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4222243A (en) * | 1977-06-10 | 1980-09-16 | Rolls-Royce Limited | Fuel burners for gas turbine engines |
| US5351477A (en) * | 1993-12-21 | 1994-10-04 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| US6109038A (en) * | 1998-01-21 | 2000-08-29 | Siemens Westinghouse Power Corporation | Combustor with two stage primary fuel assembly |
| EP1058063A1 (fr) * | 1999-05-31 | 2000-12-06 | Nuovo Pignone Holding S.P.A. | Injecteur de carburant liquide pour brûleurs de turbines à gaz |
| US6161387A (en) * | 1998-10-30 | 2000-12-19 | United Technologies Corporation | Multishear fuel injector |
| WO2002061339A1 (fr) * | 2001-02-02 | 2002-08-08 | Alstom (Switzerland) Ltd | Brûleur de prémélange et son mode de fonctionnement |
Family Cites Families (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2616258A (en) * | 1946-01-09 | 1952-11-04 | Bendix Aviat Corp | Jet engine combustion apparatus, including pilot burner for ignition and vaporization of main fuel supply |
| US4027473A (en) * | 1976-03-05 | 1977-06-07 | United Technologies Corporation | Fuel distribution valve |
| US4903478A (en) * | 1987-06-25 | 1990-02-27 | General Electric Company | Dual manifold fuel system |
| US4817389A (en) * | 1987-09-24 | 1989-04-04 | United Technologies Corporation | Fuel injection system |
| US5321949A (en) | 1991-07-12 | 1994-06-21 | General Electric Company | Staged fuel delivery system with secondary distribution valve |
| US5226287A (en) * | 1991-07-19 | 1993-07-13 | General Electric Company | Compressor stall recovery apparatus |
| CA2072275A1 (fr) | 1991-08-12 | 1993-02-13 | Phillip D. Napoli | Systeme d'alimentation en carburant pour double chambre annulaire de combustion |
| US5211005A (en) * | 1992-04-16 | 1993-05-18 | Avco Corporation | High density fuel injection manifold |
| US5303542A (en) * | 1992-11-16 | 1994-04-19 | General Electric Company | Fuel supply control method for a gas turbine engine |
| US5402634A (en) * | 1993-10-22 | 1995-04-04 | United Technologies Corporation | Fuel supply system for a staged combustor |
| DE4446945B4 (de) | 1994-12-28 | 2005-03-17 | Alstom | Gasbetriebener Vormischbrenner |
| US5778676A (en) | 1996-01-02 | 1998-07-14 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| GB9607010D0 (en) * | 1996-04-03 | 1996-06-05 | Rolls Royce Plc | Gas turbine engine combustion equipment |
| GB2312250A (en) * | 1996-04-18 | 1997-10-22 | Rolls Royce Plc | Staged gas turbine fuel system with a single supply manifold, to which the main burners are connected through valves. |
| US5899075A (en) | 1997-03-17 | 1999-05-04 | General Electric Company | Turbine engine combustor with fuel-air mixer |
| DE19815914B4 (de) * | 1998-04-09 | 2005-05-04 | Alstom | Verteiler |
| DE59810344D1 (de) * | 1998-07-27 | 2004-01-15 | Alstom Switzerland Ltd | Verfahren zum Betrieb einer Gasturbinenbrennkammer mit gasförmigem Brennstoff |
| US6813889B2 (en) | 2001-08-29 | 2004-11-09 | Hitachi, Ltd. | Gas turbine combustor and operating method thereof |
-
2001
- 2001-12-12 DE DE10160997A patent/DE10160997A1/de not_active Withdrawn
-
2002
- 2002-10-19 DE DE50211162T patent/DE50211162D1/de not_active Expired - Lifetime
- 2002-10-19 EP EP02023428A patent/EP1319895B1/fr not_active Expired - Lifetime
- 2002-12-12 US US10/316,936 patent/US6945053B2/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4222243A (en) * | 1977-06-10 | 1980-09-16 | Rolls-Royce Limited | Fuel burners for gas turbine engines |
| US5351477A (en) * | 1993-12-21 | 1994-10-04 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| US6109038A (en) * | 1998-01-21 | 2000-08-29 | Siemens Westinghouse Power Corporation | Combustor with two stage primary fuel assembly |
| US6161387A (en) * | 1998-10-30 | 2000-12-19 | United Technologies Corporation | Multishear fuel injector |
| EP1058063A1 (fr) * | 1999-05-31 | 2000-12-06 | Nuovo Pignone Holding S.P.A. | Injecteur de carburant liquide pour brûleurs de turbines à gaz |
| WO2002061339A1 (fr) * | 2001-02-02 | 2002-08-08 | Alstom (Switzerland) Ltd | Brûleur de prémélange et son mode de fonctionnement |
Also Published As
| Publication number | Publication date |
|---|---|
| DE50211162D1 (de) | 2007-12-20 |
| DE10160997A1 (de) | 2003-07-03 |
| US20030106321A1 (en) | 2003-06-12 |
| EP1319895B1 (fr) | 2007-11-07 |
| US6945053B2 (en) | 2005-09-20 |
| EP1319895A2 (fr) | 2003-06-18 |
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