EP0851172A3 - Burner for operating a combustion chamber with a liquid and/or gaseous fuel - Google Patents
Burner for operating a combustion chamber with a liquid and/or gaseous fuel Download PDFInfo
- Publication number
- EP0851172A3 EP0851172A3 EP97810838A EP97810838A EP0851172A3 EP 0851172 A3 EP0851172 A3 EP 0851172A3 EP 97810838 A EP97810838 A EP 97810838A EP 97810838 A EP97810838 A EP 97810838A EP 0851172 A3 EP0851172 A3 EP 0851172A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- burner
- operating
- liquid
- interior
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
- F23D17/002—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
-
- 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
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
-
- 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
- F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
- F23C2900/07002—Premix burners with air inlet slots obtained between offset curved wall surfaces, e.g. double cone burners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2209/00—Safety arrangements
- F23D2209/10—Flame flashback
Abstract
Bei einem Brenner zum Betrieb einer Brennkammmer mit einem flüssigen und/oder gasförmigen Brennstoff (12, 16) wird die dazu benötigte Verbrennungsluft (7) durch tangentiale Lufteintrittskanäle (5, 6) in einen Innenraum des Brenners geführt. Durch diese Strömungsführung entsteht im Innenraum eine Drallströmung, welche am Ausgang des Brenners eine Rückströmzone induziert. Um die sich dort bildende Flammenfront zu stabilisieren, wird bei jedem den Brenner bildenden Teilkörper (1, 2) mindestens eine Zone (27) vorgesehen, innerhalb welcher Eintrittsöffnungen (29) für die Eindüsung einer Zusatzluft (32) in die Drallströmung (7a) vorgesehen sind. Durch diese Eindüsung bildet sich an der Innenwand der Teilkörper (1, 2) einen Film, welcher verhindert, dass die Flamme entlang der Innenwand der Teilkörper (1, 2) in den Innenraum des Brenners zurückschlagen kann. In the case of a burner for operating a combustion chamber with a liquid and / or gaseous fuel (12, 16), the combustion air (7) required for this purpose is conducted through tangential air inlet ducts (5, 6) into an interior of the burner. This flow control creates a swirl flow in the interior, which induces a backflow zone at the burner outlet. In order to stabilize the flame front formed there, at least one zone (27) is provided in each partial body (1, 2) forming the burner, within which inlet openings (29) are provided for the injection of additional air (32) into the swirl flow (7a) are. As a result of this injection, a film forms on the inner wall of the partial bodies (1, 2), which prevents the flame from striking back into the interior of the burner along the inner wall of the partial bodies (1, 2).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19654116 | 1996-12-23 | ||
DE19654116A DE19654116A1 (en) | 1996-12-23 | 1996-12-23 | Burner for operating a combustion chamber with a liquid and / or gaseous fuel |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0851172A2 EP0851172A2 (en) | 1998-07-01 |
EP0851172A3 true EP0851172A3 (en) | 1999-06-09 |
EP0851172B1 EP0851172B1 (en) | 2003-07-16 |
Family
ID=7816084
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97810838A Expired - Lifetime EP0851172B1 (en) | 1996-12-23 | 1997-11-07 | Burner and method for operating a combustion chamber with a liquid and/or gaseous fuel |
Country Status (3)
Country | Link |
---|---|
US (1) | US5921770A (en) |
EP (1) | EP0851172B1 (en) |
DE (2) | DE19654116A1 (en) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6141954A (en) * | 1998-05-18 | 2000-11-07 | United Technologies Corporation | Premixing fuel injector with improved flame disgorgement capacity |
DE59812944D1 (en) * | 1998-09-16 | 2005-08-25 | Alstom Technology Ltd Baden | Method for preventing flow instabilities in a burner |
EP1001214B1 (en) * | 1998-11-09 | 2004-09-15 | ALSTOM Technology Ltd | Burner |
EP1002992B1 (en) * | 1998-11-18 | 2004-09-29 | ALSTOM Technology Ltd | Burner |
DE10051221A1 (en) * | 2000-10-16 | 2002-07-11 | Alstom Switzerland Ltd | Burner with staged fuel injection |
CN101069039B (en) * | 2004-11-30 | 2011-10-19 | 阿尔斯托姆科技有限公司 | Method and device for burning hydrogen in a premix burner |
WO2009109454A1 (en) | 2008-03-07 | 2009-09-11 | Alstom Technology Ltd | Method and burner arrangement for the production of hot gas, and use of said method |
JP5453322B2 (en) | 2008-03-07 | 2014-03-26 | アルストム テクノロジー リミテッド | Burner device and use of burner device |
CH703655A1 (en) | 2010-08-27 | 2012-02-29 | Alstom Technology Ltd | Premix FOR A GAS TURBINE. |
EP2685163B1 (en) | 2012-07-10 | 2020-03-25 | Ansaldo Energia Switzerland AG | Premix burner of the multi-cone type for a gas turbine |
EP2685161B1 (en) * | 2012-07-10 | 2018-01-17 | Ansaldo Energia Switzerland AG | Combustor arrangement, especially for a gas turbine |
EP2685162A1 (en) | 2012-07-10 | 2014-01-15 | Alstom Technology Ltd | Premix burner of the multi-cone type for a gas turbine and method for operating such a burner |
EP2685160B1 (en) * | 2012-07-10 | 2018-02-21 | Ansaldo Energia Switzerland AG | Premix burner of the multi-cone type for a gas turbine |
GB2512894A (en) * | 2013-04-10 | 2014-10-15 | David Thomas Bell | Inward firing multiple zoned gas burner |
EP3299720B1 (en) | 2016-09-22 | 2020-11-04 | Ansaldo Energia IP UK Limited | Combustor front assembly for a gas turbine |
KR101990767B1 (en) | 2017-08-09 | 2019-06-20 | 한국기계연구원 | Double-cone gas turbine burner and method for providing air to the burner |
DE102018005192B3 (en) | 2018-07-02 | 2019-12-05 | Truma Gerätetechnik GmbH & Co. KG | burner device |
US11852319B2 (en) * | 2021-02-26 | 2023-12-26 | Armando Parra | Control means for vortex flame device |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3958416A (en) * | 1974-12-12 | 1976-05-25 | General Motors Corporation | Combustion apparatus |
DE4409918A1 (en) * | 1994-03-23 | 1995-09-28 | Abb Management Ag | Low calorific value fuel burner for combustion chamber |
EP0704657A2 (en) * | 1994-10-01 | 1996-04-03 | ABB Management AG | Burner |
DE19545310A1 (en) * | 1995-12-05 | 1997-06-12 | Asea Brown Boveri | Pre-mixing burner for mixing fuel and combustion air before ignition |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR758974A (en) * | 1933-07-28 | 1934-01-26 | Indugas Ind U Gasofen Bauges M | Adjustable flame length gas burner |
US2665748A (en) * | 1949-05-27 | 1954-01-12 | Frank H Cornelius | Fuel burner |
US3951584A (en) * | 1974-05-23 | 1976-04-20 | Midland-Ross Corporation | Self-stabilizing burner |
US3975141A (en) * | 1974-06-25 | 1976-08-17 | The United States Of America As Represented By The Secretary Of The Army | Combustion liner swirler |
CH674561A5 (en) | 1987-12-21 | 1990-06-15 | Bbc Brown Boveri & Cie | |
CH680157A5 (en) * | 1989-12-01 | 1992-06-30 | Asea Brown Boveri | |
DE4330083A1 (en) * | 1993-09-06 | 1995-03-09 | Abb Research Ltd | Method of operating a premix burner |
DE19545036A1 (en) * | 1995-12-02 | 1997-06-05 | Abb Research Ltd | Premix burner |
-
1996
- 1996-12-23 DE DE19654116A patent/DE19654116A1/en not_active Withdrawn
-
1997
- 1997-11-07 DE DE59710441T patent/DE59710441D1/en not_active Expired - Lifetime
- 1997-11-07 EP EP97810838A patent/EP0851172B1/en not_active Expired - Lifetime
- 1997-11-20 US US08/975,301 patent/US5921770A/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3958416A (en) * | 1974-12-12 | 1976-05-25 | General Motors Corporation | Combustion apparatus |
DE4409918A1 (en) * | 1994-03-23 | 1995-09-28 | Abb Management Ag | Low calorific value fuel burner for combustion chamber |
EP0704657A2 (en) * | 1994-10-01 | 1996-04-03 | ABB Management AG | Burner |
DE19545310A1 (en) * | 1995-12-05 | 1997-06-12 | Asea Brown Boveri | Pre-mixing burner for mixing fuel and combustion air before ignition |
Also Published As
Publication number | Publication date |
---|---|
US5921770A (en) | 1999-07-13 |
EP0851172A2 (en) | 1998-07-01 |
DE59710441D1 (en) | 2003-08-21 |
DE19654116A1 (en) | 1998-06-25 |
EP0851172B1 (en) | 2003-07-16 |
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