EP1918641A3 - Burner device and method for injecting a fuel-oxidant mixture into a combustion chamber - Google Patents
Burner device and method for injecting a fuel-oxidant mixture into a combustion chamber Download PDFInfo
- Publication number
- EP1918641A3 EP1918641A3 EP07119000A EP07119000A EP1918641A3 EP 1918641 A3 EP1918641 A3 EP 1918641A3 EP 07119000 A EP07119000 A EP 07119000A EP 07119000 A EP07119000 A EP 07119000A EP 1918641 A3 EP1918641 A3 EP 1918641A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- fuel
- combustion chamber
- injecting
- nozzles
- oxidant mixture
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/62—Mixing devices; Mixing tubes
- F23D14/64—Mixing devices; Mixing tubes with injectors
-
- 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
- F23C5/00—Disposition of burners with respect to the combustion chamber or to one another; Mounting of burners in combustion apparatus
-
- 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
- F23C5/00—Disposition of burners with respect to the combustion chamber or to one another; Mounting of burners in combustion apparatus
- F23C5/02—Structural details of mounting
- F23C5/06—Provision for adjustment of burner position during operation
-
- 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
- F23C9/00—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
- F23C9/006—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber the recirculation taking place in the combustion chamber
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/48—Nozzles
- F23D14/58—Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration
- F23D14/583—Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration of elongated shape, e.g. slits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N1/00—Regulating fuel supply
- F23N1/02—Regulating fuel supply conjointly with air supply
- F23N1/022—Regulating fuel supply conjointly with air supply using electronic means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N2237/00—Controlling
- F23N2237/02—Controlling two or more burners
-
- 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
- F23R2900/03282—High speed injection of air and/or fuel inducing internal recirculation
Abstract
Es wird eine Brennervorrichtung bereitgestellt, umfassend eine Brennkammer mit einem Brennraum und eine Einblaseinrichtung zum Einblasen eines Brennstoff-Oxidator-Gemischs in den Brennraum, wobei die Einblaseinrichtung eine Mehrzahl von an einer Kreislinie angeordneten Düsen aufweist, die Düsen jeweils einen Düsenraum aufweisen, Brennstoffdüsen oder Brennstoffröhren zum Einkoppeln von Brennstoff in die Düsenräume münden, über eine Zuführungseinrichtung Oxidator in die Düsenräume zur Gemischerzeugung einkoppelbar ist, und wobei Düsenöffnungen der Düsen in dem Brennraum als Langlöcher ausgebildet sind. There is provided a burner apparatus comprising a combustor having a combustion chamber and a sparger for injecting a fuel-oxidant mixture into the combustion chamber, the sparger having a plurality of nozzles arranged in a circle, the nozzles each having a nozzle space, fuel nozzles or fuel tubes for injecting fuel into the nozzle chambers open, can be coupled via a feed oxidizer in the nozzle chambers for generating mixtures, and wherein nozzle openings of the nozzles are formed in the combustion chamber as slots.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006051286A DE102006051286A1 (en) | 2006-10-26 | 2006-10-26 | Combustion device, has combustion chamber with combustion space and air injecting device including multiple nozzles arranged on circular line, where nozzles have openings formed as slotted holes in combustion space |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1918641A2 EP1918641A2 (en) | 2008-05-07 |
EP1918641A3 true EP1918641A3 (en) | 2013-01-30 |
Family
ID=38961117
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07119000A Withdrawn EP1918641A3 (en) | 2006-10-26 | 2007-10-22 | Burner device and method for injecting a fuel-oxidant mixture into a combustion chamber |
Country Status (3)
Country | Link |
---|---|
US (1) | US20080131824A1 (en) |
EP (1) | EP1918641A3 (en) |
DE (1) | DE102006051286A1 (en) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090214991A1 (en) * | 2008-02-18 | 2009-08-27 | Applied Materials, Inc. | Apparatus and methods for supplying fuel employed by abatement systems to effectively abate effluents |
US11460188B2 (en) | 2013-02-14 | 2022-10-04 | Clearsign Technologies Corporation | Ultra low emissions firetube boiler burner |
US10386062B2 (en) | 2013-02-14 | 2019-08-20 | Clearsign Combustion Corporation | Method for operating a combustion system including a perforated flame holder |
US10119704B2 (en) | 2013-02-14 | 2018-11-06 | Clearsign Combustion Corporation | Burner system including a non-planar perforated flame holder |
EP2789915A1 (en) * | 2013-04-10 | 2014-10-15 | Alstom Technology Ltd | Method for operating a combustion chamber and combustion chamber |
ITTO20130070U1 (en) * | 2013-04-29 | 2014-10-30 | Indesit Co Spa | GAS BURNER SYSTEM, IN PARTICULAR FOR A COOKING APPLIANCE FOR FOOD |
CN105579776B (en) | 2013-10-07 | 2018-07-06 | 克利尔赛恩燃烧公司 | With the premix fuel burner for having hole flame holder |
CN105960565B (en) | 2014-01-24 | 2019-11-12 | 克利尔赛恩燃烧公司 | Low NOxMultitubular boiler |
CN106016362B (en) * | 2016-05-16 | 2018-10-09 | 中国科学院工程热物理研究所 | A kind of soft combustion chamber of gas turbine and its control method |
WO2018208695A1 (en) * | 2017-05-08 | 2018-11-15 | Clearsign Combustion Corporation | Combustion system including a mixing tube and a perforated flame holder |
DE102022103746A1 (en) | 2022-02-17 | 2023-08-17 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Burner system for generating hot gas |
DE102022105076A1 (en) | 2022-03-03 | 2023-09-07 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Feeding device, burner system and method |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040000146A1 (en) * | 2001-08-29 | 2004-01-01 | Hiroshi Inoue | Gas turbine combustor and operating method thereof |
US20040020210A1 (en) * | 2001-06-29 | 2004-02-05 | Katsunori Tanaka | Fuel injection nozzle for gas turbine combustor, gas turbine combustor, and gas turbine |
WO2004053395A1 (en) * | 2002-12-11 | 2004-06-24 | Alstom Technology Ltd | Method and device for combustion of a fuel |
WO2006027989A1 (en) * | 2004-09-10 | 2006-03-16 | Mitsubishi Heavy Industries, Ltd. | Gas turbine combustor |
Family Cites Families (50)
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US2143487A (en) * | 1939-01-10 | Gas burner | ||
US1425343A (en) * | 1921-04-14 | 1922-08-08 | Alfred G Schumann | Oil or gas burner |
US1874970A (en) * | 1931-04-03 | 1932-08-30 | Columbia Burner Company | Gas burner spud |
US2672191A (en) * | 1951-01-27 | 1954-03-16 | Sinclair Refining Co | Apparatus |
DE1074920B (en) * | 1955-07-07 | 1960-02-04 | Ing habil Fritz A F Schmidt Murnau Dr (Obb) | Method and device for regulating gas turbine combustion chambers with subdivided combustion and several pressure levels |
US3043577A (en) * | 1960-10-20 | 1962-07-10 | Walter V Berry | Lance with conduits for mixing gases located interiorly |
DE1800612A1 (en) * | 1968-10-02 | 1970-05-27 | Hertel Dr Ing Heinrich | Combustion chamber, especially for jet engines |
US3521824A (en) * | 1968-10-11 | 1970-07-28 | Delavan Manufacturing Co | Air-liquid flat spray nozzle |
US3570471A (en) * | 1969-02-14 | 1971-03-16 | Thermo Electron Corp | Radiant tube having uniform high-temperature distribution |
US3887134A (en) * | 1969-04-01 | 1975-06-03 | Mohr & Sons John | Gas burner |
US3635644A (en) * | 1970-01-19 | 1972-01-18 | Columbia Gas Syst | Infrared burner and method of increasing the heat flux radiated therefrom |
US4044549A (en) * | 1972-12-11 | 1977-08-30 | Zwick Eugene B | Low emission combustion process and apparatus |
US3834627A (en) * | 1973-04-02 | 1974-09-10 | Avco Corp | Flat air-blast fuel injector |
CH577627A5 (en) * | 1974-04-03 | 1976-07-15 | Bbc Sulzer Turbomaschinen | |
DE2528671C2 (en) * | 1975-06-27 | 1985-12-19 | Klöckner-Humboldt-Deutz AG, 5000 Köln | Combustion chamber for liquid and gas fuels |
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US5622489A (en) * | 1995-04-13 | 1997-04-22 | Monro; Richard J. | Fuel atomizer and apparatus and method for reducing NOx |
IT1277266B1 (en) * | 1995-10-17 | 1997-11-05 | Enrico Sebastiani | GAS APPLIANCE FOR FLUID HEATING |
US5622054A (en) * | 1995-12-22 | 1997-04-22 | General Electric Company | Low NOx lobed mixer fuel injector |
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DE19914666B4 (en) * | 1999-03-31 | 2009-08-20 | Alstom | Burner for a heat generator |
US6672862B2 (en) * | 2000-03-24 | 2004-01-06 | North American Manufacturing Company | Premix burner with integral mixers and supplementary burner system |
DE10056243A1 (en) * | 2000-11-14 | 2002-05-23 | Alstom Switzerland Ltd | Combustion chamber and method for operating this combustion chamber |
EP1255074B1 (en) * | 2001-05-01 | 2005-11-23 | Alstom Technology Ltd | Oscillation reduction in a combustion chamber |
JP4610796B2 (en) * | 2001-06-13 | 2011-01-12 | 三菱重工業株式会社 | Gas turbine combustor |
JP4610800B2 (en) * | 2001-06-29 | 2011-01-12 | 三菱重工業株式会社 | Gas turbine combustor |
JP2003065537A (en) * | 2001-08-24 | 2003-03-05 | Mitsubishi Heavy Ind Ltd | Gas turbine combustor |
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US6986255B2 (en) * | 2002-10-24 | 2006-01-17 | Rolls-Royce Plc | Piloted airblast lean direct fuel injector with modified air splitter |
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EP1568942A1 (en) * | 2004-02-24 | 2005-08-31 | Siemens Aktiengesellschaft | Premix Burner and Method for Combusting a Low-calorific Gas |
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-
2006
- 2006-10-26 DE DE102006051286A patent/DE102006051286A1/en not_active Ceased
-
2007
- 2007-10-22 EP EP07119000A patent/EP1918641A3/en not_active Withdrawn
- 2007-10-25 US US11/978,205 patent/US20080131824A1/en not_active Abandoned
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040020210A1 (en) * | 2001-06-29 | 2004-02-05 | Katsunori Tanaka | Fuel injection nozzle for gas turbine combustor, gas turbine combustor, and gas turbine |
US20040000146A1 (en) * | 2001-08-29 | 2004-01-01 | Hiroshi Inoue | Gas turbine combustor and operating method thereof |
WO2004053395A1 (en) * | 2002-12-11 | 2004-06-24 | Alstom Technology Ltd | Method and device for combustion of a fuel |
WO2006027989A1 (en) * | 2004-09-10 | 2006-03-16 | Mitsubishi Heavy Industries, Ltd. | Gas turbine combustor |
Also Published As
Publication number | Publication date |
---|---|
DE102006051286A1 (en) | 2008-04-30 |
US20080131824A1 (en) | 2008-06-05 |
EP1918641A2 (en) | 2008-05-07 |
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Legal Events
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PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
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RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: WS-WAERMEPROZESSTECHNIK GMBH Owner name: DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. |
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RIC1 | Information provided on ipc code assigned before grant |
Ipc: F23D 14/02 20060101ALI20121224BHEP Ipc: F23D 14/58 20060101ALI20121224BHEP Ipc: F23C 9/00 20060101ALI20121224BHEP Ipc: F23D 14/64 20060101AFI20121224BHEP |
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18D | Application deemed to be withdrawn |
Effective date: 20130731 |