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 PDF

Info

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Withdrawn
Application number
EP07119000A
Other languages
German (de)
French (fr)
Other versions
EP1918641A2 (en
Inventor
Claus Wahl
Manfred Aigner
Harald Schütz
Oliver Lammel
Rainer Lückerath
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
WS Warmeprozesstechnik GmbH
Original Assignee
Deutsches Zentrum fuer Luft und Raumfahrt eV
WS Warmeprozesstechnik GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Deutsches Zentrum fuer Luft und Raumfahrt eV, WS Warmeprozesstechnik GmbH filed Critical Deutsches Zentrum fuer Luft und Raumfahrt eV
Publication of EP1918641A2 publication Critical patent/EP1918641A2/en
Publication of EP1918641A3 publication Critical patent/EP1918641A3/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/62Mixing devices; Mixing tubes
    • F23D14/64Mixing devices; Mixing tubes with injectors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C5/00Disposition of burners with respect to the combustion chamber or to one another; Mounting of burners in combustion apparatus
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C5/00Disposition of burners with respect to the combustion chamber or to one another; Mounting of burners in combustion apparatus
    • F23C5/02Structural details of mounting
    • F23C5/06Provision for adjustment of burner position during operation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C9/00Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
    • F23C9/006Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber the recirculation taking place in the combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/48Nozzles
    • F23D14/58Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration
    • F23D14/583Nozzles 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N1/00Regulating fuel supply
    • F23N1/02Regulating fuel supply conjointly with air supply
    • F23N1/022Regulating fuel supply conjointly with air supply using electronic means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N2237/00Controlling
    • F23N2237/02Controlling two or more burners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03282High 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.

Figure imgaf001
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.
Figure imgaf001

EP07119000A 2006-10-26 2007-10-22 Burner device and method for injecting a fuel-oxidant mixture into a combustion chamber Withdrawn EP1918641A3 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US4223214A (en) * 1978-01-09 1980-09-16 American Solar Systems, Inc. Solar tracking device
US4218020A (en) * 1979-02-23 1980-08-19 General Motors Corporation Elliptical airblast nozzle
DE3061595D1 (en) * 1979-05-18 1983-02-17 Rolls Royce Combustion apparatus for gas turbine engines
JPS57187531A (en) * 1981-05-12 1982-11-18 Hitachi Ltd Low nox gas turbine burner
JP2713627B2 (en) * 1989-03-20 1998-02-16 株式会社日立製作所 Gas turbine combustor, gas turbine equipment including the same, and combustion method
ATE124528T1 (en) * 1990-10-17 1995-07-15 Asea Brown Boveri COMBUSTION CHAMBER OF A GAS TURBINE.
US5207064A (en) * 1990-11-21 1993-05-04 General Electric Company Staged, mixed combustor assembly having low emissions
JPH06272862A (en) * 1993-03-18 1994-09-27 Hitachi Ltd Method and apparatus for mixing fuel into air
US5730591A (en) * 1993-04-12 1998-03-24 North American Manufacturing Company Method and apparatus for aggregate treatment
US5460512A (en) * 1993-05-27 1995-10-24 Coen Company, Inc. Vibration-resistant low NOx burner
GB9325708D0 (en) * 1993-12-16 1994-02-16 Rolls Royce Plc A gas turbine engine combustion chamber
GB2284884B (en) * 1993-12-16 1997-12-10 Rolls Royce Plc A gas turbine engine combustion chamber
AU681271B2 (en) * 1994-06-07 1997-08-21 Westinghouse Electric Corporation Method and apparatus for sequentially staged combustion using a catalyst
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
DE19615910B4 (en) * 1996-04-22 2006-09-14 Alstom burner arrangement
US6059566A (en) * 1997-07-25 2000-05-09 Maxon Corporation Burner apparatus
US6119459A (en) * 1998-08-18 2000-09-19 Alliedsignal Inc. Elliptical axial combustor swirler
US6024301A (en) * 1998-10-16 2000-02-15 Combustion Components Associates, Inc. Low NOx liquid fuel oil atomizer spray plate and fabrication method thereof
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
US6814307B2 (en) * 2002-01-24 2004-11-09 Combustion Components Associates, Inc. Low NOx liquid fuel oil atomizer spray plate and fabrication method thereof
US6986255B2 (en) * 2002-10-24 2006-01-17 Rolls-Royce Plc Piloted airblast lean direct fuel injector with modified air splitter
DE10326720A1 (en) * 2003-06-06 2004-12-23 Rolls-Royce Deutschland Ltd & Co Kg Burner for a gas turbine combustor
EP1568942A1 (en) * 2004-02-24 2005-08-31 Siemens Aktiengesellschaft Premix Burner and Method for Combusting a Low-calorific Gas
US7425127B2 (en) * 2004-06-10 2008-09-16 Georgia Tech Research Corporation Stagnation point reverse flow combustor
US7168949B2 (en) * 2004-06-10 2007-01-30 Georgia Tech Research Center Stagnation point reverse flow combustor for a combustion system
DE102004049491A1 (en) * 2004-10-11 2006-04-20 Alstom Technology Ltd premix
US7402038B2 (en) * 2005-04-22 2008-07-22 The North American Manufacturing Company, Ltd. Combustion method and apparatus

Patent Citations (4)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
EP1918641A3 (en) Burner device and method for injecting a fuel-oxidant mixture into a combustion chamber
CH707752A2 (en) Premixing system for a gas turbine.
EP1064498B1 (en) Burner for a gas turbine
CH703548A2 (en) Fuel injection head with surface features for flame stabilization and method for generating a fuel injection head.
EP1614964A3 (en) Burner
DE102010038122A1 (en) Combustor head end baffles for reducing mis-distribution of fuel in a multi-nozzle arrangement
EP1355111A3 (en) Burner with lateral outlets for flameless oxidation
MY157599A (en) Combustion cavity layouts for fuel staging in trapped vortex combustors
DE102011055475A1 (en) System and method for injecting fuel
DE4439619A1 (en) Method and device for operating a premix burner
CH697790B1 (en) Nozzle for directing a fluid into a combustion chamber assembly.
CH701946B1 (en) Fuel injector with staged premix in multiple tubes.
DE102010037608A1 (en) System and method using a low emission gas turbine cycle with partial air separation
DE2355127A1 (en) BURNER FOR A GAS TURBINE
EP2023025A3 (en) Constant pressure nozzle and method for mixing with same
DE112014004695B4 (en) Fuel injector for a gas turbine
CH697861B8 (en) Gas turbine and method for operating a gas turbine.
EP2402652A1 (en) Burner
DE102005042889A1 (en) Gas turbine group
DE1401826A1 (en) Combustion device for hydrocarbon fuels
EP1512912A2 (en) Homogeneous mixture formation by swirled injection of the fuel
EP1342951A3 (en) Mobile heating apparatus with fuel inlet
DE1526882B1 (en) COMBUSTION DEVICE FOR A GAS TURBINE ENGINE
EP1754937A3 (en) Burner head and method of combusting fuel
DE112012002595T5 (en) Phase and amplitude adjusted fuel injector

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK RS

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.

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK RS

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

AKY No designation fees paid
REG Reference to a national code

Ref country code: DE

Ref legal event code: R108

Effective date: 20131002

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20130731