EP0807787A3 - Burner - Google Patents

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Info

Publication number
EP0807787A3
EP0807787A3 EP97810221A EP97810221A EP0807787A3 EP 0807787 A3 EP0807787 A3 EP 0807787A3 EP 97810221 A EP97810221 A EP 97810221A EP 97810221 A EP97810221 A EP 97810221A EP 0807787 A3 EP0807787 A3 EP 0807787A3
Authority
EP
European Patent Office
Prior art keywords
burner
overlap
air inlet
fuel
overlap angle
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
Application number
EP97810221A
Other languages
German (de)
French (fr)
Other versions
EP0807787A2 (en
EP0807787B1 (en
Inventor
Klaus Dr. Döbbeling
Hans Peter Knöpfel
Dieter Winkler
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.)
General Electric Switzerland GmbH
Original Assignee
ABB Research Ltd Switzerland
ABB Research Ltd Sweden
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 ABB Research Ltd Switzerland, ABB Research Ltd Sweden filed Critical ABB Research Ltd Switzerland
Publication of EP0807787A2 publication Critical patent/EP0807787A2/en
Publication of EP0807787A3 publication Critical patent/EP0807787A3/en
Application granted granted Critical
Publication of EP0807787B1 publication Critical patent/EP0807787B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D17/00Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
    • 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 
    • F23C7/00Combustion apparatus characterised by arrangements for air supply
    • F23C7/002Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • 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 
    • F23C2900/00Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
    • F23C2900/07002Premix burners with air inlet slots obtained between offset curved wall surfaces, e.g. double cone burners

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)

Abstract

Bei einem Brenner der Doppelkegelbauart zum Verbrennen von flüssigen (12) und gasförmigen Brennstoffen (16) überlappen sich die mindestens zwei Teilkegelkörper (1, 2) zumindestens teilweise, wobei der Überlappungswinkel (δ) in Strömungsrichtung des Brenners zunimmt und gleichzeitig mit Zunahme des Überlappungswinkels (δ) der Abstand der Brennstoffinjektoren (15) von der Lufteintrittsebene (21) in den Brenner zunimmt. Dadurch fallen die Lufteintrittsebene (21) und die Brennstoffinjektionsebene (22) nicht mehr zusammen. Mit der Erfindung wird eine bessere Vormischung des gasförmigen Brennstoffes (16) mit der Verbrennungsluft erreicht, was zu geringeren NOx-Emissionen des Brenners und zu einer geringeren thermischen Belastung der Brennerfront führt.

Figure 00000001
In a burner of the double-cone type for burning liquid (12) and gaseous fuels (16), the at least two partial cone bodies (1, 2) overlap at least partially, the overlap angle (δ) increasing in the flow direction of the burner and at the same time as the overlap angle ( δ) the distance of the fuel injectors (15) from the air inlet plane (21) into the burner increases. As a result, the air inlet level (21) and the fuel injection level (22) no longer coincide. The invention achieves a better premixing of the gaseous fuel (16) with the combustion air, which leads to lower NOx emissions from the burner and to a lower thermal load on the burner front.
Figure 00000001

EP97810221A 1996-05-17 1997-04-14 Burner Expired - Lifetime EP0807787B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19619873 1996-05-17
DE19619873A DE19619873A1 (en) 1996-05-17 1996-05-17 burner

Publications (3)

Publication Number Publication Date
EP0807787A2 EP0807787A2 (en) 1997-11-19
EP0807787A3 true EP0807787A3 (en) 1999-03-24
EP0807787B1 EP0807787B1 (en) 2003-05-28

Family

ID=7794546

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97810221A Expired - Lifetime EP0807787B1 (en) 1996-05-17 1997-04-14 Burner

Country Status (5)

Country Link
US (1) US5921766A (en)
EP (1) EP0807787B1 (en)
JP (1) JP3863631B2 (en)
CN (1) CN1117243C (en)
DE (2) DE19619873A1 (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ATE244380T1 (en) * 1997-11-21 2003-07-15 Alstom BURNER FOR OPERATION OF A HEAT GENERATOR
US6141954A (en) * 1998-05-18 2000-11-07 United Technologies Corporation Premixing fuel injector with improved flame disgorgement capacity
EP1262714A1 (en) * 2001-06-01 2002-12-04 ALSTOM (Switzerland) Ltd Burner with exhausts recirculation
DE10333671A1 (en) 2003-07-24 2005-08-04 Alstom Technology Ltd Method for reducing the NOx emissions of a burner assembly comprising several burners and burner arrangement for carrying out the method
US7097448B2 (en) * 2004-05-07 2006-08-29 Peter Chesney Vortex type gas lamp
CA2786597A1 (en) 2010-01-06 2011-07-14 The Outdoor Greatroom Company LLLP Fire container assembly
US10281140B2 (en) 2014-07-15 2019-05-07 Chevron U.S.A. Inc. Low NOx combustion method and apparatus
US11852319B2 (en) * 2021-02-26 2023-12-26 Armando Parra Control means for vortex flame device

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5340306A (en) * 1991-12-23 1994-08-23 Asea Brown Boveri Ltd. Device for mixing two gaseous components and burner in which this device is employed
EP0641971A2 (en) * 1993-09-06 1995-03-08 Abb Research Ltd. Method for operating a premix burner
WO1995023316A1 (en) * 1994-02-24 1995-08-31 United Technologies Corporation Tangential entry fuel nozzle

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3570471A (en) * 1969-02-14 1971-03-16 Thermo Electron Corp Radiant tube having uniform high-temperature distribution
DE3662462D1 (en) * 1985-07-30 1989-04-20 Bbc Brown Boveri & Cie Dual combustor
CH674561A5 (en) * 1987-12-21 1990-06-15 Bbc Brown Boveri & Cie
EP0481111B1 (en) * 1990-10-17 1995-06-28 Asea Brown Boveri Ag Gas-turbine combustion chamber
US5307634A (en) * 1992-02-26 1994-05-03 United Technologies Corporation Premix gas nozzle
DE4304213A1 (en) * 1993-02-12 1994-08-18 Abb Research Ltd Burner for operating an internal combustion engine, a combustion chamber of a gas turbine group or a combustion system
DE19502796B4 (en) * 1995-01-30 2004-10-28 Alstom burner

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5340306A (en) * 1991-12-23 1994-08-23 Asea Brown Boveri Ltd. Device for mixing two gaseous components and burner in which this device is employed
EP0641971A2 (en) * 1993-09-06 1995-03-08 Abb Research Ltd. Method for operating a premix burner
WO1995023316A1 (en) * 1994-02-24 1995-08-31 United Technologies Corporation Tangential entry fuel nozzle

Also Published As

Publication number Publication date
US5921766A (en) 1999-07-13
EP0807787A2 (en) 1997-11-19
JPH1068511A (en) 1998-03-10
JP3863631B2 (en) 2006-12-27
DE19619873A1 (en) 1997-11-20
EP0807787B1 (en) 2003-05-28
CN1117243C (en) 2003-08-06
CN1172227A (en) 1998-02-04
DE59710156D1 (en) 2003-07-03

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