WO2010037627A3 - Brenner und verfahren zum betrieb eines brenners - Google Patents

Brenner und verfahren zum betrieb eines brenners Download PDF

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Publication number
WO2010037627A3
WO2010037627A3 PCT/EP2009/061846 EP2009061846W WO2010037627A3 WO 2010037627 A3 WO2010037627 A3 WO 2010037627A3 EP 2009061846 W EP2009061846 W EP 2009061846W WO 2010037627 A3 WO2010037627 A3 WO 2010037627A3
Authority
WO
WIPO (PCT)
Prior art keywords
channel
burner
operating
fuel
separating means
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.)
Ceased
Application number
PCT/EP2009/061846
Other languages
English (en)
French (fr)
Other versions
WO2010037627A2 (de
Inventor
Bernd Prade
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.)
Siemens AG
Siemens Corp
Original Assignee
Siemens AG
Siemens Corp
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 Siemens AG, Siemens Corp filed Critical Siemens AG
Priority to EP09782950.1A priority Critical patent/EP2329196B1/de
Priority to US13/121,955 priority patent/US9217569B2/en
Priority to CN200980138879.3A priority patent/CN102171515B/zh
Publication of WO2010037627A2 publication Critical patent/WO2010037627A2/de
Publication of WO2010037627A3 publication Critical patent/WO2010037627A3/de
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex
    • F23R3/14Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26Controlling the air flow
    • 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
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/36Supply of different fuels
    • 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
    • F23R2900/00002Gas turbine combustors adapted for fuels having low heating value [LHV]

Landscapes

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

Abstract

Es wird ein Brenner (100) ein Verfahren zum Betrieb eines Brenners (100) vorgestellt. Der Brenner (100) umfasst einen Kanal 1 mit einer Mischzone (2) und mit einer Oxidationsmittelzufuhr insbesondere Luftzufuhr (16) und mindestens einer Brennstoffzufuhr zum Eindüsen von Brennstoff, wobei im Kanal (1) ein Trennmittel (15) vorgesehen ist, welcher den Kanal (1) über einen weiten Bereich des Kanals in mindestens zwei getrennte Kanäle, nämlich einen ersten Kanal (3a) und einem zweiten Kanal (3b) teilt. Das Verfahren zum Betrieb eines Brenners (100) mit einem Kanal (1) umfasst eine Vormischzone (2), in die ein Oxidationsmassenstrom und Brennstoff eingedüst wird, wobei mittels eines Trennmittels (15) im Kanal (1) und die mindestens zwei sich dadurch ausbildenden getrennten erster und zweiter Kanal (3a), (3b) zwei in wesentlichen separate Strömungspfade ausgebildet werden.
PCT/EP2009/061846 2008-10-01 2009-09-14 Brenner und verfahren zum betrieb eines brenners Ceased WO2010037627A2 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP09782950.1A EP2329196B1 (de) 2008-10-01 2009-09-14 Brenner und verfahren zum betrieb eines brenners
US13/121,955 US9217569B2 (en) 2008-10-01 2009-09-14 Burner and method for operating a burner
CN200980138879.3A CN102171515B (zh) 2008-10-01 2009-09-14 燃烧器和用于运行燃烧器的方法

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP08017321.4 2008-10-01
EP08017321A EP2312215A1 (de) 2008-10-01 2008-10-01 Brenner und Verfahren zum Betrieb eines Brenners

Publications (2)

Publication Number Publication Date
WO2010037627A2 WO2010037627A2 (de) 2010-04-08
WO2010037627A3 true WO2010037627A3 (de) 2010-06-10

Family

ID=41800811

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2009/061846 Ceased WO2010037627A2 (de) 2008-10-01 2009-09-14 Brenner und verfahren zum betrieb eines brenners

Country Status (5)

Country Link
US (1) US9217569B2 (de)
EP (2) EP2312215A1 (de)
CN (1) CN102171515B (de)
RU (1) RU2011117310A (de)
WO (1) WO2010037627A2 (de)

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IT1399989B1 (it) 2010-05-05 2013-05-09 Avio Spa Gruppo di iniezione per un combustore di una turbina a gas
BR112013010886A2 (pt) 2010-11-05 2016-08-02 Thermochem Recovery Int Inc sistema de circulação de sólidos e processo para captura e conversão de sólidos reativos
US9217563B2 (en) * 2011-07-26 2015-12-22 Jabil Circuit, Inc. LED lighting assembly having electrically conductive heat sink for providing power directly to an LED light source
AU2012315914B2 (en) 2011-09-27 2015-07-09 Thermochem Recovery International, Inc. System and method for syngas clean-up
ES2940894T3 (es) 2016-02-16 2023-05-12 Thermochem Recovery Int Inc Sistema y método de generación de gas producto de energía integrada de dos etapas
EP3433340B1 (de) 2016-03-25 2022-06-29 ThermoChem Recovery International, Inc. Dreistufiges energieintegriertes produktgaserzeugungssystem
US10364398B2 (en) 2016-08-30 2019-07-30 Thermochem Recovery International, Inc. Method of producing product gas from multiple carbonaceous feedstock streams mixed with a reduced-pressure mixing gas
US9920926B1 (en) 2017-07-10 2018-03-20 Thermochem Recovery International, Inc. Pulse combustion heat exchanger system and method
US10099200B1 (en) 2017-10-24 2018-10-16 Thermochem Recovery International, Inc. Liquid fuel production system having parallel product gas generation
US11555157B2 (en) 2020-03-10 2023-01-17 Thermochem Recovery International, Inc. System and method for liquid fuel production from carbonaceous materials using recycled conditioned syngas
US11466223B2 (en) 2020-09-04 2022-10-11 Thermochem Recovery International, Inc. Two-stage syngas production with separate char and product gas inputs into the second stage
US11835235B1 (en) * 2023-02-02 2023-12-05 Pratt & Whitney Canada Corp. Combustor with helix air and fuel mixing passage

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US5359847A (en) * 1993-06-01 1994-11-01 Westinghouse Electric Corporation Dual fuel ultra-low NOX combustor
US20050268618A1 (en) * 2004-06-08 2005-12-08 General Electric Company Burner tube and method for mixing air and gas in a gas turbine engine
US20070275337A1 (en) * 2004-02-24 2007-11-29 Andreas Heilos Premix burner and method for burning a low-calorie combustion gas

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Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4534166A (en) * 1980-10-01 1985-08-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Flow modifying device
US5359847A (en) * 1993-06-01 1994-11-01 Westinghouse Electric Corporation Dual fuel ultra-low NOX combustor
US5359847B1 (en) * 1993-06-01 1996-04-09 Westinghouse Electric Corp Dual fuel ultra-flow nox combustor
US20070275337A1 (en) * 2004-02-24 2007-11-29 Andreas Heilos Premix burner and method for burning a low-calorie combustion gas
US20050268618A1 (en) * 2004-06-08 2005-12-08 General Electric Company Burner tube and method for mixing air and gas in a gas turbine engine

Also Published As

Publication number Publication date
EP2312215A1 (de) 2011-04-20
US20110179797A1 (en) 2011-07-28
WO2010037627A2 (de) 2010-04-08
EP2329196A2 (de) 2011-06-08
US9217569B2 (en) 2015-12-22
CN102171515B (zh) 2014-05-28
RU2011117310A (ru) 2012-11-10
EP2329196B1 (de) 2015-01-28
CN102171515A (zh) 2011-08-31

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