DE502005003648D1 - PREMIUM BURNER ASSEMBLY FOR OPERATING A COMBUSTION CHAMBER AND METHOD FOR OPERATING A COMBUSTION CHAMBER - Google Patents

PREMIUM BURNER ASSEMBLY FOR OPERATING A COMBUSTION CHAMBER AND METHOD FOR OPERATING A COMBUSTION CHAMBER

Info

Publication number
DE502005003648D1
DE502005003648D1 DE502005003648T DE502005003648T DE502005003648D1 DE 502005003648 D1 DE502005003648 D1 DE 502005003648D1 DE 502005003648 T DE502005003648 T DE 502005003648T DE 502005003648 T DE502005003648 T DE 502005003648T DE 502005003648 D1 DE502005003648 D1 DE 502005003648D1
Authority
DE
Germany
Prior art keywords
operating
combustion chamber
swirl
cone
shell segments
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.)
Active
Application number
DE502005003648T
Other languages
German (de)
Inventor
Marcos Elena De
Christian Steinbach
Nicolas Ulibari
Planta Martin Andrea Von
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 Technology GmbH
Original Assignee
Alstom Technology AG
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 Alstom Technology AG filed Critical Alstom Technology AG
Publication of DE502005003648D1 publication Critical patent/DE502005003648D1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • 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 
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

A premix burner is disclosed for operating a combustion chamber with a gaseous and/or liquid fuel, having a swirl generator for inducing a swirl flow in an incoming combustion air flow and a device for injecting fuel into the swirl flow, the swirl generator having at least two cone shell segments which fit together to form a flow body and together enclose a conically formed swirl space with a cone angle gamma and air inlet slits directed tangentially to the length of the cone. At least at the downstream end region of the swirl generator, a shaped element enclosing the cone shell segments with an inside wall facing the cone shell segments is provided, and that the cone shell segments end in the inside wall in a flush manner while maintaining their shape.
DE502005003648T 2004-02-12 2005-02-09 PREMIUM BURNER ASSEMBLY FOR OPERATING A COMBUSTION CHAMBER AND METHOD FOR OPERATING A COMBUSTION CHAMBER Active DE502005003648D1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH2102004 2004-02-12
PCT/EP2005/050579 WO2005078348A1 (en) 2004-02-12 2005-02-09 Premixing burner arrangement for operating a burner chamber and method for operating a burner chamber

Publications (1)

Publication Number Publication Date
DE502005003648D1 true DE502005003648D1 (en) 2008-05-21

Family

ID=34842438

Family Applications (1)

Application Number Title Priority Date Filing Date
DE502005003648T Active DE502005003648D1 (en) 2004-02-12 2005-02-09 PREMIUM BURNER ASSEMBLY FOR OPERATING A COMBUSTION CHAMBER AND METHOD FOR OPERATING A COMBUSTION CHAMBER

Country Status (10)

Country Link
US (1) US20070042307A1 (en)
EP (1) EP1714081B1 (en)
CN (1) CN1942710A (en)
AT (1) ATE391887T1 (en)
BR (1) BRPI0507640A (en)
CA (1) CA2555481A1 (en)
DE (1) DE502005003648D1 (en)
MX (1) MXPA06008994A (en)
MY (1) MY141577A (en)
WO (1) WO2005078348A1 (en)

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WO2006094939A1 (en) * 2005-03-09 2006-09-14 Alstom Technology Ltd Burner comprising a premix for combustion chamber
DE502006007733D1 (en) * 2005-03-09 2010-10-07 Alstom Technology Ltd PREMIUM BURNER FOR PRODUCING AN IGNITABLE FUEL AIR MIXTURE
DE102007043626A1 (en) 2007-09-13 2009-03-19 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine lean burn burner with fuel nozzle with controlled fuel inhomogeneity
CN101709884B (en) * 2009-11-25 2012-07-04 北京航空航天大学 Premixing and pre-evaporating combustion chamber
TW201229437A (en) * 2011-01-11 2012-07-16 Pro Iroda Ind Inc Device for increasing flame height
TW201303226A (en) * 2011-07-06 2013-01-16 Pro Iroda Ind Inc Flame set with lifting device
JP2015512500A (en) * 2012-03-29 2015-04-27 アルストム テクノロジー リミテッドＡＬＳＴＯＭ Ｔｅｃｈｎｏｌｏｇｙ Ｌｔｄ Gas turbine combustor
US8813967B2 (en) * 2012-05-02 2014-08-26 Alstom Technology Ltd Adjustable mill classifier
EP2685160B1 (en) 2012-07-10 2018-02-21 Ansaldo Energia Switzerland AG Premix burner of the multi-cone type 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
RU2570989C2 (en) * 2012-07-10 2015-12-20 Альстом Текнолоджи Лтд Gas turbine combustion chamber axial swirler
EP2703721B1 (en) 2012-08-31 2019-05-22 Ansaldo Energia IP UK Limited Premix burner
US20150153065A1 (en) * 2013-12-04 2015-06-04 Normand Brais Burner
DE102021002508A1 (en) * 2021-05-12 2022-11-17 Martin GmbH für Umwelt- und Energietechnik Nozzle for injecting gas into an incinerator with a tube and a swirler, flue with such a nozzle and method for using such a nozzle

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US3845903A (en) * 1973-08-15 1974-11-05 Dunham Bush Inc One piece radial vane diffuser and method of manufacturing the same
CA999812A (en) * 1975-06-27 1976-11-16 Thomas D. Brown Oil burner assembly with air swirler providing blue flame combustion
JPS5535885A (en) * 1978-09-06 1980-03-13 Kobe Steel Ltd Combustion method capable of minimizing production of nitrogen oxide and smoke
US4464108A (en) * 1980-11-21 1984-08-07 Donald Korenyi Combustion apparatus
IL64452A (en) * 1981-12-04 1985-11-29 Itzhak Wiesel Burner
CH660403A5 (en) * 1983-08-30 1987-04-15 Bbc Brown Boveri & Cie AXIAL SWIRL FOR GENERATING TURNING FLOWS.
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US5470224A (en) * 1993-07-16 1995-11-28 Radian Corporation Apparatus and method for reducing NOx , CO and hydrocarbon emissions when burning gaseous fuels
DE4424639A1 (en) * 1994-07-13 1996-01-18 Abb Research Ltd Method and device for fuel distribution in a burner suitable for both liquid and gaseous fuels
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DE10164099A1 (en) * 2001-12-24 2003-07-03 Alstom Switzerland Ltd Burner with staged fuel injection
US7070637B1 (en) * 2003-01-21 2006-07-04 The Board Of Trustees Of The University Of Illinois Apparatus for separating particles from a fluid

Also Published As

Publication number Publication date
CA2555481A1 (en) 2005-08-25
BRPI0507640A (en) 2007-07-10
EP1714081A1 (en) 2006-10-25
MY141577A (en) 2010-05-14
MXPA06008994A (en) 2006-12-14
US20070042307A1 (en) 2007-02-22
EP1714081B1 (en) 2008-04-09
WO2005078348A1 (en) 2005-08-25
CN1942710A (en) 2007-04-04
ATE391887T1 (en) 2008-04-15

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