NO330494B1 - Vaeskebrennstoffinjektor for brennere i gassturbiner - Google Patents

Vaeskebrennstoffinjektor for brennere i gassturbiner Download PDF

Info

Publication number
NO330494B1
NO330494B1 NO20002764A NO20002764A NO330494B1 NO 330494 B1 NO330494 B1 NO 330494B1 NO 20002764 A NO20002764 A NO 20002764A NO 20002764 A NO20002764 A NO 20002764A NO 330494 B1 NO330494 B1 NO 330494B1
Authority
NO
Norway
Prior art keywords
holes
liquid fuel
compressed air
fuel
fuel injector
Prior art date
Application number
NO20002764A
Other languages
English (en)
Norwegian (no)
Other versions
NO20002764D0 (no
NO20002764L (no
Inventor
Anthony Dean
Luciano Mei
Alessio Miliani
Original Assignee
Nuovo Pignone Spa
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 Nuovo Pignone Spa filed Critical Nuovo Pignone Spa
Publication of NO20002764D0 publication Critical patent/NO20002764D0/no
Publication of NO20002764L publication Critical patent/NO20002764L/no
Publication of NO330494B1 publication Critical patent/NO330494B1/no

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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/101—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Gas Burners (AREA)
NO20002764A 1999-05-31 2000-05-30 Vaeskebrennstoffinjektor for brennere i gassturbiner NO330494B1 (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT1999MI001204A ITMI991204A1 (it) 1999-05-31 1999-05-31 Iniettore di combustibile liquido per bruciatori in turbine a gas

Publications (3)

Publication Number Publication Date
NO20002764D0 NO20002764D0 (no) 2000-05-30
NO20002764L NO20002764L (no) 2000-12-01
NO330494B1 true NO330494B1 (no) 2011-05-02

Family

ID=11383079

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20002764A NO330494B1 (no) 1999-05-31 2000-05-30 Vaeskebrennstoffinjektor for brennere i gassturbiner

Country Status (12)

Country Link
US (1) US6334309B1 (fr)
EP (1) EP1058063B1 (fr)
AR (1) AR024165A1 (fr)
BR (1) BR0002534A (fr)
DE (1) DE60037850T2 (fr)
DZ (1) DZ3084A1 (fr)
EG (1) EG22570A (fr)
ES (1) ES2300247T3 (fr)
IT (1) ITMI991204A1 (fr)
MX (1) MXPA00005371A (fr)
NO (1) NO330494B1 (fr)
RU (1) RU2224953C2 (fr)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10160997A1 (de) * 2001-12-12 2003-07-03 Rolls Royce Deutschland Magervormischbrenner für eine Gasturbine sowie Verfahren zum Betrieb eines Magervormischbrenners
EP1499800B1 (fr) * 2002-04-26 2011-06-29 Rolls-Royce Corporation Module de premelange de combustible pour chambre de combustion de turbine a gaz
DE10219354A1 (de) * 2002-04-30 2003-11-13 Rolls Royce Deutschland Gasturbinenbrennkammer mit gezielter Kraftstoffeinbringung zur Verbesserung der Homogenität des Kraftstoff-Luft-Gemisches
US7007486B2 (en) * 2003-03-26 2006-03-07 The Boeing Company Apparatus and method for selecting a flow mixture
US7127899B2 (en) * 2004-02-26 2006-10-31 United Technologies Corporation Non-swirl dry low NOx (DLN) combustor
CN101365913A (zh) * 2005-11-04 2009-02-11 阿尔斯托姆科技有限公司 燃料喷管
EP2023041A1 (fr) * 2007-07-27 2009-02-11 Siemens Aktiengesellschaft Brûleur à prémélange et procédé de mise en oeuvre du brûleur
DE102007043626A1 (de) 2007-09-13 2009-03-19 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenmagerbrenner mit Kraftstoffdüse mit kontrollierter Kraftstoffinhomogenität
US9121609B2 (en) 2008-10-14 2015-09-01 General Electric Company Method and apparatus for introducing diluent flow into a combustor
US20100089022A1 (en) * 2008-10-14 2010-04-15 General Electric Company Method and apparatus of fuel nozzle diluent introduction
US20100089020A1 (en) * 2008-10-14 2010-04-15 General Electric Company Metering of diluent flow in combustor
US8567199B2 (en) * 2008-10-14 2013-10-29 General Electric Company Method and apparatus of introducing diluent flow into a combustor
EP2253888B1 (fr) * 2009-05-14 2013-10-16 Alstom Technology Ltd Brûleur d'une turbine à gaz ayant un générateur de vortex avec une lance à combustible
US9010119B2 (en) * 2010-11-03 2015-04-21 General Electric Company Premixing nozzle
US20130232978A1 (en) * 2012-03-12 2013-09-12 Zhongtao Dai Fuel air premixer for gas turbine engine
EP2743588A1 (fr) 2012-12-11 2014-06-18 Siemens Aktiengesellschaft Positionnement d'injecteur de carburant en retrait
US9759425B2 (en) * 2013-03-12 2017-09-12 General Electric Company System and method having multi-tube fuel nozzle with multiple fuel injectors
US9534787B2 (en) 2013-03-12 2017-01-03 General Electric Company Micromixing cap assembly
US9765973B2 (en) 2013-03-12 2017-09-19 General Electric Company System and method for tube level air flow conditioning
US9671112B2 (en) 2013-03-12 2017-06-06 General Electric Company Air diffuser for a head end of a combustor
US9528444B2 (en) 2013-03-12 2016-12-27 General Electric Company System having multi-tube fuel nozzle with floating arrangement of mixing tubes
US9650959B2 (en) 2013-03-12 2017-05-16 General Electric Company Fuel-air mixing system with mixing chambers of various lengths for gas turbine system
US9651259B2 (en) 2013-03-12 2017-05-16 General Electric Company Multi-injector micromixing system
JP6191918B2 (ja) * 2014-03-20 2017-09-06 三菱日立パワーシステムズ株式会社 ノズル、バーナ、燃焼器、ガスタービン、ガスタービンシステム
US10288291B2 (en) * 2014-08-15 2019-05-14 General Electric Company Air-shielded fuel injection assembly to facilitate reduced NOx emissions in a combustor system
KR101657535B1 (ko) * 2015-05-21 2016-09-19 두산중공업 주식회사 버닝 저감 연료공급노즐.
DE102017223113A1 (de) * 2017-12-18 2019-06-19 Sms Group Gmbh Brenner
KR102119879B1 (ko) * 2018-03-07 2020-06-08 두산중공업 주식회사 파일럿 연료 분사 장치, 이를 구비한 연료 노즐 및 가스 터빈
US11371708B2 (en) * 2018-04-06 2022-06-28 General Electric Company Premixer for low emissions gas turbine combustor

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4198815A (en) 1975-12-24 1980-04-22 General Electric Company Central injection fuel carburetor
US5461865A (en) 1994-02-24 1995-10-31 United Technologies Corporation Tangential entry fuel nozzle
US5822992A (en) 1995-10-19 1998-10-20 General Electric Company Low emissions combustor premixer
US5778676A (en) 1996-01-02 1998-07-14 General Electric Company Dual fuel mixer for gas turbine combustor
DE19803879C1 (de) * 1998-01-31 1999-08-26 Mtu Muenchen Gmbh Zweistoffbrenner

Also Published As

Publication number Publication date
AR024165A1 (es) 2002-09-04
ITMI991204A1 (it) 2000-12-01
DE60037850D1 (de) 2008-03-13
DE60037850T2 (de) 2009-01-22
EG22570A (en) 2003-04-30
BR0002534A (pt) 2001-05-22
MXPA00005371A (es) 2002-04-24
ITMI991204A0 (it) 1999-05-31
NO20002764D0 (no) 2000-05-30
EP1058063B1 (fr) 2008-01-23
ES2300247T3 (es) 2008-06-16
NO20002764L (no) 2000-12-01
RU2224953C2 (ru) 2004-02-27
US6334309B1 (en) 2002-01-01
EP1058063A1 (fr) 2000-12-06
DZ3084A1 (fr) 2004-06-20

Similar Documents

Publication Publication Date Title
NO330494B1 (no) Vaeskebrennstoffinjektor for brennere i gassturbiner
US4891936A (en) Turbine combustor with tangential fuel injection and bender jets
JP3169663U (ja) ガスタービン燃焼器に用いられる予混合バーナ
US8099940B2 (en) Low cross-talk gas turbine fuel injector
US10794596B2 (en) Dual fuel nozzle with liquid filming atomization for a gas turbine engine
CN108700298B (zh) 燃烧装置及燃气轮机
JP6118024B2 (ja) 燃焼器ノズル及び燃焼器ノズルの製造方法
US20100083664A1 (en) Method and apparatus for assembling gas turbine engine
US10228137B2 (en) Dual fuel nozzle with swirling axial gas injection for a gas turbine engine
CN109073227A (zh) 用于内燃机的燃料喷射器和分级燃料输送方法
US6662565B2 (en) Fuel injectors
US9719681B2 (en) System and method for supplying fuel
CN101713549A (zh) 用于在燃气涡轮机中混合空气-燃料的系统及方法
US11713881B2 (en) Premixer for a combustor
JP2012122479A (ja) 空気多段拡散ノズルを作動させる方法
CA2577770A1 (fr) Lance pour bruleur hybride
US20120227407A1 (en) Burner for a turbine
CN108626748B (zh) 具有液体燃料末梢的双燃料型燃料喷嘴
US20170227224A1 (en) Fuel injector for combustion engine system, and engine operating method
JP2012122715A (ja) 空気多段拡散ノズル
RU2747655C2 (ru) Горелка промежуточного подогрева для газовой турбины и газовая турбина, содержащая такую горелку промежуточного подогрева
US20150323189A1 (en) Multi-fuel turbine combustor, multi-fuel turbine comprising such a combustor and corresponding method
US10955141B2 (en) Dual-fuel fuel nozzle with gas and liquid fuel capability
RU97104278A (ru) Гиперзвуковой криогенный воздушно-реактивный двигатель
RU158108U1 (ru) Привод газотурбинный

Legal Events

Date Code Title Description
MK1K Patent expired