CN102563697B - 用于点燃燃烧器的装置和方法 - Google Patents

用于点燃燃烧器的装置和方法 Download PDF

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Publication number
CN102563697B
CN102563697B CN201110370086.3A CN201110370086A CN102563697B CN 102563697 B CN102563697 B CN 102563697B CN 201110370086 A CN201110370086 A CN 201110370086A CN 102563697 B CN102563697 B CN 102563697B
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CN
China
Prior art keywords
nozzle
central body
igniter
center body
fuel
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
CN201110370086.3A
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English (en)
Chinese (zh)
Other versions
CN102563697A (zh
Inventor
A·W·克鲁尔
G·D·迈尔斯
J·H·维斯特莫尔兰德三世
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General Electric Company PLC
Original Assignee
General Electric Co
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.)
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Publication date
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Publication of CN102563697A publication Critical patent/CN102563697A/zh
Application granted granted Critical
Publication of CN102563697B publication Critical patent/CN102563697B/zh
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P13/00—Sparking plugs structurally combined with other parts of internal-combustion engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23Q—IGNITION; EXTINGUISHING-DEVICES
    • F23Q3/00—Igniters using electrically-produced sparks
    • F23Q3/008—Structurally associated with fluid-fuel burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P23/00—Other ignition
    • F02P23/04—Other physical ignition means, e.g. using laser rays
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2207/00—Ignition devices associated with burner
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00006—Using laser for starting or improving the combustion process
    • 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)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Spark Plugs (AREA)
CN201110370086.3A 2010-11-11 2011-11-11 用于点燃燃烧器的装置和方法 Active CN102563697B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/944,135 US8534040B2 (en) 2010-11-11 2010-11-11 Apparatus and method for igniting a combustor
US12/944135 2010-11-11

Publications (2)

Publication Number Publication Date
CN102563697A CN102563697A (zh) 2012-07-11
CN102563697B true CN102563697B (zh) 2015-11-25

Family

ID=45999061

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110370086.3A Active CN102563697B (zh) 2010-11-11 2011-11-11 用于点燃燃烧器的装置和方法

Country Status (5)

Country Link
US (1) US8534040B2 (enExample)
JP (1) JP5960969B2 (enExample)
CN (1) CN102563697B (enExample)
DE (1) DE102011055241B4 (enExample)
FR (1) FR2967479B1 (enExample)

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GB2489963B (en) * 2011-04-13 2015-11-04 Rolls Royce Plc Fuel injector arrangement having an igniter
US8763401B2 (en) * 2011-05-30 2014-07-01 Pratt & Whitney Canada Corp. Integrated fuel nozzle and ignition assembly for gas turbine engines
US9707530B2 (en) * 2012-08-21 2017-07-18 Uop Llc Methane conversion apparatus and process using a supersonic flow reactor
US10160697B2 (en) * 2012-08-21 2018-12-25 Uop Llc Methane conversion apparatus and process using a supersonic flow reactor
US10029957B2 (en) * 2012-08-21 2018-07-24 Uop Llc Methane conversion apparatus and process using a supersonic flow reactor
US9689615B2 (en) * 2012-08-21 2017-06-27 Uop Llc Steady state high temperature reactor
US9656229B2 (en) * 2012-08-21 2017-05-23 Uop Llc Methane conversion apparatus and process using a supersonic flow reactor
US9021781B2 (en) * 2013-01-04 2015-05-05 General Electric Company Fuel injector having an ignitor for igniting a combustor of a gas turbine
EP2940389A1 (en) * 2014-05-02 2015-11-04 Siemens Aktiengesellschaft Combustor burner arrangement
US20160003150A1 (en) * 2014-07-03 2016-01-07 General Electric Company Igniter tip with cooling passage
US9964043B2 (en) 2014-11-11 2018-05-08 General Electric Company Premixing nozzle with integral liquid evaporator
US10711699B2 (en) * 2017-07-07 2020-07-14 Woodward, Inc. Auxiliary torch ignition
US11519334B2 (en) * 2017-07-31 2022-12-06 General Electric Company Torch igniter for a combustor
KR102046457B1 (ko) * 2017-11-09 2019-11-19 두산중공업 주식회사 연소기 및 이를 포함하는 가스 터빈
RU2755240C2 (ru) * 2017-12-26 2021-09-14 Ансальдо Энергия Свитзерленд Аг Горелка для камеры сгорания газотурбинной энергосиловой установки, камера сгорания газотурбинной энергосиловой установки, содержащая такую горелку, и газотурбинная энергосиловая установка, содержащая такую камеру сгорания
US11421601B2 (en) 2019-03-28 2022-08-23 Woodward, Inc. Second stage combustion for igniter
US20210172376A1 (en) * 2019-12-10 2021-06-10 General Electric Company Combustor ignition timing
CN116209823A (zh) 2020-06-23 2023-06-02 伍德沃德有限公司 针对功率生成发动机的点火系统
US11326521B2 (en) 2020-06-30 2022-05-10 General Electric Company Methods of igniting liquid fuel in a turbomachine
US11543130B1 (en) * 2021-06-28 2023-01-03 Collins Engine Nozzles, Inc. Passive secondary air assist nozzles

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4938019A (en) * 1987-10-16 1990-07-03 Fuel Systems Textron Inc. Fuel nozzle and igniter assembly
US5267442A (en) * 1992-11-17 1993-12-07 United Technologies Corporation Fuel nozzle with eccentric primary circuit orifice
CN1637248A (zh) * 2004-01-06 2005-07-13 通用电气公司 减少和/或消除燃烧衬套组件中稀释空气泄漏的装置和方法
EP1010945B1 (en) * 1998-12-18 2008-06-25 General Electric Company Fuel injector bar for a gas turbine combustor

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US2676460A (en) * 1950-03-23 1954-04-27 United Aircraft Corp Burner construction of the can-an-nular type having means for distributing airflow to each can
FR2269646B1 (enExample) 1974-04-30 1976-12-17 Snecma
DE2618771A1 (de) 1976-04-29 1977-11-17 Friedrich Gutbrod Hoehenverstellbarer schachtrahmen
US4249103A (en) 1979-02-02 1981-02-03 General Electric Company Breech-assembled igniter device
US4947640A (en) 1989-02-28 1990-08-14 University Of Tennessee Research Corporation Gas turbine engine photon ignition system
US5163287A (en) 1989-12-22 1992-11-17 Sundstrand Corporation Stored energy combustor with fuel injector containing igniter means for accommodating thermal expansion
US5228283A (en) 1990-05-01 1993-07-20 General Electric Company Method of reducing nox emissions in a gas turbine engine
CH684962A5 (de) * 1991-07-03 1995-02-15 Asea Brown Boveri Brenner zum Betrieb einer Brennkraftmaschine, einer Brennkammer einer Gasturbogruppe oder einer Feuerungsanlage.
JP2524003Y2 (ja) * 1992-12-22 1997-01-29 工業技術院長 燃料噴射弁
US5515681A (en) * 1993-05-26 1996-05-14 Simmonds Precision Engine Systems Commonly housed electrostatic fuel atomizer and igniter apparatus for combustors
US5367869A (en) * 1993-06-23 1994-11-29 Simmonds Precision Engine Systems Laser ignition methods and apparatus for combustors
JP2001193932A (ja) * 2000-01-11 2001-07-17 Kawasaki Steel Corp パイロットバーナ、加熱装置及び発電設備
DE10112864A1 (de) 2001-03-16 2002-09-19 Alstom Switzerland Ltd Verfahren zum Zünden einer thermischen Turbomaschine
US6698207B1 (en) * 2002-09-11 2004-03-02 Siemens Westinghouse Power Corporation Flame-holding, single-mode nozzle assembly with tip cooling
EP1929208A1 (en) * 2005-09-30 2008-06-11 Ansaldo Energia S.P.A. Method for starting a gas turbine equipped with a gas burner, and axial swirler for said burner
EP2180166B1 (en) * 2007-07-12 2014-09-10 Imagineering, Inc. Device for ignition, chemical reaction acceleration or flame holding, speed-type internal combustion engine and furnace
FR2919672B1 (fr) 2007-07-30 2014-02-14 Snecma Injecteur de carburant dans une chambre de combustion de turbomachine
US20090165436A1 (en) 2007-12-28 2009-07-02 General Electric Company Premixed, preswirled plasma-assisted pilot

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4938019A (en) * 1987-10-16 1990-07-03 Fuel Systems Textron Inc. Fuel nozzle and igniter assembly
US5267442A (en) * 1992-11-17 1993-12-07 United Technologies Corporation Fuel nozzle with eccentric primary circuit orifice
EP1010945B1 (en) * 1998-12-18 2008-06-25 General Electric Company Fuel injector bar for a gas turbine combustor
CN1637248A (zh) * 2004-01-06 2005-07-13 通用电气公司 减少和/或消除燃烧衬套组件中稀释空气泄漏的装置和方法

Also Published As

Publication number Publication date
FR2967479A1 (fr) 2012-05-18
DE102011055241B4 (de) 2022-12-08
JP2012107855A (ja) 2012-06-07
US8534040B2 (en) 2013-09-17
DE102011055241A1 (de) 2012-05-16
CN102563697A (zh) 2012-07-11
US20120117976A1 (en) 2012-05-17
FR2967479B1 (fr) 2017-04-14
JP5960969B2 (ja) 2016-08-02

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SE01 Entry into force of request for substantive examination
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GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20240108

Address after: Swiss Baden

Patentee after: GENERAL ELECTRIC CO. LTD.

Address before: New York, United States

Patentee before: General Electric Co.

TR01 Transfer of patent right