TW532464U - Optimized combustor - Google Patents

Optimized combustor

Info

Publication number
TW532464U
TW532464U TW090212451U TW90212451U TW532464U TW 532464 U TW532464 U TW 532464U TW 090212451 U TW090212451 U TW 090212451U TW 90212451 U TW90212451 U TW 90212451U TW 532464 U TW532464 U TW 532464U
Authority
TW
Taiwan
Prior art keywords
combustor
optimized
optimized combustor
Prior art date
Application number
TW090212451U
Other languages
English (en)
Inventor
Alan S Feitelberg
Kevin Michael Elward
Robert Lee Hillis
Milton Bradford Hilt
John Francis Love
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of TW532464U publication Critical patent/TW532464U/zh

Links

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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • F02C7/055—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with intake grids, screens or guards
    • 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
    • F23R3/06—Arrangement of apertures along the flame tube

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Of Fluid Fuel (AREA)
TW090212451U 1998-03-18 1999-05-07 Optimized combustor TW532464U (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/040,978 US6192689B1 (en) 1998-03-18 1998-03-18 Reduced emissions gas turbine combustor

Publications (1)

Publication Number Publication Date
TW532464U true TW532464U (en) 2003-05-11

Family

ID=21914052

Family Applications (1)

Application Number Title Priority Date Filing Date
TW090212451U TW532464U (en) 1998-03-18 1999-05-07 Optimized combustor

Country Status (5)

Country Link
US (1) US6192689B1 (zh)
EP (1) EP0943868B1 (zh)
JP (1) JP3770749B2 (zh)
KR (1) KR100312540B1 (zh)
TW (1) TW532464U (zh)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6101814A (en) * 1999-04-15 2000-08-15 United Technologies Corporation Low emissions can combustor with dilution hole arrangement for a turbine engine
DE10020598A1 (de) 2000-04-27 2002-03-07 Rolls Royce Deutschland Gasturbinenbrennkammer mit Zuleitungsöffnungen
US6966186B2 (en) * 2002-05-01 2005-11-22 Siemens Westinghouse Power Corporation Non-catalytic combustor for reducing NOx emissions
US20060130486A1 (en) * 2004-12-17 2006-06-22 Danis Allen M Method and apparatus for assembling gas turbine engine combustors
US7614235B2 (en) * 2005-03-01 2009-11-10 United Technologies Corporation Combustor cooling hole pattern
FR2892180B1 (fr) * 2005-10-18 2008-02-01 Snecma Sa Amelioration des perfomances d'une chambre de combustion par multiperforation des parois
US7887322B2 (en) 2006-09-12 2011-02-15 General Electric Company Mixing hole arrangement and method for improving homogeneity of an air and fuel mixture in a combustor
US20100018211A1 (en) * 2008-07-23 2010-01-28 General Electric Company Gas turbine transition piece having dilution holes
US7895841B2 (en) * 2006-07-14 2011-03-01 General Electric Company Method and apparatus to facilitate reducing NOx emissions in turbine engines
US7669422B2 (en) * 2006-07-26 2010-03-02 General Electric Company Combustor liner and method of fabricating same
US7905094B2 (en) * 2007-09-28 2011-03-15 Honeywell International Inc. Combustor systems with liners having improved cooling hole patterns
US20090223201A1 (en) * 2008-03-10 2009-09-10 Anand Ashok K Methods of Injecting Diluent Into A Gas Turbine Assembly
DE102008026463A1 (de) * 2008-06-03 2009-12-10 E.On Ruhrgas Ag Verbrennungseinrichtung für eine Gasturbinenanlage
US20100037622A1 (en) * 2008-08-18 2010-02-18 General Electric Company Contoured Impingement Sleeve Holes
US20130276450A1 (en) * 2012-04-24 2013-10-24 General Electric Company Combustor apparatus for stoichiometric combustion
US9453646B2 (en) 2015-01-29 2016-09-27 General Electric Company Method for air entry in liner to reduce water requirement to control NOx
US10724741B2 (en) 2016-05-10 2020-07-28 General Electric Company Combustors and methods of assembling the same
KR102436151B1 (ko) * 2020-11-05 2022-08-26 한국전력공사 가스 터빈 연소 제어 시스템 및 방법
EP4202301A1 (en) * 2021-12-21 2023-06-28 General Electric Company Combustor with dilution openings
US11774100B2 (en) * 2022-01-14 2023-10-03 General Electric Company Combustor fuel nozzle assembly

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2595999A (en) 1943-11-23 1952-05-06 Westinghouse Electric Corp Power plant combustion apparatus having apertured combustion chamber walls
BE501690A (zh) 1950-03-07
US2947485A (en) 1954-02-05 1960-08-02 Bauer Bros Co Disc refiner
FR1493144A (fr) 1966-08-19 1967-08-25 Lucas Industries Ltd Perfectionnements aux appareils de combustion pour moteurs de turbines à gaz
JPS4724483Y1 (zh) 1970-12-22 1972-08-02
US4205524A (en) * 1974-03-29 1980-06-03 Phillips Petroleum Company Methods of operating combustors
US4269032A (en) 1979-06-13 1981-05-26 General Motors Corporation Waffle pattern porous material
JPS5741524A (en) 1980-08-25 1982-03-08 Hitachi Ltd Combustion method of gas turbine and combustor for gas turbine
JPH06105670B2 (ja) 1987-05-22 1994-12-21 株式会社安川電機 磁性膜の製造方法
JPH0617635A (ja) 1992-07-01 1994-01-25 Shizuoka Mitsubishi Fuso Jidosha Hanbai Kk 吸送液機能を有するタンク
JPH08261468A (ja) 1995-03-28 1996-10-11 Toshiba Corp ガスタービン燃焼器
JPH1171218A (ja) 1997-08-29 1999-03-16 Kobe Tennenbutsu Kagaku Kk 植物成長促進剤
US6101814A (en) * 1999-04-15 2000-08-15 United Technologies Corporation Low emissions can combustor with dilution hole arrangement for a turbine engine

Also Published As

Publication number Publication date
JPH11311416A (ja) 1999-11-09
KR19990077875A (ko) 1999-10-25
JP3770749B2 (ja) 2006-04-26
KR100312540B1 (ko) 2001-11-03
EP0943868B1 (en) 2012-05-09
EP0943868A3 (en) 2000-03-22
EP0943868A2 (en) 1999-09-22
US6192689B1 (en) 2001-02-27

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Legal Events

Date Code Title Description
GD4K Issue of patent certificate for granted utility model filed before june 30, 2004
MK4K Expiration of patent term of a granted utility model