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DE60236594D1 - Drehströmungsfeuerung - Google Patents

Drehströmungsfeuerung

Info

Publication number
DE60236594D1
DE60236594D1 DE60236594T DE60236594T DE60236594D1 DE 60236594 D1 DE60236594 D1 DE 60236594D1 DE 60236594 T DE60236594 T DE 60236594T DE 60236594 T DE60236594 T DE 60236594T DE 60236594 D1 DE60236594 D1 DE 60236594D1
Authority
DE
Germany
Prior art keywords
drehströmungsfeuerung
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.)
Expired - Lifetime
Application number
DE60236594T
Other languages
English (en)
Inventor
Peter J Stuttaford
Aleksandar Kojovic
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.)
Pratt and Whitney Canada Corp
Original Assignee
Pratt and Whitney Canada 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 Pratt and Whitney Canada Corp filed Critical Pratt and Whitney Canada Corp
Application granted granted Critical
Publication of DE60236594D1 publication Critical patent/DE60236594D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F23R3/34—Feeding into different combustion zones
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • 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
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/58—Cyclone or vortex type combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00014—Pilot burners specially adapted for ignition of main burners in furnaces or gas turbines
    • 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
    • F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
DE60236594T 2001-07-13 2002-07-08 Drehströmungsfeuerung Expired - Lifetime DE60236594D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/903,636 US6543231B2 (en) 2001-07-13 2001-07-13 Cyclone combustor
PCT/CA2002/001036 WO2003006888A1 (en) 2001-07-13 2002-07-08 Cyclone combustor

Publications (1)

Publication Number Publication Date
DE60236594D1 true DE60236594D1 (de) 2010-07-15

Family

ID=25417840

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60236594T Expired - Lifetime DE60236594D1 (de) 2001-07-13 2002-07-08 Drehströmungsfeuerung

Country Status (6)

Country Link
US (1) US6543231B2 (de)
EP (1) EP1407197B1 (de)
JP (1) JP4115389B2 (de)
CA (1) CA2449501C (de)
DE (1) DE60236594D1 (de)
WO (1) WO2003006888A1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112050256A (zh) * 2020-09-18 2020-12-08 中国航发四川燃气涡轮研究院 一种多级旋流部分预混的地面燃机燃烧室头部

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7310534B2 (en) * 2003-12-16 2007-12-18 Sony Ericsson Mobile Communications Ab Location status indicator for mobile phones
JP4971582B2 (ja) * 2004-02-16 2012-07-11 帝人ファーマ株式会社 酸素濃縮装置
EP1847778A1 (de) * 2006-04-21 2007-10-24 Siemens Aktiengesellschaft Vormischverbrennungsanlage für Gasturbine und Verfahren zum Betrieb
US9080770B2 (en) 2011-06-06 2015-07-14 Honeywell International Inc. Reverse-flow annular combustor for reduced emissions
US20130089823A1 (en) * 2011-10-07 2013-04-11 General Electric Company Combustor
US9400110B2 (en) 2012-10-19 2016-07-26 Honeywell International Inc. Reverse-flow annular combustor for reduced emissions
US9541292B2 (en) 2013-03-12 2017-01-10 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9127843B2 (en) 2013-03-12 2015-09-08 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9228747B2 (en) 2013-03-12 2016-01-05 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9366187B2 (en) 2013-03-12 2016-06-14 Pratt & Whitney Canada Corp. Slinger combustor
US9958161B2 (en) 2013-03-12 2018-05-01 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
JP6395363B2 (ja) * 2013-10-11 2018-09-26 川崎重工業株式会社 ガスタービンの燃料噴射装置
US11156164B2 (en) 2019-05-21 2021-10-26 General Electric Company System and method for high frequency accoustic dampers with caps
US11174792B2 (en) 2019-05-21 2021-11-16 General Electric Company System and method for high frequency acoustic dampers with baffles

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US297549A (en) 1884-04-29 And john wagner
US2411663A (en) 1943-03-01 1946-11-26 Stewart Warner Corp Heater
US2579614A (en) 1944-06-23 1951-12-25 Allis Chalmers Mfg Co Combustion chamber with rotating fuel and air stream surrounding a flame core
GB719379A (en) 1950-11-17 1954-12-01 Power Jets Res & Dev Ltd Improvements in combustion apparatus
NL95825C (de) 1950-11-17
US4891936A (en) 1987-12-28 1990-01-09 Sundstrand Corporation Turbine combustor with tangential fuel injection and bender jets
US4928481A (en) * 1988-07-13 1990-05-29 Prutech Ii Staged low NOx premix gas turbine combustor
US4936090A (en) 1988-07-15 1990-06-26 Sundstrand Corporation Assuring reliable starting of turbine engines
US4967563A (en) 1988-12-12 1990-11-06 Sundstrand Corporation Turbine engine with high efficiency fuel atomization
US5214911A (en) 1989-12-21 1993-06-01 Sundstrand Corporation Method and apparatus for high altitude starting of gas turbine engine
US5277022A (en) 1990-06-22 1994-01-11 Sundstrand Corporation Air blast fuel injecton system
US5377483A (en) * 1993-07-07 1995-01-03 Mowill; R. Jan Process for single stage premixed constant fuel/air ratio combustion
US5450724A (en) * 1993-08-27 1995-09-19 Northern Research & Engineering Corporation Gas turbine apparatus including fuel and air mixer
US5479781A (en) 1993-09-02 1996-01-02 General Electric Company Low emission combustor having tangential lean direct injection
GB2284884B (en) * 1993-12-16 1997-12-10 Rolls Royce Plc A gas turbine engine combustion chamber
US5596873A (en) 1994-09-14 1997-01-28 General Electric Company Gas turbine combustor with a plurality of circumferentially spaced pre-mixers
JP3012166B2 (ja) * 1995-02-01 2000-02-21 川崎重工業株式会社 ガスタービン燃焼システム
EP0731316A1 (de) 1995-02-24 1996-09-11 R. Jan Mowill Sternförmiges, einstufiges, emissionsarmes Verbrennungssystem
GB9505067D0 (en) * 1995-03-14 1995-05-03 Europ Gas Turbines Ltd Combustor and operating method for gas or liquid-fuelled turbine
US5791137A (en) 1995-11-13 1998-08-11 United Technologies Corporation Radial inflow dual fuel injector
US6250066B1 (en) * 1996-11-26 2001-06-26 Honeywell International Inc. Combustor with dilution bypass system and venturi jet deflector
US5850732A (en) 1997-05-13 1998-12-22 Capstone Turbine Corporation Low emissions combustion system for a gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112050256A (zh) * 2020-09-18 2020-12-08 中国航发四川燃气涡轮研究院 一种多级旋流部分预混的地面燃机燃烧室头部

Also Published As

Publication number Publication date
JP2004534199A (ja) 2004-11-11
CA2449501C (en) 2010-08-03
CA2449501A1 (en) 2003-01-23
EP1407197B1 (de) 2010-06-02
EP1407197A1 (de) 2004-04-14
US20030010031A1 (en) 2003-01-16
JP4115389B2 (ja) 2008-07-09
US6543231B2 (en) 2003-04-08
WO2003006888A1 (en) 2003-01-23

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