DE69311191D1 - Dualringbrennkamer - Google Patents

Dualringbrennkamer

Info

Publication number
DE69311191D1
DE69311191D1 DE69311191T DE69311191T DE69311191D1 DE 69311191 D1 DE69311191 D1 DE 69311191D1 DE 69311191 T DE69311191 T DE 69311191T DE 69311191 T DE69311191 T DE 69311191T DE 69311191 D1 DE69311191 D1 DE 69311191D1
Authority
DE
Germany
Prior art keywords
dual ring
ring burner
burner
dual
ring
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
DE69311191T
Other languages
English (en)
Other versions
DE69311191T2 (de
Inventor
Joseph Frank Savelli
Byron Andres Pritchard
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 Co
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.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE69311191D1 publication Critical patent/DE69311191D1/de
Publication of DE69311191T2 publication Critical patent/DE69311191T2/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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
DE69311191T 1992-03-30 1993-03-25 Dualringbrennkamer Expired - Lifetime DE69311191T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US85975992A 1992-03-30 1992-03-30

Publications (2)

Publication Number Publication Date
DE69311191D1 true DE69311191D1 (de) 1997-07-10
DE69311191T2 DE69311191T2 (de) 1998-01-22

Family

ID=25331633

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69311191T Expired - Lifetime DE69311191T2 (de) 1992-03-30 1993-03-25 Dualringbrennkamer

Country Status (5)

Country Link
US (1) US5285635A (de)
EP (1) EP0564172B1 (de)
JP (1) JP2599881B2 (de)
CA (1) CA2089302C (de)
DE (1) DE69311191T2 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2257781B (en) * 1991-04-30 1995-04-12 Rolls Royce Plc Combustion chamber assembly in a gas turbine engine
US5406799A (en) * 1992-06-12 1995-04-18 United Technologies Corporation Combustion chamber
US5421158A (en) * 1994-10-21 1995-06-06 General Electric Company Segmented centerbody for a double annular combustor
CA2216115A1 (en) * 1995-03-08 1996-09-12 Bmw Rolls-Royce Gmbh Axially stepped double-ring combustion chamber for a gas turbine
US5974781A (en) * 1995-12-26 1999-11-02 General Electric Company Hybrid can-annular combustor for axial staging in low NOx combustors
US5657633A (en) * 1995-12-29 1997-08-19 General Electric Company Centerbody for a multiple annular combustor
DE19745683A1 (de) * 1997-10-16 1999-04-22 Bmw Rolls Royce Gmbh Aufhängung einer ringförmigen Gasturbinen-Brennkammer
US6212870B1 (en) 1998-09-22 2001-04-10 General Electric Company Self fixturing combustor dome assembly
US6502400B1 (en) * 2000-05-20 2003-01-07 General Electric Company Combustor dome assembly and method of assembling the same
US6449952B1 (en) 2001-04-17 2002-09-17 General Electric Company Removable cowl for gas turbine combustor
FR2829228B1 (fr) * 2001-08-28 2005-07-15 Snecma Moteurs Chambre de combustion annulaire a double tete etagee
FR2856468B1 (fr) * 2003-06-17 2007-11-23 Snecma Moteurs Chambre de combustion annulaire de turbomachine
US7506511B2 (en) * 2003-12-23 2009-03-24 Honeywell International Inc. Reduced exhaust emissions gas turbine engine combustor
US20060052867A1 (en) * 2004-09-07 2006-03-09 Medtronic, Inc Replacement prosthetic heart valve, system and method of implant
FR2897145B1 (fr) * 2006-02-08 2013-01-18 Snecma Chambre de combustion annulaire de turbomachine a fixations alternees.
FR2897144B1 (fr) * 2006-02-08 2008-05-02 Snecma Sa Chambre de combustion de turbomachine a fentes tangentielles
US7874157B2 (en) * 2008-06-05 2011-01-25 General Electric Company Coanda pilot nozzle for low emission combustors
US9243802B2 (en) 2011-12-07 2016-01-26 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9194586B2 (en) 2011-12-07 2015-11-24 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9416972B2 (en) 2011-12-07 2016-08-16 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9228747B2 (en) * 2013-03-12 2016-01-05 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
WO2014152875A1 (en) 2013-03-14 2014-09-25 United Technologies Corporation Gas turbine engine architecture with nested concentric combustor
WO2014201135A1 (en) 2013-06-11 2014-12-18 United Technologies Corporation Combustor with axial staging for a gas turbine engine
US10330320B2 (en) * 2013-10-24 2019-06-25 United Technologies Corporation Circumferentially and axially staged annular combustor for gas turbine engine
US20160201918A1 (en) * 2014-09-18 2016-07-14 Rolls-Royce Canada, Ltd. Small arrayed swirler system for reduced emissions and noise
RU2596901C1 (ru) * 2015-09-07 2016-09-10 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Способ снижения выбросов вредных веществ в газотурбинном двигателе

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2503006A (en) * 1945-04-24 1950-04-04 Edward A Stalker Gas turbine engine with controllable auxiliary jet
US2565843A (en) * 1949-06-02 1951-08-28 Elliott Co Multiple tubular combustion chamber
US2686401A (en) * 1950-08-02 1954-08-17 United Aircraft Corp Fuel manifold for gas turbine power plants
US2996884A (en) * 1959-03-11 1961-08-22 Rolls Royce Combustion chamber
US3132483A (en) * 1960-04-25 1964-05-12 Rolls Royce Gas turbine engine combustion chamber
FR2402068A1 (fr) * 1977-09-02 1979-03-30 Snecma Chambre de combustion anti-pollution
US4194358A (en) * 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
JPS5914693A (ja) * 1982-07-16 1984-01-25 松下電器産業株式会社 プリント基板装置の製造方法
JPS6120770A (ja) * 1984-07-10 1986-01-29 Matsushita Electric Ind Co Ltd プラテン駆動装置
JPH0684817B2 (ja) * 1988-08-08 1994-10-26 株式会社日立製作所 ガスタービン燃焼器及びその運転方法
US5197289A (en) * 1990-11-26 1993-03-30 General Electric Company Double dome combustor

Also Published As

Publication number Publication date
DE69311191T2 (de) 1998-01-22
CA2089302C (en) 2004-07-06
JP2599881B2 (ja) 1997-04-16
JPH0618041A (ja) 1994-01-25
US5285635A (en) 1994-02-15
EP0564172A1 (de) 1993-10-06
EP0564172B1 (de) 1997-06-04
CA2089302A1 (en) 1993-10-01

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN