FR2673455B1 - - Google Patents

Info

Publication number
FR2673455B1
FR2673455B1 FR9102389A FR9102389A FR2673455B1 FR 2673455 B1 FR2673455 B1 FR 2673455B1 FR 9102389 A FR9102389 A FR 9102389A FR 9102389 A FR9102389 A FR 9102389A FR 2673455 B1 FR2673455 B1 FR 2673455B1
Authority
FR
France
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 - Fee Related
Application number
FR9102389A
Other languages
French (fr)
Other versions
FR2673455A1 (fr
Inventor
Gerard Barbier
Yves
Georges
Xavier Bardey
Marie
Henri
Michel Desaulty
Andre
Albert
Serge Meunier
Marcel
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR9102389A priority Critical patent/FR2673455A1/fr
Priority to JP4026742A priority patent/JPH04316922A/ja
Priority to US07/840,812 priority patent/US5261239A/en
Priority to EP92400489A priority patent/EP0501877A1/fr
Publication of FR2673455A1 publication Critical patent/FR2673455A1/fr
Application granted granted Critical
Publication of FR2673455B1 publication Critical patent/FR2673455B1/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54Reverse-flow combustion chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34Feeding into different combustion zones

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Fuel-Injection Apparatus (AREA)
FR9102389A 1991-02-28 1991-02-28 Chambre de combustion a premelange pauvre munie d'une enceinte a contre-courant destinee a stabiliser la flamme du premelange. Granted FR2673455A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR9102389A FR2673455A1 (fr) 1991-02-28 1991-02-28 Chambre de combustion a premelange pauvre munie d'une enceinte a contre-courant destinee a stabiliser la flamme du premelange.
JP4026742A JPH04316922A (ja) 1991-02-28 1992-02-13 ターボ機械用燃焼室
US07/840,812 US5261239A (en) 1991-02-28 1992-02-25 Lean premixture combustion-chamber comprising a counterflow enclosure to stabilize the premixture flame
EP92400489A EP0501877A1 (fr) 1991-02-28 1992-02-26 Chambre de combustion à prémélange pauvre munie d'une enceinte à contre-courant destinée à stabiliser la flamme du prémélange

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9102389A FR2673455A1 (fr) 1991-02-28 1991-02-28 Chambre de combustion a premelange pauvre munie d'une enceinte a contre-courant destinee a stabiliser la flamme du premelange.

Publications (2)

Publication Number Publication Date
FR2673455A1 FR2673455A1 (fr) 1992-09-04
FR2673455B1 true FR2673455B1 (US20020128544A1-20020912-P00008.png) 1994-12-16

Family

ID=9410188

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9102389A Granted FR2673455A1 (fr) 1991-02-28 1991-02-28 Chambre de combustion a premelange pauvre munie d'une enceinte a contre-courant destinee a stabiliser la flamme du premelange.

Country Status (4)

Country Link
US (1) US5261239A (US20020128544A1-20020912-P00008.png)
EP (1) EP0501877A1 (US20020128544A1-20020912-P00008.png)
JP (1) JPH04316922A (US20020128544A1-20020912-P00008.png)
FR (1) FR2673455A1 (US20020128544A1-20020912-P00008.png)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5813232A (en) * 1995-06-05 1998-09-29 Allison Engine Company, Inc. Dry low emission combustor for gas turbine engines
DE69625744T2 (de) * 1995-06-05 2003-10-16 Rolls Royce Corp Magervormischbrenner mit niedrigem NOx-Ausstoss für industrielle Gasturbinen
DE19728375A1 (de) * 1997-07-03 1999-01-07 Bmw Rolls Royce Gmbh Betriebsverfahren für eine axial gestufte Brennkammer einer Fluggasturbine
US20110219779A1 (en) * 2010-03-11 2011-09-15 Honeywell International Inc. Low emission combustion systems and methods for gas turbine engines
US20120304660A1 (en) * 2011-06-06 2012-12-06 Kupratis Daniel B Turbomachine combustors having different flow paths
US9194586B2 (en) * 2011-12-07 2015-11-24 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US10976052B2 (en) * 2017-10-25 2021-04-13 General Electric Company Volute trapped vortex combustor assembly
US11828469B2 (en) * 2022-03-03 2023-11-28 General Electric Company Adaptive trapped vortex combustor

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3899884A (en) * 1970-12-02 1975-08-19 Gen Electric Combustor systems
FR2221621B1 (US20020128544A1-20020912-P00008.png) * 1973-03-13 1976-09-10 Snecma
US4168609A (en) * 1977-12-01 1979-09-25 United Technologies Corporation Folded-over pilot burner
JPS5847928A (ja) * 1981-09-18 1983-03-19 Hitachi Ltd ガスタ−ビン燃焼器
JPS60240833A (ja) * 1984-05-15 1985-11-29 Hitachi Ltd ガスタ−ビン燃焼方法及びガスタ−ビン燃焼器

Also Published As

Publication number Publication date
JPH04316922A (ja) 1992-11-09
US5261239A (en) 1993-11-16
FR2673455A1 (fr) 1992-09-04
EP0501877A1 (fr) 1992-09-02

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Legal Events

Date Code Title Description
ST Notification of lapse