FR2673705B1 - - Google Patents

Info

Publication number
FR2673705B1
FR2673705B1 FR9102647A FR9102647A FR2673705B1 FR 2673705 B1 FR2673705 B1 FR 2673705B1 FR 9102647 A FR9102647 A FR 9102647A FR 9102647 A FR9102647 A FR 9102647A FR 2673705 B1 FR2673705 B1 FR 2673705B1
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
FR9102647A
Other languages
French (fr)
Other versions
FR2673705A1 (fr
Inventor
Gerard Bayle-Laboure
Joseph
Jacques Pascalmaunand
Jacques Pidevois
Eloi
Jacques Rauner
Alois
Antoine
Patrick Rossi
Jacques
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 FR9102647A priority Critical patent/FR2673705A1/fr
Publication of FR2673705A1 publication Critical patent/FR2673705A1/fr
Application granted granted Critical
Publication of FR2673705B1 publication Critical patent/FR2673705B1/fr
Granted 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR9102647A 1991-03-06 1991-03-06 Chambre de combustion de turbomachine munie d'un dispositif anti-cokefaction du fond de ladite chambre. Granted FR2673705A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9102647A FR2673705A1 (fr) 1991-03-06 1991-03-06 Chambre de combustion de turbomachine munie d'un dispositif anti-cokefaction du fond de ladite chambre.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9102647A FR2673705A1 (fr) 1991-03-06 1991-03-06 Chambre de combustion de turbomachine munie d'un dispositif anti-cokefaction du fond de ladite chambre.

Publications (2)

Publication Number Publication Date
FR2673705A1 FR2673705A1 (fr) 1992-09-11
FR2673705B1 true FR2673705B1 (US08066781-20111129-C00013.png) 1994-12-16

Family

ID=9410379

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9102647A Granted FR2673705A1 (fr) 1991-03-06 1991-03-06 Chambre de combustion de turbomachine munie d'un dispositif anti-cokefaction du fond de ladite chambre.

Country Status (1)

Country Link
FR (1) FR2673705A1 (US08066781-20111129-C00013.png)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5816050A (en) * 1994-07-13 1998-10-06 Volvo Aero Corporation Low-emission combustion chamber for gas turbine engines
DE10348604A1 (de) * 2003-10-20 2005-07-28 Rolls-Royce Deutschland Ltd & Co Kg Kraftstoffeinspritzdüse mit filmartiger Kraftstoffplatzierung
FR2951246B1 (fr) 2009-10-13 2011-11-11 Snecma Injecteur multi-point pour une chambre de combustion de turbomachine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3498055A (en) * 1968-10-16 1970-03-03 United Aircraft Corp Smoke reduction combustion chamber
IL42390A0 (en) * 1972-08-02 1973-07-30 Gen Electric Impingement cooled combustor dome
GB1563124A (en) * 1975-12-24 1980-03-19 Gen Electric Gas turbine fuel injection systems
US4653278A (en) * 1985-08-23 1987-03-31 General Electric Company Gas turbine engine carburetor
DE3642122C1 (de) * 1986-12-10 1988-06-09 Mtu Muenchen Gmbh Brennstoffeinspritzvorrichtung

Also Published As

Publication number Publication date
FR2673705A1 (fr) 1992-09-11

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Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse

Effective date: 20101130