FR2097587A5 - - Google Patents

Info

Publication number
FR2097587A5
FR2097587A5 FR7025907A FR7025907A FR2097587A5 FR 2097587 A5 FR2097587 A5 FR 2097587A5 FR 7025907 A FR7025907 A FR 7025907A FR 7025907 A FR7025907 A FR 7025907A FR 2097587 A5 FR2097587 A5 FR 2097587A5
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
Application number
FR7025907A
Other languages
French (fr)
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 FR7025907A priority Critical patent/FR2097587A5/fr
Application granted granted Critical
Publication of FR2097587A5 publication Critical patent/FR2097587A5/fr
Expired 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR7025907A 1970-07-10 1970-07-10 Expired FR2097587A5 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7025907A FR2097587A5 (en) 1970-07-10 1970-07-10

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7025907A FR2097587A5 (en) 1970-07-10 1970-07-10

Publications (1)

Publication Number Publication Date
FR2097587A5 true FR2097587A5 (en) 1972-03-03

Family

ID=9058657

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7025907A Expired FR2097587A5 (en) 1970-07-10 1970-07-10

Country Status (1)

Country Link
FR (1) FR2097587A5 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2586792A1 (en) * 1985-09-03 1987-03-06 Snecma CONNECTING DEVICE BETWEEN A BURNER RING OR FLAME RING IN COMPOSITE MATERIAL AND A POST-COMBUSTION CHAMBER CHANNEL OF A TURBOJETACTOR
US4730453A (en) * 1985-10-23 1988-03-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Afterburner fuel injection system

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2586792A1 (en) * 1985-09-03 1987-03-06 Snecma CONNECTING DEVICE BETWEEN A BURNER RING OR FLAME RING IN COMPOSITE MATERIAL AND A POST-COMBUSTION CHAMBER CHANNEL OF A TURBOJETACTOR
EP0234137A1 (en) * 1985-09-03 1987-09-02 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Attaching means for a flame holder, or annular burner, of composite material for a turbo jet
US4724671A (en) * 1985-09-03 1988-02-16 Societe Nationale D'etude Et De Constructions De Moteurs D'aviation "S.N.E.C.M.A." Device for connecting a burner ring or flame holder to an afterburner duct of a turbojet engine
US4730453A (en) * 1985-10-23 1988-03-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Afterburner fuel injection system

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Legal Events

Date Code Title Description
ST Notification of lapse