FR1207017A - Ignition device for turbojet afterburner system - Google Patents

Ignition device for turbojet afterburner system

Info

Publication number
FR1207017A
FR1207017A FR1207017DA FR1207017A FR 1207017 A FR1207017 A FR 1207017A FR 1207017D A FR1207017D A FR 1207017DA FR 1207017 A FR1207017 A FR 1207017A
Authority
FR
France
Prior art keywords
ignition device
afterburner system
turbojet
turbojet afterburner
ignition
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
Application number
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.)
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 FR1207017A publication Critical patent/FR1207017A/en
Expired 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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous 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
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20Flame 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)
FR1207017D 1958-05-29 1958-05-29 Ignition device for turbojet afterburner system Expired FR1207017A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1207017T 1958-05-29

Publications (1)

Publication Number Publication Date
FR1207017A true FR1207017A (en) 1960-02-12

Family

ID=9673826

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1207017D Expired FR1207017A (en) 1958-05-29 1958-05-29 Ignition device for turbojet afterburner system

Country Status (1)

Country Link
FR (1) FR1207017A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2297327A1 (en) * 1975-01-08 1976-08-06 Gen Electric FLAME STABILIZER FOR TURBO-REACTOR

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2297327A1 (en) * 1975-01-08 1976-08-06 Gen Electric FLAME STABILIZER FOR TURBO-REACTOR

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