FR2709342B1 - Post combustion device of a turbojet engine. - Google Patents

Post combustion device of a turbojet engine.

Info

Publication number
FR2709342B1
FR2709342B1 FR9310220A FR9310220A FR2709342B1 FR 2709342 B1 FR2709342 B1 FR 2709342B1 FR 9310220 A FR9310220 A FR 9310220A FR 9310220 A FR9310220 A FR 9310220A FR 2709342 B1 FR2709342 B1 FR 2709342B1
Authority
FR
France
Prior art keywords
combustion device
turbojet engine
post combustion
post
turbojet
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 - Fee Related
Application number
FR9310220A
Other languages
French (fr)
Other versions
FR2709342A1 (en
Inventor
Capelle Jean-Yves
Cot Fabrice
Desaulty Michel
Laverdant Alain
Le Letty Eric
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 FR9310220A priority Critical patent/FR2709342B1/en
Publication of FR2709342A1 publication Critical patent/FR2709342A1/en
Application granted granted Critical
Publication of FR2709342B1 publication Critical patent/FR2709342B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F23R3/02—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
FR9310220A 1993-08-25 1993-08-25 Post combustion device of a turbojet engine. Expired - Fee Related FR2709342B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9310220A FR2709342B1 (en) 1993-08-25 1993-08-25 Post combustion device of a turbojet engine.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9310220A FR2709342B1 (en) 1993-08-25 1993-08-25 Post combustion device of a turbojet engine.

Publications (2)

Publication Number Publication Date
FR2709342A1 FR2709342A1 (en) 1995-03-03
FR2709342B1 true FR2709342B1 (en) 1995-09-22

Family

ID=9450376

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9310220A Expired - Fee Related FR2709342B1 (en) 1993-08-25 1993-08-25 Post combustion device of a turbojet engine.

Country Status (1)

Country Link
FR (1) FR2709342B1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102200292A (en) * 2010-03-26 2011-09-28 北京航空航天大学 Flame stabilizing device and method for supporting plate with cavities

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5685140A (en) * 1995-06-21 1997-11-11 United Technologies Corporation Method for distributing fuel within an augmentor
FR2770284B1 (en) * 1997-10-23 1999-11-19 Snecma CARBIDE AND OPTIMIZED COOLING FLAME HANGER
US6463739B1 (en) * 2001-02-05 2002-10-15 General Electric Company Afterburner heat shield
US6415609B1 (en) * 2001-03-15 2002-07-09 General Electric Company Replaceable afterburner heat shield
FR2869953B1 (en) * 2004-05-05 2008-07-04 Snecma Moteurs Sa DEVICE FOR SUPPLYING AIR AND FUEL FROM A RING-BURNER IN A POSTCOMBUSTION CHAMBER
FR2873411B1 (en) * 2004-07-21 2009-08-21 Snecma Moteurs Sa TURBOREACTOR WITH PROTECTIVE MEANS FOR A FUEL INJECTION DEVICE, INJECTION DEVICE AND PROTECTIVE COVER FOR THE TURBOJET ENGINE
FR2873408B1 (en) * 2004-07-23 2008-10-17 Snecma Moteurs Sa TURBOREACTOR WITH A PROTECTION SCREEN OF THE FUEL RAMP OF A BURNER RING, THE BURNER RING AND THE PROTECTION SCREEN
US7856827B2 (en) * 2006-03-14 2010-12-28 United Technologies Corporation Structural track support of spraybars/tubing
FR2899316B1 (en) * 2006-03-30 2008-05-16 Snecma Sa ARM-FIRE ARM OF A POST-COMBUSTION CHAMBER
FR2909419B1 (en) * 2006-11-30 2009-01-16 Snecma Sa FLAME HOOK WITH THERMAL PROTECTION SCREEN
FR2928202A1 (en) * 2008-02-29 2009-09-04 Snecma Sa FLAME HOOK FOR HEATER CHANNEL OF A TURBOJET ENGINE WITH A DISCHARGE SOLE, HEATING CHANNEL AND TURBOJET COMPRISING A HEATING CHANNEL.
FR2935464B1 (en) 2008-09-01 2018-10-26 Safran Aircraft Engines DEVICE FOR FASTENING AN ARM ATTACHED FLAME ON A POST-COMBUSTION HOUSING.
FR2950416B1 (en) * 2009-09-23 2012-04-20 Snecma FLAME-APPARATUS DEVICE COMPRISING AN ARM SUPPORT AND A MONOBLOCS HEAT PROTECTION SCREEN
JP5573656B2 (en) * 2010-12-22 2014-08-20 株式会社Ｉｈｉ Afterburner and aircraft engine
US10280791B2 (en) * 2016-07-11 2019-05-07 United Technologies Corporation Tuned mass damper for tubes
FR3121959B1 (en) * 2021-04-19 2024-02-09 Safran Aircraft Engines IMPROVED FUEL INJECTION DEVICE FOR TURBOJET AFTERCOMBUSTION
FR3122719A1 (en) * 2021-05-04 2022-11-11 Safran Aircraft Engines FLAME HOLDER FOR TURBOJET AFTERCOMBUSTION INCLUDING ARMS WITH SERRATED TRAILING EDGES

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3153319A (en) * 1952-07-25 1964-10-20 Young Alec David Jet noise suppression means
GB1153034A (en) * 1965-09-21 1969-05-21 Rolls Royce Combustion Apparatus
US3648800A (en) * 1970-04-27 1972-03-14 Gen Electric Coanda expansion exhaust nozzle suppressor
US3698186A (en) * 1970-12-24 1972-10-17 United Aircraft Corp Afterburner combustion apparatus
US3747345A (en) * 1972-07-24 1973-07-24 United Aircraft Corp Shortened afterburner construction for turbine engine
IL93630A0 (en) * 1989-03-27 1990-12-23 Gen Electric Flameholder for gas turbine engine afterburner

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102200292A (en) * 2010-03-26 2011-09-28 北京航空航天大学 Flame stabilizing device and method for supporting plate with cavities
CN102200292B (en) * 2010-03-26 2015-01-21 北京航空航天大学 Flame stabilizing device and method for supporting plate with cavities

Also Published As

Publication number Publication date
FR2709342A1 (en) 1995-03-03

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Legal Events

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CD Change of name or company name
TP Transmission of property
CD Change of name or company name
ST Notification of lapse

Effective date: 20100430