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

Post combustion device of a turbojet engine.

Info

Publication number: FR2709342B1
Authority: FR; France
Prior art keywords: combustion device; turbojet engine; post combustion; post; turbojet
Prior art date: 1993-08-25
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.)

1993-08-25

Filing date

1993-08-25

Publication date

1995-09-22

1993-08-25 Application filed by SNECMA SAS filed Critical SNECMA SAS

1993-08-25 Priority to FR9310220A priority Critical patent/FR2709342B1/en

1995-03-03 Publication of FR2709342A1 publication Critical patent/FR2709342A1/en

1995-09-22 Application granted granted Critical

1995-09-22 Publication of FR2709342B1 publication Critical patent/FR2709342B1/en

2013-08-25 Anticipated expiration legal-status Critical

Status Expired - Fee Related legal-status Critical Current

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

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Gas Burners (AREA)

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

1993
- 1993-08-25 FR FR9310220A patent/FR2709342B1/en not_active Expired - Fee Related

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

Similar Documents

Publication	Publication Date	Title
FR2709342B1 (en)	1995-09-22	Post combustion device of a turbojet engine.
FR2770486B1 (en)	2000-01-28	DEVICE FOR HANGING AN ENGINE ON AN AIRCRAFT
FR2745605B1 (en)	1998-04-30	FUEL INJECTION DEVICE FOR AIRCRAFT STATOREACTOR
DE59407154D1 (en)	1998-11-26	COMBUSTION ENGINE
DE68905316D1 (en)	1993-04-15	TWO-STROKE COMBUSTION ENGINE.
FR2713703B1 (en)	1998-05-22	Engine exhaust gas cleaning device.
FR2693767B1 (en)	1996-04-12	FUEL INJECTION DEVICE FOR A TWO-STROKE ENGINE.
FR2750169B1 (en)	1998-08-21	FUEL INJECTION DEVICE FOR A STATOREACTOR OPERATING AT A HIGH NUMBER OF MACH
FR2689192B1 (en)	1994-05-27	DEVICE FOR FIXING A FLYWHEEL ON THE CRANKSHAFT OF AN INTERNAL COMBUSTION ENGINE AND ITS FLYWHEEL.
FR2694611B1 (en)	1995-07-07	DEVICE FOR FIXING A CLUTCH ON A CRANKSHAFT.
DE68905094D1 (en)	1993-04-08	TWO-STROKE COMBUSTION ENGINE.
FR2712924B1 (en)	1996-10-11	Internal combustion engine device actuation mechanism.
FR2745851B1 (en)	2001-09-07	FUEL SUPPLY DEVICE
FR2731746B1 (en)	1997-04-11	EXHAUST DEVICE FOR A COMBUSTION ENGINE
FR2694537B1 (en)	1994-10-28	Device for attaching a turbomachine to an aircraft structure.
FR2568317B1 (en)	1991-10-31	FUEL INJECTION DEVICE
FR2697582B1 (en)	1994-12-02	Fuel detection device in an oil tank of a turbojet engine.
FR2778698B1 (en)	2001-05-04	FUEL INJECTION DEVICE
FR2653168B1 (en)	1992-03-06	DEVICE FOR CLEANING AND CONTROLLING INJECTORS FOR PETROL ENGINES.
DK147792A (en)	1993-05-21	combustion engine
FR2675205B1 (en)	1995-05-19	SPARK ARRESTER DEVICE EXIT FROM AN EXPLOSION ENGINE.
FR2733579B1 (en)	1998-08-14	KEROSENE COMBUSTION DEVICE
FR2772838B1 (en)	2000-09-22	FUEL COOLING DEVICE OF AN ENGINE, ESPECIALLY A DIESEL ENGINE
FR2663371B1 (en)	1994-09-16	DEVICE OF A CIRCUIT FOR RECYCLING THE CRANKCASE GASES OF AN ENGINE.
FR2689180B1 (en)	1995-07-13	DEVICE FOR SUPERCHARGING AN INTERNAL COMBUSTION ENGINE USING TWO PARALLEL COMPRESSORS.

Legal Events

Date	Code	Title	Description
2002-01-25	CD	Change of name or company name
2002-01-25	TP	Transmission of property
2006-02-10	CD	Change of name or company name
2010-05-21	ST	Notification of lapse	Effective date: 20100430