FR2873168B1 - TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBER - Google Patents

TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBER

Info

Publication number
FR2873168B1
FR2873168B1 FR0407909A FR0407909A FR2873168B1 FR 2873168 B1 FR2873168 B1 FR 2873168B1 FR 0407909 A FR0407909 A FR 0407909A FR 0407909 A FR0407909 A FR 0407909A FR 2873168 B1 FR2873168 B1 FR 2873168B1
Authority
FR
France
Prior art keywords
turboreactor
combustion chamber
secured
ignition post
post
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
FR0407909A
Other languages
French (fr)
Other versions
FR2873168A1 (en
Inventor
Sebastien Pierre Louis Baboeuf
Sabine Constance Maud Charpenel
Didier Noel Durand
Jacques A Roche
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 Moteurs SA
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 Moteurs SA filed Critical SNECMA Moteurs SA
Priority to FR0407909A priority Critical patent/FR2873168B1/en
Priority to EP05291480A priority patent/EP1621817B1/en
Priority to DE602005012560T priority patent/DE602005012560D1/en
Priority to CA002511875A priority patent/CA2511875A1/en
Priority to RU2005122513/06A priority patent/RU2005122513A/en
Priority to US11/181,924 priority patent/US20060292504A1/en
Publication of FR2873168A1 publication Critical patent/FR2873168A1/en
Application granted granted Critical
Publication of FR2873168B1 publication Critical patent/FR2873168B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
FR0407909A 2004-07-16 2004-07-16 TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBER Expired - Fee Related FR2873168B1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR0407909A FR2873168B1 (en) 2004-07-16 2004-07-16 TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBER
EP05291480A EP1621817B1 (en) 2004-07-16 2005-07-08 Afterburner with assured ignition
DE602005012560T DE602005012560D1 (en) 2004-07-16 2005-07-08 Afterburner with secured ignition
CA002511875A CA2511875A1 (en) 2004-07-16 2005-07-13 Afterburner with secure lighting
RU2005122513/06A RU2005122513A (en) 2004-07-16 2005-07-15 HIGH RELIABLE IGNITION CAMERA AND TURBO-REACTIVE ENGINE
US11/181,924 US20060292504A1 (en) 2004-07-16 2005-07-15 After-burner chamber with secure ignition

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0407909A FR2873168B1 (en) 2004-07-16 2004-07-16 TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBER

Publications (2)

Publication Number Publication Date
FR2873168A1 FR2873168A1 (en) 2006-01-20
FR2873168B1 true FR2873168B1 (en) 2008-10-31

Family

ID=34947700

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0407909A Expired - Fee Related FR2873168B1 (en) 2004-07-16 2004-07-16 TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBER

Country Status (6)

Country Link
US (1) US20060292504A1 (en)
EP (1) EP1621817B1 (en)
CA (1) CA2511875A1 (en)
DE (1) DE602005012560D1 (en)
FR (1) FR2873168B1 (en)
RU (1) RU2005122513A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2900460B1 (en) * 2006-04-28 2012-10-05 Snecma ANNULAR POST-COMBUSTION SYSTEM OF A TURBOMACHINE
FR2942640B1 (en) 2009-03-02 2011-05-06 Snecma POST-COMBUSTION CHAMBER FOR TURBOMACHINE
US8893502B2 (en) * 2011-10-14 2014-11-25 United Technologies Corporation Augmentor spray bar with tip support bushing
CN105716106B (en) * 2014-12-04 2019-07-05 中国航空工业集团公司沈阳发动机设计研究所 A kind of device for realizing hot-shot ignition on exerciser
FR3039220B1 (en) * 2015-07-24 2017-08-11 Snecma POSTCOMBUSTION DIPOSITIVE FOR TURBOREACTOR
FR3097298B1 (en) 2019-06-12 2021-06-04 Safran Aircraft Engines CANDLE INTEGRATED INTO THE FLAME HOLDER
FR3107570B1 (en) * 2020-02-26 2022-02-04 Safran Aircraft Engines POST-COMBUSTION BURNER WITH OPTIMIZED INTEGRATION

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB842197A (en) * 1958-07-23 1960-07-20 Gen Electric Improvements in afterburner combustion equipment of a gas turbine jet propulsion engine
DE1133185B (en) * 1959-04-21 1962-07-12 Snecma Combustion device on recoil engines, especially for post-combustion
US3016706A (en) * 1960-09-09 1962-01-16 United Aircraft Corp Jet ignition system
GB938553A (en) * 1961-05-09 1963-10-02 Rolls Royce Reheat combustion apparatus for a gas turbine engine
DE1240746B (en) * 1964-08-08 1967-05-18 Heinkel Ag Ernst Jet nozzle, especially for the afterburner of an aircraft engine, with mechanically controlled jet deflection
US3765178A (en) * 1972-09-08 1973-10-16 Gen Electric Afterburner flameholder
US3931707A (en) * 1975-01-08 1976-01-13 General Electric Company Augmentor flameholding apparatus
US4170109A (en) * 1977-11-09 1979-10-09 United Technologies Corporation Thrust augmentor having swirled flows for combustion stabilization
US4315401A (en) * 1979-11-30 1982-02-16 United Technologies Corporation Afterburner flameholder construction
US5396761A (en) 1994-04-25 1995-03-14 General Electric Company Gas turbine engine ignition flameholder with internal impingement cooling
FR2770284B1 (en) * 1997-10-23 1999-11-19 Snecma CARBIDE AND OPTIMIZED COOLING FLAME HANGER
US7437876B2 (en) * 2005-03-25 2008-10-21 General Electric Company Augmenter swirler pilot

Also Published As

Publication number Publication date
US20060292504A1 (en) 2006-12-28
DE602005012560D1 (en) 2009-03-19
EP1621817A1 (en) 2006-02-01
RU2005122513A (en) 2007-01-20
FR2873168A1 (en) 2006-01-20
EP1621817B1 (en) 2009-01-28
CA2511875A1 (en) 2006-01-16

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Legal Events

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

Effective date: 20110331