FR2873168B1 - TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBER - Google Patents
TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBERInfo
- 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
Links
- 238000002485 combustion reaction Methods 0.000 title 1
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)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Exhaust Gas After Treatment (AREA)
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 |
DE602005012560T DE602005012560D1 (en) | 2004-07-16 | 2005-07-08 | Afterburner with secured ignition |
EP05291480A EP1621817B1 (en) | 2004-07-16 | 2005-07-08 | Afterburner with assured ignition |
CA002511875A CA2511875A1 (en) | 2004-07-16 | 2005-07-13 | Afterburner with secure lighting |
US11/181,924 US20060292504A1 (en) | 2004-07-16 | 2005-07-15 | After-burner chamber with secure ignition |
RU2005122513/06A RU2005122513A (en) | 2004-07-16 | 2005-07-15 | HIGH RELIABLE IGNITION CAMERA AND TURBO-REACTIVE ENGINE |
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 (8)
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 |
EP4276357A1 (en) | 2022-05-11 | 2023-11-15 | Rolls-Royce plc | A combustion system |
Family Cites Families (12)
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 |
-
2004
- 2004-07-16 FR FR0407909A patent/FR2873168B1/en not_active Expired - Fee Related
-
2005
- 2005-07-08 EP EP05291480A patent/EP1621817B1/en active Active
- 2005-07-08 DE DE602005012560T patent/DE602005012560D1/en active Active
- 2005-07-13 CA CA002511875A patent/CA2511875A1/en not_active Abandoned
- 2005-07-15 RU RU2005122513/06A patent/RU2005122513A/en not_active Application Discontinuation
- 2005-07-15 US US11/181,924 patent/US20060292504A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
DE602005012560D1 (en) | 2009-03-19 |
FR2873168A1 (en) | 2006-01-20 |
CA2511875A1 (en) | 2006-01-16 |
EP1621817B1 (en) | 2009-01-28 |
RU2005122513A (en) | 2007-01-20 |
US20060292504A1 (en) | 2006-12-28 |
EP1621817A1 (en) | 2006-02-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
ST | Notification of lapse |
Effective date: 20110331 |