FR2958014B1 - COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWN - Google Patents
COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWNInfo
- Publication number
- FR2958014B1 FR2958014B1 FR1052106A FR1052106A FR2958014B1 FR 2958014 B1 FR2958014 B1 FR 2958014B1 FR 1052106 A FR1052106 A FR 1052106A FR 1052106 A FR1052106 A FR 1052106A FR 2958014 B1 FR2958014 B1 FR 2958014B1
- Authority
- FR
- France
- Prior art keywords
- combustion chamber
- injectors
- same crown
- shifting longitudinally
- injection systems
- 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.)
- Active
Links
- 238000002485 combustion reaction Methods 0.000 title abstract 3
- 238000002347 injection Methods 0.000 abstract 3
- 239000007924 injection Substances 0.000 abstract 3
- 239000000446 fuel Substances 0.000 abstract 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
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1052106A FR2958014B1 (en) | 2010-03-23 | 2010-03-23 | COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWN |
PCT/FR2011/050605 WO2011117533A2 (en) | 2010-03-23 | 2011-03-22 | Combustion chamber comprising injectors offset longitudinally on the same ring |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1052106A FR2958014B1 (en) | 2010-03-23 | 2010-03-23 | COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWN |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2958014A1 FR2958014A1 (en) | 2011-09-30 |
FR2958014B1 true FR2958014B1 (en) | 2013-12-13 |
Family
ID=43037849
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1052106A Active FR2958014B1 (en) | 2010-03-23 | 2010-03-23 | COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWN |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2958014B1 (en) |
WO (1) | WO2011117533A2 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10513984B2 (en) | 2015-08-25 | 2019-12-24 | General Electric Company | System for suppressing acoustic noise within a gas turbine combustor |
US10197275B2 (en) | 2016-05-03 | 2019-02-05 | General Electric Company | High frequency acoustic damper for combustor liners |
US10415480B2 (en) | 2017-04-13 | 2019-09-17 | General Electric Company | Gas turbine engine fuel manifold damper and method of dynamics attenuation |
US11149948B2 (en) | 2017-08-21 | 2021-10-19 | General Electric Company | Fuel nozzle with angled main injection ports and radial main injection ports |
US11156162B2 (en) | 2018-05-23 | 2021-10-26 | General Electric Company | Fluid manifold damper for gas turbine engine |
US11506125B2 (en) | 2018-08-01 | 2022-11-22 | General Electric Company | Fluid manifold assembly for gas turbine engine |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4336096B4 (en) * | 1992-11-13 | 2004-07-08 | Alstom | Device for reducing vibrations in combustion chambers |
FR2727193B1 (en) | 1994-11-23 | 1996-12-20 | Snecma | TWO-HEAD COMBUSTION CHAMBER OPERATING AT FULL GAS SLOW MOTION |
SE9802707L (en) * | 1998-08-11 | 2000-02-12 | Abb Ab | Burner chamber device and method for reducing the influence of acoustic pressure fluctuations in a burner chamber device |
EP1125087B1 (en) * | 1998-08-31 | 2005-05-18 | Siemens Aktiengesellschaft | Burner assembly |
FR2829228B1 (en) | 2001-08-28 | 2005-07-15 | Snecma Moteurs | ANNULAR COMBUSTION CHAMBER WITH DOUBLE HEADED HEAD |
EP1524469A1 (en) * | 2003-10-13 | 2005-04-20 | Siemens Aktiengesellschaft | Premix burner for a gas turbine |
-
2010
- 2010-03-23 FR FR1052106A patent/FR2958014B1/en active Active
-
2011
- 2011-03-22 WO PCT/FR2011/050605 patent/WO2011117533A2/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
FR2958014A1 (en) | 2011-09-30 |
WO2011117533A3 (en) | 2012-05-31 |
WO2011117533A2 (en) | 2011-09-29 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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Year of fee payment: 11 |
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Year of fee payment: 12 |
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Year of fee payment: 15 |