FR2896575B1 - Chambre de combustion annulaire d'une turbomachine - Google Patents
Chambre de combustion annulaire d'une turbomachineInfo
- Publication number
- FR2896575B1 FR2896575B1 FR0650269A FR0650269A FR2896575B1 FR 2896575 B1 FR2896575 B1 FR 2896575B1 FR 0650269 A FR0650269 A FR 0650269A FR 0650269 A FR0650269 A FR 0650269A FR 2896575 B1 FR2896575 B1 FR 2896575B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- combustion chamber
- annular combustion
- annular
- chamber
- 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 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2211/00—Thermal dilatation prevention or compensation
-
- 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
- F23R2900/00005—Preventing fatigue failures or reducing mechanical stress in gas turbine components
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0650269A FR2896575B1 (fr) | 2006-01-26 | 2006-01-26 | Chambre de combustion annulaire d'une turbomachine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0650269A FR2896575B1 (fr) | 2006-01-26 | 2006-01-26 | Chambre de combustion annulaire d'une turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2896575A1 FR2896575A1 (fr) | 2007-07-27 |
FR2896575B1 true FR2896575B1 (fr) | 2013-01-18 |
Family
ID=37054396
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0650269A Active FR2896575B1 (fr) | 2006-01-26 | 2006-01-26 | Chambre de combustion annulaire d'une turbomachine |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2896575B1 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2935465B1 (fr) * | 2008-08-29 | 2013-09-20 | Snecma | Fixation d'un deflecteur en cmc sur un fond de chambre par pincage a l'aide d'un support metallique. |
FR2998039B1 (fr) * | 2012-11-09 | 2014-11-14 | Snecma | Chambre de combustion pour une turbomachine |
US10281153B2 (en) | 2016-02-25 | 2019-05-07 | General Electric Company | Combustor assembly |
US10378771B2 (en) | 2016-02-25 | 2019-08-13 | General Electric Company | Combustor assembly |
US10473332B2 (en) | 2016-02-25 | 2019-11-12 | General Electric Company | Combustor assembly |
FR3081539B1 (fr) * | 2018-05-23 | 2021-06-04 | Safran Aircraft Engines | Fond de chambre de combustion de turbomachine |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2555965A (en) * | 1950-03-24 | 1951-06-05 | Gen Electric | End cap for fluid fuel combustors |
GB700705A (en) * | 1951-03-27 | 1953-12-09 | Lucas Industries Ltd | Combustion chambers for jet propulsion engines, gas turbines or other prime movers |
US3064425A (en) * | 1959-10-05 | 1962-11-20 | Gen Motors Corp | Combustion liner |
US4413477A (en) * | 1980-12-29 | 1983-11-08 | General Electric Company | Liner assembly for gas turbine combustor |
DE4223733C2 (de) * | 1992-07-18 | 1995-05-18 | Gutehoffnungshuette Man | Verbindung von Mischrohr und Flammrohr einer Gasturbine |
US5291732A (en) * | 1993-02-08 | 1994-03-08 | General Electric Company | Combustor liner support assembly |
FR2825786B1 (fr) * | 2001-06-06 | 2003-10-17 | Snecma Moteurs | Fixation de casquettes metalliques sur des parois de chambre de combustion cmc de turbomachine |
FR2825784B1 (fr) * | 2001-06-06 | 2003-08-29 | Snecma Moteurs | Accrochage de chambre de combustion cmc de turbomachine utilisant les trous de dilution |
FR2855249B1 (fr) * | 2003-05-20 | 2005-07-08 | Snecma Moteurs | Chambre de combustion ayant une liaison souple entre un fond de chambre et une paroi de chambre |
-
2006
- 2006-01-26 FR FR0650269A patent/FR2896575B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR2896575A1 (fr) | 2007-07-27 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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CD | Change of name or company name |
Owner name: SNECMA, FR Effective date: 20170713 |
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PLFP | Fee payment |
Year of fee payment: 13 |
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PLFP | Fee payment |
Year of fee payment: 15 |
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PLFP | Fee payment |
Year of fee payment: 16 |
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PLFP | Fee payment |
Year of fee payment: 17 |
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PLFP | Fee payment |
Year of fee payment: 18 |
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PLFP | Fee payment |
Year of fee payment: 19 |