FR2699227B1 - Ensemble monobloc de post-combustion d'une turbine à gaz. - Google Patents
Ensemble monobloc de post-combustion d'une turbine à gaz.Info
- Publication number
- FR2699227B1 FR2699227B1 FR9215120A FR9215120A FR2699227B1 FR 2699227 B1 FR2699227 B1 FR 2699227B1 FR 9215120 A FR9215120 A FR 9215120A FR 9215120 A FR9215120 A FR 9215120A FR 2699227 B1 FR2699227 B1 FR 2699227B1
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- combustion assembly
- piece post
- post
- piece
- 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
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)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9215120A FR2699227B1 (fr) | 1992-12-16 | 1992-12-16 | Ensemble monobloc de post-combustion d'une turbine à gaz. |
GB9323505A GB2273556B (en) | 1992-12-16 | 1993-11-15 | Afterburner unit for a gas turbine |
US08/162,879 US5367874A (en) | 1992-12-16 | 1993-12-08 | Integral composite gas turbine afterburner structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9215120A FR2699227B1 (fr) | 1992-12-16 | 1992-12-16 | Ensemble monobloc de post-combustion d'une turbine à gaz. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2699227A1 FR2699227A1 (fr) | 1994-06-17 |
FR2699227B1 true FR2699227B1 (fr) | 1995-01-13 |
Family
ID=9436630
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9215120A Expired - Fee Related FR2699227B1 (fr) | 1992-12-16 | 1992-12-16 | Ensemble monobloc de post-combustion d'une turbine à gaz. |
Country Status (3)
Country | Link |
---|---|
US (1) | US5367874A (fr) |
FR (1) | FR2699227B1 (fr) |
GB (1) | GB2273556B (fr) |
Families Citing this family (15)
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 |
US5927067A (en) * | 1997-11-13 | 1999-07-27 | United Technologies Corporation | Self-cleaning augmentor fuel manifold |
US6301875B1 (en) * | 2000-05-31 | 2001-10-16 | Coen Company, Inc. | Turbine exhaust gas duct heater |
US7616985B2 (en) * | 2002-07-16 | 2009-11-10 | Xenogen Corporation | Method and apparatus for 3-D imaging of internal light sources |
US7370467B2 (en) * | 2003-07-29 | 2008-05-13 | Pratt & Whitney Canada Corp. | Turbofan case and method of making |
EP1783330A3 (fr) * | 2003-07-29 | 2011-03-09 | Pratt & Whitney Canada Corp. | Carter de turboréacteur à double flux |
FR2865502B1 (fr) | 2004-01-23 | 2006-03-03 | Snecma Moteurs | Bras monobloc accroche-flammes pour un dispositif de post combustion d'un turboreacteur a double flux |
US7334409B2 (en) * | 2004-05-19 | 2008-02-26 | Alltech, Inc. | Retractable afterburner for jet engine |
US6983601B2 (en) * | 2004-05-28 | 2006-01-10 | General Electric Company | Method and apparatus for gas turbine engines |
US9938900B2 (en) | 2011-05-26 | 2018-04-10 | United Technologies Corporation | Ceramic matrix composite turbine exhaust case for a gas turbine engine |
CN105674332B (zh) * | 2016-01-19 | 2017-12-26 | 西北工业大学 | 一种预蒸发式一体化加力燃烧室 |
CN106678868B (zh) * | 2016-11-18 | 2019-03-01 | 西北工业大学 | 一种偏转整流支板火焰稳定器的一体化加力燃烧室 |
US11118481B2 (en) | 2017-02-06 | 2021-09-14 | Raytheon Technologies Corporation | Ceramic matrix composite turbine exhaust assembly for a gas turbine engine |
FR3121973A1 (fr) * | 2021-04-19 | 2022-10-21 | Safran Aircraft Engines | Cône de diffusion pour partie arrière de turboréacteur intégrant un anneau accroche-flamme en bord de fuite |
GB2615335B (en) * | 2022-02-04 | 2024-05-08 | Rolls Royce Plc | A reheat assembly |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1132384B (de) * | 1958-05-03 | 1962-06-28 | Rolls Royce | Nachbrenneinrichtung fuer Gasturbinenstrahltriebwerke |
US3176465A (en) * | 1962-08-27 | 1965-04-06 | Gen Electric | Vapor fuel injector flameholder |
US3170294A (en) * | 1963-03-20 | 1965-02-23 | Robert E Meyer | Oxygen injection system |
DE1923150A1 (de) * | 1968-05-08 | 1970-01-15 | Man Turbo Gmbh | Zweistromturbinenstrahltriebwerk |
DE2255306C3 (de) * | 1972-11-11 | 1975-06-12 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Aerodynamische Flammenhalterung für luftatmende Strahltriebwerke |
CA1050770A (fr) * | 1976-11-26 | 1979-03-20 | General Electric Company | Porte-flamme amovible |
GB1605162A (en) * | 1977-01-21 | 1982-08-25 | Rolls Royce | Reheat systems for gas turbine engines |
US4185458A (en) * | 1978-05-11 | 1980-01-29 | The United States Of America As Represented By The Secretary Of The Air Force | Turbofan augmentor flameholder |
FR2587455B1 (fr) * | 1985-09-18 | 1987-10-30 | Snecma | Procede de fabrication d'un anneau bruleur en materiau composite et anneau bruleur realise suivant ledit procede |
-
1992
- 1992-12-16 FR FR9215120A patent/FR2699227B1/fr not_active Expired - Fee Related
-
1993
- 1993-11-15 GB GB9323505A patent/GB2273556B/en not_active Expired - Fee Related
- 1993-12-08 US US08/162,879 patent/US5367874A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US5367874A (en) | 1994-11-29 |
FR2699227A1 (fr) | 1994-06-17 |
GB9323505D0 (en) | 1994-01-05 |
GB2273556B (en) | 1996-02-28 |
GB2273556A (en) | 1994-06-22 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2699227B1 (fr) | Ensemble monobloc de post-combustion d'une turbine à gaz. | |
FR2708338B1 (fr) | Brûleur de turbine à gaz. | |
FR2692318B1 (fr) | Aubage fixe de distribution des gaz chauds d'une turbo-machine. | |
BR9305965A (pt) | Isqueiro a gás à prova de crianças | |
DE59208715D1 (de) | Gasturbinen-Brennkammer | |
FR2697287B1 (fr) | Diffuseur d'échappement de turbine à gaz. | |
FR2692006B1 (fr) | Ensemble segmenté formant le trajet d'écoulement d'une turbine. | |
DE69631991D1 (de) | Gasturbinenbrennkammer | |
ITMI922517A0 (it) | Struttura d'anello perfezionata per turbina a gas | |
FR2699963B1 (fr) | Générateur de gaz à combustion rapprochée. | |
ITMI941431A0 (it) | Bruciatore di gas a diffusore perfezionato | |
EP0728989A3 (fr) | Appareil de combustion pour moteur de turbine à gaz | |
DE59610235D1 (de) | Gasturbinenbrennkammer | |
GB9220937D0 (en) | Gas turbine engine combustor | |
FR2706021B1 (fr) | Chambre de combustion comprenant un ensemble séparateur de gaz. | |
DE59604547D1 (de) | Katalytische gasturbinenbrenner | |
FR2699226B1 (fr) | Ensemble de post-combustion d'une turbine à gaz. | |
FR2728014B1 (fr) | Support d'ailettes, notamment pour turbine a gaz | |
FR2728016B1 (fr) | Distributeur monobloc non-sectorise d'un stator de turbine de turbomachine | |
FR2728015B1 (fr) | Distributeur monobloc sectorise d'un stator de turbine de turbomachine | |
FR2691235B1 (fr) | Chambre de combustion comprenant un ensemble separateur des gaz. | |
DE59208713D1 (de) | Gasturbinen-Brennkammer | |
FR2698431B1 (fr) | Montage d'un détecteur de gaz dans un four de cuisson. | |
FR2705885B1 (fr) | Ensemble de pose d'une prothèse unicompartimentale du genou. | |
FR2698681B1 (fr) | Chaudière de récupération en sortie de turbine à gaz. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
TP | Transmission of property | ||
ST | Notification of lapse |