FR2391359A2 - Chambre de combustion pour turbomachines - Google Patents
Chambre de combustion pour turbomachinesInfo
- Publication number
- FR2391359A2 FR2391359A2 FR7716071A FR7716071A FR2391359A2 FR 2391359 A2 FR2391359 A2 FR 2391359A2 FR 7716071 A FR7716071 A FR 7716071A FR 7716071 A FR7716071 A FR 7716071A FR 2391359 A2 FR2391359 A2 FR 2391359A2
- Authority
- FR
- France
- Prior art keywords
- combustion chamber
- air
- speeds
- gas turbine
- air streams
- 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.)
- Granted
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
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
Le présent certificat d'addition décrit un certain nombre de perfectionnements à la disposition du brevet principal consistant à intercaler entre chaque injecteur ou groupe d'injecteurs et le fond d'une chambre de combustion, une partie intermédiaire de dimension réduite par rapport à celle de la chambre Ces perfectionnements consistent d'une part à aménager des dispositifs de refroidissement pour les extrémités de la partie intermédiaire, et d'autre part à augmenter le volume de la zone de recirculation dans le fond de la chambre. Application aux chambres de combustion de tout type, pour moteurs à turbines à gaz.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7716071A FR2391359A2 (fr) | 1977-05-18 | 1977-05-18 | Chambre de combustion pour turbomachines |
US05/812,636 US4162611A (en) | 1976-07-07 | 1977-07-05 | Combustion chamber for turbo engines |
GB28040/77A GB1539136A (en) | 1976-07-07 | 1977-07-05 | Gas turbine combustion chambers |
DE2730791A DE2730791C2 (de) | 1976-07-07 | 1977-07-07 | Brennkammer für Gasturbinentriebwerke |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7716071A FR2391359A2 (fr) | 1977-05-18 | 1977-05-18 | Chambre de combustion pour turbomachines |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2391359A2 true FR2391359A2 (fr) | 1978-12-15 |
FR2391359B2 FR2391359B2 (fr) | 1983-05-13 |
Family
ID=9191290
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7716071A Granted FR2391359A2 (fr) | 1976-07-07 | 1977-05-18 | Chambre de combustion pour turbomachines |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2391359A2 (fr) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2560668A1 (fr) * | 1983-11-26 | 1985-09-06 | Rolls Royce | Appareil de combustion pour turbo-moteur |
FR2572463A1 (fr) * | 1984-10-30 | 1986-05-02 | Snecma | Systeme d'injection a geometrie variable. |
FR2588919A1 (fr) * | 1985-10-18 | 1987-04-24 | Snecma | Dispositif d'injection a bol sectorise |
US4754600A (en) * | 1986-03-20 | 1988-07-05 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) | Axial-centripetal swirler injection apparatus |
US20230072621A1 (en) * | 2021-09-06 | 2023-03-09 | Rolls-Royce Plc | Controlling soot |
-
1977
- 1977-05-18 FR FR7716071A patent/FR2391359A2/fr active Granted
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2560668A1 (fr) * | 1983-11-26 | 1985-09-06 | Rolls Royce | Appareil de combustion pour turbo-moteur |
FR2572463A1 (fr) * | 1984-10-30 | 1986-05-02 | Snecma | Systeme d'injection a geometrie variable. |
EP0182687B1 (fr) * | 1984-10-30 | 1988-08-03 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Système d'injection à géométrie variable |
FR2588919A1 (fr) * | 1985-10-18 | 1987-04-24 | Snecma | Dispositif d'injection a bol sectorise |
EP0224397A1 (fr) * | 1985-10-18 | 1987-06-03 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Dispositif d'injection à bol sectorisé |
US4696157A (en) * | 1985-10-18 | 1987-09-29 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Fuel and air injection system for a turbojet engine |
US4754600A (en) * | 1986-03-20 | 1988-07-05 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) | Axial-centripetal swirler injection apparatus |
US20230072621A1 (en) * | 2021-09-06 | 2023-03-09 | Rolls-Royce Plc | Controlling soot |
Also Published As
Publication number | Publication date |
---|---|
FR2391359B2 (fr) | 1983-05-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CL | Concession to grant licences |