CH364144A - Brennkammer für Gasturbinen - Google Patents
Brennkammer für GasturbinenInfo
- Publication number
- CH364144A CH364144A CH6202158A CH6202158A CH364144A CH 364144 A CH364144 A CH 364144A CH 6202158 A CH6202158 A CH 6202158A CH 6202158 A CH6202158 A CH 6202158A CH 364144 A CH364144 A CH 364144A
- Authority
- CH
- Switzerland
- Prior art keywords
- combustion chamber
- gas turbines
- turbines
- gas
- combustion
- Prior art date
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
- F23R3/06—Arrangement of apertures along the flame tube
- F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
-
- 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
-
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
- F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
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 (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US542809A US2973624A (en) | 1955-10-26 | 1955-10-26 | Cowled dome liners |
GB1272058A GB845971A (en) | 1958-07-21 | 1958-04-22 | Improvements relating to combustion chambers for gas turbine engines |
DEG24415A DE1107455B (de) | 1958-04-28 | 1958-04-28 | Brennkammer fuer ein Gasturbinentriebwerk |
FR1195188D FR1195188A (fr) | 1958-07-21 | 1958-04-30 | Manchon intérieur de chambre de combustion pour les moteurs à turbine à gaz |
CH6202158A CH364144A (de) | 1958-07-21 | 1958-07-21 | Brennkammer für Gasturbinen |
BE586496A BE586496Q (fr) | 1958-07-21 | 1960-01-13 | Manchon interieur de chambre de combustion pour les moteurs à turbine à gaz |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH6202158A CH364144A (de) | 1958-07-21 | 1958-07-21 | Brennkammer für Gasturbinen |
Publications (1)
Publication Number | Publication Date |
---|---|
CH364144A true CH364144A (de) | 1962-08-31 |
Family
ID=4524033
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH6202158A CH364144A (de) | 1955-10-26 | 1958-07-21 | Brennkammer für Gasturbinen |
Country Status (4)
Country | Link |
---|---|
BE (1) | BE586496Q (fr) |
CH (1) | CH364144A (fr) |
FR (1) | FR1195188A (fr) |
GB (1) | GB845971A (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL257968A (fr) * | 1959-11-20 | |||
GB943250A (en) * | 1962-02-01 | 1963-12-04 | Rolls Royce | Improvements in or relating to gas turbine combustion chambers |
GB2034874A (en) * | 1978-11-03 | 1980-06-11 | Gen Electric | Gas turbine engine combustor |
EP0035869B1 (fr) * | 1980-03-05 | 1984-07-11 | Hitachi, Ltd. | Chambre de combustion pour turbine à gaz |
GB2125950B (en) * | 1982-08-16 | 1986-09-24 | Gen Electric | Gas turbine combustor |
FR2599821B1 (fr) * | 1986-06-04 | 1988-09-02 | Snecma | Chambre de combustion pour turbomachines a orifices de melange assurant le positionnement de la paroi chaude sur la paroi froide |
GB2221979B (en) * | 1988-08-17 | 1992-03-25 | Rolls Royce Plc | A combustion chamber for a gas turbine engine |
DE4444961A1 (de) * | 1994-12-16 | 1996-06-20 | Mtu Muenchen Gmbh | Einrichtung zur Kühlung insbesondere der Rückwand des Flammrohrs einer Brennkammer für Gasturbinentriebwerke |
-
1958
- 1958-04-22 GB GB1272058A patent/GB845971A/en not_active Expired
- 1958-04-30 FR FR1195188D patent/FR1195188A/fr not_active Expired
- 1958-07-21 CH CH6202158A patent/CH364144A/de unknown
-
1960
- 1960-01-13 BE BE586496A patent/BE586496Q/fr active
Also Published As
Publication number | Publication date |
---|---|
GB845971A (en) | 1960-08-24 |
BE586496Q (fr) | 1960-05-03 |
FR1195188A (fr) | 1959-11-16 |
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