CH351449A - Gas turbine installation combustion device - Google Patents
Gas turbine installation combustion deviceInfo
- Publication number
- CH351449A CH351449A CH351449DA CH351449A CH 351449 A CH351449 A CH 351449A CH 351449D A CH351449D A CH 351449DA CH 351449 A CH351449 A CH 351449A
- Authority
- CH
- Switzerland
- Prior art keywords
- gas turbine
- combustion device
- turbine installation
- installation combustion
- gas
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
- F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/264—Ignition
-
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
-
- 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
- F23R3/34—Feeding into different combustion zones
-
- 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
- F23R3/34—Feeding into different combustion zones
- F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB351449X | 1955-04-05 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH351449A true CH351449A (en) | 1961-01-15 |
Family
ID=10374347
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH351449D CH351449A (en) | 1955-04-05 | 1956-04-05 | Gas turbine installation combustion device |
Country Status (4)
Country | Link |
---|---|
BE (1) | BE546730A (en) |
CH (1) | CH351449A (en) |
FR (1) | FR1144928A (en) |
GB (1) | GB788557A (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1102491B (en) * | 1957-10-19 | 1961-03-16 | Bristol Siddeley Engines Ltd | Combustion device for a gas turbine engine |
CZ308533B6 (en) * | 2016-05-19 | 2020-10-29 | První Brněnská Strojírna Velká Bíteš, A.S. | Small turbine engine with ignition system |
CN109340822A (en) * | 2018-10-08 | 2019-02-15 | 西北工业大学 | The spiral evaporation tube of discount vibram outlet shape baffle plate built in tiny engine combustion chamber |
US11708793B2 (en) | 2020-12-23 | 2023-07-25 | Collins Engine Nozzles, Inc. | Torch ignitors with gas assist start |
CN114151200A (en) * | 2021-10-20 | 2022-03-08 | 中国航发四川燃气涡轮研究院 | Igniter |
CN117869126A (en) * | 2024-03-12 | 2024-04-12 | 西安航天动力研究所 | Direct-current ignition structure of rocket engine combustion chamber |
-
0
- BE BE546730D patent/BE546730A/xx unknown
-
1955
- 1955-04-05 GB GB9886/55A patent/GB788557A/en not_active Expired
-
1956
- 1956-03-29 FR FR1144928D patent/FR1144928A/en not_active Expired
- 1956-04-05 CH CH351449D patent/CH351449A/en unknown
Also Published As
Publication number | Publication date |
---|---|
BE546730A (en) | |
FR1144928A (en) | 1957-10-18 |
GB788557A (en) | 1958-01-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR1111569A (en) | Gas turbine installation | |
FR1097374A (en) | Air cooling device for gas turbines | |
CH317633A (en) | Gas turbine installation combustion device | |
CH327080A (en) | Gas turbine propellant device | |
FR1107114A (en) | Gas turbine | |
FR1228673A (en) | Gas generator device | |
CH351449A (en) | Gas turbine installation combustion device | |
FR1186524A (en) | Fuel injection devices for gas turbines | |
FR1062016A (en) | Gas turbine starter | |
CH341029A (en) | Gas turbine plant | |
FR1131310A (en) | Gas turbine | |
CH358990A (en) | Gas turbine plant | |
FR1176289A (en) | Ignition device for gas turbine engines and rocket engines | |
FR1110045A (en) | Device for taking a gas sample | |
FR1082511A (en) | Starting device for gas turbine installation | |
FR1160587A (en) | Gas turbo-engine installation | |
FR1129302A (en) | Fuel supply device for gas turbines | |
CH339782A (en) | Gas turbine plant | |
CH360546A (en) | Gas turbine plant | |
CH364386A (en) | Gas turbine plant | |
FR1281702A (en) | Adjustable guide vane bearing device for gas turbines or hot air turbines | |
FR1140720A (en) | Exhaust gas turbine | |
FR1117908A (en) | Ignition device for gas burners | |
CH326311A (en) | Gas turbine installation liquid fuel combustion device | |
CH310034A (en) | Combustion device for gas turbine installation. |