CH351449A - Dispositif de combustion d'installation à turbine à gaz - Google Patents
Dispositif de combustion d'installation à turbine à gazInfo
- 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 (fr) | 1961-01-15 |
Family
ID=10374347
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH351449D CH351449A (fr) | 1955-04-05 | 1956-04-05 | Dispositif de combustion d'installation à turbine à gaz |
Country Status (4)
| Country | Link |
|---|---|
| BE (1) | BE546730A (fr) |
| CH (1) | CH351449A (fr) |
| FR (1) | FR1144928A (fr) |
| GB (1) | GB788557A (fr) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1102491B (de) * | 1957-10-19 | 1961-03-16 | Bristol Siddeley Engines Ltd | Verbrennungseinrichtung fuer ein Gasturbinentriebwerk |
| CZ308533B6 (cs) * | 2016-05-19 | 2020-10-29 | První Brněnská Strojírna Velká Bíteš, A.S. | Malý turbínový motor se zapalovacím systémem |
| CN109340822A (zh) * | 2018-10-08 | 2019-02-15 | 西北工业大学 | 微型发动机燃烧室内置圆缺形折流板螺旋式蒸发管 |
| US11708793B2 (en) * | 2020-12-23 | 2023-07-25 | Collins Engine Nozzles, Inc. | Torch ignitors with gas assist start |
| CN114151200A (zh) * | 2021-10-20 | 2022-03-08 | 中国航发四川燃气涡轮研究院 | 点火器 |
| CN117869126A (zh) * | 2024-03-12 | 2024-04-12 | 西安航天动力研究所 | 一种火箭发动机燃烧室的直流式点火结构 |
-
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/fr not_active Expired
- 1956-04-05 CH CH351449D patent/CH351449A/fr unknown
Also Published As
| Publication number | Publication date |
|---|---|
| GB788557A (en) | 1958-01-02 |
| BE546730A (fr) | |
| FR1144928A (fr) | 1957-10-18 |
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