CH326697A - Dispositif de combustion à combustible liquide - Google Patents
Dispositif de combustion à combustible liquideInfo
- Publication number
- CH326697A CH326697A CH326697DA CH326697A CH 326697 A CH326697 A CH 326697A CH 326697D A CH326697D A CH 326697DA CH 326697 A CH326697 A CH 326697A
- Authority
- CH
- Switzerland
- Prior art keywords
- casing
- fuel
- liquid fuel
- oxidant
- conduit
- 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
- F23R3/16—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
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB326697X | 1952-12-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH326697A true CH326697A (fr) | 1957-12-31 |
Family
ID=10342233
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH326697D CH326697A (fr) | 1952-12-20 | 1953-12-11 | Dispositif de combustion à combustible liquide |
Country Status (2)
Country | Link |
---|---|
BE (1) | BE525083A (ko) |
CH (1) | CH326697A (ko) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2996288A1 (fr) * | 2012-10-01 | 2014-04-04 | Turbomeca | Injecteur a double circuit de chambre de combustion de turbomachine. |
CN104704294B (zh) * | 2012-10-01 | 2016-11-30 | 涡轮梅坎公司 | 涡轮发动机燃烧室的双回路喷射器 |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB780493A (en) * | 1954-07-20 | 1957-08-07 | Rolls Royce | Improvements relating to combustion equipment for gas-turbine engines |
US2930195A (en) * | 1956-02-14 | 1960-03-29 | United Aircraft Corp | Oscillating flow combustion chamber |
-
0
- BE BE525083D patent/BE525083A/xx unknown
-
1953
- 1953-12-11 CH CH326697D patent/CH326697A/fr unknown
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2996288A1 (fr) * | 2012-10-01 | 2014-04-04 | Turbomeca | Injecteur a double circuit de chambre de combustion de turbomachine. |
WO2014053730A3 (fr) * | 2012-10-01 | 2014-07-17 | Turbomeca | Injecteur a double circuit de chambre de combustion de turbomachine |
CN104704294A (zh) * | 2012-10-01 | 2015-06-10 | 涡轮梅坎公司 | 涡轮发动机燃烧室的双回路喷射器 |
JP2015531448A (ja) * | 2012-10-01 | 2015-11-02 | ターボメカTurbomeca | タービンエンジンの燃焼室のための2つの回路の噴射器 |
CN104704294B (zh) * | 2012-10-01 | 2016-11-30 | 涡轮梅坎公司 | 涡轮发动机燃烧室的双回路喷射器 |
US9927125B2 (en) | 2012-10-01 | 2018-03-27 | Turbomeca | Two-circuit injector for a turbine engine combustion chamber |
Also Published As
Publication number | Publication date |
---|---|
BE525083A (ko) |
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