FR1166520A - Brûleur-veilleuse pour réacteurs - Google Patents
Brûleur-veilleuse pour réacteursInfo
- Publication number
- FR1166520A FR1166520A FR1166520DA FR1166520A FR 1166520 A FR1166520 A FR 1166520A FR 1166520D A FR1166520D A FR 1166520DA FR 1166520 A FR1166520 A FR 1166520A
- Authority
- FR
- France
- Prior art keywords
- reactors
- pilot burner
- burner
- pilot
- 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.)
- Expired
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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
-
- 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
- F23R3/28—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 |
---|---|---|---|
GB3543456A GB812209A (en) | 1956-11-20 | Pilot burner for jet engines |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1166520A true FR1166520A (fr) | 1958-11-12 |
Family
ID=10377674
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1166520D Expired FR1166520A (fr) | 1956-11-20 | 1956-12-12 | Brûleur-veilleuse pour réacteurs |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1166520A (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2402077A1 (fr) * | 1975-06-30 | 1979-03-30 | Gen Electric | Dispositif d'ejection manoeuvrable en vol pour un moteur a turbine a gaz |
EP0059490A1 (fr) * | 1981-03-04 | 1982-09-08 | BBC Aktiengesellschaft Brown, Boveri & Cie. | Chambre de combustion annulaire avec brûleur annulaire pour turbines à gaz |
FR2706588A1 (fr) * | 1993-06-16 | 1994-12-23 | Snecma | Système d'injection de carburant pour chambre de combustion. |
-
1956
- 1956-12-12 FR FR1166520D patent/FR1166520A/fr not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2402077A1 (fr) * | 1975-06-30 | 1979-03-30 | Gen Electric | Dispositif d'ejection manoeuvrable en vol pour un moteur a turbine a gaz |
EP0059490A1 (fr) * | 1981-03-04 | 1982-09-08 | BBC Aktiengesellschaft Brown, Boveri & Cie. | Chambre de combustion annulaire avec brûleur annulaire pour turbines à gaz |
FR2706588A1 (fr) * | 1993-06-16 | 1994-12-23 | Snecma | Système d'injection de carburant pour chambre de combustion. |
US5437159A (en) * | 1993-06-16 | 1995-08-01 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation (S.N.E.C.M.A.) | Fuel injection system for a gas turbine combustor including radial fuel spray arms and V-gutter flameholders |
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