GB726491A - Improvements in internal combustion engines through which a continuous gaseous stream is flowing and in particular in turbo-jet and turbo-prop engines - Google Patents
Improvements in internal combustion engines through which a continuous gaseous stream is flowing and in particular in turbo-jet and turbo-prop enginesInfo
- Publication number
- GB726491A GB726491A GB19410/53A GB1941053A GB726491A GB 726491 A GB726491 A GB 726491A GB 19410/53 A GB19410/53 A GB 19410/53A GB 1941053 A GB1941053 A GB 1941053A GB 726491 A GB726491 A GB 726491A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbo
- engines
- fuel
- jet
- flowing
- 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
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/32—Control of fuel supply characterised by throttling of fuel
- F02C9/34—Joint control of separate flows to main and auxiliary burners
-
- 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
- F23R3/346—Feeding into different combustion zones for staged combustion
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
726,491. Gas turbine plant. OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AERONAUTIQUES O.N.E.R.A. July 13, 1953 [July 16, 1952], No. 19410/53. Class 110 (3). [Also in Group XII] The combustion chamber of a gas turbine engine is supplied with fuel through a main ejector 3 and auxiliary injectors 7, fuel being supplied by a pump 11 through a spring-loaded slide valve 9. As the fuel pressure rises, the valve member 12 first allows fuel to pass through conduit 4 to the main injector and then through further conduits 8a, 8b, 8c to the auxiliary injectors 7.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR726491X | 1952-07-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB726491A true GB726491A (en) | 1955-03-16 |
Family
ID=9110713
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB19410/53A Expired GB726491A (en) | 1952-07-16 | 1953-07-13 | Improvements in internal combustion engines through which a continuous gaseous stream is flowing and in particular in turbo-jet and turbo-prop engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB726491A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2926495A (en) * | 1955-12-29 | 1960-03-01 | Gen Electric | Fuel injection nozzle |
US3082603A (en) * | 1955-10-28 | 1963-03-26 | Snecma | Combustion chamber with primary and secondary air flows |
FR2446443A1 (en) * | 1979-01-12 | 1980-08-08 | Gen Electric | IMPROVED COMBUSTION CHAMBER FOR A GAS TURBINE AND OPERATING METHOD |
FR2488942A1 (en) * | 1980-08-25 | 1982-02-26 | Hitachi Ltd | COMBUSTION PROCESS AND APPARATUS FOR GAS TURBINE |
GB2239056A (en) * | 1989-10-25 | 1991-06-19 | Derek Lowe | Selective fuel supply to gas turbine engine fuel injectors |
US5752380A (en) * | 1996-10-16 | 1998-05-19 | Capstone Turbine Corporation | Liquid fuel pressurization and control system |
EP1067337A1 (en) * | 1999-07-07 | 2001-01-10 | ROLLS-ROYCE plc | Combustion chamber with staged fuel injection |
-
1953
- 1953-07-13 GB GB19410/53A patent/GB726491A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3082603A (en) * | 1955-10-28 | 1963-03-26 | Snecma | Combustion chamber with primary and secondary air flows |
US2926495A (en) * | 1955-12-29 | 1960-03-01 | Gen Electric | Fuel injection nozzle |
FR2446443A1 (en) * | 1979-01-12 | 1980-08-08 | Gen Electric | IMPROVED COMBUSTION CHAMBER FOR A GAS TURBINE AND OPERATING METHOD |
FR2488942A1 (en) * | 1980-08-25 | 1982-02-26 | Hitachi Ltd | COMBUSTION PROCESS AND APPARATUS FOR GAS TURBINE |
GB2239056A (en) * | 1989-10-25 | 1991-06-19 | Derek Lowe | Selective fuel supply to gas turbine engine fuel injectors |
US5752380A (en) * | 1996-10-16 | 1998-05-19 | Capstone Turbine Corporation | Liquid fuel pressurization and control system |
EP1067337A1 (en) * | 1999-07-07 | 2001-01-10 | ROLLS-ROYCE plc | Combustion chamber with staged fuel injection |
US6412282B1 (en) | 1999-07-07 | 2002-07-02 | Rolls-Royce Plc | Combustion chamber |
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