CH399833A - Steuereinrichtung für die Brennstoffzufuhr zu Strahltriebwerken - Google Patents
Steuereinrichtung für die Brennstoffzufuhr zu StrahltriebwerkenInfo
- Publication number
- CH399833A CH399833A CH1235461A CH1235461A CH399833A CH 399833 A CH399833 A CH 399833A CH 1235461 A CH1235461 A CH 1235461A CH 1235461 A CH1235461 A CH 1235461A CH 399833 A CH399833 A CH 399833A
- Authority
- CH
- Switzerland
- Prior art keywords
- control device
- fuel supply
- jet engines
- engines
- jet
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/15—Control or regulation
- F02K1/16—Control or regulation conjointly with another control
- F02K1/17—Control or regulation conjointly with another control with control of 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
- F02C9/16—Control of working fluid flow
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Feeding And Controlling Fuel (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US65095A US3085395A (en) | 1960-10-26 | 1960-10-26 | Afterburner fuel control |
Publications (1)
Publication Number | Publication Date |
---|---|
CH399833A true CH399833A (de) | 1965-09-30 |
Family
ID=22060305
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH1235461A CH399833A (de) | 1960-10-26 | 1961-10-25 | Steuereinrichtung für die Brennstoffzufuhr zu Strahltriebwerken |
Country Status (5)
Country | Link |
---|---|
US (1) | US3085395A (de) |
BE (1) | BE609584A (de) |
CH (1) | CH399833A (de) |
GB (1) | GB934125A (de) |
SE (1) | SE340545B (de) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3301309A (en) * | 1965-01-21 | 1967-01-31 | Dowty Fuel Syst Ltd | Fuel control systems for gas turbine engines |
GB0720703D0 (en) * | 2007-10-23 | 2007-12-05 | Rolls Royce Plc | Gas turbine engine reheat fuel system |
CN115680903B (zh) * | 2022-08-31 | 2024-05-03 | 中国航发四川燃气涡轮研究院 | 可回收旁路引气控制方法 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2953899A (en) * | 1951-05-17 | 1960-09-27 | Honeywell Regulator Co | Fuel flow controller for gas turbines and jet propulsion units |
US2820340A (en) * | 1952-12-30 | 1958-01-21 | Gen Motors Corp | Turbojet engine fuel and nozzle control system |
US2916876A (en) * | 1954-06-28 | 1959-12-15 | Rolls Royce | Reheat fuel-system for gas-turbine engine |
US2921433A (en) * | 1956-01-20 | 1960-01-19 | United Aircraft Corp | Afterburner control for a multispool gas turbine power plant |
US2988883A (en) * | 1956-04-02 | 1961-06-20 | Thompson Ramo Wooldridge Inc | Fuel supply control system for supplying multiple combustion zones in afterburners |
US2879643A (en) * | 1956-06-04 | 1959-03-31 | Holley Carburetor Co | Engine fuel regulating system including automatic minimum flow adjustment |
US2856754A (en) * | 1956-11-01 | 1958-10-21 | United Aircraft Corp | Fuel control including minimum fuel flow limiting for a split-turbine type power plant |
US2988875A (en) * | 1956-11-21 | 1961-06-20 | United Aircraft Corp | Afterburner fuel control having multiple sets of nozzles |
-
1960
- 1960-10-26 US US65095A patent/US3085395A/en not_active Expired - Lifetime
-
1961
- 1961-10-20 GB GB37710/61A patent/GB934125A/en not_active Expired
- 1961-10-25 BE BE609584A patent/BE609584A/fr unknown
- 1961-10-25 CH CH1235461A patent/CH399833A/de unknown
-
1964
- 1964-07-09 SE SE08388/64A patent/SE340545B/xx unknown
Also Published As
Publication number | Publication date |
---|---|
SE340545B (de) | 1971-11-22 |
BE609584A (fr) | 1962-02-15 |
US3085395A (en) | 1963-04-16 |
GB934125A (en) | 1963-08-14 |
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