GB8320649D0 - Augmentor fuel control system - Google Patents
Augmentor fuel control systemInfo
- Publication number
- GB8320649D0 GB8320649D0 GB838320649A GB8320649A GB8320649D0 GB 8320649 D0 GB8320649 D0 GB 8320649D0 GB 838320649 A GB838320649 A GB 838320649A GB 8320649 A GB8320649 A GB 8320649A GB 8320649 D0 GB8320649 D0 GB 8320649D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- control system
- fuel control
- augmentor fuel
- augmentor
- fuel
- 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.)
- Withdrawn
Links
Classifications
-
- 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
- F02C9/263—Control of fuel supply by means of fuel metering valves
-
- 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
- F02C7/22—Fuel supply systems
- F02C7/228—Dividing fuel between various burners
-
- 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)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Feeding And Controlling Fuel (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US40722982A | 1982-08-11 | 1982-08-11 |
Publications (2)
Publication Number | Publication Date |
---|---|
GB8320649D0 true GB8320649D0 (en) | 1983-09-01 |
GB2125110A GB2125110A (en) | 1984-02-29 |
Family
ID=23611178
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08320649A Withdrawn GB2125110A (en) | 1982-08-11 | 1983-08-01 | Gas turbine augmentor fuel control system |
Country Status (3)
Country | Link |
---|---|
JP (1) | JPS5946327A (en) |
DE (1) | DE3327740A1 (en) |
GB (1) | GB2125110A (en) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3543908C1 (en) * | 1985-12-12 | 1987-01-29 | Mtu Muenchen Gmbh | Device for controlling the fuel supply to the afterburner of a bypass gas turbine jet engine |
US5036657A (en) * | 1987-06-25 | 1991-08-06 | General Electric Company | Dual manifold fuel system |
US4903478A (en) * | 1987-06-25 | 1990-02-27 | General Electric Company | Dual manifold fuel system |
US4825649A (en) * | 1987-10-22 | 1989-05-02 | United Technologies Corporation | Shutoff and pressure regulating valve |
US4876857A (en) * | 1988-08-15 | 1989-10-31 | Allied-Signal Inc. | Shut off/pressure regulating valve for turbine engine |
US5111653A (en) * | 1990-04-11 | 1992-05-12 | Woodward Governor Company | Fuel delivery system with capacity monitor |
US5339636A (en) * | 1992-12-04 | 1994-08-23 | United Technologies Corporation | Fuel splitter valve assembly for gas turbine |
GB9226886D0 (en) * | 1992-12-23 | 1993-02-17 | Dowty Defence And Fuels System | Flow distribution valve |
GB2320063B (en) * | 1993-12-09 | 1998-07-15 | United Technologies Corp | Fuel staging system |
US5442922A (en) * | 1993-12-09 | 1995-08-22 | United Technologies Corporation | Fuel staging system |
US5772182A (en) * | 1996-04-17 | 1998-06-30 | United Technologies Corporation | Fuel flow control valve |
US6092546A (en) * | 1997-12-12 | 2000-07-25 | Alliedsignal Inc. | Fuel flow divider and pressurizing valve for gas turbine |
US6079198A (en) * | 1998-04-29 | 2000-06-27 | General Electric Co. | Pressure compensated fuel delivery system for the combustors of turbomachinery |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1423363A (en) * | 1972-06-21 | 1976-02-04 | Lucas Industries Ltd | Fuel control apparatus for gas turbine engine reheat systems |
GB1456976A (en) * | 1973-03-13 | 1976-12-01 | Lucas Industries Ltd | Fuel control system for a gas turbine engine reheat system |
GB2014758B (en) * | 1978-02-17 | 1982-07-14 | Lucas Industries Ltd | Fuel control for a gas turbine engine reheat system |
-
1983
- 1983-08-01 GB GB08320649A patent/GB2125110A/en not_active Withdrawn
- 1983-08-01 DE DE19833327740 patent/DE3327740A1/en not_active Withdrawn
- 1983-08-11 JP JP14790483A patent/JPS5946327A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
DE3327740A1 (en) | 1984-02-16 |
GB2125110A (en) | 1984-02-29 |
JPS5946327A (en) | 1984-03-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |