GB680667A - Method of regulating gas turbine plants - Google Patents
Method of regulating gas turbine plantsInfo
- Publication number
- GB680667A GB680667A GB10973/50A GB1097350A GB680667A GB 680667 A GB680667 A GB 680667A GB 10973/50 A GB10973/50 A GB 10973/50A GB 1097350 A GB1097350 A GB 1097350A GB 680667 A GB680667 A GB 680667A
- Authority
- GB
- United Kingdom
- Prior art keywords
- point
- circuit
- plant
- turbine
- returned
- 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
- 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
- F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Feeding And Controlling Fuel (AREA)
Abstract
680,667. Gas turbine plant. MASCHINENFABRIK OERLIKON. May 3, 1950 [May 16, 1949], No. 10973/50. Class 110(iii) In a gas turbine plant, air from the working cycle of the plant is used to transmit the impulses from a speed governor driven by the turbine to a valve controlling the fuel supply. In the plant shown air compressed in a compressor 1 is heated in a heat exchanger 2 by the exhaust gases from the turbine 4 and then fed to a combustion chamber 3 supplying the turbine 4. The fuel supply to the combustion chamber 3 is controlled by altering the pressure above the level of the fuel in the chamber 8. For this purpose, the chamber 8 is connected at point 14 to a conduit 15 through which control air is taken from the working fluid circuit at point 12 and returned at point 13. The point 14 lies between a fixed orifice 10 and a valve 7 operated direct by a speed governor 6. The control air may be discharged to atmosphere instead of being returned to the circuit. A plurality of control air streams branched off from the circuit at various points and returned to the circuit at a point of lower pressure may be employed.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH680667X | 1949-05-16 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB680667A true GB680667A (en) | 1952-10-08 |
Family
ID=4528444
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB10973/50A Expired GB680667A (en) | 1949-05-16 | 1951-05-03 | Method of regulating gas turbine plants |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB680667A (en) |
-
1951
- 1951-05-03 GB GB10973/50A patent/GB680667A/en not_active Expired
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