GB785192A - Multi-shaft gas turbine plants - Google Patents
Multi-shaft gas turbine plantsInfo
- Publication number
- GB785192A GB785192A GB9476/56A GB947656A GB785192A GB 785192 A GB785192 A GB 785192A GB 9476/56 A GB9476/56 A GB 9476/56A GB 947656 A GB947656 A GB 947656A GB 785192 A GB785192 A GB 785192A
- Authority
- GB
- United Kingdom
- Prior art keywords
- compressor
- turbine
- gas turbine
- fuel
- plant
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/36—Open cycles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
785,192. Gas turbine plant. SULZER FRERES SOC. ANON, March 27, 1956 [April 5, 1955], No. 9476/56. Class 110 (3). In a gas turbine plant comprising a high-pressure turbine 1 supplying useful output connected in series with a low-pressure turbine 4 driving an axial flow compressor 6 which discharges through an exhaust gas heat exchanger 8 to a combustion chamber 9 feeding the turbine 1, the output of the plant is controlled by adjusting together the fuel supply and the angle of incidence of at least some of the guide blades of the compressor according to a predetermined function. The guide blades of at least the initial stages of the compressor 6 are adjustable by a device 12 acting through a mechanism 13. Simultaneously the fuel supply is adjusted through an impulse pipe or other connection 14. The fuel may be liquid, solid or gaseous. If a gaseous fuel is supplied by a compressor driven by the turbine 4, this compressor should also be provided with adjustable guide vanes. A number of turbines may be arranged in series some of which may supply useful power and the remainder arranged to drive compressors. These turbines may be arranged on the shafts 3, 5 or on independent shafts.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH785192X | 1955-04-05 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB785192A true GB785192A (en) | 1957-10-23 |
Family
ID=4536529
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9476/56A Expired GB785192A (en) | 1955-04-05 | 1956-03-27 | Multi-shaft gas turbine plants |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB785192A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1167597B (en) * | 1959-03-17 | 1964-04-09 | Bendix Corp | Control device for an engine, in particular for gas turbine jet engines |
-
1956
- 1956-03-27 GB GB9476/56A patent/GB785192A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1167597B (en) * | 1959-03-17 | 1964-04-09 | Bendix Corp | Control device for an engine, in particular for gas turbine jet engines |
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