GB622053A - Improvements in or relating to gas turbine plant - Google Patents
Improvements in or relating to gas turbine plantInfo
- Publication number
- GB622053A GB622053A GB6386/47A GB638647A GB622053A GB 622053 A GB622053 A GB 622053A GB 6386/47 A GB6386/47 A GB 6386/47A GB 638647 A GB638647 A GB 638647A GB 622053 A GB622053 A GB 622053A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- useful power
- power turbine
- load
- gas turbine
- 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
622,053. Gas turbine plant. MASCHINENFABRIK OERLIKON. March 6, 1947, No. 6386. Convention date, April 15, 1946. Drawings to Specification. [Class 110(iii)] In a gas turbine plant for driving a vehicle in which the turbine driving the compressor is separate from the useful power turbine, the temperature of the working gas for the former turbine is variable independently of the speed and load conditions of the power turbine. On gradients, where an increased load is accompanied by a reduced speed of the useful power turbine, the load is taken by increasing the temperature at the compresser turbine inlet and thereby providing air at an increased pressure for the combustion chamber of the useful power turbine. The useful power turbine may be in series with the compresser turbine with reheating before the latter. Or, the two turbines and their combustion chambers may operate in parallel.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH622053X | 1946-04-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB622053A true GB622053A (en) | 1949-04-26 |
Family
ID=4524149
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB6386/47A Expired GB622053A (en) | 1946-04-15 | 1947-03-06 | Improvements in or relating to gas turbine plant |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB622053A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3054257A (en) * | 1953-03-10 | 1962-09-18 | Garrett Corp | Gas turbine power plant for vehicles |
| FR2099644A1 (en) * | 1970-07-28 | 1972-03-17 | Mitsui Shipbuilding Eng | |
| US3765170A (en) * | 1970-12-27 | 1973-10-16 | Toyota Motor Co Ltd | Composite gas turbine set |
-
1947
- 1947-03-06 GB GB6386/47A patent/GB622053A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3054257A (en) * | 1953-03-10 | 1962-09-18 | Garrett Corp | Gas turbine power plant for vehicles |
| FR2099644A1 (en) * | 1970-07-28 | 1972-03-17 | Mitsui Shipbuilding Eng | |
| US3765170A (en) * | 1970-12-27 | 1973-10-16 | Toyota Motor Co Ltd | Composite gas turbine set |
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