GB632493A - Explosion internal combustion turbine plant and process for working the same - Google Patents
Explosion internal combustion turbine plant and process for working the sameInfo
- Publication number
- GB632493A GB632493A GB3543547A GB3543547A GB632493A GB 632493 A GB632493 A GB 632493A GB 3543547 A GB3543547 A GB 3543547A GB 3543547 A GB3543547 A GB 3543547A GB 632493 A GB632493 A GB 632493A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- gas
- air
- pair
- compressors
- 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
- F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
- F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants
Abstract
632,493. Gas turbine plant. FRANCIS, E. L. M. (Inffeld, K. L. M. von). Dec. 31, 1947, No. 35435. [Class 110(iii)] In a gas turbine plant, air and blast furnace gas compressed, respectively, in multi-stage axial-flow compressors 29, 30, 31 and 27, 28 are burnt in two pairs of valved explosion chambers 4, 5, 6, 7 and delivered to turbines 1, 2 which exhaust to a dual flow drum turbine 3. The exhaust from turbine 3 is used to generate steam supplied to a steam turbine 36. The combustion chambers of a pair delivers to a separate impulse turbine with two blade rings, e.g., 8, 9 on a common shaft. One pair of impulse turbines drives the gas compressors 27, 28 and the other pair, the air compressors 29-31. Scavenging air from the combustion chambers is admitted by valves 18-21 to the nozzle chamber of the turbine 3. For starting, the pipe connections of the gas pump 28 are altered to permit it to operate as an air pump for the chambers 4, 5 and the left-hand set is then run up to speed through a fluid coupling 34 by an electric motor 33. The gas turbine 3 and steam turbine-36 drive an electric generator 35.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3543547A GB632493A (en) | 1947-12-31 | 1947-12-31 | Explosion internal combustion turbine plant and process for working the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3543547A GB632493A (en) | 1947-12-31 | 1947-12-31 | Explosion internal combustion turbine plant and process for working the same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB632493A true GB632493A (en) | 1949-11-28 |
Family
ID=10377686
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3543547A Expired GB632493A (en) | 1947-12-31 | 1947-12-31 | Explosion internal combustion turbine plant and process for working the same |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB632493A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3241314A (en) * | 1962-08-02 | 1966-03-22 | Bristol Siddeley Engines Ltd | Gas turbine power plant |
-
1947
- 1947-12-31 GB GB3543547A patent/GB632493A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3241314A (en) * | 1962-08-02 | 1966-03-22 | Bristol Siddeley Engines Ltd | Gas turbine power plant |
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