GB277655A - Improvements in explosion turbines - Google Patents
Improvements in explosion turbinesInfo
- Publication number
- GB277655A GB277655A GB23754/27A GB2375427A GB277655A GB 277655 A GB277655 A GB 277655A GB 23754/27 A GB23754/27 A GB 23754/27A GB 2375427 A GB2375427 A GB 2375427A GB 277655 A GB277655 A GB 277655A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valves
- stator
- rotor
- opened
- 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
- F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
Abstract
277,655. Bernales, H. de. Sept. 14, 1926, [Convention date]. Working-fluid supply; cooling parts.-A gas turbine comprises a pocketed stator and a pocketed rotor; the stator pockets are provided with admission valves 12 which are opened when a rotor pocket reaches a corresponding stator pocket, the explosion taking place when the pockets are facing one another, and with exhaust and scavenging air valves 14, 13 which are opened when the rotor pocket has passed. The stator pocket next in front is then opened to the admission. The valves are actuated by cam discs 18, 19 on the rotor shaft. Compressors 29, 27 supply the mixture and scavenging air to manifolds 28<a>, 28, 26, 25 feeding the valve chambers. To prevent the compressed mixture opening the admission valves 12 there are provided valves 12<a> opened by projections 12<b> on the stems of the former valves. The rotor is cooled by water which passes through ports 7 in the side walls to a casing 8 whence it is withdrawn by a circulating pump 11. A thermo-siphon cooling arrangement is provided for the stator.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR277655X | 1926-09-14 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB277655A true GB277655A (en) | 1927-12-22 |
Family
ID=8886484
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB23754/27A Expired GB277655A (en) | 1926-09-14 | 1927-09-09 | Improvements in explosion turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB277655A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2325706A (en) * | 1997-05-28 | 1998-12-02 | Thomas Anthony Hollings | Intermittant combustion jet engine |
| CN105927289A (en) * | 2016-05-25 | 2016-09-07 | 中国科学院工程热物理研究所 | Device for naturally cooling stator cascade of gas turbine and manufacturing method thereof |
-
1927
- 1927-09-09 GB GB23754/27A patent/GB277655A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2325706A (en) * | 1997-05-28 | 1998-12-02 | Thomas Anthony Hollings | Intermittant combustion jet engine |
| CN105927289A (en) * | 2016-05-25 | 2016-09-07 | 中国科学院工程热物理研究所 | Device for naturally cooling stator cascade of gas turbine and manufacturing method thereof |
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