GB142959A - Internal combustion turbine - Google Patents
Internal combustion turbineInfo
- Publication number
- GB142959A GB142959A GB519319A GB519319A GB142959A GB 142959 A GB142959 A GB 142959A GB 519319 A GB519319 A GB 519319A GB 519319 A GB519319 A GB 519319A GB 142959 A GB142959 A GB 142959A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- shaft
- combustion
- compressors
- eccentric
- 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
142,959. Nicholls, R. E. March 3, 1919. Working - fluid supply; arrangement of bearings.-In an internal - combustion turbine, the charge is compressed by three compressors J past valves K<2> and pipes L into three valved combustion chambers A. The discharge valve a<3> of each combustion chamber is periodically opened by an eccentric 11<4> on the turbine shaft 11<7> to deliver the ignited charge to the nozzles F and the turbine F<2>. A spring-loaded sleeve valve a<4> effects a rapid release of the gases on starting. The compressor pistons K are reciprocated by a rotary cam I on the shaft H<8>, which may be connected directly to the shaft H<7> or geared therewith so as to rotate at twice the turbine speed, giving two explosions in each combustion chamber for one revolution of the turbine. The bearing H<1> is arranged outside the casing, and a diaphragm H<6> affords a thrust bearing for the shaft H'. The space between the diaphragm H<6> and a plug H<5> provides an oil bath for the eccentric H<4> or other gear working the valves. 'The number of combustion chambers and compressors may be varied.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB519319A GB142959A (en) | 1919-03-03 | 1919-03-03 | Internal combustion turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB519319A GB142959A (en) | 1919-03-03 | 1919-03-03 | Internal combustion turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB142959A true GB142959A (en) | 1920-05-20 |
Family
ID=9791451
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB519319A Expired GB142959A (en) | 1919-03-03 | 1919-03-03 | Internal combustion turbine |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB142959A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2551006A (en) * | 1948-05-19 | 1951-05-01 | Waverly V Johnson | Turbine type internal-combustion engine |
| US2687613A (en) * | 1950-04-19 | 1954-08-31 | Craigon Adam | Gas turbine power plant |
| US2856753A (en) * | 1955-04-19 | 1958-10-21 | Herzog Richard | Internal-combustion turbine engine |
-
1919
- 1919-03-03 GB GB519319A patent/GB142959A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2551006A (en) * | 1948-05-19 | 1951-05-01 | Waverly V Johnson | Turbine type internal-combustion engine |
| US2687613A (en) * | 1950-04-19 | 1954-08-31 | Craigon Adam | Gas turbine power plant |
| US2856753A (en) * | 1955-04-19 | 1958-10-21 | Herzog Richard | Internal-combustion turbine engine |
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