GB182939A - Internal combustion turbine - Google Patents
Internal combustion turbineInfo
- Publication number
- GB182939A GB182939A GB1085321A GB1085321A GB182939A GB 182939 A GB182939 A GB 182939A GB 1085321 A GB1085321 A GB 1085321A GB 1085321 A GB1085321 A GB 1085321A GB 182939 A GB182939 A GB 182939A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pipes
- pockets
- rotor
- explosions
- stator
- 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
- F02C5/06—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
182,939. Le Compagnon, A. April 13, 1921. Working-fluid supply; cooling parts.-Diametrically-o p p o s e d pockets a in the conical periphery of the rotor B, in which explosions are timed to take place simultaneously, are permanently connected by pipes to avoid unbalanced pressures due to asynchronous explosions. The pockets receive an explosive mixture from one of pipes 5, 5<1>, the explosion is effected when the prokets register with recesses 1, 1<1>, and expansion takes place as the pockets reach recesses 2, 3, 4 and 2<1>, 3<1>, 4<1>. Two circular spring-pressed members engage grooves on either side of the pockets in the rotor and the stator to prevent leakage. The engine is water-cooled through passages b, c in the rotor, and passages d, e in the stator, supplied through pipes h from the hollow rotating shaft. Explosive mixture is supplied to the admission pipes 5, 5 by pumps 10, 12 actuated from the rotor shaft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1085321A GB182939A (en) | 1921-04-13 | 1921-04-13 | Internal combustion turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1085321A GB182939A (en) | 1921-04-13 | 1921-04-13 | Internal combustion turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB182939A true GB182939A (en) | 1922-07-13 |
Family
ID=9975514
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1085321A Expired GB182939A (en) | 1921-04-13 | 1921-04-13 | Internal combustion turbine |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB182939A (en) |
-
1921
- 1921-04-13 GB GB1085321A patent/GB182939A/en not_active Expired
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