GB123339A - A Rotary Internal Combustion Engine. - Google Patents
A Rotary Internal Combustion Engine.Info
- Publication number
- GB123339A GB123339A GB1298617A GB1298617A GB123339A GB 123339 A GB123339 A GB 123339A GB 1298617 A GB1298617 A GB 1298617A GB 1298617 A GB1298617 A GB 1298617A GB 123339 A GB123339 A GB 123339A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- combustion engine
- internal combustion
- 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
- F02C5/02—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
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
123,339. Hall, J. W. Feb. 16, 1918. Jet-wheels; cooling parts; working-fluid supply. -In an internal-combustion turbine wherein the combustion chamber is formed by a stator pocket A registering with a rotor pocket B, a pipe D supplies gas direct to the pocket B and by way of a groove C in the rotor to the pocket A, and after ignition by a plug. H the gas exhausts through a pipe F, subsequent rotor pockets E evacuating any unexhausted gas left in the pocket A. A number of sets of pockets may be co-axially arranged along the rotor and stator. Cooling air may be drawn through the rotor by forming the spokes as inclined fan blades.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1298617A GB123339A (en) | 1918-02-16 | 1918-02-16 | A Rotary Internal Combustion Engine. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1298617A GB123339A (en) | 1918-02-16 | 1918-02-16 | A Rotary Internal Combustion Engine. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB123339A true GB123339A (en) | 1919-02-17 |
Family
ID=32345785
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1298617A Expired GB123339A (en) | 1918-02-16 | 1918-02-16 | A Rotary Internal Combustion Engine. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB123339A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3769793A (en) * | 1972-08-02 | 1973-11-06 | F Wilson | Power plant |
-
1918
- 1918-02-16 GB GB1298617A patent/GB123339A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3769793A (en) * | 1972-08-02 | 1973-11-06 | F Wilson | Power plant |
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