GB191408707A - Improvements in Direct Acting Internal Combustion Turbines. - Google Patents
Improvements in Direct Acting Internal Combustion Turbines.Info
- Publication number
- GB191408707A GB191408707A GB191408707DA GB191408707A GB 191408707 A GB191408707 A GB 191408707A GB 191408707D A GB191408707D A GB 191408707DA GB 191408707 A GB191408707 A GB 191408707A
- Authority
- GB
- United Kingdom
- Prior art keywords
- passages
- blades
- stator
- rotor
- combustion turbines
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Sliding Valves (AREA)
Abstract
8707. Heilmann, J. J. April 17, 1913, [Convention date]. Working-fluid supply. -Relates to multipleexpansion modifications of the radial-flow internal-combustion turbines described in Specification 4518/11. The compressed gases are admitted by a distributing-valve 1 and rotating sleeve 21 to explosion chambers formed by passages 8 in the stator member 2, passages 9 in the rotor member 3, and reaction pockets 10 in the concentric stator member 4. Ignition is effected by plugs 11, and the exhaust gases expand through blades 13 in the stator member 4, blades 15 in the rotor member 5, and finally through stator blades 17 into discharge chambers 18 acting as silencers. The rotor members are connected by a common end disk to the central shaft. A number of turbines having successively staggered working passages may be arranged on the same shaft.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE191408707X | 1913-04-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB191408707A true GB191408707A (en) | 1914-11-05 |
Family
ID=32513723
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB191408707D Expired GB191408707A (en) | 1913-04-17 | 1914-04-06 | Improvements in Direct Acting Internal Combustion Turbines. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB191408707A (en) |
-
1914
- 1914-04-06 GB GB191408707D patent/GB191408707A/en not_active Expired
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