GB203828A - Combustion turbine combination specially for driving vehicles such as motor cars and the like - Google Patents
Combustion turbine combination specially for driving vehicles such as motor cars and the likeInfo
- Publication number
- GB203828A GB203828A GB1821722A GB1821722A GB203828A GB 203828 A GB203828 A GB 203828A GB 1821722 A GB1821722 A GB 1821722A GB 1821722 A GB1821722 A GB 1821722A GB 203828 A GB203828 A GB 203828A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wheel
- turbine
- piston
- combination
- chamber
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K15/00—Adaptations of plants for special use
- F01K15/02—Adaptations of plants for special use for driving vehicles, e.g. locomotives
- F01K15/025—Adaptations of plants for special use for driving vehicles, e.g. locomotives the vehicle being a steam locomotive
Abstract
203,828. Fries, G., and Schneider, H. July 3, 1922. No Patent granted (Scaling fee not paid). Working-fluid supply; driving and transmitting mechanism, special applications of. - Relates to an internal-combustion turbine combination comprising two turbines connected to one another by a differential gear through the driven member of which power is transmitted. Fig. 2 shows one-half of the combination. The carrier b of the planet wheel c is furnished with a helically - toothed wheel d which drives an air compressor of the axially-sliding abutment type through a similar wheel e and spur wheels. The compressed air passes by a pipe m into a distributor comprising a cylinder o having spaced slots p and rotating in a cylinder q. The compressed air passes by pipes r to two valves s, each portion being then mixed with gaseous fuel and passed to an explosion chamber t having one end formed with a crown of guide vanes leading to the turbine wheel u. Between the guide vanes and the turbine wheel is inserted a disc valve w, with openings corresponding with the guide-vane openings, controlled by a piston 1 subjected to the pressure of the explosive chamber and the pressure of a spring. On igition of the gases the piston is driven up, causing the disc w to turn and allow the gases to flow across the turbine wheel. As the pressure falls the spring returns the piston to its lowest position. To use one turbine only of the combination, the bevel wheel 5 is stopped by means of a brake 7, 8. The number of revolutions of the carrier c is thereby reduced by one-half and the speed of the compressor correspondingly reduced. The explosion chamber is cooled by a cone 10 filled with water and by steam or water injected into the chamber by way of a valve 11.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1821722A GB203828A (en) | 1922-07-03 | 1922-07-03 | Combustion turbine combination specially for driving vehicles such as motor cars and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1821722A GB203828A (en) | 1922-07-03 | 1922-07-03 | Combustion turbine combination specially for driving vehicles such as motor cars and the like |
Publications (1)
Publication Number | Publication Date |
---|---|
GB203828A true GB203828A (en) | 1923-09-20 |
Family
ID=10108652
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1821722A Expired GB203828A (en) | 1922-07-03 | 1922-07-03 | Combustion turbine combination specially for driving vehicles such as motor cars and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB203828A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2443186A (en) * | 1944-01-03 | 1948-06-15 | Foulks Edwin David | Jet propulsion fuel feeding and exhaust control device |
US2583872A (en) * | 1947-08-02 | 1952-01-29 | United Aircraft Corp | Gas turbine power plant, including planetary gearing between a compressor, turbine, and power consumer |
-
1922
- 1922-07-03 GB GB1821722A patent/GB203828A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2443186A (en) * | 1944-01-03 | 1948-06-15 | Foulks Edwin David | Jet propulsion fuel feeding and exhaust control device |
US2583872A (en) * | 1947-08-02 | 1952-01-29 | United Aircraft Corp | Gas turbine power plant, including planetary gearing between a compressor, turbine, and power consumer |
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