GB174179A - Improvements in or relating to internal combustion turbines - Google Patents
Improvements in or relating to internal combustion turbinesInfo
- Publication number
- GB174179A GB174179A GB2948620A GB2948620A GB174179A GB 174179 A GB174179 A GB 174179A GB 2948620 A GB2948620 A GB 2948620A GB 2948620 A GB2948620 A GB 2948620A GB 174179 A GB174179 A GB 174179A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- relating
- internal combustion
- nozzles
- secured
- 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)
- Supercharger (AREA)
Abstract
174,179. Garland, J. Oct. 19, 1920. Working-fluid supply. - In an internal-combustion turbine, compressed air for scavenging and charging the stationary combustion chambers 5 is supplied periodically through ports 9 in a disc secured to the turbine shaft 2. Fuel is injected through nozzles 10 controlled by camoperated valves 11, and after ignition by an electrically-heated coil 13 in a recess 14 the gases are delivered to the turbine nozzles 15 which are periodically uncovered by a ported disc 17 secured to the shaft.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2948620A GB174179A (en) | 1920-10-19 | 1920-10-19 | Improvements in or relating to internal combustion turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2948620A GB174179A (en) | 1920-10-19 | 1920-10-19 | Improvements in or relating to internal combustion turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB174179A true GB174179A (en) | 1922-01-19 |
Family
ID=10292296
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2948620A Expired GB174179A (en) | 1920-10-19 | 1920-10-19 | Improvements in or relating to internal combustion turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB174179A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2485813A (en) * | 1945-04-30 | 1949-10-25 | Bert G Carison | Compressor-turbine engine |
US2542628A (en) * | 1946-10-25 | 1951-02-20 | Elbert E Christopher | Turbojet propulsion apparatus with separate combustion discharge jets |
US2557198A (en) * | 1947-05-21 | 1951-06-19 | American Locomotive Co | Gas turbine |
US2620122A (en) * | 1945-10-09 | 1952-12-02 | Herman H Curry | Combination propeller and diffuser inlet assembly |
-
1920
- 1920-10-19 GB GB2948620A patent/GB174179A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2485813A (en) * | 1945-04-30 | 1949-10-25 | Bert G Carison | Compressor-turbine engine |
US2620122A (en) * | 1945-10-09 | 1952-12-02 | Herman H Curry | Combination propeller and diffuser inlet assembly |
US2542628A (en) * | 1946-10-25 | 1951-02-20 | Elbert E Christopher | Turbojet propulsion apparatus with separate combustion discharge jets |
US2557198A (en) * | 1947-05-21 | 1951-06-19 | American Locomotive Co | Gas turbine |
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