GB464874A - Improvements in or connected with internal combustion turbines - Google Patents
Improvements in or connected with internal combustion turbinesInfo
- Publication number
- GB464874A GB464874A GB3508835A GB3508835A GB464874A GB 464874 A GB464874 A GB 464874A GB 3508835 A GB3508835 A GB 3508835A GB 3508835 A GB3508835 A GB 3508835A GB 464874 A GB464874 A GB 464874A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- piston
- admitted
- cam
- passage
- 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)
- Diaphragms For Cameras (AREA)
Abstract
464,874. Elastic - fluid turbines. RAINIER, J. W. Dec. 18, 1935, No. 35088. [Class 110 (iii)] A turbine rotor 24 on a shaft 6 has helical blades 25, of constant, or varying pitch contained within a shrouding 26. Gas from two or more carburetters is admitted to compression cylinders 1a through inlets 1e, compressed in each by a piston 2, fired by a plug 7. and admitted to an inlet chamber 12 to the turbine by way of a passage 11 in a cam-operated valve 10. A cam 5 controls the movement of piston rods 3. In a modified arrangement the ignited gases are led to a piston extension of each valve 10 to force the valve upwards until the passage 11 opens to connect the compression cylinder and the chamber 12. Packing rings 27, 37, are provided upon the rotor. Cooling water from a pump enters the hollow shaft at 40 and passes to a collector 41. Further cooling spaces 9b and 43 are provided.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3508835A GB464874A (en) | 1935-12-18 | 1935-12-18 | Improvements in or connected with internal combustion turbines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3508835A GB464874A (en) | 1935-12-18 | 1935-12-18 | Improvements in or connected with internal combustion turbines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB464874A true GB464874A (en) | 1937-04-27 |
Family
ID=10373650
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3508835A Expired GB464874A (en) | 1935-12-18 | 1935-12-18 | Improvements in or connected with internal combustion turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB464874A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2355768A (en) * | 1999-11-01 | 2001-05-02 | Kofi Abaka Jackson | Turbine/compressor rotor with helical blade |
-
1935
- 1935-12-18 GB GB3508835A patent/GB464874A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2355768A (en) * | 1999-11-01 | 2001-05-02 | Kofi Abaka Jackson | Turbine/compressor rotor with helical blade |
| GB2355768B (en) * | 1999-11-01 | 2004-03-17 | Kofi Abaka Jackson | Compressor or turbine rotor having spirally curved blades |
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