GB498683A - Improvements in and relating to internal combustion turbines - Google Patents
Improvements in and relating to internal combustion turbinesInfo
- Publication number
- GB498683A GB498683A GB1921937A GB1921937A GB498683A GB 498683 A GB498683 A GB 498683A GB 1921937 A GB1921937 A GB 1921937A GB 1921937 A GB1921937 A GB 1921937A GB 498683 A GB498683 A GB 498683A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- casing
- shaft
- bearings
- chambers
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
498,683. Elastic-fluid turbines. OPPENHEIM, H. July 10, 1937, No. 19219. [Class 110 (iii)] An internal-combustion turbine, having the rotor shaft bearings 45, 46, 47 disposed at the end walls of the casing 2, has the members 8, 17 driven from the shaft I controlling the inlet and exhaust ports of the combustion chambers 4 mounted on ball bearings 14, 15. The rotor 3 and the hollow blades 24, 25 are cooled by a stream of air drawn in through the pipe 33 under centrifugal action. A disc 50 which is attached to the shaft 1 and acts as an oil screen, is so constructed that a cooling current of air is drawn through the bearing 47 and across the labyrinthine packing 52. Chambers 37, 38 and 39 are provided to convey cooling fluid to the combustion chambers, exhaust manifold and the casing walls adjacent the rotor bearings respectively. The parts 12, 42 of the casing supporting the bear. ings are made of heat-conducting light metal. The combustible mixture is fired by heated filaments energized by the moving contact 18.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1921937A GB498683A (en) | 1937-07-10 | 1937-07-10 | Improvements in and relating to internal combustion turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1921937A GB498683A (en) | 1937-07-10 | 1937-07-10 | Improvements in and relating to internal combustion turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB498683A true GB498683A (en) | 1939-01-10 |
Family
ID=10125704
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1921937A Expired GB498683A (en) | 1937-07-10 | 1937-07-10 | Improvements in and relating to internal combustion turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB498683A (en) |
-
1937
- 1937-07-10 GB GB1921937A patent/GB498683A/en not_active Expired
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