GB651248A - Improvements in or relating to internal combustion engines - Google Patents
Improvements in or relating to internal combustion enginesInfo
- Publication number
- GB651248A GB651248A GB33399/48A GB3339948A GB651248A GB 651248 A GB651248 A GB 651248A GB 33399/48 A GB33399/48 A GB 33399/48A GB 3339948 A GB3339948 A GB 3339948A GB 651248 A GB651248 A GB 651248A
- Authority
- GB
- United Kingdom
- Prior art keywords
- casing
- dec
- exhaust
- plug
- pockets
- 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
- F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
- F02C5/04—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant the combustion chambers being formed at least partly in the turbine rotor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
651,248. Gas turbines. WALOSZEK, F. Dec. 29, 1948, Nos. 33399 and 33400. Convention dates, Dec. 31, 1947 and Dec. 23, 1948. [Class 110(iii)] A turbine rotor with pockets 2 rotates within a casing having an inlet 3 and an exhaust 4. Combustible mixture is compressed by a centrifugal pump on the turbine shaft and delivered to the rotor pockets 2 at 3. The mixture is fired by a sparking plug 5 and burns up to the exhaust 4. The casing from the plug 5 to the exhaust has a jacket 10 through which air is forced by a second pump. The plug 5 is needed only for starting. The tips of the rotor pockets may run close to the casing or may be separated from the casing over the region 5, 4 by a small distance which decreases towards 4.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR651248X | 1947-12-31 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB651248A true GB651248A (en) | 1951-03-14 |
Family
ID=9004494
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB33399/48A Expired GB651248A (en) | 1947-12-31 | 1948-12-29 | Improvements in or relating to internal combustion engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB651248A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2008029432A2 (en) * | 2006-09-04 | 2008-03-13 | Franco Saponara | Impact turbine apparatus with intermittent combustion |
-
1948
- 1948-12-29 GB GB33399/48A patent/GB651248A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2008029432A2 (en) * | 2006-09-04 | 2008-03-13 | Franco Saponara | Impact turbine apparatus with intermittent combustion |
| WO2008029432A3 (en) * | 2006-09-04 | 2008-05-22 | Franco Saponara | Impact turbine apparatus with intermittent combustion |
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