GB730383A - Improvements in or relating to gas turbines - Google Patents
Improvements in or relating to gas turbinesInfo
- Publication number
- GB730383A GB730383A GB330752A GB330752A GB730383A GB 730383 A GB730383 A GB 730383A GB 330752 A GB330752 A GB 330752A GB 330752 A GB330752 A GB 330752A GB 730383 A GB730383 A GB 730383A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rings
- ports
- rotor
- feb
- stator
- 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)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
Abstract
730,383. Gas turbine plant. McCARTY, M. J. Feb. 6, 1953 [Feb. 7, 1952], No. 3307/52. Class 110 (3). An intermittent combustion gas turbine engine comprises four concentric rings 2, 3, 4, 5 of which the rings 4, 5 form the stator and the rings 2, 3 the rotor. When the rings 2, 3 rotate air is drawn into the spaces 8a formed between the rings 2, 5 through ports 7 in a plate joining the stator rings. Further rotation of rings 2, 3 causes this gas to be compressed in the space 8b from which it is discharged through wedge-shaped ports 9 controlled by sliding valves 6 into the combustion chambers 12 formed in the outer rotor ring 3. When the valves 6 are fully closed by rotation of the ring 2, fuel is injected at 11 and ignited by sparking plugs at the points 10. The combustion gases leaving the combustion chambers 12 inpinge on the fins 14 and drive the rotor in the anti-clockwise direction and are exhausted through ports 13.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB330752A GB730383A (en) | 1952-02-07 | 1952-02-07 | Improvements in or relating to gas turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB330752A GB730383A (en) | 1952-02-07 | 1952-02-07 | Improvements in or relating to gas turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB730383A true GB730383A (en) | 1955-05-25 |
Family
ID=9755845
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB330752A Expired GB730383A (en) | 1952-02-07 | 1952-02-07 | Improvements in or relating to gas turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB730383A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2006030255A1 (en) * | 2004-09-16 | 2006-03-23 | Antioco Lampis | Four-stroke endothermic engine with rotating drum |
CN112211724A (en) * | 2020-10-14 | 2021-01-12 | 赵呈印 | Engine and aircraft |
-
1952
- 1952-02-07 GB GB330752A patent/GB730383A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2006030255A1 (en) * | 2004-09-16 | 2006-03-23 | Antioco Lampis | Four-stroke endothermic engine with rotating drum |
CN112211724A (en) * | 2020-10-14 | 2021-01-12 | 赵呈印 | Engine and aircraft |
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