GB347245A - Improvements in or relating to gas turbines - Google Patents
Improvements in or relating to gas turbinesInfo
- Publication number
- GB347245A GB347245A GB3948429A GB3948429A GB347245A GB 347245 A GB347245 A GB 347245A GB 3948429 A GB3948429 A GB 3948429A GB 3948429 A GB3948429 A GB 3948429A GB 347245 A GB347245 A GB 347245A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbines
- pressure
- chamber
- gas turbines
- ignition
- 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
347,245. Gas turbines. MARGONI, C., 22, Via Roma, Trieste, Italy. Dec. 24, 1929, No. 39484. [Class 110 (iii).] The combustion chambers 9, 10 of a gas turbine are opened automatically to a pressure chamber 5 when ignition occurs by valves 15, 16 actuated by pistons 27, 28. Gases remaining in the chambers 9, 10 after discharge are passed by automatically operated valves 19, 20 to an exhaust 18, and may be used in the low pressure turbine 3. The turbines 2, 3, arranged on separate shafts 4, 41, have duplicate sets of blades so that they may be reversed. They are controlled by ported valveplates 38. If the pressure in the chamber 5 becomes excessive, a pressure-responsive device 45 interrupts the ignition. Turbines 8 driving auxiliaries may be supplied from the chamber 5.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3948429A GB347245A (en) | 1929-12-24 | 1929-12-24 | Improvements in or relating to gas turbines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3948429A GB347245A (en) | 1929-12-24 | 1929-12-24 | Improvements in or relating to gas turbines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB347245A true GB347245A (en) | 1931-04-24 |
Family
ID=10409797
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3948429A Expired GB347245A (en) | 1929-12-24 | 1929-12-24 | Improvements in or relating to gas turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB347245A (en) |
-
1929
- 1929-12-24 GB GB3948429A patent/GB347245A/en not_active Expired
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