GB701175A - Improvements in or relating to a gas turbine plant - Google Patents
Improvements in or relating to a gas turbine plantInfo
- Publication number
- GB701175A GB701175A GB19294/51A GB1929451A GB701175A GB 701175 A GB701175 A GB 701175A GB 19294/51 A GB19294/51 A GB 19294/51A GB 1929451 A GB1929451 A GB 1929451A GB 701175 A GB701175 A GB 701175A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- combustion chamber
- return valve
- fuel
- pipe
- 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
- F02C5/10—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Abstract
701,175. Gas turbine plant. MASCHINENFABRIK AUGSBURG-NURNBERG AKT.-GES. Aug. 15, 1951 [Aug. 18, 1950], No. 19294/51: Class 110 (3). [Also in Groups XII and XXIX] A gas turbine plant comprises an oscillating column combustion chamber and a turbine arranged in the feed pipe of the combustion chamber so as to be, driven by the air or mixture drawn in. The combustion chamber 1 is supplied with fuel by a pipe 7 which is ignited by the igniter 10. This causes a pressure wave to travel towards the open end of the combustion chamber. A flow is prevented in the opposite direction by the non-return valve 3. At the open end of the combustion chamber, to which a diffuser 9 is preferably fitted, the advancing pressure wave is converted into a returning negative pressure wave which travelling back down the tube causes the intake of fresh air through the valve 3 and the ignition of the new mixture. The fuel may be supplied continuously or intermittently, and may be injected, by means of the pressure changes in the combustion chamber acting through, a pipe 5 and non-return valve 6 or the fuel in a pressure-tight tank 4. The fuel is injected through non-return valve 8 and pipe 7. The non-return valve 3 is formed from a number of tubes 12 which lead to an annular chamber and open transversely of the flow. The turbine 2 is connected in front of the non-return valve 3. In a modification a heat exchanger heated by the combustion gases is placed between the turbine 2 and non-return valve 3. In another modification, the heat exchanger is arranged before the turbine. In a further modification, a compressor driven by the turbine may supply air to the inlet of the combustion chamber through a heat exchanger heated by the combustion gases. The plant is suitable for the combustion of all solid pulverulent fuels as well as liquid and gaseous fuels when using light volatile liquid or gaseous fuels, the injection of the fuels may take place in a carburetter or a gas-air mixer in front of the turbine. Specification 368,564, [Group XXXIIII], is referred to.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE701175X | 1950-08-18 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB701175A true GB701175A (en) | 1953-12-16 |
Family
ID=6610576
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB19294/51A Expired GB701175A (en) | 1950-08-18 | 1951-08-15 | Improvements in or relating to a gas turbine plant |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB701175A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU214950U1 (en) * | 2022-08-08 | 2022-11-22 | ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ Военная академия Ракетных войск стратегического назначения имени Петра Великого МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ | GAS TURBINE ENGINE WITH EXTERNAL PULSE COMBUSTION CHAMBER AND FREE TURBINE |
-
1951
- 1951-08-15 GB GB19294/51A patent/GB701175A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU214950U1 (en) * | 2022-08-08 | 2022-11-22 | ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ Военная академия Ракетных войск стратегического назначения имени Петра Великого МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ | GAS TURBINE ENGINE WITH EXTERNAL PULSE COMBUSTION CHAMBER AND FREE TURBINE |
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