GB533330A - Generating combustion products for power purposes - Google Patents
Generating combustion products for power purposesInfo
- Publication number
- GB533330A GB533330A GB2891239A GB2891239A GB533330A GB 533330 A GB533330 A GB 533330A GB 2891239 A GB2891239 A GB 2891239A GB 2891239 A GB2891239 A GB 2891239A GB 533330 A GB533330 A GB 533330A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chambers
- combustion products
- chamber
- generating combustion
- turbines
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
533,330. Gas turbines. HALLOWELL, E. Oct. 28, 1939, No. 28912. [Class 110 (iii)] A column of gas in a tapering conduit 12, 16, 13 between two explosion chambers 10, 11 is caused to oscillate by periodic explosions in the chambers and the maximum velocities exceed that of sound. Gases pass by conduits 17, 18 to turbines 19, 20 and fresh air enters by an unvalved port 23. Fuel is admitted to chambers 10, 11 by pipes 21, 22. An auxiliary explosion chamber for starting the plant is arranged at the side of chamber 10 and opens into it by a spring-loaded valve which is normally closed. A pair of chambers oppositely and tangentially arranged in respect of the passages 12, 13 may be used in place of the single chambers 10, 11.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2891239A GB533330A (en) | 1939-10-28 | 1939-10-28 | Generating combustion products for power purposes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2891239A GB533330A (en) | 1939-10-28 | 1939-10-28 | Generating combustion products for power purposes |
Publications (1)
Publication Number | Publication Date |
---|---|
GB533330A true GB533330A (en) | 1941-02-11 |
Family
ID=10283192
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2891239A Expired GB533330A (en) | 1939-10-28 | 1939-10-28 | Generating combustion products for power purposes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB533330A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2796735A (en) * | 1956-08-20 | 1957-06-25 | Jr Albert G Bodine | Acoustic jet engine with flow deflection fluid pumping characteristics |
US2838102A (en) * | 1954-08-28 | 1958-06-10 | Junkers & Co | Pulse jet burner system |
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 |
-
1939
- 1939-10-28 GB GB2891239A patent/GB533330A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2838102A (en) * | 1954-08-28 | 1958-06-10 | Junkers & Co | Pulse jet burner system |
US2796735A (en) * | 1956-08-20 | 1957-06-25 | Jr Albert G Bodine | Acoustic jet engine with flow deflection fluid pumping characteristics |
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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