GB671539A - Improvements in a gas turbine plant operating on the open system, for delivering a large useful power of short duration - Google Patents
Improvements in a gas turbine plant operating on the open system, for delivering a large useful power of short durationInfo
- Publication number
- GB671539A GB671539A GB926/50A GB92650A GB671539A GB 671539 A GB671539 A GB 671539A GB 926/50 A GB926/50 A GB 926/50A GB 92650 A GB92650 A GB 92650A GB 671539 A GB671539 A GB 671539A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- valves
- combustion chamber
- compressor
- water
- 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
- 238000002485 combustion reaction Methods 0.000 abstract 5
- 239000007789 gas Substances 0.000 abstract 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract 5
- 239000000446 fuel Substances 0.000 abstract 2
- 239000007788 liquid Substances 0.000 abstract 2
- 239000000567 combustion gas Substances 0.000 abstract 1
- 239000003779 heat-resistant material Substances 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- 230000001105 regulatory effect Effects 0.000 abstract 1
- 239000004449 solid propellant Substances 0.000 abstract 1
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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/14—Gas-turbine plants having means for storing energy, e.g. for meeting peak loads
- F02C6/16—Gas-turbine plants having means for storing energy, e.g. for meeting peak loads for storing compressed air
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/16—Mechanical energy storage, e.g. flywheels or pressurised fluids
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
671,539. Gas turbine plant. SVENSKA TURBINFABRIKS AKTIEBOLAGET LJUNGSTROM. Jan. 13, 1950 [Jan. 19, 1949], No. 926/50. Class 110 (iii) An open circuit gas turbine plant comprising a turbine 15, Fig. 1, a combustion chamber 11 or recuperator and a compressor unit 2 separately driven independently of the turbine has one or more accumulators for storing air supplied by the compressor unit which is admitted to the turbine according to need. Each accumulator consists of a chamber 8 connected at its lower portion through a channel 10 with a body of water 9, the level of which is comparatively high as compared with the change of level of the water in the accumulator, and at its top with the compressor and turbine. The compressor unit 2 is driven by an electric motor 1 and during air charging periods the valves 4 and 6 are open and the valve 5 closed. When air is withdrawn from the accumulator, valves 5 and 6 are opened and valve 4 may be open or closed depending on whether the compressor unit 2 is in operation. Liquid fuel is supplied to the combustion chamber by a pump 12. Valves 5 and fuel supply valves 14 are controlled by a speed governor 18. In a modification, two accumulators are provided. The second accumulator is used to store combustible gas supplied by a compressor driven by an electric motor. In. another embodiment water is sprayed into the combustion chamber and the amount of water injected is controlled by the speed governor 18. In a further embodiment, Fig. 4, the combustion chamber 11 is replaced by a recuperator 27. The heat resistant material 28 of high heat capacity is heated by combustion gases from a combustion chamber 30 in which a liquid or solid fuel may be burnt. These gases leave the chamber 30 through a conduit 33. When the recuperator is supplying heat to the air from the compressor the valves 29 and 34 are closed and the valve 5 opened. The temperature of the gases supplied to the' turbine is controlled by a thermostat which actuates a valve 26 regulating the amount of water sprayed into the recuperator.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE671539X | 1949-01-19 | ||
SE281557X | 1949-01-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB671539A true GB671539A (en) | 1952-05-07 |
Family
ID=73543348
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB926/50A Expired GB671539A (en) | 1949-01-19 | 1950-01-13 | Improvements in a gas turbine plant operating on the open system, for delivering a large useful power of short duration |
Country Status (2)
Country | Link |
---|---|
CH (1) | CH281557A (en) |
GB (1) | GB671539A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2125377A1 (en) * | 1971-02-12 | 1972-09-29 | Gulf Oil Corp | |
GB2000229A (en) * | 1977-06-16 | 1979-01-04 | Lundberg R | Apparatus and method for multiplying the output of a generating unit |
GB2195402A (en) * | 1986-09-10 | 1988-04-07 | Kershaw H A | A method of power generation and it's use in a propulsion device |
WO2023197458A1 (en) * | 2022-04-12 | 2023-10-19 | 西安热工研究院有限公司 | Gas turbine system coupled with energy storage system and having adjustable compression flow, and control method |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE960137C (en) * | 1953-10-02 | 1957-03-14 | Wilhelm Siebrecht Dr Ing | Open constant pressure gas turbine system with pressure accumulator for peak load |
DE2810890A1 (en) * | 1978-03-13 | 1979-09-27 | Messerschmitt Boelkow Blohm | THERMAL STORAGE |
-
1950
- 1950-01-13 GB GB926/50A patent/GB671539A/en not_active Expired
- 1950-01-14 CH CH281557D patent/CH281557A/en unknown
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2125377A1 (en) * | 1971-02-12 | 1972-09-29 | Gulf Oil Corp | |
GB2000229A (en) * | 1977-06-16 | 1979-01-04 | Lundberg R | Apparatus and method for multiplying the output of a generating unit |
GB2000229B (en) * | 1977-06-16 | 1982-02-24 | Lundberg R | Apparatus and method for multiplying the output of a generating unit |
GB2195402A (en) * | 1986-09-10 | 1988-04-07 | Kershaw H A | A method of power generation and it's use in a propulsion device |
WO2023197458A1 (en) * | 2022-04-12 | 2023-10-19 | 西安热工研究院有限公司 | Gas turbine system coupled with energy storage system and having adjustable compression flow, and control method |
Also Published As
Publication number | Publication date |
---|---|
CH281557A (en) | 1952-03-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3956892A (en) | Fuel-air regulating system for hot gas engines | |
NO179023B (en) | Internal combustion engine with closed cycle | |
US2365616A (en) | Regulating apparatus for gas turbine plants | |
GB1151200A (en) | Reserve Power Gas Turbine-Generators and Methods of Operating same in "Spinning Reserve" | |
GB1487711A (en) | Thermal power plant | |
GB671539A (en) | Improvements in a gas turbine plant operating on the open system, for delivering a large useful power of short duration | |
US3171465A (en) | Furnace for intermittent combustion | |
GB772287A (en) | Power system incorporating a gas turbine | |
GB604114A (en) | Improvements in regenerative gas turbine plants | |
GB905663A (en) | Power plant including a gas turbine | |
GB492831A (en) | Improvements in gas turbine plants of the continuous combustion type | |
GB416463A (en) | Improvements in constant pressure gas turbine plant | |
GB749263A (en) | Improvements in or relating to a gas-turbine installation with an auxiliary or after-burning chamber | |
GB722230A (en) | Improvements in gas turbine plant | |
SE7315325L (en) | ||
GB651319A (en) | Improvements in or relating to gas turbine engine power plants | |
GB652048A (en) | Improvements relating to exhaust driven turbines on reciprocating internal combustion engines | |
GB366773A (en) | Improvements in or relating to gas turbine aggregates | |
GB1473542A (en) | Mobile power units | |
US2677062A (en) | Gas turbine power plant | |
GB612237A (en) | Improvements in or relating to gas turbine plants | |
GB858397A (en) | Improvements in or relating to turbines | |
GB488538A (en) | Means for regulating and starting thermal power plants | |
GB784220A (en) | Improved means for supplying sterilised gas under pressure | |
SU840422A1 (en) | Heat generating turbine operation mode control method |