GB2556011B - Equipment for gas turbine output increasing and efficiency improvement - Google Patents
Equipment for gas turbine output increasing and efficiency improvement Download PDFInfo
- Publication number
- GB2556011B GB2556011B GB1803289.6A GB201803289A GB2556011B GB 2556011 B GB2556011 B GB 2556011B GB 201803289 A GB201803289 A GB 201803289A GB 2556011 B GB2556011 B GB 2556011B
- Authority
- GB
- United Kingdom
- Prior art keywords
- equipment
- gas turbine
- efficiency improvement
- turbine output
- output increasing
- 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.)
- Active
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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
-
- C—CHEMISTRY; METALLURGY
- C07—ORGANIC CHEMISTRY
- C07D—HETEROCYCLIC COMPOUNDS
- C07D498/00—Heterocyclic compounds containing in the condensed system at least one hetero ring having nitrogen and oxygen atoms as the only ring hetero atoms
- C07D498/02—Heterocyclic compounds containing in the condensed system at least one hetero ring having nitrogen and oxygen atoms as the only ring hetero atoms in which the condensed system contains two hetero rings
- C07D498/04—Ortho-condensed systems
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
-
- 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
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/CZ2015/000099 WO2017036431A1 (en) | 2015-08-31 | 2015-08-31 | Equipment for gas turbine output increasing and efficiency improvement |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201803289D0 GB201803289D0 (en) | 2018-04-11 |
GB2556011A GB2556011A (en) | 2018-05-16 |
GB2556011B true GB2556011B (en) | 2021-02-24 |
Family
ID=54251267
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1803289.6A Active GB2556011B (en) | 2015-08-31 | 2015-08-31 | Equipment for gas turbine output increasing and efficiency improvement |
Country Status (2)
Country | Link |
---|---|
GB (1) | GB2556011B (en) |
WO (1) | WO2017036431A1 (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2592749A (en) * | 1947-01-16 | 1952-04-15 | Rateau Soc | Gas turbine engine associated with a gas producer under pressure |
US4058974A (en) * | 1975-05-14 | 1977-11-22 | Bbc Brown Boveri & Company Limited | Combined gas/steam power plant with pressurized-gas generator |
US4729217A (en) * | 1984-01-31 | 1988-03-08 | Bbc Brown, Boveri & Company, Limited | Combined gas/steam power station plant |
GB2229733A (en) * | 1989-03-24 | 1990-10-03 | Gen Electric | Hydrocarbon combustion apparatus and method |
WO1999014473A1 (en) * | 1997-09-12 | 1999-03-25 | Texaco Development Corporation | Synthesis gas expander located immediately upstream of combustion turbine |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US586688A (en) | 1897-07-20 | Pump for acids or other liquids | ||
US5347806A (en) | 1993-04-23 | 1994-09-20 | Cascaded Advanced Turbine Limited Partnership | Cascaded advanced high efficiency multi-shaft reheat turbine with intercooling and recuperation |
US6644015B2 (en) | 2001-10-29 | 2003-11-11 | Hmx, Inc. | Turbojet with precompressor injected oxidizer |
-
2015
- 2015-08-31 WO PCT/CZ2015/000099 patent/WO2017036431A1/en active Application Filing
- 2015-08-31 GB GB1803289.6A patent/GB2556011B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2592749A (en) * | 1947-01-16 | 1952-04-15 | Rateau Soc | Gas turbine engine associated with a gas producer under pressure |
US4058974A (en) * | 1975-05-14 | 1977-11-22 | Bbc Brown Boveri & Company Limited | Combined gas/steam power plant with pressurized-gas generator |
US4729217A (en) * | 1984-01-31 | 1988-03-08 | Bbc Brown, Boveri & Company, Limited | Combined gas/steam power station plant |
GB2229733A (en) * | 1989-03-24 | 1990-10-03 | Gen Electric | Hydrocarbon combustion apparatus and method |
WO1999014473A1 (en) * | 1997-09-12 | 1999-03-25 | Texaco Development Corporation | Synthesis gas expander located immediately upstream of combustion turbine |
Also Published As
Publication number | Publication date |
---|---|
WO2017036431A1 (en) | 2017-03-09 |
GB201803289D0 (en) | 2018-04-11 |
GB2556011A (en) | 2018-05-16 |
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