GB2356671B - Gas turbine engine - Google Patents
Gas turbine engineInfo
- Publication number
- GB2356671B GB2356671B GB9927957A GB9927957A GB2356671B GB 2356671 B GB2356671 B GB 2356671B GB 9927957 A GB9927957 A GB 9927957A GB 9927957 A GB9927957 A GB 9927957A GB 2356671 B GB2356671 B GB 2356671B
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- turbine engine
- engine
- gas
- turbine
- 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 - Fee Related
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
- 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
- F02C7/12—Cooling of plants
-
- 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
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
- F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9927957A GB2356671B (en) | 1999-11-27 | 1999-11-27 | Gas turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9927957A GB2356671B (en) | 1999-11-27 | 1999-11-27 | Gas turbine engine |
Publications (3)
Publication Number | Publication Date |
---|---|
GB9927957D0 GB9927957D0 (en) | 2000-01-26 |
GB2356671A GB2356671A (en) | 2001-05-30 |
GB2356671B true GB2356671B (en) | 2003-10-29 |
Family
ID=10865188
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9927957A Expired - Fee Related GB2356671B (en) | 1999-11-27 | 1999-11-27 | Gas turbine engine |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2356671B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2587021A1 (en) * | 2011-10-24 | 2013-05-01 | Siemens Aktiengesellschaft | Gas turbine and method for guiding compressed fluid in a gas turbine |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2064008A (en) * | 1979-11-07 | 1981-06-10 | Alsthom Atlantique | A Cooling System for a Gas Turbine Engine |
GB2260578A (en) * | 1991-09-25 | 1993-04-21 | Mtu Muenchen Gmbh | Heat transfer between fuel and air in supersonic jet engine |
US5255505A (en) * | 1992-02-21 | 1993-10-26 | Westinghouse Electric Corp. | System for capturing heat transferred from compressed cooling air in a gas turbine |
WO1997038219A1 (en) * | 1996-04-04 | 1997-10-16 | Westinghouse Electric Corporation | Closed-loop air cooling system for a turbine engine |
-
1999
- 1999-11-27 GB GB9927957A patent/GB2356671B/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2064008A (en) * | 1979-11-07 | 1981-06-10 | Alsthom Atlantique | A Cooling System for a Gas Turbine Engine |
GB2260578A (en) * | 1991-09-25 | 1993-04-21 | Mtu Muenchen Gmbh | Heat transfer between fuel and air in supersonic jet engine |
US5255505A (en) * | 1992-02-21 | 1993-10-26 | Westinghouse Electric Corp. | System for capturing heat transferred from compressed cooling air in a gas turbine |
WO1997038219A1 (en) * | 1996-04-04 | 1997-10-16 | Westinghouse Electric Corporation | Closed-loop air cooling system for a turbine engine |
Also Published As
Publication number | Publication date |
---|---|
GB9927957D0 (en) | 2000-01-26 |
GB2356671A (en) | 2001-05-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20051127 |