GB1212511A - Improvements in power generating plant - Google Patents
Improvements in power generating plantInfo
- Publication number
- GB1212511A GB1212511A GB3494567A GB3494567A GB1212511A GB 1212511 A GB1212511 A GB 1212511A GB 3494567 A GB3494567 A GB 3494567A GB 3494567 A GB3494567 A GB 3494567A GB 1212511 A GB1212511 A GB 1212511A
- Authority
- GB
- United Kingdom
- Prior art keywords
- line
- combustion chamber
- air
- compressor
- chamber
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K21/00—Steam engine plants not otherwise provided for
- F01K21/04—Steam engine plants not otherwise provided for using mixtures of steam and gas; Plants generating or heating steam by bringing water or steam into direct contact with hot gas
- F01K21/047—Steam engine plants not otherwise provided for using mixtures of steam and gas; Plants generating or heating steam by bringing water or steam into direct contact with hot gas having at least one combustion gas turbine
-
- 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
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
- F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
-
- 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
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
- F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
- F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
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
1,212,511. Gas turbine plant. UNITED KINGDOM ATOMIC ENERGY AUTHORITY. April 22, 1968 [Jan.23, 1967; July 28, 1967], Nos.3409/67 and 34945/67. Heading F1G. In a gas turbine plant, air flowing through a low-pressure compressor 11a, 11b is cooled between the stages by demineralized water passing through a cooler 12, the water then effecting additional cooling of the air in coolers 13, 14 whilst further air compression is effected in compressors 7, 8. The air from compressor 7 passes to a combustion chamber 1 where it is burnt with fuel supplied through line 3 in substantially stoichiometric proportion. The preheated water is also injected into the combustion chamber 1 through line 4 in a manner described in Specification 1,212, 512 to cool the chamber walls and to solidify corrosive combustion products. The gas-steam mixture leaving the combustion chamber 1 drives a high-pressure turbine 5 connected to compressors 7, 8, and then passes through a reheat combustion chamber 17 to a lower pressure turbine 9 driving compressor 11a, 11b and an alternator 10. The reheat chamber 17 is supplied with fuel through line 3a and with compressed air tapped through line 18. The demineralized water may be additionally preheated by passing it through a boiler utilizing turbine exhaust heat. The plant includes an electric starter motor 16.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB340967 | 1967-01-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1212511A true GB1212511A (en) | 1970-11-18 |
Family
ID=9757792
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3494567A Expired GB1212511A (en) | 1967-01-23 | 1967-01-23 | Improvements in power generating plant |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1212511A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2230864A1 (en) * | 1973-05-22 | 1974-12-20 | Electricite De France | Fluid transfer system for gas turbine installation - compressor heat exchangers uses hot exhaust to heat injection fluid |
EP0076529A1 (en) * | 1981-09-18 | 1983-04-13 | BBC Aktiengesellschaft Brown, Boveri & Cie. | NOx reduction for gas turbines by water injection into the combustion chamber |
FR2558893A1 (en) * | 1984-02-01 | 1985-08-02 | Fluor Corp | METHOD FOR PRODUCING ENERGY USING A GAS TURBINE |
GB2227796A (en) * | 1988-12-06 | 1990-08-08 | Gen Electric | Turbine engine |
CH683019A5 (en) * | 1990-06-12 | 1993-12-31 | Asea Brown Boveri | Gas turbine arrangement. |
WO1998037314A1 (en) * | 1997-02-18 | 1998-08-27 | Nikolai Nikolaev Kolev | Method and installation with a gas-steam turbine and heat utilization |
EP2679784A1 (en) * | 2012-06-26 | 2014-01-01 | General Electric Company | Hot water injection for turbomachine |
-
1967
- 1967-01-23 GB GB3494567A patent/GB1212511A/en not_active Expired
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2230864A1 (en) * | 1973-05-22 | 1974-12-20 | Electricite De France | Fluid transfer system for gas turbine installation - compressor heat exchangers uses hot exhaust to heat injection fluid |
EP0076529A1 (en) * | 1981-09-18 | 1983-04-13 | BBC Aktiengesellschaft Brown, Boveri & Cie. | NOx reduction for gas turbines by water injection into the combustion chamber |
FR2558893A1 (en) * | 1984-02-01 | 1985-08-02 | Fluor Corp | METHOD FOR PRODUCING ENERGY USING A GAS TURBINE |
EP0150990A2 (en) * | 1984-02-01 | 1985-08-07 | Fluor Corporation | Process for producing power |
GB2153912A (en) * | 1984-02-01 | 1985-08-29 | Fluor Corp | Process for producing power |
EP0150990A3 (en) * | 1984-02-01 | 1986-11-26 | Fluor Corporation | Process for producing power |
GB2227796A (en) * | 1988-12-06 | 1990-08-08 | Gen Electric | Turbine engine |
GB2227796B (en) * | 1988-12-06 | 1993-06-09 | Gen Electric | Turbine engine |
CH683019A5 (en) * | 1990-06-12 | 1993-12-31 | Asea Brown Boveri | Gas turbine arrangement. |
WO1998037314A1 (en) * | 1997-02-18 | 1998-08-27 | Nikolai Nikolaev Kolev | Method and installation with a gas-steam turbine and heat utilization |
EP2679784A1 (en) * | 2012-06-26 | 2014-01-01 | General Electric Company | Hot water injection for turbomachine |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |