GB861924A - Improvements in or relating to binary fluid power plants - Google Patents
Improvements in or relating to binary fluid power plantsInfo
- Publication number
- GB861924A GB861924A GB16500/57A GB1650057A GB861924A GB 861924 A GB861924 A GB 861924A GB 16500/57 A GB16500/57 A GB 16500/57A GB 1650057 A GB1650057 A GB 1650057A GB 861924 A GB861924 A GB 861924A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas
- combustion
- turbine
- gases
- combustion space
- 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
- F01K23/00—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
- F01K23/02—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
- F01K23/06—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
- F01K23/08—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle with working fluid of one cycle heating the fluid in another cycle
-
- 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
-
- 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
- F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F22—STEAM GENERATION
- F22B—METHODS OF STEAM GENERATION; STEAM BOILERS
- F22B21/00—Water-tube boilers of vertical or steeply-inclined type, i.e. the water-tube sets being arranged vertically or substantially vertically
- F22B21/34—Water-tube boilers of vertical or steeply-inclined type, i.e. the water-tube sets being arranged vertically or substantially vertically built-up from water tubes grouped in panel form surrounding the combustion chamber, i.e. radiation boilers
- F22B21/341—Vertical radiation boilers with combustion in the lower part
- F22B21/343—Vertical radiation boilers with combustion in the lower part the vertical radiation combustion chamber being connected at its upper part to a sidewards convection chamber
- F22B21/345—Vertical radiation boilers with combustion in the lower part the vertical radiation combustion chamber being connected at its upper part to a sidewards convection chamber with a tube bundle between an upper and a lower drum in the convection pass
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F22—STEAM GENERATION
- F22G—SUPERHEATING OF STEAM
- F22G1/00—Steam superheating characterised by heating method
- F22G1/16—Steam superheating characterised by heating method by using a separate heat source independent from heat supply of the steam boiler, e.g. by electricity, by auxiliary combustion of fuel oil
-
- 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
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
Abstract
861,924. Generating combustion products under pressure; gasefying solid and liquid fuels. BABCOCK & WILCOX Ltd. May 24, 1957 [May 24, 1956], No. 16500/57. Classes 51 (1), 55 (1) and 55 (2). [Also in Group XXVI] In a binary fluid turbine power plant, an ashforming fuel and a free-oxygen containing gas, such as air, under pressure are passed into a first combustion zone, the ratio of fuel to oxygen being insufficient for complete combustion, the fuel being partially burned in the first combustion zone thereby producing gaseous combustible products which contain entrained solids and vaporized ash products. The gaseous products and entrained solids are then passed through a first cooling zone where they are cooled by heat exchange with a vaporizable fluid so as to condense substantially all of the vaporized ash products, the entrained solids are then removed from the combustible gaseous products, and the cleaned combustible gaseous products are then burned, so as to produce clean, hot combustion gas under pressure which is expanded through a gas turbine, the vaporizable fluid being vaporized under pressure, the vapour being superheated and the superheated vapour expanded through a vapour turbine. In Fig. 1, ash-forming fuel and air under pressure are introduced into the combustion space 12 by means of the injector 10 and the fuel is partially burned so as to produce a combustible gas containing carbon monoxide and hydrogen. The combustible gas is then passed through a bank of steam generator tubes 26 and is thereby cooled and the vaporized ash products are condensed. The combustible gas then flows over a bank of superheater tubes 32 and interstage reheater tube banks 34, 36 and finally discharges through a Venturi nozzle 38 where washing liquid such as water is sprayed into the gas. The gas and water mixture then passes into a gaswater separator 40, the clean gas passing through outlet 42 and the water and ash products pass into a liquid-solid separator 44, the ash products being returned into the combustion space by means of the conveyer 46. The clean combustible gas enters the second combustion space 50 where it is burned with air under pressure supplied through the duct 52, and the resulting clean combustion gas is cooled by flowing across interstage reheater tube banks 56, 58 and superheater tubes 60, the cooled combustion gases finally discharging through duct 62 into the gas turbine 64 which drives the air compressor 14 also an electric generator 66. Steam from the second superheater 60 passes to the highpressure steam turbine 68, the exhaust of which passes through reheaters 34, 58 before entering the intermediate pressure turbine 70, the exhaust of which passes through reheaters 36, 56 before entering the low-pressure turbine 72 the exhaust of which is condensed and returned to the steam generator 26. The steam turbines drive an electric generator 76. In Fig. 2 the clean combustible gas discharged from the gas-water separator 40 is divided into two streams, one of which is fed to the second combustion space where it is partially burned with air under pressure supplied through the duct 82, the combustion gases being subsequently cooled by flowing across the interstage reheaters 86, 88 and the superheater 90, the cooled gases then passing through duct 91 to the gas turbine 92 from which they are led to a fourth combustion space 100. The remainder of the combustible gas from the separator 40 flows to a third combustion space 94 where it is completely burned with air under pressure supplied through the duct 95. The combustion gases are cooled in flowing across the interstage reheaters 97, 98 and the gases then enter turbine 99 from which they discharge into the fourth combustion space 100. The exhaust gases from the turbine 92 which contain combustible gases and the gases from the turbine 99 which contain excess oxygen are caused to burn in the fourth combustion space 100 by means of catalysts 101, the combustion gases finally passing to turbine 102. The turbines 92, 99 and 102 drive the air compressor 14 and an electric generator. The plant includes steam turbines 68, 70, 72 as in the first embodiment. In a third embodiment, the gases from the first combustion space 12 after cooling are fed to a gas cleaning device which operates both as a mechanical separator for separating out solid particles carried by the gas and as an electrostatic precipitator, the cleaned gases then passing to the second combustion space 50 as in the first embodiment. In Fig. 4, the gases from the first combustion space 12 after cooling in the gas pass flow through a gas cleaning device 380 where the gas is washed by water sprayed from ring 382 on to a liquid surface expanding device 384. The liquid collects in the lower portion of the cleaning device and is then passed through a solid-liquid separator 44 as in Fig. 1. The clean combustible gas is then passed through a heater 390 in the gas cooling pass 24 and then enters a second combustion space 50 where it is burned with air under pressure from the compressor 14, combustion catalysts 392 being disposed in the combustion space. The combustion gases finally enter the gas turbine 64 which drives the air compressor 14 and an electric generator. The plant includes steam turbines 68, 70, 72 as in the first embodiment.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US861924XA | 1956-05-24 | 1956-05-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB861924A true GB861924A (en) | 1961-03-01 |
Family
ID=22196904
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB16500/57A Expired GB861924A (en) | 1956-05-24 | 1957-05-24 | Improvements in or relating to binary fluid power plants |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB861924A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2425546A1 (en) * | 1978-05-08 | 1979-12-07 | Johnson Matthey Co Ltd | APPARATUS AND METHOD FOR IMPROVING THE EFFICIENCY OF ENERGY PRODUCTION FACILITIES |
EP0069243A1 (en) * | 1981-06-24 | 1983-01-12 | Kraftwerk Union Aktiengesellschaft | Hot gas system |
GB2191215A (en) * | 1986-06-03 | 1987-12-09 | Humphreys & Glasgow Ltd | Power from carbonaceous fuel |
GB2199842A (en) * | 1986-12-30 | 1988-07-20 | Us Energy | Power generating system and method utilizing hydropyrolysis |
FR2644846A1 (en) * | 1989-03-24 | 1990-09-28 | Gen Electric | DEVICE AND METHOD FOR COMBUSTING HYDROCARBON WITH LOW NOX CONTENT IN THE DRY CONDITION |
US5103630A (en) * | 1989-03-24 | 1992-04-14 | General Electric Company | Dry low NOx hydrocarbon combustion apparatus |
US7516620B2 (en) | 2005-03-01 | 2009-04-14 | Jupiter Oxygen Corporation | Module-based oxy-fuel boiler |
GB2526819A (en) * | 2014-06-03 | 2015-12-09 | Chinook End Stage Recycling Ltd | Waste management |
EP2447481A3 (en) * | 2010-10-27 | 2016-03-09 | Mitsubishi Hitachi Power Systems, Ltd. | Thermal power plant |
-
1957
- 1957-05-24 GB GB16500/57A patent/GB861924A/en not_active Expired
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2425546A1 (en) * | 1978-05-08 | 1979-12-07 | Johnson Matthey Co Ltd | APPARATUS AND METHOD FOR IMPROVING THE EFFICIENCY OF ENERGY PRODUCTION FACILITIES |
EP0069243A1 (en) * | 1981-06-24 | 1983-01-12 | Kraftwerk Union Aktiengesellschaft | Hot gas system |
GB2191215A (en) * | 1986-06-03 | 1987-12-09 | Humphreys & Glasgow Ltd | Power from carbonaceous fuel |
GB2199842A (en) * | 1986-12-30 | 1988-07-20 | Us Energy | Power generating system and method utilizing hydropyrolysis |
USRE35061E (en) * | 1989-03-24 | 1995-10-17 | General Electric Company | Dry low NOx hydrocarbon combustion apparatus |
GB2229733A (en) * | 1989-03-24 | 1990-10-03 | Gen Electric | Hydrocarbon combustion apparatus and method |
US5103630A (en) * | 1989-03-24 | 1992-04-14 | General Electric Company | Dry low NOx hydrocarbon combustion apparatus |
GB2229733B (en) * | 1989-03-24 | 1992-10-14 | Gen Electric | Hydrocarbon combustion apparatus and method |
FR2644846A1 (en) * | 1989-03-24 | 1990-09-28 | Gen Electric | DEVICE AND METHOD FOR COMBUSTING HYDROCARBON WITH LOW NOX CONTENT IN THE DRY CONDITION |
US7516620B2 (en) | 2005-03-01 | 2009-04-14 | Jupiter Oxygen Corporation | Module-based oxy-fuel boiler |
EA012129B1 (en) * | 2005-03-01 | 2009-08-28 | Юпитер Оксиген Корпорейшн | Module-based oxy-fuel boiler |
US8082737B2 (en) | 2005-03-01 | 2011-12-27 | Jupiter Oxygen Corporation | Module-based oxy-fuel boiler |
US8752383B2 (en) | 2005-03-01 | 2014-06-17 | Jupiter Oxygen Corporation | Module-based oxy-fuel boiler |
EP2447481A3 (en) * | 2010-10-27 | 2016-03-09 | Mitsubishi Hitachi Power Systems, Ltd. | Thermal power plant |
GB2526819A (en) * | 2014-06-03 | 2015-12-09 | Chinook End Stage Recycling Ltd | Waste management |
WO2015185915A1 (en) * | 2014-06-03 | 2015-12-10 | Chinook End-Stage Recycling Limited | Waste management |
GB2526819B (en) * | 2014-06-03 | 2018-07-04 | Chinook End Stage Recycling Ltd | Waste management |
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