EP0086504A2 - A process for generating mechanical power - Google Patents
A process for generating mechanical power Download PDFInfo
- Publication number
- EP0086504A2 EP0086504A2 EP83200018A EP83200018A EP0086504A2 EP 0086504 A2 EP0086504 A2 EP 0086504A2 EP 83200018 A EP83200018 A EP 83200018A EP 83200018 A EP83200018 A EP 83200018A EP 0086504 A2 EP0086504 A2 EP 0086504A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- range
- steam
- temperature
- gaseous fuel
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 22
- 239000000446 fuel Substances 0.000 claims abstract description 47
- 239000007789 gas Substances 0.000 claims abstract description 36
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 26
- 239000000203 mixture Substances 0.000 claims abstract description 22
- 238000002485 combustion reaction Methods 0.000 claims abstract description 19
- 239000000567 combustion gas Substances 0.000 claims abstract description 6
- 239000002803 fossil fuel Substances 0.000 claims description 5
- 230000003647 oxidation Effects 0.000 claims description 4
- 238000007254 oxidation reaction Methods 0.000 claims description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 3
- 239000001301 oxygen Substances 0.000 claims description 3
- 229910052760 oxygen Inorganic materials 0.000 claims description 3
- 230000008016 vaporization Effects 0.000 claims description 3
- 238000010438 heat treatment Methods 0.000 claims description 2
- 239000008236 heating water Substances 0.000 abstract description 2
- 239000002918 waste heat Substances 0.000 abstract description 2
- 238000001704 evaporation Methods 0.000 abstract 1
- 239000002737 fuel gas Substances 0.000 abstract 1
- 239000003570 air Substances 0.000 description 21
- 239000012535 impurity Substances 0.000 description 3
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 3
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 2
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000002309 gasification Methods 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 239000003208 petroleum Substances 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000004071 soot Substances 0.000 description 2
- 238000003786 synthesis reaction Methods 0.000 description 2
- 238000009834 vaporization Methods 0.000 description 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- OTMSDBZUPAUEDD-UHFFFAOYSA-N Ethane Chemical compound CC OTMSDBZUPAUEDD-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 239000003546 flue gas Substances 0.000 description 1
- 239000013505 freshwater Substances 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000003077 lignite Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 239000001294 propane Substances 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 239000002002 slurry Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
Images
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
Definitions
- the invention relates to a process for generating mechanical power by burning a gaseous fuel in the combustion chamber of a gas turbine and expanding the resulting hot combustion gas in the gas turbine, characterized in that the gaseous fuel is premixed with steam and the mixture thus formed is introduced into the combustion chamber.
- a larger quantity of steam is advantageously mixed with the fuel than in the event of a fuel producing a less hot flame during combustion, such as carbon monoxide or synthesis gas generated by means of air.
- the gaseous fuel can be mixed with the steam in any conceivable manner.
- gaseous fuel having a temperature in the range from 40 to 100°C is preferably contacted with water having a temperature in the range from 80 to 200°C, at a pressure in the range from 10 to 30 bar.
- water having a temperature in the range from 80 to 200°C at a pressure in the range from 10 to 30 bar.
- the water and fuel are advantageously contacted with each other by spraying the water in the top of a column and allowing the gaseous fuel to rise from the bottom of the column so that fine droplets of water are vaporized in the rising gas stream when they drop down in the column.
- the fuel/steam mixture leaves the column at the top. It has then a temperature in the range from 130 to 160°C.
- the fuel/steam mixture is subsequently preferably further heated to a temperature in the range from 250 to 450°C by indirect heat exchange.
- the offgas is now advantageously first introduced into a steam boiler in which it is used for generating steam at a temperature in the range from 450 to 500°C and a pressure in the range from 40 to 60 bar.
- the offgas leaves the steam boiler at a temperature in the range from 150 to 250°C and is subsequently preferably used for heating water to a temperature in the range from 130 to 200°C by indirect heat exchange.
- Said water is advantageously at least . partly used for vaporization in the gaseous fuel as described hereinbefore.
- gaseous fuel for example methane, ethane and propane
- a fuel obtained by partial oxidation of a fossil fuel for example hard coal, brown coal, petroleum or a petroleum fraction, with oxygen, air or oxygen-enriched air at a pressure of 10-100 bar.
- any gas turbine is generally equipped with an air compressor designed for supplying a sufficient quantity of air at adequately high pressure (15-25 bar) in order to keep the outlet temperature of the combustion chamber within the temperatures permitted for the gas turbine, namely 900-1100°C, even without steam having been supplied to the fuel.
- the extra excess air of the gas turbine compressor resulting from the addition of steam is preferably used for the partial oxidation of extra fossil fuel.
- a larger quantity of gaseous fuel is then generated than is required for generating the maximum quantity of mechanical power for which the turbine has been designed.
- This extra quantity of gaseous fuel is advantageously used for supplying heat to the inlet side of the steam boiler described hereinbefore in the course of complete combustion.
- the offgas from the gas turbine is then advantageously heated by burning part of the gaseous fuel therein.
- the offgas is preferably heated to a temperature that is 50 to 75°C higher than the desired temperature of the steam to be generated in the steam boiler arranged downstream by indirect heat exchange between the boiler feed water and the heated turbine offgas.
- a quantity of 10 to 30% of the gaseous fuel can suitably be used for heating the turbine offgas.
- This method makes it possible to produce steam at 80 bar and 550°C.
- the mechanical power generated in the gas turbine is advantageously converted into electric power by means of a dynamo.
- the steam produced in the'steam boiler can also be used for electrical power generation by means of a steam turbine and a dynamo.
- a fuel for example heavy oil
- a gasification reactor 2 where said fuel is partially burnt by reaction with air supplied through a line 3, to form a raw gas mixture substantially consisting of H 21 CO and N 2 .
- the air stream from the line 3 originates from an air compressor 6 via lines 4 and 40, which compressor is an integral part of the apparatus.
- the raw gas mixture leaves the reactor 2 via a line 7 at a temperature in the range from 1200 to 1400°C.
- a waste heat boiler 8 It is cooled to a temperature in the range from 250 to 400°C in a waste heat boiler 8 by heat exchange with boiler feed water that is supplied via a line 9 at a temperature in the range from 150 to 300°C and is vaporized to steam in the boiler 8, which steam leaves the boiler 8 through a line 10 at a temperature in the range from 250 to 325°C.
- the raw gas mixture leaves the boiler 8 via a line 11 and is further cooled in a heat exchanger 13 to a temperature in the range from 150 to 200°C by means of cold boiler feed water that is introduced via a line 14.
- the raw gas mixture is subsequently passed via a line 15 to a soot-removing unit 16 where it is scrubbed with an aqueous stream that is supplied through a line 17.
- the substantially clean gas mixture is discharged via a line 18 and an aqueous soot slurry that is drained from the apparatus through a line 19.
- the substantially clean gas mixture is freed of the remaining solid impurities, mainly soot, in a scrubber 20.
- This is effected by washing the mixture countercurrently to fresh water that is supplied via a line 21 and an aqueous recycle stream reaching the column 20 via a line 22.
- the latter stream 22 is a branch stream of a stream 23 that is drawn off at the bottom of the column 20 and is split into the stream 17 and a recycle stream that is recycled to the column 20 via a line 24 and a cooler 25.
- the gas mixture now substantially purified from solid impurities is discharged from the column 20 via a line 26 to a gas purification unit 27 where the gas mixture is freed of gaseous impurities, mainly H 2 S, at a temperature in the range from 40 to 150°C. It is discharged from the unit 27 via a line 28 and subsequently split into two streams by means of the lines 29 and 30.
- the gas mixture stream in the line 30 is passed to a column 31 where said stream is sprinkled with droplets of water from a sprinkler 37 from which water vaporizes at low temperatures of 80-180°C. Said water is introduced into the apparatus through a line 32 and subsequently combined with a recycle water stream leaving the column 31 via a line 33.
- the combined water stream is passed via a line 34 to a boiler 35 in which it is heated from a temperature in the range from 80 to 130°C to a temperature in the range from 120 to 180°C.
- the stream leaves the boiler 35 through a line 36 in which it is passed to the sprinkler 37.
- a quantity of the water sprinkled by the sprinkler 37 is vaporized and entrained by the rising gas mixture.
- the gas mixture thus treated has a water vapour content in the range from 10 to 20% by volume and a temperature in the range from 120 to 140°C.
- a heat exchanger 39 in which it is heated to a temperature in the range from 250 to 450°C by heat exchange with hot air originating from the compressor 6 from which it is discharged via a line 40.
- the compressed air from the line 40 is split into two branch streams.
- the first stream is passed to the reactor 2 via the line 4 and the line 3.
- the second stream is conducted to a combustion chamber 43 of a turbine 44 through a line 48.
- the combustion chamber 43 the mixture of gaseous fuel and steam with compressed air from the air compressor 6 is ignited and the combustion gas thus formed, which has a temperature in the range from 900 to 1100°C and a pressure in the range from 10 to 20 bar, is expanded in the turbine 44 by which mechanical power is generated.
- the expanded combustion gas is passed via line 45 to a boiler 35 at a temperature in the range from 500 to 550°C and substantially atmospheric pressure, in which boiler it is cooled by heat exchange with water that is supplied through a line 46, is vaporized and discharged as steam via a line 47.
- a branch stream of the gas mixture is passed to the boiler 35 via the line 29 and completely burnt with the excess air in the gas turbine exhaust gas (45).
- the offgas from the boiler 35 leaves the latter via line 49 at a temperature in the range from 125 to 150°C after heat exchange with water in the line 34. It leaves the apparatus via a stack 50.
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)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
Abstract
Description
- The invention relates to a process for generating mechanical power by burning a gaseous fuel in the combustion chamber of a gas turbine and expanding the resulting hot combustion gas in the gas turbine, characterized in that the gaseous fuel is premixed with steam and the mixture thus formed is introduced into the combustion chamber.
- By thoroughly premixing the gaseous fuel with steam it is ensured that in the combustion of said fuel in the combustion chamber of a gas turbine less nitrogen oxides are formed. The same object can also be aimed at by injecting water or steam into the flame in the combustion chamber, but by thoroughly premixing steam and gaseous fuel up to 35% of steam can be saved compared with the method in which steam is injected into the flame. Preferably a quantity of 0.1-1.0 kg of steam per kg of gaseous fuel is mixed with said fuel and the mixture is passed to the combustion chamber of the turbine. Within the limits set the quantity of steam depends on the type of gaseous fuel. For example, in the event of a fuel producing a very hot flame during combustion, such as hydrogen or synthesis gas generated by means of pure oxygen, a larger quantity of steam is advantageously mixed with the fuel than in the event of a fuel producing a less hot flame during combustion, such as carbon monoxide or synthesis gas generated by means of air.
- The gaseous fuel can be mixed with the steam in any conceivable manner. However, gaseous fuel having a temperature in the range from 40 to 100°C is preferably contacted with water having a temperature in the range from 80 to 200°C, at a pressure in the range from 10 to 30 bar. Thus, at least part of the water vaporizes in the gaseous fuel and the steam generated by vaporization is at the same time thoroughly mixed with the fuel. The water and fuel are advantageously contacted with each other by spraying the water in the top of a column and allowing the gaseous fuel to rise from the bottom of the column so that fine droplets of water are vaporized in the rising gas stream when they drop down in the column. The fuel/steam mixture leaves the column at the top. It has then a temperature in the range from 130 to 160°C.
- The fuel/steam mixture is subsequently preferably further heated to a temperature in the range from 250 to 450°C by indirect heat exchange.
- It is subsequently burnt with air in the combustion chamber of a gas turbine and the hot combustion gas is expanded in the turbine. On leaving the turbine the offgas has a temperature in the range from 500 to 550°C at substantially atmospheric pressure. The offgas is now advantageously first introduced into a steam boiler in which it is used for generating steam at a temperature in the range from 450 to 500°C and a pressure in the range from 40 to 60 bar. The offgas leaves the steam boiler at a temperature in the range from 150 to 250°C and is subsequently preferably used for heating water to a temperature in the range from 130 to 200°C by indirect heat exchange. Said water is advantageously at least . partly used for vaporization in the gaseous fuel as described hereinbefore. By said process low-temperature heat from the flue gas between 125°C and 200°C is effectively used to save compressed air.
- Although any gaseous fuel, for example methane, ethane and propane, can be used for the process according to the invention, preference is given to a fuel obtained by partial oxidation of a fossil fuel, for example hard coal, brown coal, petroleum or a petroleum fraction, with oxygen, air or oxygen-enriched air at a pressure of 10-100 bar.
- Since in the present process steam is mixed with the gaseous fuel less air is required in the combustion chamber of the turbine than in the case where no steam is added to the fuel.
- Now, any gas turbine is generally equipped with an air compressor designed for supplying a sufficient quantity of air at adequately high pressure (15-25 bar) in order to keep the outlet temperature of the combustion chamber within the temperatures permitted for the gas turbine, namely 900-1100°C, even without steam having been supplied to the fuel.
- Consequently, when using a gasification product as fuel, there is mostly already an excess of air, since the fuel has a calorific value of far below 10,000 kcal/ton. Said air is advantageously used to gasify the fossil fuel, but in the event of 02 being used for the gasifier, it can be used, for example, as plant process air or instrument air.
- According to the invention the extra excess air of the gas turbine compressor resulting from the addition of steam is preferably used for the partial oxidation of extra fossil fuel. A larger quantity of gaseous fuel is then generated than is required for generating the maximum quantity of mechanical power for which the turbine has been designed.
- This extra quantity of gaseous fuel is advantageously used for supplying heat to the inlet side of the steam boiler described hereinbefore in the course of complete combustion.
- The offgas from the gas turbine is then advantageously heated by burning part of the gaseous fuel therein. In this manner the offgas is preferably heated to a temperature that is 50 to 75°C higher than the desired temperature of the steam to be generated in the steam boiler arranged downstream by indirect heat exchange between the boiler feed water and the heated turbine offgas.
- By mixing the gaseous fuel with steam before burning it in the turbine combustion chamber according to the invention, a quantity of 10 to 30% of the gaseous fuel can suitably be used for heating the turbine offgas. This method makes it possible to produce steam at 80 bar and 550°C. The mechanical power generated in the gas turbine is advantageously converted into electric power by means of a dynamo. The steam produced in the'steam boiler can also be used for electrical power generation by means of a steam turbine and a dynamo.
- The invention will now be further illustrated with reference to the Figure giving a diagrammatic representation of the apparatus in which the process according to the invention is carried out. The auxiliary equipment to be used therein, such as pumps, compressors, valves, cleaning devices and control instruments, have been omitted for ease of review.
- However, the invention is by no means limited to this description of the Figure.
- A fuel, for example heavy oil, is passed through a
line 1 to agasification reactor 2, where said fuel is partially burnt by reaction with air supplied through aline 3, to form a raw gas mixture substantially consisting of H21 CO and N2. The air stream from theline 3 originates from anair compressor 6 vialines reactor 2 via aline 7 at a temperature in the range from 1200 to 1400°C. It is cooled to a temperature in the range from 250 to 400°C in awaste heat boiler 8 by heat exchange with boiler feed water that is supplied via aline 9 at a temperature in the range from 150 to 300°C and is vaporized to steam in theboiler 8, which steam leaves theboiler 8 through aline 10 at a temperature in the range from 250 to 325°C. The raw gas mixture leaves theboiler 8 via aline 11 and is further cooled in aheat exchanger 13 to a temperature in the range from 150 to 200°C by means of cold boiler feed water that is introduced via aline 14. The raw gas mixture is subsequently passed via aline 15 to a soot-removingunit 16 where it is scrubbed with an aqueous stream that is supplied through aline 17. This results in a substantially clean gas mixture that is discharged via aline 18 and an aqueous soot slurry that is drained from the apparatus through aline 19. The substantially clean gas mixture is freed of the remaining solid impurities, mainly soot, in ascrubber 20. This is effected by washing the mixture countercurrently to fresh water that is supplied via aline 21 and an aqueous recycle stream reaching thecolumn 20 via aline 22. Thelatter stream 22 is a branch stream of astream 23 that is drawn off at the bottom of thecolumn 20 and is split into thestream 17 and a recycle stream that is recycled to thecolumn 20 via aline 24 and a cooler 25. - The gas mixture now substantially purified from solid impurities is discharged from the
column 20 via aline 26 to agas purification unit 27 where the gas mixture is freed of gaseous impurities, mainly H2S, at a temperature in the range from 40 to 150°C. It is discharged from theunit 27 via aline 28 and subsequently split into two streams by means of thelines line 30 is passed to acolumn 31 where said stream is sprinkled with droplets of water from asprinkler 37 from which water vaporizes at low temperatures of 80-180°C. Said water is introduced into the apparatus through aline 32 and subsequently combined with a recycle water stream leaving thecolumn 31 via aline 33. The combined water stream is passed via aline 34 to aboiler 35 in which it is heated from a temperature in the range from 80 to 130°C to a temperature in the range from 120 to 180°C. The stream leaves theboiler 35 through aline 36 in which it is passed to thesprinkler 37. In the column 31 a quantity of the water sprinkled by thesprinkler 37 is vaporized and entrained by the rising gas mixture. The gas mixture thus treated has a water vapour content in the range from 10 to 20% by volume and a temperature in the range from 120 to 140°C. It is conducted via aline 38 to aheat exchanger 39 in which it is heated to a temperature in the range from 250 to 450°C by heat exchange with hot air originating from thecompressor 6 from which it is discharged via aline 40. The compressed air from theline 40 is split into two branch streams. The first stream is passed to thereactor 2 via theline 4 and theline 3. The second stream is conducted to a combustion chamber 43 of aturbine 44 through aline 48. In the combustion chamber 43 the mixture of gaseous fuel and steam with compressed air from theair compressor 6 is ignited and the combustion gas thus formed, which has a temperature in the range from 900 to 1100°C and a pressure in the range from 10 to 20 bar, is expanded in theturbine 44 by which mechanical power is generated. The expanded combustion gas is passed vialine 45 to aboiler 35 at a temperature in the range from 500 to 550°C and substantially atmospheric pressure, in which boiler it is cooled by heat exchange with water that is supplied through aline 46, is vaporized and discharged as steam via aline 47. To increase the gas inlet temperature in the boiler 35 a branch stream of the gas mixture is passed to theboiler 35 via theline 29 and completely burnt with the excess air in the gas turbine exhaust gas (45). The offgas from theboiler 35 leaves the latter vialine 49 at a temperature in the range from 125 to 150°C after heat exchange with water in theline 34. It leaves the apparatus via astack 50.
Claims (12)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL8200585A NL191444C (en) | 1982-02-16 | 1982-02-16 | Method for generating mechanical energy and generating steam using a gas turbine. |
NL8200585 | 1982-02-16 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0086504A2 true EP0086504A2 (en) | 1983-08-24 |
EP0086504A3 EP0086504A3 (en) | 1985-03-06 |
EP0086504B1 EP0086504B1 (en) | 1988-03-09 |
Family
ID=19839266
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP83200018A Expired EP0086504B1 (en) | 1982-02-16 | 1983-01-05 | A process for generating mechanical power |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP0086504B1 (en) |
JP (1) | JPS58150030A (en) |
AU (1) | AU555824B2 (en) |
CA (1) | CA1222382A (en) |
DE (1) | DE3375936D1 (en) |
NL (1) | NL191444C (en) |
ZA (1) | ZA83985B (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0207620A2 (en) * | 1985-06-04 | 1987-01-07 | Imperial Chemical Industries Plc | Energy recovery |
EP0238835A2 (en) * | 1986-03-04 | 1987-09-30 | Mitsubishi Gas Chemical Company, Inc. | Method for energy recovery from oxidation reactor off-gas |
US4733528A (en) * | 1984-03-02 | 1988-03-29 | Imperial Chemical Industries Plc | Energy recovery |
EP0318706A1 (en) * | 1987-11-30 | 1989-06-07 | General Electric Company | Water spray ejector system for steam injected engine |
EP0384781A1 (en) * | 1989-02-23 | 1990-08-29 | Jacobs Engineering Limited | Improvements in operating flexibility in integrated gasification combined cycle power stations |
US5054279A (en) * | 1987-11-30 | 1991-10-08 | General Electric Company | Water spray ejector system for steam injected engine |
EP0588392A1 (en) * | 1992-07-13 | 1994-03-23 | N.V. Kema | Steam and gas turbine power plant using moistened natural gas |
WO1995000747A1 (en) * | 1993-06-24 | 1995-01-05 | Siemens Aktiengesellschaft | Method of operating a cogas plant, and a cogas plant operated by this method |
EP1211401A1 (en) * | 2000-11-09 | 2002-06-05 | General Electric Company | Fuel gas moisturization system control |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4597256A (en) * | 1985-04-16 | 1986-07-01 | International Power Technology, Inc. | Method and apparatus for improved shutdown procedures in dual fluid Cheng cycle engines |
DE60033738T2 (en) * | 1999-07-01 | 2007-11-08 | General Electric Co. | Device for humidifying and heating fuel gas |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2005656A1 (en) * | 1970-02-07 | 1971-08-19 | Metallgesellschat Ag | Open gas turbine plant |
FR2202230A1 (en) * | 1972-10-09 | 1974-05-03 | Mitsubishi Heavy Ind Ltd | |
EP0081996A2 (en) * | 1981-12-10 | 1983-06-22 | Mitsubishi Gas Chemical Company, Inc. | Regenerative gas turbine cycle |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5949410B2 (en) * | 1975-06-20 | 1984-12-03 | 株式会社日立製作所 | Control method for gasification power plant |
DE3012172A1 (en) * | 1980-03-28 | 1981-10-08 | Kraftwerk Union AG, 4330 Mülheim | GAS TURBINE WITH STICKOXYDEMISSIO REDUCED BY STEAM INJECTION |
-
1982
- 1982-02-16 NL NL8200585A patent/NL191444C/en not_active IP Right Cessation
-
1983
- 1983-01-05 EP EP83200018A patent/EP0086504B1/en not_active Expired
- 1983-01-05 DE DE8383200018T patent/DE3375936D1/en not_active Expired
- 1983-02-14 CA CA000421501A patent/CA1222382A/en not_active Expired
- 1983-02-14 JP JP58021769A patent/JPS58150030A/en active Granted
- 1983-02-14 AU AU11383/83A patent/AU555824B2/en not_active Ceased
- 1983-02-14 ZA ZA83985A patent/ZA83985B/en unknown
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2005656A1 (en) * | 1970-02-07 | 1971-08-19 | Metallgesellschat Ag | Open gas turbine plant |
FR2202230A1 (en) * | 1972-10-09 | 1974-05-03 | Mitsubishi Heavy Ind Ltd | |
EP0081996A2 (en) * | 1981-12-10 | 1983-06-22 | Mitsubishi Gas Chemical Company, Inc. | Regenerative gas turbine cycle |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4733528A (en) * | 1984-03-02 | 1988-03-29 | Imperial Chemical Industries Plc | Energy recovery |
EP0207620A2 (en) * | 1985-06-04 | 1987-01-07 | Imperial Chemical Industries Plc | Energy recovery |
EP0207620A3 (en) * | 1985-06-04 | 1988-12-14 | Imperial Chemical Industries Plc | Energy recovery |
AU583385B2 (en) * | 1985-06-04 | 1989-04-27 | Imperial Chemical Industries Plc | Energy recovery |
EP0238835A2 (en) * | 1986-03-04 | 1987-09-30 | Mitsubishi Gas Chemical Company, Inc. | Method for energy recovery from oxidation reactor off-gas |
EP0238835A3 (en) * | 1986-03-04 | 1989-01-25 | Mitsubishi Gas Chemical Company, Inc. | Method for energy recovery from oxidation reactor off-gas |
EP0318706A1 (en) * | 1987-11-30 | 1989-06-07 | General Electric Company | Water spray ejector system for steam injected engine |
US5054279A (en) * | 1987-11-30 | 1991-10-08 | General Electric Company | Water spray ejector system for steam injected engine |
EP0384781A1 (en) * | 1989-02-23 | 1990-08-29 | Jacobs Engineering Limited | Improvements in operating flexibility in integrated gasification combined cycle power stations |
AU630919B2 (en) * | 1989-02-23 | 1992-11-12 | H & G Process Contracting Limited | Improvements in operating flexibility in integrated gasification combined cycle power stations |
EP0588392A1 (en) * | 1992-07-13 | 1994-03-23 | N.V. Kema | Steam and gas turbine power plant using moistened natural gas |
WO1995000747A1 (en) * | 1993-06-24 | 1995-01-05 | Siemens Aktiengesellschaft | Method of operating a cogas plant, and a cogas plant operated by this method |
EP1211401A1 (en) * | 2000-11-09 | 2002-06-05 | General Electric Company | Fuel gas moisturization system control |
US6502402B1 (en) | 2000-11-09 | 2003-01-07 | General Electric Company | Fuel moisturization control |
Also Published As
Publication number | Publication date |
---|---|
EP0086504B1 (en) | 1988-03-09 |
JPS58150030A (en) | 1983-09-06 |
DE3375936D1 (en) | 1988-04-14 |
AU1138383A (en) | 1983-08-25 |
ZA83985B (en) | 1984-03-28 |
EP0086504A3 (en) | 1985-03-06 |
NL191444C (en) | 1995-07-04 |
NL191444B (en) | 1995-03-01 |
NL8200585A (en) | 1983-09-16 |
CA1222382A (en) | 1987-06-02 |
JPH0475372B2 (en) | 1992-11-30 |
AU555824B2 (en) | 1986-10-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6588212B1 (en) | Combustion turbine fuel inlet temperature management for maximum power outlet | |
US5345756A (en) | Partial oxidation process with production of power | |
US5295350A (en) | Combined power cycle with liquefied natural gas (LNG) and synthesis or fuel gas | |
CN101016490B (en) | A method of treating a gaseous mixture comprising hydrogen and carbon dioxide | |
US3731485A (en) | Open-cycle gas turbine plant | |
EP0603997B1 (en) | Power generation process | |
KR100334197B1 (en) | Partial Oxidation Power System | |
CN101063050B (en) | Coal gas production method | |
EP0086504B1 (en) | A process for generating mechanical power | |
US6152984A (en) | Integrated direct reduction iron system | |
WO2003080503A1 (en) | Method for producing syngas with recycling of water | |
JPH0250888B2 (en) | ||
CN1041108C (en) | Coal gaslfication electric power generation plant | |
BR102014012494A2 (en) | gasification system, method and system | |
JPS608077B2 (en) | Method for producing synthesis gas consisting of H↓2 and CO along with power | |
CN116221715A (en) | Oxygen-enriched combustion system | |
van der Burgt et al. | IGCC: COST REDUCTION POTENTIAL 1998 EPRI/GTC GASIFICATION TECHNOLOGIES CONFERENCE | |
AU2002318439A1 (en) | Combustion turbine fuel inlet temperature management for maximum power output |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 19830105 |
|
AK | Designated contracting states |
Designated state(s): BE DE FR GB IT |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Designated state(s): BE DE FR GB IT |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): BE DE FR GB IT |
|
ITF | It: translation for a ep patent filed | ||
REF | Corresponds to: |
Ref document number: 3375936 Country of ref document: DE Date of ref document: 19880414 |
|
ET | Fr: translation filed | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
ITTA | It: last paid annual fee | ||
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 19971125 Year of fee payment: 16 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 19971222 Year of fee payment: 16 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: BE Payment date: 19971229 Year of fee payment: 16 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 19980205 Year of fee payment: 16 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19990105 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19990131 |
|
BERE | Be: lapsed |
Owner name: SHELL INTERNATIONALE RESEARCH MAATSCHAPPIJ B.V. Effective date: 19990131 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 19990105 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19990930 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19991103 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST |