EP1604102A1 - Humid air turbine cycle with carbon dioxide recovery - Google Patents
Humid air turbine cycle with carbon dioxide recoveryInfo
- Publication number
- EP1604102A1 EP1604102A1 EP03716695A EP03716695A EP1604102A1 EP 1604102 A1 EP1604102 A1 EP 1604102A1 EP 03716695 A EP03716695 A EP 03716695A EP 03716695 A EP03716695 A EP 03716695A EP 1604102 A1 EP1604102 A1 EP 1604102A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- carbon dioxide
- gas
- exhaust
- plant
- humid
- 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.)
- Withdrawn
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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
- F02C1/08—Semi-closed cycles
-
- 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
- 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
- F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
-
- 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
- F02C3/34—Gas-turbine plants characterised by the use of combustion products as the working fluid with recycling of part of the working fluid, i.e. semi-closed cycles with combustion products in the closed part of the cycle
Definitions
- the field of the invention is carbon dioxide recovery, and especially carbon dioxide recovery from humid air turbine cycle.
- Combustion gases, and especially flue gases from gas turbines often comprise a substantial quantity of carbon dioxide, which is a known greenhouse gas.
- carbon dioxide which is a known greenhouse gas.
- membranes may be removed from various gas streams with one or more membranes as described in U.S. Pat. No. 4,130,403 to Cooley et. al., U.S. Pat. No. 4,639,257 to Duckett et. al., or U.S. Pat. No. 5,233,837 to Callahan.
- Membrane processes typically exhibit relatively high selectivity towards a particular gas component.
- membrane processes can generally be operated without energy consuming circulation (e.g. , heating and/or cooling requirements that are often needed for solvent based carbon dioxide removal).
- membrane life time is less than desirable, or the feed gas requires pretreatment before contacting the membrane.
- membrane systems typically operate at a relatively high pressure differential, which either necessitates a blower or other pressure increasing equipment for low pressure feed gases or disqualifies membrane systems for such low pressure feed gases.
- carbon dioxide may be removed using physical or chemical solvents, and numerous process configurations for solvents are known in the art.
- Physical solvent processes are particularly advantageous where the acid gas partial pressure in the feed gas is relatively high.
- all, or almost all physical solvents exhibit only limited usefulness for the removal of carbon dioxide from flue gases which are typically near atmospheric pressure, and especially where the flue gas has a relatively low carbon dioxide content.
- chemical solvents may be employed to scrub the feed gas, wherein the chemical solvent is regenerated downstream to recover the carbon dioxide. Scrubbing gases with chemical solvents typically allows removal of carbon dioxide from a feed gas at relatively low pressure.
- such methods are often energy intensive as well as costly and problems with corrosion and solvent degradation frequently arise (see e.g., U.S. Pat. No. 2,065,112, U.S. Pat. No. 2,399,142, U.S. Pat. No. 2,377,966, U.S. Pat. No. 4,477,419, or U.S. Pat. No. 3,137,654).
- the size of the recovery equipment as well as the power consumed by a blower typically increases substantially to overcome the pressure drop in the recovery equipment.
- the present invention is directed to methods and configurations of carbon dioxide removal from flue gases in which at least part of the flue gas is compressed to a higher pressure thereby improving carbon dioxide removal efficiency.
- a plant will include a combustor that combusts a fuel in the presence of heated humid air to produce an exhaust that is expanded in an expander.
- a compressor (operationally coupled to the expander) compresses air and at least a portion of the exhaust from the expander to form a compressed mixed gas from which carbon dioxide is removed in an acid gas removal unit, and a humidifier humidifies the so formed carbon dioxide depleted compressed mixed gas to produce the heated humid air.
- the heated humid air is heated using the exhaust as heat source, and that the humidifier uses water that is heated by at least one of the compressed mixed gas and the exhaust gas.
- preferred acid gas removal units include a membrane unit or employ a solvent (e.g., an amine-based solvent).
- part of the compressed mixed gas may also be fed to the combustor, and a cooler provides cooling for the expanded exhaust thereby condensing water from the expanded exhaust.
- the acid gas removal unit comprises an autorefrigeration unit
- the autorefrigeration unit removes carbon dioxide from a first portion of the compressed mixed gas, and that a humidifier humidifies a second portion of the compressed mixed gas to form the heated humid air.
- a plant may include a turbine combustor, and particularly a humid air turbine combustor that receives fuel and humid carbon dioxide depleted air, wherein at least part of the humid carbon dioxide depleted air is formed from an exhaust gas of the humid air turbine combustor after a portion of the carbon dioxide has been removed for recovery.
- the carbon dioxide in such configurations is advantageously extracted from the carbon dioxide containing air (mixture of fresh air and recycle flue gas that contains the carbon dioxide) using a membrane unit or a solvent.
- contemplated plants in which carbon dioxide is removed from an exhaust gas of a turbine combustor may therefore include a compressor that compresses air and at least a portion of the exhaust gas (recycle gas) to form a compressed mixed gas, wherein carbon dioxide is removed from the compressed mixed gas in an acid gas removal unit.
- a compressor that compresses air and at least a portion of the exhaust gas (recycle gas) to form a compressed mixed gas, wherein carbon dioxide is removed from the compressed mixed gas in an acid gas removal unit.
- Figure 1 is a schematic view of an exemplary configuration for carbon dioxide recovery from exhaust gas using a membrane or solvent in the acid gas removal unit.
- Figure 2 is a schematic view of an exemplary configuration for carbon dioxide recovery from exhaust gas using an autorefrigeration unit in the acid gas removal unit.
- Figure 3 is a schematic view of another exemplary configuration for carbon dioxide recovery from exhaust gas using partial humidification.
- the inventor has discovered that carbon dioxide contained in the exhaust gas of a gas turbine can be recovered at pressure by recycling at least part of the exhaust gas back to a compressor to increase the partial pressure of the carbon dioxide in the compressed gas, and to thereby facilitate removal of the carbon dioxide using appropriate acid gas removal technologies (e.g., using a physical or chemical solvent, a carbon dioxide specific membrane, or an autorefrigeration process).
- appropriate acid gas removal technologies e.g., using a physical or chemical solvent, a carbon dioxide specific membrane, or an autorefrigeration process.
- an exemplary plant 100 includes a humid air turbine cycle for generation of power, wherein at least part of the expanded exhaust is recycled back to the compressor for carbon dioxide recovery at elevated pressure. More specifically, the combustor 110 receives fuel 112 and heated humid air 114' and produces exhaust 116 which is subsequently expanded in expander 120. The heat in expanded exhaust 118 is then at least partially recovered in recuperator 170, which heats humid air 114 from humidifier 180, which provides heat for a steam generator, and which further heats water for the humidifier 180 via economizer 170'.
- One portion of the expanded and cooled exhaust 118A is vented, while another portion of the expanded and cooled exhaust 118B is cooled in cooler 140 to form cooled expanded exhaust stream 118' (while condensing and separating out a substantial portion of the water), which is combined with air 132 and compressed in compressor 130 that is operationally coupled to the expander 120.
- compressor 130 provides a compressed mixed gas 134 that is cooled in aftercooler 160, thereby heating at least a portion of the water employed in the humidifier.
- the so cooled compressed mixed gas 134 is then fed to the acid gas removal unit 150 (preferably a solvent based acid gas removal unit or a membrane based carbon dioxide removal unit).
- Carbon dioxide product stream 152 leaves the plant (e.g., as commercial product) while the carbon dioxide depleted compressed mixed gas 136 is fed to the humidifier 180.
- Humidifier 180 produces humid gas stream 114 from the carbon dioxide depleted compressed mixed gas 136, wherein the humid gas stream 114 is heated in the recuperator 170 to form heated humid gas stream 114', which is fed into combustor 110 (The terms “humid gas stream” and “humid air” are used interchangeably herein).
- a plant may comprise a combustor that combusts a fuel in the presence of humid air, wherein the combustor produces an exhaust that is expanded in an expander to form an expanded exhaust; a compressor operationally coupled to the expander, wherein the compressor compresses air and at least a portion of the expanded exhaust to form a compressed mixed gas; an acid gas removal unit that removes carbon dioxide from the compressed mixed gas to form a carbon dioxide depleted compressed mixed gas; and a humidifier that humidifies the carbon dioxide depleted compressed mixed gas to form the humid air.
- plant 200 includes a humid air turbine cycle for generation of power, wherein at least part of the expanded exhaust is recycled back to the compressor for carbon dioxide recovery at elevated pressure.
- the combustor 210 receives fuel 212 and heated humid air 214' and produces exhaust 216, which is then expanded in expander 220.
- the heat in expanded exhaust 218 is then at least partially recovered in recuperator 270, which heats humid air 214 from humidifier 280, which provides heat for a steam generator (not shown), and which further heats water for the humidifier 280 via economizer 270'.
- the expanded and cooled exhaust 218 is cooled in cooler 240 to form cooled expanded exhaust stream 218' (while condensing and separating out a substantial portion of the water), which is combined with air 232 and compressed in compressor 230 that is operationally coupled to the expander 220.
- compressor 230 provides a compressed mixed gas 234 that is cooled in aftercooler 260, thereby heating at least a portion of the water employed in the humidifier.
- the so cooled compressed mixed gas 234 is then split into a first stream 234A that is fed to the humidifier 280 and a second stream 234B that is fed to the autorefrigeration unit 250.
- Carbon dioxide product stream 252 leaves the plant (e.g., as commercial product) while the carbon dioxide depleted exhaust gas 238 leaves the plant as exhaust.
- Humidifier 280 produces humid gas stream 214 from the first stream 234A, wherein the humid gas stream 214 is heated in the recuperator 270 to form heated humid gas stream 214', which is then fed into combustor 210.
- a plant may include a combustor that combusts a fuel in the presence of humid air, wherein the combustor produces an exhaust that is expanded in an expander to form an expanded exhaust; a compressor operationally coupled to the expander, wherein the compressor compresses air and at least a portion of the expanded exhaust to form a compressed mixed gas; an autorefrigeration unit that removes carbon dioxide from a first portion of the compressed mixed gas; and a humidifier that humidifies a second portion of the compressed mixed gas to form the humid air.
- an exemplary plant 300 includes a gas turbine (e.g., the large scale General Electric 7FA+e) with a capability of up to 20 to 30% air extraction in a humid air turbine cycle for generation of power, wherein at least part of the expanded exhaust is recycled back to the compressor for carbon dioxide recovery at elevated pressure.
- gas turbine e.g., the large scale General Electric 7FA+e
- combustor 310 receives fuel 312 and heated humid air 314' to produce exhaust 316 which is expanded in expander 320.
- the heat in expanded exhaust 318 is at least partially recovered in heat recovery steam generator 370.
- One portion of the expanded and cooled exhaust 318 A is vented, while another portion of the expanded and cooled exhaust 318B is cooled in cooler 340 to form cooled expanded exhaust stream 318' (while condensing and separating out a substantial portion of the water), which is combined with air 332 and compressed in compressor 330 that is operationally coupled to the expander 320.
- compressor 330 provides a compressed mixed gas 334.
- One portion of the compressed mixed gas 334A is directly fed to the combustor 310 (in a manner similar to what is practiced in conventional gas turbines), while another portion of the compressed mixed gas 334B is cooled in aftercooler 360, thereby heating at least a portion of the water employed in the humidifier.
- the so cooled compressed mixed gas 334B is then fed to the acid gas removal unit 350 (preferably a solvent based acid gas removal unit or a membrane based carbon dioxide removal unit).
- Carbon dioxide product stream 352 leaves the plant (e.g., as commercial product) while the carbon dioxide depleted compressed mixed gas 336 is fed to the humidifier 380.
- Humidifier 380 produces humid gas stream 314 from the carbon dioxide depleted compressed mixed gas 336, wherein the humid gas stream 314 is heated in the aftercooler 360 to form heated humid gas stream 314', which is fed into combustor 310.
- contemplated configurations significantly facilitate recovery of carbon dioxide contained in flue gas with relatively low carbon dioxide partial pressure, which is particularly desirable in the case of a gas turbine where a large amount of excess air is employed. Consequently, the size of the carbon dioxide recovery equipment as well as the power consumed by the blower to overcome the pressure drop of the carbon dioxide recovery equipment (e.g., direct contact cooler and the absorber) may be significantly reduced in configurations according to the inventive subject matter when compared to numerous known configurations.
- exhaust gas recycling may be employed in numerous configurations that include a turbine driving a load (e.g., generator or compressor), it is generally preferred that plant configurations in which exhaust is at least partially recycled are plants that include a humid air turbine (HAT), and an exemplary plant that includes a HAT is described in U.S. Pat. No. 4,829,763 to Rao, which is incorporated by reference herein.
- HAT humid air turbine
- FIG. 4 contemplated configurations include a HAT cycle
- previously existing difficulties of known HAT cycles may be overcome by contemplated carbon dioxide removal configurations.
- previously known HAT cycle configurations typically required customized turbo machinery in which the compressor of the gas turbine needed to be significantly smaller than the expander.
- contemplated configurations are not only expected to improve the economics of carbon dioxide recovery in gas turbine based plants, but also to implement carbon dioxide recovery to existing recuperated gas turbines (e.g., recuperated gas turbines commercially available from Sulzer Turbo or MAN GHH Borsig).
- configurations and methods according to the inventive subject matter may also be utilized in relatively small power plants with a capacity of 10 MW or less to recover carbon dioxide from the combustion gases.
- contemplated configurations and methods may be included in all plants in which a gas turbine are employed to drive a compressor or generator.
- the so isolated carbon dioxide may be utilized in a variety of processes, and particularly contemplated processes include urea plants, and enhanced oil recovery.
- isolated carbon dioxide may be sold for medical or nutritional use, employed in freezing processes, or pumped into mines, the ocean, or other locations where carbon dioxide may be at least temporarily sequestered.
- the makeup water to the humidifier in contemplated configurations may be provided by various sources, including waste water (e.g., from within the plant), recycled water, or fresh water.
- waste water e.g., from within the plant
- recycled water e.g., from within the plant
- particularly preferred methods and configurations include physical solvent based processes (see e.g., U.S. Pat. No. 2,863,527, U.S. Pat. No. 2,926,751, U.S. Pat. No. 3,505,784, U.S. Pat. No. 2,649,166, or U.S. Pat. No. 3,773,896, all incorporated by reference herein), chemical solvent based processes (see e.g., U.S. Pat. No. 3,563,695, or U.S. Pat. No. 2,177,068, both incorporated by reference herein), membrane processes (see e.g., U.S. Pat. No. 4,705,540 or U.S. Pat. No. 4,741,744, both incorporated by reference herein), and autorefrigeration (see e.g., U.S. Pat. No. 6,301,927, incorporated by reference herein).
- physical solvent based processes see e.g., U.S. Pat. No. 2,863,527, U.
- the quantity of recycled expanded exhaust 118B may vary considerably and will depend, among other factors, on the particular carbon dioxide removal unit and/or partial pressure of the carbon dioxide in the compressed mixed gas. Thus, it is generally contemplated that the amount of recycled expanded exhaust 118B may be within the range of 0 vol% and 100 vol% of the total expanded exhaust 118. However, and particularly where the exhaust gas has a relatively low carbon dioxide partial pressure, it is preferred that the amount of recycled expanded exhaust 118B is between about 25 vol% and 75 vol% of the total expanded exhaust 118.
- autorefrigeration is employed as depicted in Figure 2
- suitable quantities of compressed mixed gas stream 234B will be in the range between about 20 vol% and 80 vol%.
- contemplated configurations include a partial HAT configuration as depicted in Figure 3
- the quantity of mixed compressed gas 334 A that is directly routed to the combustor may advantageously be between about 5 vol% and 50 vol%.
- the quantity of mixed compressed gas 334A may also be higher than 50 vol%.
- cooled expanded exhaust gas stream 318B that is recycled back to the compressor, it is contemplated that suitable amounts will vary considerably. However, it is generally preferred that the amount of cooled expanded exhaust gas stream 318B will be in the range between about 25 vol% to about 75 vol%.
- Mixing of the recycled cooled expanded exhaust gas stream may be performed in numerous manners, and all known manners of mixing are contemplated suitable herein. For example, where an existing plant is retrofitted to a configuration according to the inventive subject matter, mixing may be performed in a mixing vessel upstream of the compressor inlet. On the other hand, where a configuration according to the inventive subject matter is built from scratch, mixing may be performed by supplying recycled gas to the compressor inlet along with fresh air.
- a plant may include a humid air turbine combustor that receives fuel and humid carbon dioxide depleted gas stream, wherein at least part of the humid carbon dioxide depleted gas stream is formed from an exhaust gas of the humid air turbine combustor.
- Such plants may advantageously further comprise a humidifier, wherein water used in the humidifier is heated by at least one of the compressed mixed gas and the exhaust gas.
- carbon dioxide depleted gas stream refers to any gas from which at least a portion of the carbon dioxide has previously been removed.
- a plant in which carbon dioxide is removed from an exhaust gas of a turbine combustor will comprise a compressor that compresses air and at least a portion of the exhaust gas to form a compressed mixed gas, wherein carbon dioxide is removed from the compressed mixed gas in an acid gas removal unit.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Separation Using Semi-Permeable Membranes (AREA)
- Treating Waste Gases (AREA)
- Carbon And Carbon Compounds (AREA)
Abstract
Description
Claims
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/US2003/008340 WO2004083615A1 (en) | 2003-03-18 | 2003-03-18 | Humid air turbine cycle with carbon dioxide recovery |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1604102A1 true EP1604102A1 (en) | 2005-12-14 |
| EP1604102A4 EP1604102A4 (en) | 2011-09-07 |
Family
ID=33029254
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP03716695A Withdrawn EP1604102A4 (en) | 2003-03-18 | 2003-03-18 | Humid air turbine cycle with carbon dioxide recovery |
Country Status (8)
| Country | Link |
|---|---|
| EP (1) | EP1604102A4 (en) |
| JP (1) | JP4377818B2 (en) |
| CN (1) | CN100430583C (en) |
| AU (1) | AU2003220393B2 (en) |
| CA (1) | CA2519145C (en) |
| EA (1) | EA008112B1 (en) |
| MX (1) | MXPA05009856A (en) |
| WO (1) | WO2004083615A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1566529A4 (en) * | 2002-10-08 | 2008-05-07 | Kawasaki Heavy Ind Ltd | ATMOSPHERIC PRESSURE COMBUSTION TURBINE SYSTEM |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102004039164A1 (en) * | 2004-08-11 | 2006-03-02 | Alstom Technology Ltd | Method for generating energy in a gas turbine comprehensive power generation plant and power generation plant for performing the method |
| FR2891013B1 (en) * | 2005-09-16 | 2011-01-14 | Inst Francais Du Petrole | GENERATION OF ENERGY BY GAS TURBINE WITHOUT C02 EMISSION |
| US7827778B2 (en) * | 2006-11-07 | 2010-11-09 | General Electric Company | Power plants that utilize gas turbines for power generation and processes for lowering CO2 emissions |
| EP2325456B1 (en) * | 2009-11-19 | 2016-01-27 | Douglas Wilbert Paul Smith | Gas turbine cycle with water injection for generating electricity |
| JP5117431B2 (en) * | 2009-03-09 | 2013-01-16 | 株式会社日立製作所 | CO2 recovery type gas turbine plant |
| US20110094230A1 (en) * | 2009-10-27 | 2011-04-28 | Matthias Finkenrath | System and method for carbon dioxide capture in an air compression and expansion system |
| CH703770A1 (en) * | 2010-09-02 | 2012-03-15 | Alstom Technology Ltd | Method for flushing abgasrezirkulationsleitungen a gas turbine. |
| US8726628B2 (en) * | 2010-10-22 | 2014-05-20 | General Electric Company | Combined cycle power plant including a carbon dioxide collection system |
| FR2969263B1 (en) * | 2010-12-15 | 2013-01-04 | Air Liquide | INTEGRATED METHOD AND APPARATUS FOR AIR COMPRESSION AND PRODUCTION OF A CARBON DIOXIDE-RICH FLUID |
| US20130061600A1 (en) * | 2011-09-13 | 2013-03-14 | General Electric Company | Method of controlling temperature of gas turbine components using a compressed moisurized coolant |
| EP3290794A1 (en) * | 2016-09-05 | 2018-03-07 | Technip France | Method for reducing nox emission |
| JP6795419B2 (en) * | 2017-02-06 | 2020-12-02 | 三菱パワー株式会社 | Moisture utilization gas turbine |
| CN110375330B (en) * | 2019-06-06 | 2020-10-13 | 清华大学 | A kind of staged oxygen supply combustion chamber and gas turbine staged oxygen supply combustion method |
| CN116971858A (en) * | 2023-08-03 | 2023-10-31 | 河南柴油机重工有限责任公司 | Gas engine exhaust system with exhaust gas recirculation and waste heat utilization |
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| US2065112A (en) | 1933-12-01 | 1936-12-22 | Girdler Corp | Process for separating acidic gases |
| US2399142A (en) | 1942-06-22 | 1946-04-23 | Girdler Corp | Thermal dissociation of monoethanolamine salts |
| US2377966A (en) | 1943-04-10 | 1945-06-12 | Girdler Corp | Stabilization of monoethanolamine solutions |
| US3137654A (en) | 1961-03-28 | 1964-06-16 | Wayne W Johnson | Stabilization of aqueous alkanolamine solutions in gas treating processes |
| US4477419A (en) | 1983-03-03 | 1984-10-16 | The Dow Chemical Company | Process for the recovery of CO2 from flue gases |
| ZA85528B (en) * | 1984-02-01 | 1986-12-30 | Fluor Corp | Process for producing power |
| US5160096A (en) * | 1991-10-11 | 1992-11-03 | United Technologies Corporation | Gas turbine cycle |
| US5513488A (en) * | 1994-12-19 | 1996-05-07 | Foster Wheeler Development Corporation | Power process utilizing humidified combusted air to gas turbine |
| JPH10110628A (en) * | 1996-10-08 | 1998-04-28 | Hitachi Ltd | Gas turbine exhaust treatment system |
| US6256976B1 (en) * | 1997-06-27 | 2001-07-10 | Hitachi, Ltd. | Exhaust gas recirculation type combined plant |
| EP0939199B1 (en) * | 1998-02-25 | 2004-03-31 | ALSTOM Technology Ltd | Power plant and process for operating a power plant with a CO2-cycle |
| EP0953748B1 (en) * | 1998-04-28 | 2004-01-28 | ALSTOM (Switzerland) Ltd | Power plant with a CO2-cycle |
| JP2000204965A (en) * | 1999-01-14 | 2000-07-25 | Ishikawajima Harima Heavy Ind Co Ltd | Gas turbine power generation system using methane gas |
| JP4094185B2 (en) * | 1999-08-24 | 2008-06-04 | 三井造船株式会社 | Cold power generation system |
| US6578354B2 (en) * | 2000-01-21 | 2003-06-17 | Hitachi, Ltd. | Gas turbine electric power generation equipment and air humidifier |
| WO2001075277A1 (en) * | 2000-03-31 | 2001-10-11 | Northern Research And Engineering Corporation | Solid-fueled power generation system with carbon dioxide sequestration and method therefor |
| US6550252B2 (en) | 2000-10-12 | 2003-04-22 | Texaco Inc. | Nitrogen stripping of hydrotreater condensate |
| FR2825935B1 (en) * | 2001-06-14 | 2003-08-22 | Inst Francais Du Petrole | LOW CO2 EMISSIONS POWER GENERATOR AND ASSOCIATED METHOD |
-
2003
- 2003-03-18 CN CNB038261766A patent/CN100430583C/en not_active Expired - Fee Related
- 2003-03-18 WO PCT/US2003/008340 patent/WO2004083615A1/en not_active Ceased
- 2003-03-18 EP EP03716695A patent/EP1604102A4/en not_active Withdrawn
- 2003-03-18 MX MXPA05009856A patent/MXPA05009856A/en active IP Right Grant
- 2003-03-18 JP JP2004569658A patent/JP4377818B2/en not_active Expired - Fee Related
- 2003-03-18 AU AU2003220393A patent/AU2003220393B2/en not_active Ceased
- 2003-03-18 EA EA200501472A patent/EA008112B1/en unknown
- 2003-03-18 CA CA002519145A patent/CA2519145C/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1566529A4 (en) * | 2002-10-08 | 2008-05-07 | Kawasaki Heavy Ind Ltd | ATMOSPHERIC PRESSURE COMBUSTION TURBINE SYSTEM |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2006514209A (en) | 2006-04-27 |
| EA008112B1 (en) | 2007-04-27 |
| EA200501472A1 (en) | 2006-02-24 |
| CN1759233A (en) | 2006-04-12 |
| CA2519145C (en) | 2009-11-03 |
| AU2003220393B2 (en) | 2010-04-01 |
| WO2004083615A1 (en) | 2004-09-30 |
| MXPA05009856A (en) | 2005-12-06 |
| EP1604102A4 (en) | 2011-09-07 |
| CN100430583C (en) | 2008-11-05 |
| AU2003220393A1 (en) | 2004-10-11 |
| JP4377818B2 (en) | 2009-12-02 |
| CA2519145A1 (en) | 2004-09-30 |
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