EP2541175A2 - Unité de séparation d'air et systèmes l'incorporant - Google Patents
Unité de séparation d'air et systèmes l'incorporant Download PDFInfo
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- EP2541175A2 EP2541175A2 EP12173515A EP12173515A EP2541175A2 EP 2541175 A2 EP2541175 A2 EP 2541175A2 EP 12173515 A EP12173515 A EP 12173515A EP 12173515 A EP12173515 A EP 12173515A EP 2541175 A2 EP2541175 A2 EP 2541175A2
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- 238000000926 separation method Methods 0.000 title claims abstract description 16
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims abstract description 79
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 41
- 239000000446 fuel Substances 0.000 claims abstract description 17
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 claims abstract description 16
- 238000011084 recovery Methods 0.000 claims abstract description 15
- 238000000034 method Methods 0.000 claims abstract description 13
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 57
- 238000004821 distillation Methods 0.000 claims description 52
- 239000001569 carbon dioxide Substances 0.000 claims description 40
- 229910002092 carbon dioxide Inorganic materials 0.000 claims description 40
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 32
- 239000001301 oxygen Substances 0.000 claims description 32
- 229910052760 oxygen Inorganic materials 0.000 claims description 32
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 claims description 18
- 230000006835 compression Effects 0.000 claims description 15
- 238000007906 compression Methods 0.000 claims description 15
- 238000001816 cooling Methods 0.000 claims description 13
- 239000003546 flue gas Substances 0.000 claims description 13
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 8
- 238000004891 communication Methods 0.000 claims description 7
- 239000003345 natural gas Substances 0.000 claims description 4
- 239000012530 fluid Substances 0.000 claims description 3
- 239000007788 liquid Substances 0.000 abstract description 25
- 239000007789 gas Substances 0.000 abstract description 22
- 238000002485 combustion reaction Methods 0.000 abstract description 14
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 13
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 229910002091 carbon monoxide Inorganic materials 0.000 description 5
- 239000010795 gaseous waste Substances 0.000 description 5
- 239000007800 oxidant agent Substances 0.000 description 4
- 239000000047 product Substances 0.000 description 4
- 239000002826 coolant Substances 0.000 description 3
- 238000010248 power generation Methods 0.000 description 3
- 238000009833 condensation Methods 0.000 description 2
- 230000005494 condensation Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 239000007792 gaseous phase Substances 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- VUZPPFZMUPKLLV-UHFFFAOYSA-N methane;hydrate Chemical compound C.O VUZPPFZMUPKLLV-UHFFFAOYSA-N 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009919 sequestration Effects 0.000 description 2
- 239000006227 byproduct Substances 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- -1 for example Chemical compound 0.000 description 1
- 239000002803 fossil fuel Substances 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000005380 natural gas recovery Methods 0.000 description 1
- 238000004322 natural resource recovery Methods 0.000 description 1
- JCXJVPUVTGWSNB-UHFFFAOYSA-N nitrogen dioxide Inorganic materials O=[N]=O JCXJVPUVTGWSNB-UHFFFAOYSA-N 0.000 description 1
- 239000003129 oil well Substances 0.000 description 1
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
- F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
- F25J3/02—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream
- F25J3/04—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air
- F25J3/04521—Coupling of the air fractionation unit to an air gas-consuming unit, so-called integrated processes
- F25J3/04527—Integration with an oxygen consuming unit, e.g. glass facility, waste incineration or oxygen based processes in general
- F25J3/04533—Integration with an oxygen consuming unit, e.g. glass facility, waste incineration or oxygen based processes in general for the direct combustion of fuels in a power plant, so-called "oxyfuel combustion"
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- F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
- F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
- F25J3/02—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream
- F25J3/04—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air
- F25J3/04006—Providing pressurised feed air or process streams within or from the air fractionation unit
- F25J3/04078—Providing pressurised feed air or process streams within or from the air fractionation unit providing pressurized products by liquid compression and vaporisation with cold recovery, i.e. so-called internal compression
- F25J3/04084—Providing pressurised feed air or process streams within or from the air fractionation unit providing pressurized products by liquid compression and vaporisation with cold recovery, i.e. so-called internal compression of nitrogen
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- F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
- F25J3/02—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream
- F25J3/04—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air
- F25J3/04006—Providing pressurised feed air or process streams within or from the air fractionation unit
- F25J3/04078—Providing pressurised feed air or process streams within or from the air fractionation unit providing pressurized products by liquid compression and vaporisation with cold recovery, i.e. so-called internal compression
- F25J3/0409—Providing pressurised feed air or process streams within or from the air fractionation unit providing pressurized products by liquid compression and vaporisation with cold recovery, i.e. so-called internal compression of oxygen
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- F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
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- F25J3/04248—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion
- F25J3/04284—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams
- F25J3/0429—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams of feed air, e.g. used as waste or product air or expanded into an auxiliary column
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- F25J3/04248—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion
- F25J3/04284—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams
- F25J3/0429—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams of feed air, e.g. used as waste or product air or expanded into an auxiliary column
- F25J3/04296—Claude expansion, i.e. expanded into the main or high pressure column
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- F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
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- F25J3/04248—Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion
- F25J3/04375—Details relating to the work expansion, e.g. process parameter etc.
- F25J3/04387—Details relating to the work expansion, e.g. process parameter etc. using liquid or hydraulic turbine expansion
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- F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
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- F25J3/044—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air using a single pressure main column system only
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- F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
- F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
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- F25J3/04406—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air using a dual pressure main column system
- F25J3/04424—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air using a dual pressure main column system without thermally coupled high and low pressure columns, i.e. a so-called split columns
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- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
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- F25J3/04521—Coupling of the air fractionation unit to an air gas-consuming unit, so-called integrated processes
- F25J3/04563—Integration with a nitrogen consuming unit, e.g. for purging, inerting, cooling or heating
- F25J3/04569—Integration with a nitrogen consuming unit, e.g. for purging, inerting, cooling or heating for enhanced or tertiary oil recovery
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- F25J3/00—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
- F25J3/02—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream
- F25J3/04—Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air
- F25J3/04521—Coupling of the air fractionation unit to an air gas-consuming unit, so-called integrated processes
- F25J3/04563—Integration with a nitrogen consuming unit, e.g. for purging, inerting, cooling or heating
- F25J3/04575—Integration with a nitrogen consuming unit, e.g. for purging, inerting, cooling or heating for a gas expansion plant, e.g. dilution of the combustion gas in a gas turbine
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- F25J2260/00—Coupling of processes or apparatus to other units; Integrated schemes
- F25J2260/80—Integration in an installation using carbon dioxide, e.g. for EOR, sequestration, refrigeration etc.
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- F25J2290/12—Particular process parameters like pressure, temperature, ratios
Definitions
- the invention relates generally to air separation units and systems incorporating the air separation units. More particularly, the invention relates to separation of nitrogen and oxygen from air in liquid form and systems incorporating these products for use in, for example, such applications as power generation and natural resource recovery.
- Exhaust streams generated by the combustion of fossil fuels in, for example, power generation systems contain nitrogen oxides (NO x ) and carbon monoxide (CO) as byproducts during combustion.
- a method for achieving near-zero NO x is the oxy-fuel combustion process.
- pure oxygen typically in combination with a secondary gas such as carbon dioxide
- carbon dioxide is used as the oxidizer, as opposed to using air, thereby resulting in a flue gas with negligible NO x emissions.
- oxy-fuel combustion is an attractive technology for applications, such as carbon dioxide (CO 2 ) production or sequestration, that benefit from production of CO 2 with low levels of oxygen contamination.
- a CO 2 separation unit In gas turbines that operate by way of an oxy-fuel process, a CO 2 separation unit is not needed, because the main component of combustion exhaust includes primarily CO 2 , and water (H 2 O). By condensing H 2 O a high concentration stream of CO 2 may be produced and can be used for CO 2 sequestration or other CO 2 applications.
- An air separation unit separates oxygen and nitrogen and is useful as an oxygen source for an oxy-fuel process and for separately providing high purity nitrogen.
- the high purity nitrogen obtained by ASU can be used for any of various applications, such as oil or gas reservoir management in an enhanced oil or gas recovery system, for instance.
- Nitrogen and carbon dioxide can be used as injection fluids in enhanced oil recovery (EOR). Nitrogen can be an economic alternative to carbon dioxide for EOR application.
- the pressure of nitrogen injected into an oil well is greater than the minimum miscible pressure (MMP) of nitrogen and that oil.
- MMP minimum miscible pressure
- Nitrogen forming a miscible slug with oil aids in freeing the oil for recovery. Therefore, generally the gaseous low-pressure nitrogen supplied by the ASU is compressed to higher pressure before injecting into the oil reservoirs.
- the nitrogen separated from the oxygen in the ASU is afterwards compressed in gaseous phase to the desired pressure, which demands a significant amount of power.
- the present invention resides in a system including an air separation unit.
- the air separation unit includes an air compression unit configured to produce compressed air at a pressure greater than about 3 bars; a heat-exchanger unit configured to receive and cool the compressed air to produce cooled air; a first distillation unit configured to receive the cooled air and produce a first output stream comprising liquid-nitrogen; and a first pump in direct communication with the first distillation unit and configured to pressurize the first output stream to a pressure greater than atmospheric pressure.
- the invention resides in a method including the steps of compressing air in an air compression unit to a pressure greater than about 3 bars; cooling the compressed air by passing through a heat-exchanger unit; distilling the cooled air stream in a distillation unit to produce a first stream comprising liquid-nitrogen, and a second stream; and pressurizing the first stream to a pressure greater than atmospheric pressure.
- Embodiments of the present invention include an ASU that may provide clean, pressurized liquid nitrogen and oxygen output and systems integrated with the ASU.
- an oxy-fuel combined cycle power plant system 10 includes an air separation unit (ASU) 12, a combustor 14, and a power plant with cooling system 16, as depicted in FIG. 1 .
- the ASU 12 separates oxygen from air, providing a supply of oxygen as an oxidizer to the combustor 14.
- the combustor 14 is configured to burn fuel in the presence of this supplied oxygen, either alone or after mixing with CO 2 .
- Nitrogen from the ASU 12 can be stored in a reservoir management unit 18 and/or used for other applications, such as, for example, recovering natural gas from gas fields or for oil recovery. Products of combustion normally contain mainly CO 2 , H 2 O and trace emissions of CO and O 2 .
- the cooling system 16 embedded in power plant condenses H 2 O from exhaust downstream of combustor 14, resulting in exhaust gases exceeding 95% CO 2 composition.
- a system including an ASU is provided.
- the ASU is configured to liquefy nitrogen at very low temperatures.
- the ASU is also configured to liquefy oxygen.
- the liquid oxygen may be pumped to a pressure suitable for oxy-fuel combustion.
- the liquid nitrogen may be pumped to a very high pressure (300-500 bars) and injected into an oil/gas reservoir for enhanced oil /gas recovery.
- the system is configured to produce a carbon dioxide stream from exhaust products of the oxy-fuel combustor.
- the carbon dioxide stream produced here is a high-content CO 2 stream.
- a "high-content CO 2 stream” is defined as a stream having more than about 80% by volume of CO 2 .
- a high-content CO 2 stream contains more than about 90% by volume of CO 2 .
- the high-content CO 2 stream contains more than about 95% by volume of CO 2 .
- a stream "substantially free of oxygen” is defined as a stream containing less than about 1% by volume of oxygen. In one embodiment, an oxygen level of less than 10 ppm in the CO 2 exhaust stream is desirable.
- One example of an application where a high-content CO 2 stream is desirable is oil recovery from depleted oil recovery wells, where CO 2 stream injection is used to force oil from the well.
- a portion of the high-content CO 2 exhaust gases may also be recirculated to the combustor 14, for mixing with the separated O 2 from the ASU 12. Maintaining minimum CO emissions from the combustion helps in maintaining high combustion efficiency.
- system 10 comprises an ASU 12, as shown in FIG. 2 .
- the ASU 12 includes an air compression unit 20; a heat-exchanger unit 22; a first distillation unit 26; and a first pump 28.
- a "unit" may be made up of a single component or made up of more than one component.
- an air compressor unit may be one compressor or may have more than one compressors combined to produce the required air compression.
- the air compression unit 20 is configured to produce compressed air to a pressure greater than about 3 bars. In one embodiment, the air compression unit 20 is configured to produce a compressed air to a pressure greater than about 7 bars. In a further embodiment, the air compression unit 20 is configured to produce a compressed air at a pressure in a range from about 15 bars to about 60 bars. In one particular embodiment, the air compression unit 20 is configured to produce compressed air to a pressure up to about 40 bars.
- the compressed air passes through the heat-exchanger unit 22, where the air is cooled. The cooling of compressed air is attained by the heat-exchange between different streams that pass through the heat-exchanger unit 22. For example, cool nitrogen and / or oxygen streams separated from air may pass through the heat-exchanger unit 22 absorbing heat from the compressed air and, thereby, cooling the compressed air.
- the cooled, compressed air may be subjected to expansion in an expander 24, which further cools the already cooled air.
- an expander 24 is a valve introducing a pressure difference to the incoming cooled compressed air.
- the cooled compressed air gets expanded suddenly to a lower pressure, resulting in further cooled, reduced pressure-compressed air.
- the pressure of the compressed air, after passing through the expander 24 is less than about 5 bars. In one embodiment, the pressure of the air after passing through the expander 24 is less than about 3 bars.
- the expanded air coming out of the expander 24 is at atmospheric pressure.
- the cooled air passed through the expander 24 enters the first distillation unit 26.
- the first distillation unit 26 is configured to operate at a pressure greater than about 2 bars and is called as a "high-pressure distillation unit".
- an inlet pressure of the first distillation unit is in the range from about 3.5 bars to about 5 bars.
- the first distillation unit 26 operates at atmospheric pressure.
- the compressed air entering the first distillation unit 26 is generally at relatively low temperature.
- the temperature of the air entering the first distillation unit 26 is in between about -150°C and about -210°C. In one further embodiment, the temperature of the air is in the range from about -165°C to about - 185°C.
- the temperature of the air entering first distillation unit 26 is determined in part by the initial pressure of the compressed air, the ability of the heat-exchanger unit 22 to cool the compressed air and the configuration of the expander 24 to expand the cooled air.
- a high pressure compressed air ends up giving out more heat at the time of expansion compared to air compressed to a lower pressure.
- a heat-exchanger unit 22 that has low temperature coolant streams will effectively extract more heat from the compressed air compared to a heat exchanger unit 22 having higher temperature coolant streams.
- the volume, pressure difference, and the temperature of the expander 24 may change the heat extracted from the air passing through the expander 24.
- a first output stream 30 produced from the first distillation unit 26 comprises liquid nitrogen.
- the first output stream 30 produced from the first distillation unit 26 comprises more than about 25 % of the inlet compressed air mass flow and comprises high purity liquid nitrogen.
- the liquid nitrogen of first output stream 30 is of greater than 95% purity.
- the liquid nitrogen is more than about 99% pure.
- the liquid nitrogen is of more than 99.9% purity.
- the temperature of first output stream 30 produced from the first distillation unit 26 is less than about -175°C.
- the temperature of first output stream 30 is less than about -178°C.
- the temperature of the first output stream 30 is in the range from about -178°C to about -185°C.
- the pressure of the first output stream 30 is greater than atmospheric pressure. In one embodiment, the pressure of the first output stream 30 is greater than about 3 bars. In one particular embodiment, the pressure of the first output stream ranges from about 3.5 bars to about 5 bars.
- the first output stream 30 is further pressurized using a first pump 28. In one embodiment, the first pump 28 is in direct communication with the first distillation unit 26. As used herein the "direct communication" between the pump 28 and distillation unit 26 means that the first output stream 30 from the distillation unit 26 is directly pumped to high pressure without intervening expansion or gas-liquid separation. In one embodiment the first output stream 30 is pressurized to greater than about 300 bars.
- the first output stream is pressurized to greater than about 400 bars. In one embodiment, the first output stream 30 is pressurized up to about 500 bars. In one embodiment, the first pump 28 is coupled to the heat-exchanger unit 22 so that the first output stream 30 pressurized by the first pump 28 passes through the heat-exchanger unit 22 thereby cooling the incoming compressed air. As used herein "coupled” merely implies fluid communication and does not prohibit the usage of intervening parts such as valves.
- the first output stream 30 may be transported for different applications.
- the first output stream 30 passes through the heat-exchanger unit 24, thereby removing some heat from the incoming compressed air from the compressor unit 20.
- the low-temperature liquid form of the first output stream 30 is comparatively more effective than gaseous nitrogen in reducing the temperature of the incoming compressed air.
- the distillation unit 26 is left with a second output stream 32 that comprises nitrogen and oxygen ( FIG. 2 ).
- the second output stream 32 may be drawn out from the distillation unit 26 and may be subjected to further distillation, using, for example a second distillation unit 36. Depending on the pressure of the second output stream 32, it may be further subjected to expansion in a second expander 34, as shown in FIG. 2 .
- the outlet pressure of the second expander 34 is near atmospheric and the temperature of the contents in a range from about -190°C to about -195°C.
- the vapor fraction of the output contents of second expander 34 is in the range from about 0.12 to 0.18.
- the stream coming out from the second expander 34 may be in a liquid state, gaseous state, or in a liquid-gas mixed state. Therefore, depending on the requirement, the second output stream 32 optionally may be subjected to a gas-liquid separation in a separator 35. In one embodiment, both the gaseous part and liquid part of the second output stream 32 are fed into the second distillation column 36.
- the second distillation unit 36 is a low pressure distillation unit. The pressure at the distillation unit may be less than about 2 bars. In one embodiment, the low pressure distillation unit 36 works at atmospheric pressure.
- the second distillation unit 36 may have one or more outputs.
- One distillation output is third output stream 38 comprising liquid oxygen.
- the third output stream 38 is about 15 mass % or more of the inlet compressed air and comprises high purity liquid oxygen.
- the liquid oxygen of the third output stream 38 is of greater than 95% purity.
- the liquid oxygen is more than about 99% pure.
- the liquid oxygen is of more than 99.9% purity.
- the temperature of the third output stream 38 produced at the distillation unit 36 is less than about -175°C. In one embodiment, the temperature of the third output stream 38 is less than about -178°C.
- the pressure of third output stream 38 is greater than atmospheric pressure.
- the third output stream 38 is further pressurized using a second pump 39.
- the third output stream 38 is pressurized to greater than about 20 bars.
- the third output stream 38 is pressurized in a range from about 30 bars to about 60 bars.
- the third output stream is pressurized up to about 100 bars of pressure.
- the third output stream 38 produced by the distillation may be transported for different applications including oxy-fuel combustion. Similar to the first output stream 30, during conveyance to the intended application, the third output stream 38 may be routed through the heat-exchanger unit 22, thereby helping to remove heat from the compressed air from the compressor unit 20.
- the low-temperature liquid form of the third output stream 38 comprising oxygen is comparatively more effective than the gaseous oxygen in reducing the temperature of the incoming compressed air.
- one output of the second distillation unit is a fourth output stream 40 comprising nitrogen and oxygen.
- the fourth output stream 40 includes both nitrogen and oxygen in gaseous form.
- the temperature of this stream is about -190°C.
- the fourth output stream 40 measures about 40-60 % of the inlet compressed air mass flow.
- the composition of the mixed stream 40 includes about 87 mole % (of fourth output stream 40) of nitrogen and 12 mole % of oxygen.
- the fourth output stream 40 may be used for different applications, including as an oxidizer in a combustion turbine. For example, if used in a combustor that generally uses air as an oxidizer, the fourth output stream 40 will reduce the NOx emission of the combustor. In one embodiment, the stream 40 may be recycled to the air compression unit 20 or to the distillation unit 26.
- the fourth output stream 40 may contribute to the cooling of compressed air passing through the heat-exchanger unit 22.
- the pressures of compressed air supplied by the compression unit 20, the pressure differences and the resultant cooling obtained through the expanders 24, 34, and the distillation conditions in the distillation units 26, 36 may be greatly varied to achieve higher purity, higher content liquid nitrogen and/or liquid oxygen streams. All such variations are believed to be apparent to one skilled in the art considering the teachings of this disclosure.
- compressor unit 20 is configured to produce compressed air to a pressure greater than about 35 bars. In one embodiment, the pressure of the compressed air is about 40 bars.
- the high-pressure compressed air is passed through the heat-exchanger unit 22 and cooled.
- the cooled compressed air from the heat-exchanger unit is subjected to expansion in an expander 24.
- the heat-exchanger unit 22 as used herein may be one unit or a combination of multiple heat-exchanger units.
- the expander 24 expands the compressed air by quickly reducing pressure ("flashing") to atmospheric pressure such that the air rapidly cools to a liquid form with a temperature less than about -185°C.
- the cooled liquid is subjected to distillation in the first distillation unit 26 to directly produce high-purity first output stream 30 comprising liquid nitrogen and a second output stream 32 comprising liquid-oxygen.
- first output stream 30 and the second output stream 32 are in liquid forms. Therefore, in one embodiment, the first distillation unit 26 is a liquid-liquid separator.
- the first output stream 30 is a liquid nitrogen stream and the second output stream 32 is a liquid oxygen stream.
- the second output stream comprising liquid oxygen may be further subjected to pressurizing by using a pump 39 and used in different applications.
- a number of heat-exchanger units and coolant streams may be effectively used to cool the air stream that is subjected to distillation in the first distillation unit 26.
- the incoming compressed air from the compressor 20 is split in to a first stream 41 and a second stream 42 using a splitter 43.
- the first stream passes through a second heat-exchanger unit 44 and third heat-exchanger unit 45 to be cooled further.
- the first stream 41 cooled through the multiple heat-exchangers 44, 45 is expanded in the expander 24.
- the cooled air coming from expander 24 may be subjected to a liquid-gas separation in a separator 25, using the liquid part for distillation unit 26 and leaving a gaseous waste stream 46 that may be routed through one or more heat-exchanger units 22, 44, 45 to further cool the incoming compressed air.
- the second stream 42 of the compressed air from splitter 43 may be optionally used in a turbine 48 and the cooled stream 42 is mixed in a mixer 49 with the gaseous waste stream 46.
- the second stream 42 and the gaseous waste stream 46 may be mixed before passing through any of the second heat-exchanger units 22, 44, and 45.
- the gaseous waste stream 46 is passed through the third heat-exchanger 45 and then mixed with the second stream 42 before passing through the second heat-exchanger unit 44, thereby effectively cooling the cooled air stream 41 passing from the third heat-exchanger 45 to the expander 24.
- the system 50 includes an ASU 12 providing oxygen output; a combustor 14 configured to receive oxygen from ASU 12 and to combust a fuel stream 58, thereby generating a flue gas 62.
- cooling system 16 is fluidly coupled to the combustor 14 through a turbine combined cycle 64.
- the gas turbine combined cycle 64 may receive flue gas 62 from the combustor 14, and use at least a part of the energy associated with the flue gas 62 to generate electricity or perform some other work, releasing an exhaust flue gas 66.
- Exhaust flue gas 66 from the gas turbine combined cycle 64 may be passed through the cooling system 16, such as, for example, a water condensation system or HRSG, to condense water from the exhaust gas 66, and to create a carbon dioxide stream 70.
- the carbon dioxide stream 70 may be stored in a storage unit 72.
- the carbon dioxide stream 70 may be directed to applications that use "high-content" carbon dioxide, such as for example, a an oil/gas recovery system 78 after optional compression in a CO 2 compressor 76.
- at least a part of the carbon dioxide stream 70 is redirected to the combustor 14, after optional compression in a CO 2 compressor 76, to be mixed with the oxygen.
- a method of generating energy in a power plant that includes a gas turbine includes operating an ASU 12 ( FIG. 4 ) to separate oxygen from air, passing fuel to the combustor 14, and combusting the fuel stream 58 in the combustor 14, in the presence of oxygen.
- a flue gas 62 is generated, comprising carbon dioxide and water.
- the flue gas 62 of the combustor 14 may be used in operating the turbine 64, e.g., to generate electricity.
- the exhaust flue gas 66 of the turbine 64 can be passed through a water condensation system 16 to separate water from the exhaust gas 66, and to produce a high-content carbon dioxide stream 70.
- the high-content carbon dioxide stream 70 is substantially free of oxygen, for safety considerations in those situations where the presence of oxygen is a serious concern.
- the carbon dioxide stream 70 may be stored, directed to other applications such as an oil recovery system, and / or compressed and fed back to the combustor 14, e.g., in combination with the compressed oxygen.
- the liquid oxygen obtained by the ASU 12 may be pumped to the pressure suitable for oxy-fuel combustion in the combustor 14, the liquid nitrogen may be pumped to a very high pressure (300-500 bars) and can be injected to the oil/gas recovery system 78.
- the oil/gas recovery system 78 is a natural gas recovery system.
- the natural gas 58 recovered from the system 78 may be fed back to the combustor 14 for the oxy-fuel combustion or stored in a natural gas storing unit 80 for using in other applications.
- liquefying both nitrogen and oxygen in the high-pressure ASU as described above allows for these products to be pumped at very low temperatures, thereby increasing the overall efficiency of the combined gas turbine plant compared to existing plants that compress nitrogen and oxygen in gaseous phases.
- the system 50 is expected to potentially provide not only a higher overall energy efficiency but also a more compact and therefore cost-effective design compared to conventional systems using a low-pressure ASU.
- the power consumption of the integrated systems explained herein is about 20% less compared to a conventional integrated system.
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Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/174,056 US20130000352A1 (en) | 2011-06-30 | 2011-06-30 | Air separation unit and systems incorporating the same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2541175A2 true EP2541175A2 (fr) | 2013-01-02 |
| EP2541175A3 EP2541175A3 (fr) | 2018-03-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP12173515.3A Withdrawn EP2541175A3 (fr) | 2011-06-30 | 2012-06-26 | Unité de séparation d'air et systèmes l'incorporant |
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| Country | Link |
|---|---|
| US (1) | US20130000352A1 (fr) |
| EP (1) | EP2541175A3 (fr) |
| CN (1) | CN102853633B (fr) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US10106430B2 (en) | 2013-12-30 | 2018-10-23 | Saudi Arabian Oil Company | Oxycombustion systems and methods with thermally integrated ammonia synthesis |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4407135A (en) * | 1981-12-09 | 1983-10-04 | Union Carbide Corporation | Air separation process with turbine exhaust desuperheat |
| US4775399A (en) * | 1987-11-17 | 1988-10-04 | Erickson Donald C | Air fractionation improvements for nitrogen production |
| FR2700205B1 (fr) * | 1993-01-05 | 1995-02-10 | Air Liquide | Procédé et installation de production d'au moins un produit gazeux sous pression et d'au moins un liquide par distillation d'air. |
| GB9500120D0 (en) * | 1995-01-05 | 1995-03-01 | Boc Group Plc | Air separation |
| US5724805A (en) * | 1995-08-21 | 1998-03-10 | University Of Massachusetts-Lowell | Power plant with carbon dioxide capture and zero pollutant emissions |
| US5666823A (en) * | 1996-01-31 | 1997-09-16 | Air Products And Chemicals, Inc. | High pressure combustion turbine and air separation system integration |
| US7077202B2 (en) * | 2001-06-15 | 2006-07-18 | The Petroleum Oil and Gas Corporation of South Africa (Proprietary Limited) | Process for the recovery of oil from a natural oil reservoir |
| WO2003018958A1 (fr) * | 2001-08-31 | 2003-03-06 | Statoil Asa | Procede et installation permettant une recuperation de petrole amelioree et une synthese simultanee d'hydrocarbures a partir de gaz naturel |
| FR2862004B3 (fr) * | 2003-11-10 | 2005-12-23 | Air Liquide | Procede et installation d'enrichissement d'un flux gazeux en l'un de ses constituants |
| CN100424451C (zh) * | 2006-05-15 | 2008-10-08 | 白杨 | 超低压低温法空气分离氧气制备方法 |
| DE102007031759A1 (de) * | 2007-07-07 | 2009-01-08 | Linde Ag | Verfahren und Vorrichtung zur Erzeugung von gasförmigem Druckprodukt durch Tieftemperaturzerlegung von Luft |
| CA2728244A1 (fr) * | 2008-06-19 | 2009-12-23 | William Brigham | Procede de separation d'air hybride a enrichissement preliminaire non cryogenique et purification cryogenique faisant appel a un generateur de gaz ou de liquide a un seul composant |
| BR112012004591A2 (pt) * | 2009-09-01 | 2016-04-05 | Exxonmobil Upstream Res Co | sistema de turbina a gás de oxicombustível, e, método para uso com um sistema de turbina a gás de oxicombustível |
| CA2779712A1 (fr) * | 2009-12-17 | 2011-07-14 | Greatpoint Energy, Inc. | Procede integre de recuperation amelioree du petrole utilisant une injection d'azote |
-
2011
- 2011-06-30 US US13/174,056 patent/US20130000352A1/en not_active Abandoned
-
2012
- 2012-06-26 EP EP12173515.3A patent/EP2541175A3/fr not_active Withdrawn
- 2012-07-02 CN CN201210228197.5A patent/CN102853633B/zh not_active Expired - Fee Related
Non-Patent Citations (1)
| Title |
|---|
| None |
Also Published As
| Publication number | Publication date |
|---|---|
| US20130000352A1 (en) | 2013-01-03 |
| CN102853633B (zh) | 2016-08-10 |
| CN102853633A (zh) | 2013-01-02 |
| EP2541175A3 (fr) | 2018-03-21 |
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