US20130081409A1 - Methods and systems for co2 condensation - Google Patents

Methods and systems for co2 condensation Download PDF

Info

Publication number
US20130081409A1
US20130081409A1 US13/249,464 US201113249464A US2013081409A1 US 20130081409 A1 US20130081409 A1 US 20130081409A1 US 201113249464 A US201113249464 A US 201113249464A US 2013081409 A1 US2013081409 A1 US 2013081409A1
Authority
US
United States
Prior art keywords
stream
cooling
cooled
temperature
condensed
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.)
Abandoned
Application number
US13/249,464
Inventor
Miguel Angel Gonzalez Salazar
Vittorio Michelassi
Christian Vogel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US13/249,464 priority Critical patent/US20130081409A1/en
Assigned to GENERAL ELECTRIC COMPANY reassignment GENERAL ELECTRIC COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MICHELASSI, VITTORIO, GONZALEZ SALAZAR, MIGUEL ANGEL, VOGEL, CHRISTIAN
Priority to EP12775386.1A priority patent/EP2815194A2/en
Priority to BR112014005676-5A priority patent/BR112014005676B1/en
Priority to RU2014110121A priority patent/RU2606725C2/en
Priority to CA2848991A priority patent/CA2848991C/en
Priority to JP2014533380A priority patent/JP6154813B2/en
Priority to KR1020147011592A priority patent/KR101983343B1/en
Priority to MX2014003880A priority patent/MX2014003880A/en
Priority to CN201280047666.1A priority patent/CN104471335B/en
Priority to PCT/US2012/057860 priority patent/WO2013049532A2/en
Priority to AU2012315807A priority patent/AU2012315807C1/en
Publication of US20130081409A1 publication Critical patent/US20130081409A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J3/00Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
    • F25J3/08Separating gaseous impurities from gases or gaseous mixtures or from liquefied gases or liquefied gaseous mixtures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D53/00Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
    • B01D53/002Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols by condensation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/0002Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the fluid to be liquefied
    • F25J1/0027Oxides of carbon, e.g. CO2
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/003Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the kind of cold generation within the liquefaction unit for compensating heat leaks and liquid production
    • F25J1/0032Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the kind of cold generation within the liquefaction unit for compensating heat leaks and liquid production using the feed stream itself or separated fractions from it, i.e. "internal refrigeration"
    • F25J1/0035Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the kind of cold generation within the liquefaction unit for compensating heat leaks and liquid production using the feed stream itself or separated fractions from it, i.e. "internal refrigeration" by gas expansion with extraction of work
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process
    • F25J1/0225Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process using other external refrigeration means not provided before, e.g. heat driven absorption chillers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D2257/00Components to be removed
    • B01D2257/50Carbon oxides
    • B01D2257/504Carbon dioxide
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2220/00Processes or apparatus involving steps for the removal of impurities
    • F25J2220/80Separating impurities from carbon dioxide, e.g. H2O or water-soluble contaminants
    • F25J2220/82Separating low boiling, i.e. more volatile components, e.g. He, H2, CO, Air gases, CH4
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2230/00Processes or apparatus involving steps for increasing the pressure of gaseous process streams
    • F25J2230/30Compression of the feed stream
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2235/00Processes or apparatus involving steps for increasing the pressure or for conveying of liquid process streams
    • F25J2235/80Processes or apparatus involving steps for increasing the pressure or for conveying of liquid process streams the fluid being carbon dioxide
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2260/00Coupling of processes or apparatus to other units; Integrated schemes
    • F25J2260/80Integration in an installation using carbon dioxide, e.g. for EOR, sequestration, refrigeration etc.
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2270/00Refrigeration techniques used
    • F25J2270/90External refrigeration, e.g. conventional closed-loop mechanical refrigeration unit using Freon or NH3, unspecified external refrigeration
    • F25J2270/908External refrigeration, e.g. conventional closed-loop mechanical refrigeration unit using Freon or NH3, unspecified external refrigeration by regenerative chillers, i.e. oscillating or dynamic systems, e.g. Stirling refrigerator, thermoelectric ("Peltier") or magnetic refrigeration

Definitions

  • the present disclosure relates to methods and systems for carbon dioxide (CO 2 ) condensation using magneto-caloric cooling. More particularly, the present disclosure relates to methods and systems for CO 2 condensation in an intercooled compression and pumping train using magneto-caloric cooling.
  • CO 2 carbon dioxide
  • Power generating processes that are based on combustion of carbon containing fuel typically produce CO 2 as a byproduct. It may be desirable to capture or otherwise separate the CO 2 from the gas mixture to prevent the release of CO 2 into the environment and/or to utilize CO 2 in the power generation process or in other processes. It may be further desirable to liquefy/condense the separated CO 2 to facilitate transport and storage of the separated CO 2 .
  • CO 2 compression, liquefaction and pumping trains may be used to liquefy CO 2 for desired end-use applications. However, methods for condensation/liquefaction of CO 2 may be energy intensive.
  • a method of condensing carbon dioxide (CO 2 ) from a CO 2 stream includes (i) compressing and cooling the CO 2 stream to form a partially cooled CO 2 stream, wherein the partially cooled CO 2 stream is cooled to a first temperature.
  • the method includes (ii) cooling the partially cooled CO 2 stream to a second temperature by magneto-caloric cooling to form a cooled CO 2 stream.
  • the method further includes (iii) condensing at least a portion of CO 2 in the cooled CO 2 stream at the second temperature to form a condensed CO 2 stream.
  • a method of condensing carbon dioxide (CO 2 ) from a CO 2 stream includes (i) cooling the CO 2 stream in a first cooling stage comprising a first heat exchanger to form a first partially cooled CO 2 stream.
  • the method further includes (ii) compressing the first partially cooled CO 2 stream to form a first compressed CO 2 stream.
  • the method further includes (iii) cooling the first compressed CO 2 stream in a second cooling stage comprising a second heat exchanger to form a second partially cooled CO 2 stream.
  • the method further includes (iv) compressing the second partially cooled CO 2 stream to form a second compressed CO 2 stream.
  • the method further includes (v) cooling the second compressed CO 2 stream to a first temperature in a third cooling stage comprising a third heat exchanger to form a partially cooled CO 2 stream.
  • the method further includes (vi) cooling the partially cooled CO 2 stream to a second temperature by magneto-caloric cooling to form a cooled CO 2 stream.
  • the method further includes (vii) condensing at least a portion of CO 2 in the cooled CO 2 stream at the second temperature to form a condensed CO 2 stream.
  • a system for condensing carbon dioxide (CO 2 ) from a CO 2 stream includes (i) one or more compression stages configured to receive the CO 2 stream.
  • the system further includes (ii) one or more cooling stages in fluid communication with the one or more compression stages, wherein a combination of the one or more compression stages and the one or more cooling stages is configured to compress and cool the CO 2 stream to a first temperature to form a partially-cooled CO 2 stream.
  • the system further includes (iii) a magneto-caloric cooling stage configured to receive the partially-cooled CO 2 stream and cool the partially-cooled CO 2 stream to a second temperature to form a cooled CO 2 stream.
  • the system further includes (iv) a condensation stage configured to condense a portion of CO 2 in the cooled CO 2 stream at the second temperature, thereby condensing CO 2 from the cooled compressed CO 2 stream to form a condensed CO 2 stream.
  • FIG. 1 is a flow chart for a method of CO 2 condensation from a CO 2 stream, in accordance with one embodiment of the invention.
  • FIG. 2 is a flow chart for a method of CO 2 condensation from a CO 2 stream, in accordance with one embodiment of the invention.
  • FIG. 3 is a block diagram of a system for CO 2 condensation from a CO 2 stream, in accordance with one embodiment of the invention.
  • FIG. 4 is a block diagram of a system for CO 2 condensation from a CO 2 stream, in accordance with one embodiment of the invention.
  • FIG. 5 is a block diagram of a system for CO 2 condensation from a CO 2 stream, in accordance with one embodiment of the invention.
  • FIG. 6 is a block diagram of a system for CO 2 condensation from a CO 2 stream, in accordance with one embodiment of the invention.
  • FIG. 7 is a block diagram of a system for CO 2 condensation from a CO 2 stream, in accordance with one embodiment of the invention.
  • FIG. 8 is a block diagram of a system for CO 2 condensation from a CO 2 stream, in accordance with one embodiment of the invention.
  • FIG. 9 is a block diagram of a system for CO 2 condensation from a CO 2 stream, in accordance with one embodiment of the invention.
  • FIG. 10 is a pressure versus temperature diagram for CO 2 .
  • embodiments of the present invention include methods and systems suitable for CO 2 condensation.
  • liquefying and pumping of CO 2 may require high energy input.
  • a pressure of approximately 60 bar may be required to liquefy CO 2 at 20° C.
  • an intermediate magnetic cooling step advantageously lowers the CO 2 temperature to less than 0° C., significantly reducing the required work of the overall system.
  • an overall efficiency improvement of about 10 percent to about 15 percent may be possible using the methods and systems described herein.
  • Approximating language may be applied to modify any quantitative representation that could permissibly vary without resulting in a change in the basic function to which it is related. Accordingly, a value modified by a term or terms, such as “about”, is not limited to the precise value specified. In some instances, the approximating language may correspond to the precision of an instrument for measuring the value.
  • a method 10 for condensing carbon dioxide from a CO 2 stream is provided.
  • the CO 2 stream includes a CO 2 stream emitted from a gas turbine.
  • the CO 2 stream includes a CO 2 gas mixture emitted from a coal or natural gas-fired power plant.
  • the CO 2 stream further includes one more of nitrogen, nitrogen dioxide, oxygen, or water vapor.
  • the CO 2 stream further includes impurities or pollutants, examples of which include, but are not limited to, nitrogen, nitrogen oxides, sulfur oxides, carbon monoxide, hydrogen sulfide, unburnt hydrocarbons, particulate matter, and combinations thereof.
  • the CO 2 stream is substantially free of the impurities or pollutants.
  • the CO 2 stream essentially includes carbon dioxide.
  • the amount of impurities or pollutants in the CO 2 stream is less than about 50 mole percent. In some embodiments, the amount of impurities or pollutants in the CO 2 stream is less than about 20 mole percent. In some embodiments, the amount of impurities or pollutants in the CO 2 stream is in a range from about 10 mole percent to about 20 mole percent. In some embodiments, the amount of impurities or pollutants in the CO 2 stream is less than about 5 mole percent.
  • the method includes receiving a CO 2 stream 101 , as indicated in FIG. 3 , from a hydrocarbon processing, combustion, gasification or a similar power plant (not shown). As indicated in FIGS. 1 and 3 , at step 11 , the method 10 includes compressing and cooling the CO 2 stream 101 to form a partially cooled CO 2 stream 201 .
  • the CO 2 stream 101 may be compressed using or more compression stages 120 .
  • the CO 2 stream may be cooled using or more cooling stages 110 .
  • the CO 2 stream 101 may be compressed to a desired pressure by using one or more compression stages, as indicated by 120 in FIG. 3 .
  • the compression stage 120 may further include one or more compressors, such as, 121 and 122 , in some embodiments.
  • the two compressors 121 and 122 are shown as an exemplary embodiment only and the actual number of compressors and their individual configuration may vary depending on the end result desired.
  • the CO 2 stream 101 may be compressed to a pressure and temperature desired for the magnetic cooling and condensation steps 12 and 13 , respectively.
  • the CO 2 stream 101 may be compressed to a pressure in a range from about 10 bar to about 60 bar prior to the magnetic cooling step 12 .
  • the CO 2 stream 101 may be compressed to a pressure in a range from about 20 bar to about 40 bar prior to the magnetic cooling step 12 .
  • the CO 2 stream 101 may be cooled to a desired temperature by using one or more cooling stages, as indicated by 110 in FIG. 3 .
  • the cooling stage 110 may further include one or more heat exchangers, such as, 111 , 112 and 113 , in some embodiments.
  • the three heat exchangers 111 , 112 , and 113 are shown as an exemplary embodiment only and the actual number of heat exchangers and their individual configuration may vary depending on the end result desired.
  • one or more of the heat exchangers may be cooled using a cooling medium.
  • one more of the heat exchangers may be cooled using cooling air, cooling water, or both, as indicated by 115 in FIG. 3 .
  • the cooling stage may further include one or more intercoolers to cool the exhaust gas stream 101 without affecting the pressure.
  • cooling stage 110 and compression stage 120 is shown as an exemplary embodiment only and the actual configuration may vary depending on the end result desired.
  • the method may include cooling the CO 2 stream in a heat exchanger 111 prior to compressing the CO 2 stream in a compressor 121 (not shown).
  • the method further includes cooling the CO 2 stream 101 to a first temperature by expanding the CO 2 stream in one or more expanders 123 , as indicated in FIG. 8 .
  • the method includes an expansion step that decreases the pressure of the CO 2 stream 101 from absolute pressure levels greater than about 20 bar to pressure levels of around 20 bar, thereby decreasing the temperature of the CO 2 stream 101 to values lower than that may be reached by air or water cooling.
  • the expansion step it is believed that by employing the expansion step, the overall duty of the magneto-caloric cooling step 12 may be reduced, as the inlet temperature of the partially-cooled CO 2 stream to the magneto-caloric step may be lower than that without an expansion step.
  • the work extracted in the expansion step may be further used for the magneto-caloric cooling step 12 .
  • the CO 2 stream 101 may be cooled to a temperature and pressure desired for the magnetic cooling and condensation steps 12 and 13 .
  • the method includes compressing and cooling the CO 2 stream 101 to form a partially cooled CO 2 stream 201 , as indicated in FIG. 3 .
  • the method further includes cooling the CO 2 stream 101 to a first temperature by expanding the CO 2 stream in one or more expanders 123 to form the partially cooled CO 2 stream 201 , as indicated in FIG. 8 .
  • the method includes cooling the partially cooled CO 2 stream 201 to a first temperature.
  • the partially cooled CO 2 stream 201 may be cooled to a temperature in a range from about 5 degrees Celsius to about 35 degrees Celsius, prior to the magnetic cooling step 12 .
  • the partially cooled CO 2 stream 201 may be cooled to a temperature in a range from about 10 degrees Celsius to about 25 degrees Celsius, prior to the magnetic cooling step 12 .
  • CO 2 in the partially cooled CO 2 stream 201 is typically liquefied at a temperature in a range from about 20 degrees Celsius to about 25 degrees Celsius.
  • the condensation temperature is determined by the temperature of the cooling medium, which can be cooling water or air.
  • an absolute pressure of approximately 60 bar is required to liquefy CO 2 .
  • lower pressure may be advantageously used for condensing CO 2 from the partially cooled CO 2 stream 201 .
  • the method further includes, at step 12 , cooling the partially cooled CO 2 stream 201 to a second temperature by magneto-caloric cooling to form a cooled CO 2 stream 302 , as indicated in FIGS. 1 and 3 .
  • the method includes cooling the partially-cooled CO 2 stream 201 using a magneto-caloric cooling stage 200 , as indicated in FIG. 3 .
  • a magneto-caloric cooling stage 200 includes a heat exchanger 212 and an external magneto-caloric cooling device 211 .
  • the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212 , as shown in FIG. 3 .
  • the magneto-caloric cooling device 211 includes a cold and a hot heat exchanger, a permanent magnet assembly or an induction coil magnet assembly, a regenerator of magneto-caloric material, and a heat transfer fluid cycle.
  • the heat transfer fluid is pumped through the regenerator and the heat exchanger by a fluid pump (not shown).
  • the magneto-caloric cooling devices works on an active magnetic regeneration cycle (AMR) and provides cooling power to a heat transfer fluid by sequential magnetization and demagnetization of the magneto-caloric regenerator with flow reversal heat transfer flow.
  • AMR active magnetic regeneration cycle
  • the sequential magnetization and demagnetization of the magneto-caloric regenerator may be provided for by a rotary set-up where the regenerator passes through a bore of the magnet system.
  • the sequential magnetization and demagnetization of the magneto-caloric regenerator may be provided for by a reciprocating linear device.
  • An exemplary magnet assembly and magneto-caloric cooling device are described in U.S.
  • the heat at the hot heat exchanger may be delivered to the ambient environment. In some other embodiments, the heat at the hot heat exchanger may be delivered to the return flow of the condensed and liquefied CO 2 after the pumping of the liquid CO 2 , as described herein later.
  • the magneto-caloric cooling stage further includes a heat exchanger 212 , wherein the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212 .
  • the heat exchanger 212 is in fluid communication with the one or more cooling stages 110 and the one or more compression stages 120 .
  • the heat exchanger 212 is in fluid communication with the partially cooled CO 2 stream 201 generated after the compression and cooling step 11 .
  • the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212 such that the partially cooled CO 2 stream 201 is cooled to the second temperature.
  • the second temperature is in a range of from about 0 degrees Celsius to about ⁇ 25 degrees Celsius.
  • the second temperature is in a range of from about 5 degrees Celsius to about ⁇ 20 degrees Celsius.
  • the step 13 of cooling the partially-cooled CO 2 stream in the magneto-caloric cooling stage results in a cooled CO 2 stream.
  • the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212 such that the partially cooled CO 2 stream 201 is cooled to the second temperature, such that CO 2 condenses from the cooled CO 2 stream.
  • the method includes compressing the CO 2 stream 101 to a pressure in a range from about 20 bar to about 40 bar, in some embodiments. As indicated in FIG. 10 , at a pressure level of 40 bar, the CO 2 condenses at a temperature of 5 C. Further, as indicated in FIG. 10 , at a pressure level of 20 bar, the CO 2 condenses at a temperature of ⁇ 20 C.
  • the method further includes, at step 13 , condensing at least a portion of CO 2 in the cooled CO 2 stream at the second temperature, thereby condensing CO 2 from the cooled CO 2 stream to form a condensed CO 2 stream 302 .
  • the method includes condensing at least a portion of CO 2 in the cooled CO 2 stream at a pressure in a range of from about 20 bar to about 60 bar.
  • the method includes condensing at least a portion of CO 2 in the cooled CO 2 stream at a pressure in a range of from about 20 bar to about 40 bar. Accordingly, the method of the present invention advantageously allows for condensation of CO 2 at a lower pressure, in some embodiments.
  • the method includes performing the steps of cooling the partially cooled CO 2 stream to form a cooled CO 2 stream 12 and condensing CO 2 from the cooled CO 2 stream 13 simultaneously. In some other embodiments, the method includes performing the steps of cooling the partially cooled CO 2 stream to form a cooled CO 2 stream 12 and condensing CO 2 from the cooled CO 2 stream 13 sequentially.
  • a cooled CO 2 stream may be generated from the partially cooled CO 2 stream 201 in the heat exchanger 212 .
  • a portion of CO 2 from the cooled CO 2 stream condenses in the heat-generator itself forming a condensed CO 2 stream 302 , as indicated in FIG. 3 .
  • a cooled CO 2 stream 301 is generated from the partially cooled CO 2 stream 201 in the heat exchanger 212 .
  • the method further includes transferring the cooled CO 2 stream 301 to a condenser 213 , as indicated in FIG. 4 .
  • a portion of CO 2 from the cooled CO 2 stream 301 condenses in the condenser 213 and forms a condensed CO 2 stream 302 , as indicated in FIG. 4 .
  • the method includes condensing at least about 95 weight percent of CO 2 in the CO 2 stream 101 to form the condensed CO 2 stream 302 . In some embodiments, the method includes condensing at least about 90 weight percent of CO 2 in the CO 2 stream 101 to form the condensed CO 2 stream 302 . In some embodiments, the method includes condensing 50 weight percent to about 90 weight percent of CO 2 in the CO 2 stream 101 to form the condensed CO 2 stream 302 . In some embodiments, the method includes condensing at least about 99 weight percent of CO 2 in the CO 2 stream 101 to form the condensed CO 2 stream 302 .
  • the CO 2 stream 101 further includes one or more components in addition to carbon dioxide.
  • the method further optionally includes generating a lean stream (indicated by dotted arrow 202 ) after the steps of magneto-caloric cooling (step 12 ) and CO 2 condensation (step 13 ).
  • the term “lean stream” 202 refers to a stream in which the CO 2 content is lower than that of the CO 2 content in the CO 2 stream 101 .
  • almost all of the CO 2 in the CO 2 stream is condensed in the step 13 .
  • the lean CO 2 stream is substantially free of CO 2 .
  • a portion of the CO 2 stream may not condense in the step 13 and the lean stream may include uncondensed CO 2 gas mixture.
  • the lean stream 202 may include one or more non-condensable components, which may not condense in the step 13 .
  • the lean stream 202 may include one or more liquid components.
  • the lean stream may be further configured to be in fluid communication with a liquid-gas separator.
  • the lean stream 202 may include one or more of nitrogen, oxygen, or sulfur dioxide.
  • the method may further include dehumidifying the CO 2 stream 101 before step 11 . In some embodiments, the method may further include dehumidifying the partially cooled CO 2 stream 201 after step 11 and before step 12 . In some embodiments, the system 100 may further include a dehumidifier configured to be in flow communication (not shown) with the CO 2 stream 101 . In some embodiments, the system 100 may further include a dehumidifier configured to be in flow communication (not shown) with the CO 2 stream 101 .
  • the method further includes circulating the condensed CO 2 stream 302 to one or more cooling stages used for cooling the CO 2 stream. As indicated in FIG. 5 , the method further includes circulating the condensed CO 2 stream to a heat exchanger 113 via a circulation loop 303 . In such embodiments, the method further includes a recuperation step where the condensed CO 2 stream is circulated back to further cool the partially cooled CO 2 stream 201 before the magneto-caloric cooling step 12 . In some embodiments, the recuperation step may increase the efficiency of the magneto-caloric step.
  • the recuperation of condensed CO 2 stream to the heat exchanger 113 may result in cooling of the partially cooled CO 2 stream 201 below the temperature required for condensation of CO 2 .
  • the method may further include condensing the CO 2 in the partially cooled CO 2 stream 201 to form a recuperated condensed CO 2 stream 501 , as indicated in FIG. 5 .
  • the method further includes increasing a pressure of the condensed CO 2 stream 302 using a pump 300 , as indicated in FIG. 3 .
  • the method may further include increasing a pressure of the recuperated condensed CO 2 stream 501 using a pump 300 , as indicated in FIG. 5 .
  • the method includes increasing a pressure of the condensed CO 2 stream 302 or the recuperated condensed CO 2 stream 502 to a pressure desired for CO 2 sequestration or end-use.
  • the method includes increasing a pressure of the condensed CO 2 stream 302 or the recuperated condensed CO 2 stream 502 to a pressure in a range from about 150 bar to about 180 bar.
  • the method further includes generating a pressurized CO 2 stream 401 after the pumping step. In some embodiments, the method further includes generating a supercritical CO 2 stream 401 after the pumping step. In some embodiments, as noted earlier, the pressurized CO 2 stream 401 may be used for enhanced oil recovery, CO 2 storage, or CO 2 sequestration.
  • a system 100 for condensing carbon dioxide (CO 2 ) from a CO 2 stream 101 is provided, as illustrated in FIGS. 3-9 .
  • the system 100 includes one or more compression stages 120 configured to receive the CO 2 stream 101 .
  • the system 100 further includes one or more cooling stages 110 in fluid communication with the one or more compression stages 120 .
  • a combination of the one or more compression stages 120 and the one or more cooling stages 110 is configured to compress and cool the CO 2 stream 101 to a first temperature to form a partially-cooled CO 2 stream 201 .
  • the system 100 further includes a magneto-caloric cooling stage 200 configured to receive the partially-cooled CO 2 stream 201 and cool the partially-cooled CO 2 stream 201 to a second temperature to form a cooled CO 2 stream 301 .
  • the magneto-caloric cooling stage 200 further includes a heat exchanger 212 , wherein the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212 .
  • the heat exchanger 212 is in fluid communication with the one or more cooling stages 110 and the one or more compression stages 120 .
  • the heat exchanger 212 is configured to condense a portion of CO 2 in the partially cooled CO 2 stream 201 to form the condensed CO 2 stream 302 .
  • the system 100 further includes a condensation stage 213 configured to condense a portion of CO 2 in the cooled CO 2 stream 301 at the second temperature, thereby condensing CO 2 from the cooled CO 2 stream 301 to form a condensed CO 2 stream 302 .
  • the system 100 further includes a pump 300 configured to receive the condensed CO 2 stream 302 and increase the pressure of the condensed CO 2 stream 302 .
  • the system further includes a circulation loop 303 configured to circulate a portion of the condensed CO 2 stream 302 to the one or more cooling stages 110 .
  • a method 20 of condensing carbon dioxide from a CO 2 stream 101 includes, at step 21 , cooling the CO 2 stream 101 in a first cooling stage including a first heat exchanger 111 to form a first partially cooled CO 2 stream 102 .
  • the method includes, at step 22 , compressing the first partially cooled CO 2 stream 102 in a first compressor 121 to form a first compressed CO 2 stream 103 .
  • the method includes, at step 23 , cooling the first compressed CO 2 stream 103 in a second cooling stage including a second heat exchanger 112 to form a second partially cooled CO 2 stream 104 .
  • the method includes, at step 24 , compressing the second partially cooled CO 2 stream 104 in a second compressor 122 to form a second compressed CO 2 stream 105 .
  • the method includes, at step 25 , cooling the second compressed CO 2 stream 105 to a first temperature in a third cooling stage comprising a third heat exchanger 113 to form a partially cooled CO 2 stream 201 .
  • the method 20 includes, at step 26 , cooling the partially cooled CO 2 stream 201 to a second temperature by magneto-caloric cooling using a magneto-caloric cooling stage 200 to form a cooled CO 2 stream (not shown).
  • a magneto-caloric cooling stage 200 includes a heat exchanger 212 and an external magneto-caloric cooling device 211 .
  • the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212 , as indicated in FIG. 3 .
  • the method includes, at step 27 , condensing at least a portion of CO 2 in the cooled CO 2 stream at the second temperature, thereby condensing CO 2 from the cooled CO 2 stream to form a condensed CO 2 stream 302 .
  • a cooled CO 2 stream is generated from the partially cooled CO 2 stream 201 in the heat exchanger 212 .
  • a portion of CO 2 from the cooled CO 2 stream condenses in the heat-generator itself forming a condensed CO 2 stream 302 , as indicated in FIG. 3 .
  • the method further includes increasing a pressure of the condensed CO 2 stream 302 using a pump 300 , as indicated in FIG. 3 .
  • the method further includes generating a pressurized CO 2 stream 401 after the pumping step.
  • the pressurized CO 2 stream 401 may be used for enhanced oil recovery, CO 2 storage, or CO 2 sequestration.
  • a method and a system for condensing CO 2 from a CO 2 stream 101 is provided.
  • the method and system is similar to the system and method illustrated in FIG. 3 , with the addition that the method further includes transferring the cooled CO 2 stream 301 to a condenser 213 , as indicated in FIG. 4 .
  • a portion of CO 2 from the cooled CO 2 stream 301 condenses in the condenser 213 and forms a condensed CO 2 stream 302 , as indicated in FIG. 4 .
  • a method and a system for condensing CO 2 from a CO 2 stream 101 is provided.
  • the method and system is similar to the system and method illustrated in FIG. 3 , with the addition that the method further includes circulating a portion of the condensed CO 2 stream 302 to the third heat exchanger 113 via a circulation loop 303 .
  • the recuperation of condensed CO 2 stream to the heat exchanger 113 may result in cooling of the second compressed CO 2 stream 105 below the temperature required for condensation of CO 2 .
  • the method may further include condensing the CO 2 in the second compressed CO 2 stream 105 to form a recuperated condensed CO 2 stream 501 , as indicated in FIG. 5 .
  • a method and system for condensing CO 2 from a CO 2 stream 101 is provided.
  • the method and system is similar to the system and method illustrated in FIG. 4 , with the addition that the method further includes circulating a portion of the condensed CO 2 stream to the third heat exchanger 113 via a circulation loop 303 .
  • the recuperation of condensed CO 2 to the heat exchanger 113 may result in cooling of the second compressed CO 2 stream 105 below the temperature required for condensation of CO 2 .
  • the method may further include condensing the CO 2 in the second compressed CO 2 stream 105 to form a recuperated condensed CO 2 stream 501 , as indicated in FIG. 6 .
  • a method and a system for condensing CO 2 from a CO 2 stream 101 is provided.
  • the method and system is similar to the system and method illustrated in FIG. 3 , with the addition that the method further includes circulating a portion of the pressurized CO 2 stream 401 to the third heat exchanger 113 via a circulation loop 403 .
  • the recuperation of pressurized CO 2 stream 401 to the third heat exchanger 113 may result in cooling of the second compressed CO 2 stream 105 below the temperature required for condensation of CO 2 .
  • the method may further include condensing the CO 2 in the second compressed CO 2 stream 105 to form a recuperated condensed CO 2 stream 501 , as indicated in FIG. 7 .
  • FIG. 8 a method and a system for condensing CO 2 from a CO 2 stream 101 is illustrated.
  • the method and system is similar to the system and method illustrated in FIG. 3 , with the addition that the method further includes forming a third partially cooled CO 2 stream 106 in the third heat exchanger 113 .
  • the method further includes cooling the third partially cooled CO 2 stream 106 to a first temperature by expanding the third partially cooled CO 2 stream 106 in one or more expanders 123 , before the magneto-caloric cooling step, to form the partially-cooled CO 2 stream 201 , as indicated in FIG. 8 .
  • FIG. 9 a method and a system for condensing CO 2 from a CO 2 stream 101 is illustrated.
  • the method and system is similar to the system and method illustrated in FIG. 8 , with the addition that the third cooling stage further comprises a fourth heat exchanger 114 , and the method further includes circulating a portion of the pressurized CO 2 stream 401 to the fourth heat exchanger 114 via a circulation loop 403 .
  • the method further includes forming a fourth partially cooled CO 2 stream 107 after the expansion step and transferring the fourth partially cooled CO 2 stream 107 to the fourth heat exchanger 114 .
  • the recuperation of pressurized CO 2 stream 401 to the fourth heat exchanger 114 may result in cooling of the fourth partially cooled CO 2 stream 107 below the temperature required for condensation of CO 2 .
  • the method may further include condensing the CO 2 in the fourth partially cooled CO 2 stream 107 to form a recuperated condensed CO 2 stream 501 , as indicated in FIG. 9 .
  • the method reduces the penalty on the less-efficient CO 2 compression step.
  • the method may reduce the overall penalty for CO 2 liquefaction and pumping by improving the efficiency of the compression and pumping system.
  • the magneto-caloric cooling stage may reduce the penalty by more than 10%.
  • the magneto-caloric cooling stage may reduce the penalty by more than 20%.
  • the overall plant efficiency may be improved by using one or more of the method embodiments, described herein.
  • some embodiments of the invention advantageously allow for improved range of operability of CO 2 compression and liquefaction systems.
  • the ambient temperature of the cooling air or cooling water may limit the range of operability.
  • Supercritical CO 2 may not liquefy at temperatures greater than about 32° C., the critical temperature of CO 2 .
  • the magnetic cooling step may advantageously allow cooling of CO 2 to the subcritical range, thereby enabling the operability of the compression and liquefaction systems under any ambient conditions.

Abstract

In accordance with one aspect of the present invention, methods of condensing carbon dioxide (CO2) from a CO2 stream are provided. The method includes (i) compressing and cooling the CO2 stream to form a partially cooled CO2 stream, wherein the partially cooled CO2 stream is cooled to a first temperature. The method includes (ii) cooling the partially cooled CO2 stream to a second temperature by magneto-caloric cooling to form a cooled CO2 stream. The method further includes (iii) condensing at least a portion of CO2 in the cooled CO2 stream to form a condensed CO2 stream. Systems for condensing carbon dioxide (CO2) from a CO2 stream are also provided

Description

    BACKGROUND
  • 1. Technical Field
  • The present disclosure relates to methods and systems for carbon dioxide (CO2) condensation using magneto-caloric cooling. More particularly, the present disclosure relates to methods and systems for CO2 condensation in an intercooled compression and pumping train using magneto-caloric cooling.
  • 2. Discussion of Related Art
  • Power generating processes that are based on combustion of carbon containing fuel typically produce CO2 as a byproduct. It may be desirable to capture or otherwise separate the CO2 from the gas mixture to prevent the release of CO2 into the environment and/or to utilize CO2 in the power generation process or in other processes. It may be further desirable to liquefy/condense the separated CO2 to facilitate transport and storage of the separated CO2. CO2 compression, liquefaction and pumping trains may be used to liquefy CO2 for desired end-use applications. However, methods for condensation/liquefaction of CO2 may be energy intensive.
  • Thus, there is a need for efficient methods and systems for condensation of CO2. Further, there is a need for efficient methods and systems for condensation of CO2 in intercooled compression and pumping trains.
  • BRIEF DESCRIPTION
  • In accordance with one aspect of the present invention, a method of condensing carbon dioxide (CO2) from a CO2 stream is provided. The method includes (i) compressing and cooling the CO2 stream to form a partially cooled CO2 stream, wherein the partially cooled CO2 stream is cooled to a first temperature. The method includes (ii) cooling the partially cooled CO2 stream to a second temperature by magneto-caloric cooling to form a cooled CO2 stream. The method further includes (iii) condensing at least a portion of CO2 in the cooled CO2 stream at the second temperature to form a condensed CO2 stream.
  • In accordance with another aspect of the present invention a method of condensing carbon dioxide (CO2) from a CO2 stream is provided. The method includes (i) cooling the CO2 stream in a first cooling stage comprising a first heat exchanger to form a first partially cooled CO2 stream. The method further includes (ii) compressing the first partially cooled CO2 stream to form a first compressed CO2 stream. The method further includes (iii) cooling the first compressed CO2 stream in a second cooling stage comprising a second heat exchanger to form a second partially cooled CO2 stream. The method further includes (iv) compressing the second partially cooled CO2 stream to form a second compressed CO2 stream. The method further includes (v) cooling the second compressed CO2 stream to a first temperature in a third cooling stage comprising a third heat exchanger to form a partially cooled CO2 stream. The method further includes (vi) cooling the partially cooled CO2 stream to a second temperature by magneto-caloric cooling to form a cooled CO2 stream. The method further includes (vii) condensing at least a portion of CO2 in the cooled CO2 stream at the second temperature to form a condensed CO2 stream.
  • In accordance with yet another aspect of the present invention, a system for condensing carbon dioxide (CO2) from a CO2 stream is provided. The system includes (i) one or more compression stages configured to receive the CO2 stream. The system further includes (ii) one or more cooling stages in fluid communication with the one or more compression stages, wherein a combination of the one or more compression stages and the one or more cooling stages is configured to compress and cool the CO2 stream to a first temperature to form a partially-cooled CO2 stream. The system further includes (iii) a magneto-caloric cooling stage configured to receive the partially-cooled CO2 stream and cool the partially-cooled CO2 stream to a second temperature to form a cooled CO2 stream. The system further includes (iv) a condensation stage configured to condense a portion of CO2 in the cooled CO2 stream at the second temperature, thereby condensing CO2 from the cooled compressed CO2 stream to form a condensed CO2 stream.
  • Other embodiments, aspects, features, and advantages of the invention will become apparent to those of ordinary skill in the art from the following detailed description, the accompanying drawings, and the appended claims.
  • BRIEF DESCRIPTION OF THE DRAWING FIGURES
  • These and other features, aspects, and advantages of the present invention will become better understood when the following detailed description is read with reference to the accompanying drawings in which like characters represent like parts throughout the drawings, wherein:
  • FIG. 1 is a flow chart for a method of CO2 condensation from a CO2 stream, in accordance with one embodiment of the invention.
  • FIG. 2 is a flow chart for a method of CO2 condensation from a CO2 stream, in accordance with one embodiment of the invention.
  • FIG. 3 is a block diagram of a system for CO2 condensation from a CO2 stream, in accordance with one embodiment of the invention.
  • FIG. 4 is a block diagram of a system for CO2 condensation from a CO2 stream, in accordance with one embodiment of the invention.
  • FIG. 5 is a block diagram of a system for CO2 condensation from a CO2 stream, in accordance with one embodiment of the invention.
  • FIG. 6 is a block diagram of a system for CO2 condensation from a CO2 stream, in accordance with one embodiment of the invention.
  • FIG. 7 is a block diagram of a system for CO2 condensation from a CO2 stream, in accordance with one embodiment of the invention.
  • FIG. 8 is a block diagram of a system for CO2 condensation from a CO2 stream, in accordance with one embodiment of the invention.
  • FIG. 9 is a block diagram of a system for CO2 condensation from a CO2 stream, in accordance with one embodiment of the invention.
  • FIG. 10 is a pressure versus temperature diagram for CO2.
  • DETAILED DESCRIPTION
  • As discussed in detail below, embodiments of the present invention include methods and systems suitable for CO2 condensation. As noted earlier, liquefying and pumping of CO2 may require high energy input. For example, a pressure of approximately 60 bar may be required to liquefy CO2 at 20° C. In some embodiments, an intermediate magnetic cooling step advantageously lowers the CO2 temperature to less than 0° C., significantly reducing the required work of the overall system. In some embodiments, depending on the coefficient of performance of the magneto-caloric cooling system, an overall efficiency improvement of about 10 percent to about 15 percent may be possible using the methods and systems described herein.
  • Approximating language, as used herein throughout the specification and claims, may be applied to modify any quantitative representation that could permissibly vary without resulting in a change in the basic function to which it is related. Accordingly, a value modified by a term or terms, such as “about”, is not limited to the precise value specified. In some instances, the approximating language may correspond to the precision of an instrument for measuring the value.
  • In the following specification and the claims, the singular forms “a”, “an” and “the” include plural referents unless the context clearly dictates otherwise.
  • In one embodiment, as shown in FIGS. 1 and 3, a method 10 for condensing carbon dioxide from a CO2 stream is provided. The term “CO2 stream”, as used herein, refers to a stream of CO2 gas mixture emitted as a result of the processing of fuels, such as, natural gas, biomass, gasoline, diesel fuel, coal, oil shale, fuel oil, tar sands, and combinations thereof. In some embodiments, the CO2 stream includes a CO2 stream emitted from a gas turbine. In particular embodiments, the CO2 stream includes a CO2 gas mixture emitted from a coal or natural gas-fired power plant.
  • In some embodiments, the CO2 stream further includes one more of nitrogen, nitrogen dioxide, oxygen, or water vapor. In some embodiments, the CO2 stream further includes impurities or pollutants, examples of which include, but are not limited to, nitrogen, nitrogen oxides, sulfur oxides, carbon monoxide, hydrogen sulfide, unburnt hydrocarbons, particulate matter, and combinations thereof. In particular embodiments, the CO2 stream is substantially free of the impurities or pollutants. In particular embodiments, the CO2 stream essentially includes carbon dioxide.
  • In some embodiments, the amount of impurities or pollutants in the CO2 stream is less than about 50 mole percent. In some embodiments, the amount of impurities or pollutants in the CO2 stream is less than about 20 mole percent. In some embodiments, the amount of impurities or pollutants in the CO2 stream is in a range from about 10 mole percent to about 20 mole percent. In some embodiments, the amount of impurities or pollutants in the CO2 stream is less than about 5 mole percent.
  • In one embodiment, the method includes receiving a CO2 stream 101, as indicated in FIG. 3, from a hydrocarbon processing, combustion, gasification or a similar power plant (not shown). As indicated in FIGS. 1 and 3, at step 11, the method 10 includes compressing and cooling the CO2 stream 101 to form a partially cooled CO2 stream 201. In some embodiments, the CO2 stream 101 may be compressed using or more compression stages 120. In some embodiments, the CO2 stream may be cooled using or more cooling stages 110.
  • In some embodiments, the CO2 stream 101 may be compressed to a desired pressure by using one or more compression stages, as indicated by 120 in FIG. 3. As indicated in FIG. 3, the compression stage 120 may further include one or more compressors, such as, 121 and 122, in some embodiments. It should be noted that in FIG. 3, the two compressors 121 and 122 are shown as an exemplary embodiment only and the actual number of compressors and their individual configuration may vary depending on the end result desired. In one embodiment, the CO2 stream 101 may be compressed to a pressure and temperature desired for the magnetic cooling and condensation steps 12 and 13, respectively. In some embodiments, the CO2 stream 101 may be compressed to a pressure in a range from about 10 bar to about 60 bar prior to the magnetic cooling step 12. In particular embodiments, the CO2 stream 101 may be compressed to a pressure in a range from about 20 bar to about 40 bar prior to the magnetic cooling step 12.
  • In some embodiments, the CO2 stream 101 may be cooled to a desired temperature by using one or more cooling stages, as indicated by 110 in FIG. 3. As indicated in FIG. 3, the cooling stage 110 may further include one or more heat exchangers, such as, 111, 112 and 113, in some embodiments. It should be noted that in FIG. 3, the three heat exchangers 111, 112, and 113 are shown as an exemplary embodiment only and the actual number of heat exchangers and their individual configuration may vary depending on the end result desired. In some embodiments, one or more of the heat exchangers may be cooled using a cooling medium. In some embodiments, one more of the heat exchangers may be cooled using cooling air, cooling water, or both, as indicated by 115 in FIG. 3. In some embodiments, the cooling stage may further include one or more intercoolers to cool the exhaust gas stream 101 without affecting the pressure.
  • It should be further noted that in FIG. 3, the configuration of cooling stage 110 and compression stage 120 is shown as an exemplary embodiment only and the actual configuration may vary depending on the end result desired. For example, in some other embodiments, the method may include cooling the CO2 stream in a heat exchanger 111 prior to compressing the CO2 stream in a compressor 121 (not shown).
  • In some embodiments, the method further includes cooling the CO2 stream 101 to a first temperature by expanding the CO2 stream in one or more expanders 123, as indicated in FIG. 8. In some embodiments the method includes an expansion step that decreases the pressure of the CO2 stream 101 from absolute pressure levels greater than about 20 bar to pressure levels of around 20 bar, thereby decreasing the temperature of the CO2 stream 101 to values lower than that may be reached by air or water cooling. Without being bound any theory, it is believed that by employing the expansion step, the overall duty of the magneto-caloric cooling step 12 may be reduced, as the inlet temperature of the partially-cooled CO2 stream to the magneto-caloric step may be lower than that without an expansion step. In some embodiments, the work extracted in the expansion step may be further used for the magneto-caloric cooling step 12.
  • In one embodiment, the CO2 stream 101 may be cooled to a temperature and pressure desired for the magnetic cooling and condensation steps 12 and 13. In one embodiment, the method includes compressing and cooling the CO2 stream 101 to form a partially cooled CO2 stream 201, as indicated in FIG. 3. In one embodiment, the method further includes cooling the CO2 stream 101 to a first temperature by expanding the CO2 stream in one or more expanders 123 to form the partially cooled CO2 stream 201, as indicated in FIG. 8.
  • In one embodiment, the method includes cooling the partially cooled CO2 stream 201 to a first temperature. In some embodiments, the partially cooled CO2 stream 201 may be cooled to a temperature in a range from about 5 degrees Celsius to about 35 degrees Celsius, prior to the magnetic cooling step 12. In particular embodiments, the partially cooled CO2 stream 201 may be cooled to a temperature in a range from about 10 degrees Celsius to about 25 degrees Celsius, prior to the magnetic cooling step 12.
  • As noted earlier, in the absence of an additional magnetic cooling step, CO2 in the partially cooled CO2 stream 201 is typically liquefied at a temperature in a range from about 20 degrees Celsius to about 25 degrees Celsius. The condensation temperature is determined by the temperature of the cooling medium, which can be cooling water or air. As shown in FIG. 10, at a condensation temperature in a range from about 20 degrees Celsius to about 25 degrees Celsius, an absolute pressure of approximately 60 bar is required to liquefy CO2. In contrast, by cooling the CO2 stream to a temperature in a range from about −25 degrees Celsius to about 0 degrees Celsius, lower pressure may be advantageously used for condensing CO2 from the partially cooled CO2 stream 201.
  • In one embodiment, the method further includes, at step 12, cooling the partially cooled CO2 stream 201 to a second temperature by magneto-caloric cooling to form a cooled CO2 stream 302, as indicated in FIGS. 1 and 3. In one embodiment, the method includes cooling the partially-cooled CO2 stream 201 using a magneto-caloric cooling stage 200, as indicated in FIG. 3.
  • In some embodiments, a magneto-caloric cooling stage 200 includes a heat exchanger 212 and an external magneto-caloric cooling device 211. In some embodiments, the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212, as shown in FIG. 3.
  • In one embodiment, the magneto-caloric cooling device 211 includes a cold and a hot heat exchanger, a permanent magnet assembly or an induction coil magnet assembly, a regenerator of magneto-caloric material, and a heat transfer fluid cycle. In one embodiment, the heat transfer fluid is pumped through the regenerator and the heat exchanger by a fluid pump (not shown).
  • In one embodiment, the magneto-caloric cooling devices works on an active magnetic regeneration cycle (AMR) and provides cooling power to a heat transfer fluid by sequential magnetization and demagnetization of the magneto-caloric regenerator with flow reversal heat transfer flow. In some embodiments, the sequential magnetization and demagnetization of the magneto-caloric regenerator may be provided for by a rotary set-up where the regenerator passes through a bore of the magnet system. In some other embodiments, the sequential magnetization and demagnetization of the magneto-caloric regenerator may be provided for by a reciprocating linear device. An exemplary magnet assembly and magneto-caloric cooling device are described in U.S. patent application Ser. No. 12/392,115, filed on Feb. 25, 2009, and incorporated herein by reference in its entirety for any and all purposes, so long as not directly contradictory with the teachings herein.
  • In some embodiments, the heat at the hot heat exchanger may be delivered to the ambient environment. In some other embodiments, the heat at the hot heat exchanger may be delivered to the return flow of the condensed and liquefied CO2 after the pumping of the liquid CO2, as described herein later.
  • As noted earlier, the magneto-caloric cooling stage further includes a heat exchanger 212, wherein the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212. In one embodiment, the heat exchanger 212 is in fluid communication with the one or more cooling stages 110 and the one or more compression stages 120. In one embodiment, the heat exchanger 212 is in fluid communication with the partially cooled CO2 stream 201 generated after the compression and cooling step 11.
  • In some embodiments, the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212 such that the partially cooled CO2 stream 201 is cooled to the second temperature. In one embodiment, the second temperature is in a range of from about 0 degrees Celsius to about −25 degrees Celsius.
  • In one embodiment, the second temperature is in a range of from about 5 degrees Celsius to about −20 degrees Celsius. As noted earlier, the step 13 of cooling the partially-cooled CO2 stream in the magneto-caloric cooling stage results in a cooled CO2 stream.
  • In some embodiments, the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212 such that the partially cooled CO2 stream 201 is cooled to the second temperature, such that CO2 condenses from the cooled CO2 stream. As noted earlier, the method includes compressing the CO2 stream 101 to a pressure in a range from about 20 bar to about 40 bar, in some embodiments. As indicated in FIG. 10, at a pressure level of 40 bar, the CO2 condenses at a temperature of 5 C. Further, as indicated in FIG. 10, at a pressure level of 20 bar, the CO2 condenses at a temperature of −20 C.
  • In one embodiment, the method further includes, at step 13, condensing at least a portion of CO2 in the cooled CO2 stream at the second temperature, thereby condensing CO2 from the cooled CO2 stream to form a condensed CO2 stream 302. In one embodiment, the method includes condensing at least a portion of CO2 in the cooled CO2 stream at a pressure in a range of from about 20 bar to about 60 bar. In one embodiment, the method includes condensing at least a portion of CO2 in the cooled CO2 stream at a pressure in a range of from about 20 bar to about 40 bar. Accordingly, the method of the present invention advantageously allows for condensation of CO2 at a lower pressure, in some embodiments.
  • In some embodiments, the method includes performing the steps of cooling the partially cooled CO2 stream to form a cooled CO2 stream 12 and condensing CO2 from the cooled CO2 stream 13 simultaneously. In some other embodiments, the method includes performing the steps of cooling the partially cooled CO2 stream to form a cooled CO2 stream 12 and condensing CO2 from the cooled CO2 stream 13 sequentially.
  • As indicated in FIG. 3, in some embodiments, a cooled CO2 stream may be generated from the partially cooled CO2 stream 201 in the heat exchanger 212. In such embodiments, a portion of CO2 from the cooled CO2 stream condenses in the heat-generator itself forming a condensed CO2 stream 302, as indicated in FIG. 3.
  • In some other embodiments, as indicated in FIG. 4, a cooled CO2 stream 301 is generated from the partially cooled CO2 stream 201 in the heat exchanger 212. The method further includes transferring the cooled CO2 stream 301 to a condenser 213, as indicated in FIG. 4. In such embodiments, a portion of CO2 from the cooled CO2 stream 301 condenses in the condenser 213 and forms a condensed CO2 stream 302, as indicated in FIG. 4.
  • In some embodiments, the method includes condensing at least about 95 weight percent of CO2 in the CO2 stream 101 to form the condensed CO2 stream 302. In some embodiments, the method includes condensing at least about 90 weight percent of CO2 in the CO2 stream 101 to form the condensed CO2 stream 302. In some embodiments, the method includes condensing 50 weight percent to about 90 weight percent of CO2 in the CO2 stream 101 to form the condensed CO2 stream 302. In some embodiments, the method includes condensing at least about 99 weight percent of CO2 in the CO2 stream 101 to form the condensed CO2 stream 302.
  • In some embodiments, as noted earlier, the CO2 stream 101 further includes one or more components in addition to carbon dioxide. In some embodiments, the method further optionally includes generating a lean stream (indicated by dotted arrow 202) after the steps of magneto-caloric cooling (step 12) and CO2 condensation (step 13). The term “lean stream” 202 refers to a stream in which the CO2 content is lower than that of the CO2 content in the CO2 stream 101. In some embodiments, as noted earlier, almost all of the CO2 in the CO2 stream is condensed in the step 13. In such embodiments, the lean CO2 stream is substantially free of CO2. In some other embodiments, as noted earlier, a portion of the CO2 stream may not condense in the step 13 and the lean stream may include uncondensed CO2 gas mixture.
  • In some embodiments, the lean stream 202 may include one or more non-condensable components, which may not condense in the step 13. In some embodiments, the lean stream 202 may include one or more liquid components. In such embodiments, the lean stream may be further configured to be in fluid communication with a liquid-gas separator. In some embodiments, the lean stream 202 may include one or more of nitrogen, oxygen, or sulfur dioxide.
  • In some embodiments, the method may further include dehumidifying the CO2 stream 101 before step 11. In some embodiments, the method may further include dehumidifying the partially cooled CO2 stream 201 after step 11 and before step 12. In some embodiments, the system 100 may further include a dehumidifier configured to be in flow communication (not shown) with the CO2 stream 101. In some embodiments, the system 100 may further include a dehumidifier configured to be in flow communication (not shown) with the CO2 stream 101.
  • In some embodiments, the method further includes circulating the condensed CO2 stream 302 to one or more cooling stages used for cooling the CO2 stream. As indicated in FIG. 5, the method further includes circulating the condensed CO2 stream to a heat exchanger 113 via a circulation loop 303. In such embodiments, the method further includes a recuperation step where the condensed CO2 stream is circulated back to further cool the partially cooled CO2 stream 201 before the magneto-caloric cooling step 12. In some embodiments, the recuperation step may increase the efficiency of the magneto-caloric step.
  • In some embodiments, the recuperation of condensed CO2 stream to the heat exchanger 113 may result in cooling of the partially cooled CO2 stream 201 below the temperature required for condensation of CO2. In some embodiments, the method may further include condensing the CO2 in the partially cooled CO2 stream 201 to form a recuperated condensed CO2 stream 501, as indicated in FIG. 5.
  • In some embodiments, the method further includes increasing a pressure of the condensed CO2 stream 302 using a pump 300, as indicated in FIG. 3. In embodiments including a recuperation step, the method may further include increasing a pressure of the recuperated condensed CO2 stream 501 using a pump 300, as indicated in FIG. 5. In some embodiments, the method includes increasing a pressure of the condensed CO2 stream 302 or the recuperated condensed CO2 stream 502 to a pressure desired for CO2 sequestration or end-use. In some embodiments, the method includes increasing a pressure of the condensed CO2 stream 302 or the recuperated condensed CO2 stream 502 to a pressure in a range from about 150 bar to about 180 bar.
  • In some embodiments, the method further includes generating a pressurized CO2 stream 401 after the pumping step. In some embodiments, the method further includes generating a supercritical CO2 stream 401 after the pumping step. In some embodiments, as noted earlier, the pressurized CO2 stream 401 may be used for enhanced oil recovery, CO2 storage, or CO2 sequestration.
  • In some embodiments, a system 100 for condensing carbon dioxide (CO2) from a CO2 stream 101 is provided, as illustrated in FIGS. 3-9. In one embodiment, the system 100 includes one or more compression stages 120 configured to receive the CO2 stream 101. The system 100 further includes one or more cooling stages 110 in fluid communication with the one or more compression stages 120. In one embodiment, a combination of the one or more compression stages 120 and the one or more cooling stages 110 is configured to compress and cool the CO2 stream 101 to a first temperature to form a partially-cooled CO2 stream 201.
  • In one embodiment, the system 100 further includes a magneto-caloric cooling stage 200 configured to receive the partially-cooled CO2 stream 201 and cool the partially-cooled CO2 stream 201 to a second temperature to form a cooled CO2 stream 301. As noted earlier, the magneto-caloric cooling stage 200 further includes a heat exchanger 212, wherein the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212. In one embodiment, the heat exchanger 212 is in fluid communication with the one or more cooling stages 110 and the one or more compression stages 120.
  • As noted earlier, in some embodiments, the heat exchanger 212 is configured to condense a portion of CO2 in the partially cooled CO2 stream 201 to form the condensed CO2 stream 302. In some other embodiments, the system 100 further includes a condensation stage 213 configured to condense a portion of CO2 in the cooled CO2 stream 301 at the second temperature, thereby condensing CO2 from the cooled CO2 stream 301 to form a condensed CO2 stream 302.
  • In some embodiments, the system 100 further includes a pump 300 configured to receive the condensed CO2 stream 302 and increase the pressure of the condensed CO2 stream 302. In some embodiments, the system further includes a circulation loop 303 configured to circulate a portion of the condensed CO2 stream 302 to the one or more cooling stages 110.
  • With the foregoing in mind, systems and methods for condensing CO2 from a CO2 stream, according to some exemplary embodiments of the invention, are further described herein. Turning now to FIGS. 2 and 3, in one embodiment, a method 20 of condensing carbon dioxide from a CO2 stream 101 is provided. In one embodiment, the method includes, at step 21, cooling the CO2 stream 101 in a first cooling stage including a first heat exchanger 111 to form a first partially cooled CO2 stream 102. In one embodiment, the method includes, at step 22, compressing the first partially cooled CO2 stream 102 in a first compressor 121 to form a first compressed CO2 stream 103. In one embodiment, the method includes, at step 23, cooling the first compressed CO2 stream 103 in a second cooling stage including a second heat exchanger 112 to form a second partially cooled CO2 stream 104. In one embodiment, the method includes, at step 24, compressing the second partially cooled CO2 stream 104 in a second compressor 122 to form a second compressed CO2 stream 105. In one embodiment, the method includes, at step 25, cooling the second compressed CO2 stream 105 to a first temperature in a third cooling stage comprising a third heat exchanger 113 to form a partially cooled CO2 stream 201.
  • In one embodiment, the method 20 includes, at step 26, cooling the partially cooled CO2 stream 201 to a second temperature by magneto-caloric cooling using a magneto-caloric cooling stage 200 to form a cooled CO2 stream (not shown). In some embodiments, a magneto-caloric cooling stage 200 includes a heat exchanger 212 and an external magneto-caloric cooling device 211. In some embodiments, the magneto-caloric cooling device 211 is configured to provide cooling to the heat exchanger 212, as indicated in FIG. 3.
  • In one embodiment, the method includes, at step 27, condensing at least a portion of CO2 in the cooled CO2 stream at the second temperature, thereby condensing CO2 from the cooled CO2 stream to form a condensed CO2 stream 302. As noted earlier, in some embodiments, a cooled CO2 stream is generated from the partially cooled CO2 stream 201 in the heat exchanger 212. In such embodiments, a portion of CO2 from the cooled CO2 stream condenses in the heat-generator itself forming a condensed CO2 stream 302, as indicated in FIG. 3.
  • In some embodiments, the method further includes increasing a pressure of the condensed CO2 stream 302 using a pump 300, as indicated in FIG. 3. In some embodiments, the method further includes generating a pressurized CO2 stream 401 after the pumping step. In some embodiments, as noted earlier, the pressurized CO2 stream 401 may be used for enhanced oil recovery, CO2 storage, or CO2 sequestration.
  • Turning now to FIG. 4, in one embodiment, a method and a system for condensing CO2 from a CO2 stream 101 is provided. The method and system is similar to the system and method illustrated in FIG. 3, with the addition that the method further includes transferring the cooled CO2 stream 301 to a condenser 213, as indicated in FIG. 4. In such embodiments, a portion of CO2 from the cooled CO2 stream 301 condenses in the condenser 213 and forms a condensed CO2 stream 302, as indicated in FIG. 4.
  • Turning now to FIG. 5, in one embodiment, a method and a system for condensing CO2 from a CO2 stream 101 is provided. The method and system is similar to the system and method illustrated in FIG. 3, with the addition that the method further includes circulating a portion of the condensed CO2 stream 302 to the third heat exchanger 113 via a circulation loop 303. As noted earlier, in some embodiments, the recuperation of condensed CO2 stream to the heat exchanger 113 may result in cooling of the second compressed CO2 stream 105 below the temperature required for condensation of CO2. In some embodiments, the method may further include condensing the CO2 in the second compressed CO2 stream 105 to form a recuperated condensed CO2 stream 501, as indicated in FIG. 5.
  • Turning now to FIG. 6, in one embodiment, a method and system for condensing CO2 from a CO2 stream 101 is provided. The method and system is similar to the system and method illustrated in FIG. 4, with the addition that the method further includes circulating a portion of the condensed CO2 stream to the third heat exchanger 113 via a circulation loop 303. As noted earlier, in some embodiments, the recuperation of condensed CO2 to the heat exchanger 113 may result in cooling of the second compressed CO2 stream 105 below the temperature required for condensation of CO2. In some embodiments, the method may further include condensing the CO2 in the second compressed CO2 stream 105 to form a recuperated condensed CO2 stream 501, as indicated in FIG. 6.
  • Turning now to FIG. 7, in one embodiment, a method and a system for condensing CO2 from a CO2 stream 101 is provided. The method and system is similar to the system and method illustrated in FIG. 3, with the addition that the method further includes circulating a portion of the pressurized CO2 stream 401 to the third heat exchanger 113 via a circulation loop 403. As noted earlier, in some embodiments, the recuperation of pressurized CO2 stream 401 to the third heat exchanger 113 may result in cooling of the second compressed CO2 stream 105 below the temperature required for condensation of CO2. In some embodiments, the method may further include condensing the CO2 in the second compressed CO2 stream 105 to form a recuperated condensed CO2 stream 501, as indicated in FIG. 7.
  • Turning now to FIG. 8, in one embodiment, a method and a system for condensing CO2 from a CO2 stream 101 is illustrated. The method and system is similar to the system and method illustrated in FIG. 3, with the addition that the method further includes forming a third partially cooled CO2 stream 106 in the third heat exchanger 113. The method further includes cooling the third partially cooled CO2 stream 106 to a first temperature by expanding the third partially cooled CO2 stream 106 in one or more expanders 123, before the magneto-caloric cooling step, to form the partially-cooled CO2 stream 201, as indicated in FIG. 8.
  • Turning now to FIG. 9, in one embodiment, a method and a system for condensing CO2 from a CO2 stream 101 is illustrated. The method and system is similar to the system and method illustrated in FIG. 8, with the addition that the third cooling stage further comprises a fourth heat exchanger 114, and the method further includes circulating a portion of the pressurized CO2 stream 401 to the fourth heat exchanger 114 via a circulation loop 403. The method further includes forming a fourth partially cooled CO2 stream 107 after the expansion step and transferring the fourth partially cooled CO2 stream 107 to the fourth heat exchanger 114. As noted earlier, in some embodiments, the recuperation of pressurized CO2 stream 401 to the fourth heat exchanger 114 may result in cooling of the fourth partially cooled CO2 stream 107 below the temperature required for condensation of CO2. In some embodiments, the method may further include condensing the CO2 in the fourth partially cooled CO2 stream 107 to form a recuperated condensed CO2 stream 501, as indicated in FIG. 9.
  • As noted earlier, some embodiments of the invention advantageously allow for cooling of the supercritical CO2 to lower temperatures and subsequent condensation at lower pressures than those available through conventional cooling methods, such as, vapor compression. Without being bound by any theory, it is believed that compression of supercritical CO2 may be less efficient than pumping liquid CO2. Thus, in some embodiments, the method reduces the penalty on the less-efficient CO2 compression step. In some embodiments, the method may reduce the overall penalty for CO2 liquefaction and pumping by improving the efficiency of the compression and pumping system. In some embodiments, the magneto-caloric cooling stage may reduce the penalty by more than 10%. In some embodiments, the magneto-caloric cooling stage may reduce the penalty by more than 20%. In some embodiments, the overall plant efficiency may be improved by using one or more of the method embodiments, described herein.
  • Further, some embodiments of the invention advantageously allow for improved range of operability of CO2 compression and liquefaction systems. In conventional CO2 compression and liquefaction systems, the ambient temperature of the cooling air or cooling water may limit the range of operability. Supercritical CO2 may not liquefy at temperatures greater than about 32° C., the critical temperature of CO2. Thus, when ambient temperatures are above 30° C., liquefaction of CO2 may be difficult without additional external cooling. In some embodiments, the magnetic cooling step may advantageously allow cooling of CO2 to the subcritical range, thereby enabling the operability of the compression and liquefaction systems under any ambient conditions.
  • This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal language of the claims.

Claims (20)

What is claimed is:
1. A method of condensing carbon dioxide (CO2) from a CO2 stream, comprising:
(i) compressing and cooling the CO2 stream to form a partially cooled CO2 stream, wherein the partially cooled CO2 stream is cooled to a first temperature;
(ii) cooling the partially cooled CO2 stream to a second temperature by magneto-caloric cooling to form a cooled CO2 stream; and
(iii) condensing at least a portion of CO2 in the cooled CO2 stream to form a condensed CO2 stream.
2. The method of claim 1, wherein step (iii) comprises condensing at least a portion of CO2 in the cooled CO2 stream at a pressure in a range of from about 20 bar to about 60 bar.
3. The method of claim 1, wherein step (iii) comprises condensing at least a portion of CO2 in the cooled CO2 stream at a pressure in a range of from about 20 bar to about 40 bar.
4. The method of claim 1, wherein the first temperature is in a range of from about 5 degrees Celsius to about 35 degrees Celsius
5. The method of claim 1, wherein the second temperature is in a range of from about 0 degrees Celsius to about −25 degrees Celsius
6. The method of claim 1, wherein step (i) comprises cooling the CO2 stream using one or more cooling stages comprising one or more heat exchangers.
7. The method of claim 1, further comprising circulating a portion of the condensed CO2 stream to one or more cooling stages used for cooling the CO2 stream.
8. The method of claim 1, wherein step (i) comprises cooling the CO2 stream to the first temperature by expanding the CO2 stream in one or more expanders.
9. The method of claim 1, wherein step (ii) comprises cooling the partially-cooled CO2 stream using a rotary magneto-caloric cooling device.
10. The method of claim 1, further comprising increasing a pressure of the condensed CO2 stream using a pump to form a pressurized CO2 stream.
11. A method of condensing carbon dioxide (CO2) from a CO2 stream, comprising:
(i) cooling the CO2 stream in a first cooling stage comprising a first heat exchanger to form a first partially cooled CO2 stream;
(ii) compressing the first partially cooled CO2 stream to form a first compressed CO2 stream;
(iii) cooling the first compressed CO2 stream in a second cooling stage comprising a second heat exchanger to form a second partially cooled CO2 stream;
(iv) compressing the second partially cooled CO2 stream to form a second compressed CO2 stream;
(v) cooling the second compressed CO2 stream to a first temperature in a third cooling stage comprising a third heat exchanger to form a partially cooled CO2 stream;
(vi) cooling the partially cooled CO2 stream to a second temperature by magneto-caloric cooling to form a cooled CO2 stream; and
(vii) condensing at least a portion of CO2 in the cooled CO2 stream at the second temperature, thereby condensing CO2 from the cooled CO2 stream to form a condensed CO2 stream.
12. The method of claim 11, further comprising circulating a portion of the condensed CO2 stream to the third heat exchanger.
13. The method of claim 11, wherein the third cooling stage further comprises an expander, and step (v) further comprises cooling the CO2 stream to a first temperature by expanding the second compressed CO2 stream in the expander.
14. The method of claim 13, wherein the third cooling stage further comprises a fourth heat exchanger, and the method further comprises circulating a portion of the condensed CO2 stream to the fourth heat exchanger.
15. A system for condensing carbon dioxide (CO2) from a CO2 stream, comprising:
(i) one or more compression stages configured to receive the CO2 stream;
(ii) one or more cooling stages in fluid communication with the one or more compression stages,
wherein a combination of the one or more compression stages and the one or more cooling stages is configured to compress and cool the CO2 stream to a first temperature to form a partially-cooled CO2 stream;
(iii) a magento-caloric cooling stage configured to receive the partially-cooled CO2 stream and cool the partially-cooled CO2 stream to a second temperature to form a cooled CO2 stream; and
(iv) a condensation stage configured to condense a portion of CO2 in the cooled CO2 stream at the second temperature, thereby condensing CO2 from the cooled CO2 stream to form a condensed CO2 stream.
16. The system of claim 15, wherein the magneto-caloric cooling stage comprises a magneto-caloric cooling device and a heat exchanger,
wherein the heat exchanger is in fluid communication with the one or more cooling stages and the one or more compression stages.
17. The system of claim 15, further comprising a pump configured to receive the condensed CO2 stream and increase the pressure of the condensed CO2 stream.
18. The system of claim 15, wherein the one or more cooling stages further comprises an expander.
19. The system of claim 15, wherein the one or more cooling stages comprises one or more heat exchangers configured to cool the CO2 stream using air, water, or combinations thereof.
20. The system of claim 15, further comprising a circulation loop configured to circulate a portion of the condensed CO2 stream to the one or more cooling stages.
US13/249,464 2011-09-30 2011-09-30 Methods and systems for co2 condensation Abandoned US20130081409A1 (en)

Priority Applications (11)

Application Number Priority Date Filing Date Title
US13/249,464 US20130081409A1 (en) 2011-09-30 2011-09-30 Methods and systems for co2 condensation
AU2012315807A AU2012315807C1 (en) 2011-09-30 2012-09-28 Methods and systems for co2 condensation
CA2848991A CA2848991C (en) 2011-09-30 2012-09-28 Methods and systems for co2 condensation
BR112014005676-5A BR112014005676B1 (en) 2011-09-30 2012-09-28 CARBON DIOXIDE CONDENSING METHOD AND CARBON DIOXIDE CONDENSING SYSTEM
RU2014110121A RU2606725C2 (en) 2011-09-30 2012-09-28 Methods and systems for condensation of co2
EP12775386.1A EP2815194A2 (en) 2011-09-30 2012-09-28 Methods and systems for co2 condensation
JP2014533380A JP6154813B2 (en) 2011-09-30 2012-09-28 CO2 condensation method and system
KR1020147011592A KR101983343B1 (en) 2011-09-30 2012-09-28 Methods and systems for co₂ condensation
MX2014003880A MX2014003880A (en) 2011-09-30 2012-09-28 Methods and systems for co2 condensation.
CN201280047666.1A CN104471335B (en) 2011-09-30 2012-09-28 For CO2The method and system of condensation
PCT/US2012/057860 WO2013049532A2 (en) 2011-09-30 2012-09-28 Methods and systems for co2 condensation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/249,464 US20130081409A1 (en) 2011-09-30 2011-09-30 Methods and systems for co2 condensation

Publications (1)

Publication Number Publication Date
US20130081409A1 true US20130081409A1 (en) 2013-04-04

Family

ID=47046861

Family Applications (1)

Application Number Title Priority Date Filing Date
US13/249,464 Abandoned US20130081409A1 (en) 2011-09-30 2011-09-30 Methods and systems for co2 condensation

Country Status (11)

Country Link
US (1) US20130081409A1 (en)
EP (1) EP2815194A2 (en)
JP (1) JP6154813B2 (en)
KR (1) KR101983343B1 (en)
CN (1) CN104471335B (en)
AU (1) AU2012315807C1 (en)
BR (1) BR112014005676B1 (en)
CA (1) CA2848991C (en)
MX (1) MX2014003880A (en)
RU (1) RU2606725C2 (en)
WO (1) WO2013049532A2 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3033397A1 (en) * 2015-03-06 2016-09-09 Air Liquide PROCESS FOR COMPRESSING AND COOLING A GASEOUS MIXTURE
US11224837B2 (en) * 2018-11-12 2022-01-18 Linde Aktiengesellschaft Post-combustion carbon dioxide capture and compression
US11635255B1 (en) * 2022-04-08 2023-04-25 Axip Energy Services, Lp Liquid or supercritical carbon dioxide capture from exhaust gas
WO2023247218A1 (en) * 2022-06-24 2023-12-28 IFP Energies Nouvelles System and method for compressing carbon dioxide with multi-stage compression and supercritical pump

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107112103A (en) * 2014-12-18 2017-08-29 巴斯夫欧洲公司 The method that magnetic thermal level joins and manufacture magnetic thermal level joins
TW201925414A (en) * 2017-09-19 2019-07-01 美商霍尼韋爾國際公司 Heat transfer methods, systems and compositions
CN109813054B (en) 2017-11-22 2021-03-30 斗山重工业建设有限公司 Carbon dioxide capture device using cold energy of liquefied natural gas and power generation system
IT201800009221A1 (en) * 2018-10-05 2020-04-05 Graf Spa SERVICE STATION FOR MEANS OF TRANSPORT
CN112678825A (en) * 2020-12-31 2021-04-20 起时超临界高新技术(广州)有限公司 Built-in heat exchange type supercritical carbon dioxide separation method and equipment

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5893275A (en) * 1997-09-04 1999-04-13 In-X Corporation Compact small volume liquid oxygen production system
US5927103A (en) * 1998-06-17 1999-07-27 Praxair Technology, Inc. Carbon dioxide production system with integral vent gas condenser
US6035662A (en) * 1998-10-13 2000-03-14 Praxair Technology, Inc. Method and apparatus for enhancing carbon dioxide recovery
US6210467B1 (en) * 1999-05-07 2001-04-03 Praxair Technology, Inc. Carbon dioxide cleaning system with improved recovery
US6293106B1 (en) * 2000-05-18 2001-09-25 Praxair Technology, Inc. Magnetic refrigeration system with multicomponent refrigerant fluid forecooling
US6467274B2 (en) * 2000-05-05 2002-10-22 University Of Victoria Innovations & Development Corp. Apparatus and methods for cooling and liquefying a fluid using magnetic refrigeration
US20080156035A1 (en) * 2004-07-16 2008-07-03 Statoil Asa Process and Apparatus for the Liquefaction of Carbon Dioxide
US20100146989A1 (en) * 2005-06-20 2010-06-17 Peter Williams Egolf Continuously rotary magnetic refrigerator or heat pump
US20110247360A1 (en) * 2009-12-15 2011-10-13 L'air Liquide Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Method of Obtaining Carbon Dioxide From Carbon Dioxide-Containing Gas Mixture
US8209988B2 (en) * 2008-09-24 2012-07-03 Husssmann Corporation Magnetic refrigeration device
US20120174621A1 (en) * 2011-01-06 2012-07-12 General Electric Company Carbon dioxide liquefaction system
US8555672B2 (en) * 2009-10-22 2013-10-15 Battelle Energy Alliance, Llc Complete liquefaction methods and apparatus
US20130319040A1 (en) * 2011-02-08 2013-12-05 Ihi Corporation Exhaust gas treatment system for oxyfuel combustion device

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1780250A (en) * 1930-03-27 1930-11-04 Frank G Campbell Method of and apparatus for liquefying gases
JPS576283A (en) * 1980-06-12 1982-01-13 Nippon Oxygen Co Ltd Carbon dioxide removal of air separator
RU2175949C2 (en) * 1999-07-27 2001-11-20 ЗАО "Центр ВМ-Технологий" Method of cleaning carbon dioxide from low-boiling impurities
US6588215B1 (en) * 2002-04-19 2003-07-08 International Business Machines Corporation Apparatus and methods for performing switching in magnetic refrigeration systems using inductively coupled thermoelectric switches
JP2008082663A (en) * 2006-09-28 2008-04-10 Toshiba Corp Magnetic refrigerating device and magnetic refrigerating method
US8293030B2 (en) * 2007-04-05 2012-10-23 Universite De Lorraine Intermetallic compounds, their use and a process for preparing the same
EP2196251A1 (en) * 2008-12-04 2010-06-16 Siemens Aktiengesellschaft Carbon dioxide separation device and method of operating such a device

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5893275A (en) * 1997-09-04 1999-04-13 In-X Corporation Compact small volume liquid oxygen production system
US5927103A (en) * 1998-06-17 1999-07-27 Praxair Technology, Inc. Carbon dioxide production system with integral vent gas condenser
US6035662A (en) * 1998-10-13 2000-03-14 Praxair Technology, Inc. Method and apparatus for enhancing carbon dioxide recovery
US6210467B1 (en) * 1999-05-07 2001-04-03 Praxair Technology, Inc. Carbon dioxide cleaning system with improved recovery
US6467274B2 (en) * 2000-05-05 2002-10-22 University Of Victoria Innovations & Development Corp. Apparatus and methods for cooling and liquefying a fluid using magnetic refrigeration
US6293106B1 (en) * 2000-05-18 2001-09-25 Praxair Technology, Inc. Magnetic refrigeration system with multicomponent refrigerant fluid forecooling
US20080156035A1 (en) * 2004-07-16 2008-07-03 Statoil Asa Process and Apparatus for the Liquefaction of Carbon Dioxide
US20100146989A1 (en) * 2005-06-20 2010-06-17 Peter Williams Egolf Continuously rotary magnetic refrigerator or heat pump
US8209988B2 (en) * 2008-09-24 2012-07-03 Husssmann Corporation Magnetic refrigeration device
US8555672B2 (en) * 2009-10-22 2013-10-15 Battelle Energy Alliance, Llc Complete liquefaction methods and apparatus
US20110247360A1 (en) * 2009-12-15 2011-10-13 L'air Liquide Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Method of Obtaining Carbon Dioxide From Carbon Dioxide-Containing Gas Mixture
US20120174621A1 (en) * 2011-01-06 2012-07-12 General Electric Company Carbon dioxide liquefaction system
US20130319040A1 (en) * 2011-02-08 2013-12-05 Ihi Corporation Exhaust gas treatment system for oxyfuel combustion device

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3033397A1 (en) * 2015-03-06 2016-09-09 Air Liquide PROCESS FOR COMPRESSING AND COOLING A GASEOUS MIXTURE
US11224837B2 (en) * 2018-11-12 2022-01-18 Linde Aktiengesellschaft Post-combustion carbon dioxide capture and compression
US11635255B1 (en) * 2022-04-08 2023-04-25 Axip Energy Services, Lp Liquid or supercritical carbon dioxide capture from exhaust gas
WO2023196743A1 (en) * 2022-04-08 2023-10-12 Axip Energy Services, Lp Liquid or supercritical carbon dioxide capture from exhaust gas
WO2023247218A1 (en) * 2022-06-24 2023-12-28 IFP Energies Nouvelles System and method for compressing carbon dioxide with multi-stage compression and supercritical pump
FR3137164A1 (en) * 2022-06-24 2023-12-29 IFP Energies Nouvelles Carbon dioxide compression system and method with multiphase compression and supercritical pump

Also Published As

Publication number Publication date
MX2014003880A (en) 2014-05-07
CN104471335B (en) 2017-11-07
CA2848991C (en) 2020-07-21
WO2013049532A2 (en) 2013-04-04
WO2013049532A3 (en) 2015-01-29
CN104471335A (en) 2015-03-25
AU2012315807A1 (en) 2014-04-10
JP6154813B2 (en) 2017-06-28
RU2014110121A (en) 2015-11-10
AU2012315807B2 (en) 2017-06-22
RU2606725C2 (en) 2017-01-10
AU2012315807C1 (en) 2017-11-16
KR20140089527A (en) 2014-07-15
BR112014005676B1 (en) 2021-07-20
BR112014005676A2 (en) 2017-04-04
JP2015507731A (en) 2015-03-12
KR101983343B1 (en) 2019-05-28
EP2815194A2 (en) 2014-12-24
CA2848991A1 (en) 2013-04-04

Similar Documents

Publication Publication Date Title
US20130081409A1 (en) Methods and systems for co2 condensation
EP3310455B1 (en) Integrated process for co2 capture from internal combustion engines of mobile sources and use in thermal power production cycle
US20130025294A1 (en) System and method for carbon dioxide removal
US8104259B2 (en) Method and system for reducing power plant emissions
US7472550B2 (en) Combined cooling and power plant with water extraction
MX2012014459A (en) Stoichiometric combustion with exhaust gas recirculation and direct contact cooler.
EP2413035A2 (en) Systems and methods for CO2 capture
CN103086375A (en) Purification of carbon dioxide
Pei et al. Waste heat recovery in CO2 compression
US9766011B2 (en) Optimized heat exchange in a CO2 de-sublimation process
Moore et al. Novel concepts for the compression of large volumes of carbon dioxide
AU2012201567B2 (en) Integrated gasification combined cycle system with vapour absorption chilling
US20130125580A1 (en) Expander and method for co2 separation
EP2541175A2 (en) Air separation unit and systems incorporating the same
Carpenter Process Reduces Carbon Emissions From Natural Gas Compression and Production
BOLLAND et al. NATURAL GAS FIRED POWER CYCLES WITH INTEGRATED CO: CAPTURE', HENRIETTE UNDRUM2 AND MICHEL V1YHRE h
Utilizing et al. Postcombustion CO2 Capture for
OLAV et al. NATURAL GAS FIRED POWER CYCLES WITH INTEGRATED CO₂ CAPTURE

Legal Events

Date Code Title Description
AS Assignment

Owner name: GENERAL ELECTRIC COMPANY, NEW YORK

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:GONZALEZ SALAZAR, MIGUEL ANGEL;MICHELASSI, VITTORIO;VOGEL, CHRISTIAN;SIGNING DATES FROM 20110811 TO 20110822;REEL/FRAME:026996/0373

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION