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US20100037627A1 - Capture and removal of gases from other gases in a gas stream - Google Patents

Capture and removal of gases from other gases in a gas stream Download PDF

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Publication number
US20100037627A1
US20100037627A1 US12/440,281 US44028107A US2010037627A1 US 20100037627 A1 US20100037627 A1 US 20100037627A1 US 44028107 A US44028107 A US 44028107A US 2010037627 A1 US2010037627 A1 US 2010037627A1
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gas stream
thermo
gases
removal
vapors
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US12/440,281
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David Proctor
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    • 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
    • F25J3/06Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by partial condensation
    • F25J3/063Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by partial condensation characterised by the separated product stream
    • F25J3/067Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by partial condensation characterised by the separated product stream separation of carbon dioxide
    • 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
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/14Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the cycle used, e.g. Stirling cycle
    • F25B9/145Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the cycle used, e.g. Stirling cycle pulse-tube cycle
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D2257/00Components to be removed
    • B01D2257/30Sulfur compounds
    • B01D2257/302Sulfur oxides
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D2257/00Components to be removed
    • B01D2257/40Nitrogen compounds
    • B01D2257/404Nitrogen oxides other than dinitrogen oxide
    • 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
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G2243/00Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes
    • F02G2243/30Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes having their pistons and displacers each in separate cylinders
    • F02G2243/50Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes having their pistons and displacers each in separate cylinders having resonance tubes
    • F02G2243/54Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes having their pistons and displacers each in separate cylinders having resonance tubes thermo-acoustic
    • 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
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2309/00Gas cycle refrigeration machines
    • F25B2309/14Compression machines, plants or systems characterised by the cycle used 
    • F25B2309/1403Pulse-tube cycles with heat input into acoustic driver
    • 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
    • F25J2210/00Processes characterised by the type or other details of the feed stream
    • F25J2210/70Flue or combustion exhaust gas
    • 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
    • F25J2215/00Processes characterised by the type or other details of the product stream
    • F25J2215/04Recovery of liquid products
    • 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
    • F25J2270/00Refrigeration techniques used
    • F25J2270/90External refrigeration, e.g. conventional closed-loop mechanical refrigeration unit using Freon or NH3, unspecified external refrigeration
    • 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
    • F25J2270/91External 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 using pulse tube refrigeration
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02CCAPTURE, STORAGE, SEQUESTRATION OR DISPOSAL OF GREENHOUSE GASES [GHG]
    • Y02C20/00Capture or disposal of greenhouse gases
    • Y02C20/40Capture or disposal of greenhouse gases of CO2

Definitions

  • the present invention is directed to the field of Thermo-acoustic Stirling Hybrid Engines and Refrigerators (TASHER) they being Stirling hybrid devices that achieve cryogenic temperatures without moving parts.
  • TASHER Thermo-acoustic Stirling Hybrid Engines and Refrigerators
  • the invention relates to a new separation method and apparatus for liquefying and removing wanted or unwanted gases from a gas stream, selectively capturing and storing liquefied gases, then allowing the release of desirable gases back into the atmosphere conserving the energy contained in the cooling accompanying their release.
  • thermo-acoustic refrigeration which can potentially be made very efficient and because it has no moving parts and requires almost no maintenance although doubt has previously been has expressed as to whether this method can economically liquefy gases so as to remove “greenhouse gases” from exhaust gases resulting from combustion.
  • thermo-acoustic refrigeration systems use conventional burners and produce levels of NOx that are way above the maximum levels permitted in many countries. Additionally, they make difficult the development of “knife edge” heat sources as are most desirable for the production of the most efficient acoustic wave in the TASHER.
  • pulse combustion burners however increases the thermal efficiency over current systems.
  • the exhaust gases from the pulse combustion system can be heat exchanged with the incoming combustion air and all combustion gases cooled together to delete the greenhouse gases.
  • thermo-acoustic cooling could be used to make an economic and effective answer to the capture and storage for commercial use of wanted gases and eventual sequestration and storage of the unwanted gases.
  • pulse combustion can release 96-98% of the available heat from a fuel with virtually no release of oxides of nitrogen or sulphur and is economical to apply while conventional burners or the use of an electric heat source are generally more expensive and less efficient to apply.
  • Sequestration of greenhouse gases is most desirable, but is difficult and expensive if underground sequestration is to be practiced. This methodology fights against the laws of nature so it requires considerable force (pressure), hence a lot of energy, to pump the greenhouse gases underground, followed by never ending monitoring to ensure safety. If the underground caverns contain resources which are, or may be, valuable, then they too are sequestrated, from economic usage.
  • a better solution would be to deposit the liquefied greenhouse gases in the sea at a depth and temperature which will keep them liquid and, for greater security, under a blanket of silts which will protect them from movement arising from the most extreme mechanical or geological perturbations.
  • the invention is a method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means including the steps of
  • FIG. 1 Shows the general arrangement of the capture process
  • FIG. 2 Shows a means of coupling thermo-acoustic refrigerators
  • FIG. 3 Shows disposal methods for carbon dioxide
  • the gas to be captured is carbon dioxide (CO 2 ) and this is cooled to a liquid state under pressure or solid state.
  • CO 2 can be passed to a repository.
  • the gas stream contains methane, this can be collected for use.
  • the oxygen and nitrogen can be passed to atmosphere but before being so sent, can act as a heat exchange medium for the incoming gas stream.
  • Gases containing CO 2 are invariably the end products of a combustion process or the natural constituents of gases from gas and oil wells. In the case of the former, these gases are normally hot and can be in the vicinity of 900° C. It is to be noted however that the invention is applicable whether or not the gas stream may be hot.
  • FIG. 1 shows the general arrangement of the capture process. Heat exchangers are shown, the first of which 1 is used to partially cool down the incoming hot gas stream containing the CO 2 . The second heat exchanger 2 is used to further cool down the now warm incoming hot gas stream containing the CO 2 using some readily available coolant such as ambient air or cold water.
  • the second heat exchanger 2 is used to remove the bulk of the water from the incoming hot gas stream prior to the refrigeration step.
  • This heat exchanger utilises a coolant such as water or ambient air 25 .
  • Both these heat exchangers may have pulsating flows, whereby the size of the heat exchangers required are considerably reduced and their thermal efficiency is boosted.
  • heat exchangers shown is not the only arrangement that can be employed it is preferred in this embodiment of the invention that a third heat exchanger 3 be used to further cool the incoming gas stream with the coldest stream of nitrogen and remnant oxygen from the refrigeration system.
  • thermo-acoustic refrigerator system 10 The energy to drive each thermo-acoustic refrigerator 30 is provided by an external pulse combustion system 15 .
  • pulse combustion enables the thermal efficiency to be markedly increased over current systems used to add heat to a Thermo-Acoustic Driver, (TAD) 41 , without incurring the penalty of increased emissions of environmentally damaging gases such as the various oxides of nitrogen.
  • TAD Thermo-Acoustic Driver
  • the exhaust gases from the pulse combustion system are heat exchanged with the incoming combustion air which enables the temperature at the hot end of the TAD to be maintained at the highest possible temperature, commensurate with the materials of construction.
  • thermo-acoustic refrigerators 30 can be used when linked together as shown in FIG. 2 .
  • This coupling method is applicable to both the thermo-acoustic driver (TAD) and thermo-acoustic Stirling Hybrid engine (TASHE) of orifice pulse tube refrigerators.
  • TAD thermo-acoustic driver
  • TASHE thermo-acoustic Stirling Hybrid engine
  • TASHER can have the drawback of being very high.
  • the TASHER can then be tuned to reduce noise and to mutually assist another TASHER with which it is joined.
  • the tuning can be achieved by conventional loud speakers placed along the TASHER.
  • the basis of this method is to form a U tube 35 with two TAD or TASHER units with the join 36 being at the coldest end of the refrigerator part where the orifice sits. There being a common orifice 38 between two of the TAD or TASHER units.
  • each TAD or TASHER unit drives the other unit. Both units will automatically go into 180° out of phase resonance when started. Should this not occur the phasing can be achieved by placing suitably tuned closed ended tubes to each TAD or TASHER unit as shown in FIG. 2 .
  • a conventional loud speaker 40 which is driven at the resonant frequency of the main TAD or TASHER unit shells but with the voltage applied at 180° out of phase to each of the loud speakers.
  • thermo-acoustic driver UTAD or UTASHER units require less energy to drive themselves than they would in total on their own. It should be noted however that the position of the side arm closed ended tubes with the loud speakers is not critical and may be placed at any suitable location.
  • the refrigeration process removes the various gases such as CO 2 ( 26 ), SOx ( 27 ) and NOx ( 28 ) from the incoming hot gas stream in a cascade process except for the nitrogen and remnant oxygen from the main combustion process or, in the case of methane sources such as gas wells, coal mine ventilation exit shafts or bio-processes that produce methane, the methane itself which is valuable.
  • gases such as CO 2 ( 26 ), SOx ( 27 ) and NOx ( 28 )
  • the remnant cold stream of nitrogen and oxygen gases is now used to cool the incoming hot gas stream in the first heat exchanger, while itself being heated up to be put 20 into the stack.
  • the methane recovery process is dictated by whether the methane is required as a gas or is itself to be liquefied. If just methane gas is required, the now cool methane is used in the first heat exchanger to cool down the incoming raw methane steam containing water vapour, CO 2 and other minor quantities of different gases which are to be separated from the methane.
  • the CO 2 ( 26 ) is now in a liquid state at high pressure or in a solid state.
  • the long term removal of CO 2 can be achieved in a variety of ways and is based on the fact that CO 2 remains in a liquid state provided the repository temperature is below 30° C. and the pressure is above 7150 kPa.
  • the repository temperature has to be below ⁇ 45° C. and the pressure has to be above 7150 kPa, if the CO 2 is to be deposited in the solid state for it to remain solid.
  • the lower the available pressure in the repository the lower the temperature has to be to keep the CO 2 in the desired state.
  • the disposal methods (shown in FIG. 3 ) all involve depositing the CO 2 using pumping means 50 below the ocean surface 70 into a deep water based environment such as the ocean or an aquifer.
  • the first method 51 involves piping liquid CO 2 at pressure to a point in the ocean where the depth is sufficient to keep the CO 2 in its liquid form and the density differences between the CO 2 and the sea water cause the CO 2 to sink to the bottom of the ocean floor which can be well away from the point of discharge.
  • the second method 52 is an extension of the first method, whereby the CO 2 is kept in a pipe 55 until it reaches the maximum depth of the ocean floor.
  • the pipe work from the point of discharge in the first method can be made of a flexible high density film allowing the CO 2 to take the pipe down to the maximum depth of the ocean floor.
  • the third method 53 involves encapsulating the liquid CO 2 in a suitable material such as high density plastic to form a “sausage” 56 like structure or a package, to which heavy solid material may be added to increase the density well above that of ocean or saline aquifer so that any currents present do not carry the “sausage” or package away from the intended drop zone.
  • a suitable material such as high density plastic
  • the “sausages” or packages can be pumped along a pipe in a similar fashion to “pigs” for oil and chemical pipelines.
  • the “sausage” like structure or package is forced along the pipe to the point of discharge as in method 51 at which point density differences take over and the “sausage” or package travels down to the ocean floor.
  • the liquid CO 2 can be used as a lubricant in the pipe for the sausage like structure.
  • Methods 52 and 53 can be combined in which the flexible plastic pipe becomes a very long “pig” or “sausage” up to several kilometers long. Once filled the pipe is sealed off and dropped to the ocean floor and a new flexible plastic pipe is placed on the pipe to recommence the filling.
  • the last method 54 involves using a drag plough 57 on a chain which contains the opening of a pipe 58 which is connected to the ship 60 at the surface which is pumping the carbon dioxide down.
  • the drag plough is pulled through silts on the sea floor such that CO 2 is deposited underneath 59 where it can remain undisturbed.
  • a mixture of solid and liquid CO 2 slush can be used in the above disposal methods.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Chemical & Material Sciences (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Analytical Chemistry (AREA)
  • Treating Waste Gases (AREA)
  • Separation By Low-Temperature Treatments (AREA)
  • Carbon And Carbon Compounds (AREA)

Abstract

A method for the selective capture and removal of gases and vapors from a gas stream using a thermo-acoustic device includes the steps of first cooling the gas stream using at least one heat exchanger and then passing the stream to a thermo-acoustic refrigeration process and removing gases in a cascade process. The gases that are captured and removed, such as CO2, can be deposited, for example, in a marine environment.

Description

    AREA OF THE INVENTION
  • The present invention is directed to the field of Thermo-acoustic Stirling Hybrid Engines and Refrigerators (TASHER) they being Stirling hybrid devices that achieve cryogenic temperatures without moving parts. In particular the invention relates to a new separation method and apparatus for liquefying and removing wanted or unwanted gases from a gas stream, selectively capturing and storing liquefied gases, then allowing the release of desirable gases back into the atmosphere conserving the energy contained in the cooling accompanying their release.
  • BACKGROUND TO THE INVENTION
  • The liquefaction of gases to enable their storage, or selective removal, has heretofore been generally achieved at costs which limit the usage of the technology, these costs, for instance, being particularly critical to the removal of greenhouse gases from the atmosphere which has importance in the field of climate change.
  • The conventional process for liquefaction of natural gas, or methane, is currently compressor based refrigeration.
  • Because of the temperatures required for this process it is usual to employ multi-stage compressors with the appropriate inter-cooling. The draw backs to this process are that it is not very efficient, multi-stage and it has a high maintenance penalty.
  • The other method of providing refrigeration is via thermo-acoustic refrigeration, which can potentially be made very efficient and because it has no moving parts and requires almost no maintenance although doubt has previously been has expressed as to whether this method can economically liquefy gases so as to remove “greenhouse gases” from exhaust gases resulting from combustion.
  • One known problem is that current thermo-acoustic refrigeration systems use conventional burners and produce levels of NOx that are way above the maximum levels permitted in many countries. Additionally, they make difficult the development of “knife edge” heat sources as are most desirable for the production of the most efficient acoustic wave in the TASHER.
  • Using pulse combustion burners however increases the thermal efficiency over current systems. The exhaust gases from the pulse combustion system can be heat exchanged with the incoming combustion air and all combustion gases cooled together to delete the greenhouse gases.
  • Combined we believe that a combination of pulse combustion and thermo-acoustic cooling could be used to make an economic and effective answer to the capture and storage for commercial use of wanted gases and eventual sequestration and storage of the unwanted gases.
  • It is known that pulse combustion can release 96-98% of the available heat from a fuel with virtually no release of oxides of nitrogen or sulphur and is economical to apply while conventional burners or the use of an electric heat source are generally more expensive and less efficient to apply.
  • We believe that the application of the technology mentioned above can overcome the drawbacks of existing TASHER units, thereby providing a more economic means of liquefaction of gases, or of cooling generally. In addition the size of units is scalable which is an essential feature in dealing with power station exhaust gases of substantial volume.
  • Sequestration of greenhouse gases is most desirable, but is difficult and expensive if underground sequestration is to be practiced. This methodology fights against the laws of nature so it requires considerable force (pressure), hence a lot of energy, to pump the greenhouse gases underground, followed by never ending monitoring to ensure safety. If the underground caverns contain resources which are, or may be, valuable, then they too are sequestrated, from economic usage.
  • A better solution would be to deposit the liquefied greenhouse gases in the sea at a depth and temperature which will keep them liquid and, for greater security, under a blanket of silts which will protect them from movement arising from the most extreme mechanical or geological perturbations.
  • Even greater security could be achieved if the gases were encased in a plastic film which will also allow their re-use if so desired.
  • The undersea methods would appear to have costs of some 25% of the costs applicable to geosequestration in terrestrial cavities.
  • Therefore, there is still a significant unfilled need for a new method and apparatus for the liquefaction of gases and selective treatment of all or some of them and the undesired gases need to be sequestrated at an economic cost which remains undemonstrated.
  • OUTLINE OF THE INVENTION
  • It is an object of the invention to provide improvements over the prior art to enable the economic liquefaction of greenhouse gases, together with more economic liquefaction of desirable gases such as methane. It is a further object of the invention to provide a means whereby, once liquefied, the gases can be separated and the undesirable gases sequestrated. It is a further object of the invention that these objects be achieved in a highly efficient manner and answer the existing needs.
  • It is also an object of the invention to determine how unwanted recovered gases and vapours may be collected and permanently disposed of for geological time scales.
  • The invention is a method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means including the steps of
      • cooling the gas stream using at least one heat exchanger;
      • passing the stream to a thermo-acoustic refrigeration process;
      • removing the gases in a cascade process.
  • In order that the invention may be more readily understood we will describe by way of non limiting example a specific embodiment of the invention with reference to the accompanying drawings.
  • BRIEF DESCRIPTION OF THE DRAWING FIGURES
  • FIG. 1 Shows the general arrangement of the capture process;
  • FIG. 2 Shows a means of coupling thermo-acoustic refrigerators;
  • FIG. 3 Shows disposal methods for carbon dioxide;
  • DESCRIPTION OF AN EMBODIMENT OF THE INVENTION
  • In the following embodiment of the invention the example of a process for the permanent removal of carbon dioxide is described however the invention is not restricted to the processing of carbon dioxide only and can equally be applied to other gases. For convenience sake however it will be described here in terms of its application to the treatment of carbon dioxide.
  • Carbon Dioxide Removal
  • In this embodiment of the invention the gas to be captured is carbon dioxide (CO2) and this is cooled to a liquid state under pressure or solid state. This CO2 can be passed to a repository.
  • If the gas stream contains methane, this can be collected for use.
  • The oxygen and nitrogen can be passed to atmosphere but before being so sent, can act as a heat exchange medium for the incoming gas stream.
  • Gases containing CO2 are invariably the end products of a combustion process or the natural constituents of gases from gas and oil wells. In the case of the former, these gases are normally hot and can be in the vicinity of 900° C. It is to be noted however that the invention is applicable whether or not the gas stream may be hot.
  • FIG. 1 shows the general arrangement of the capture process. Heat exchangers are shown, the first of which 1 is used to partially cool down the incoming hot gas stream containing the CO2. The second heat exchanger 2 is used to further cool down the now warm incoming hot gas stream containing the CO2 using some readily available coolant such as ambient air or cold water.
  • The second heat exchanger 2 is used to remove the bulk of the water from the incoming hot gas stream prior to the refrigeration step. This heat exchanger utilises a coolant such as water or ambient air 25. Both these heat exchangers may have pulsating flows, whereby the size of the heat exchangers required are considerably reduced and their thermal efficiency is boosted.
  • While the arrangement of heat exchangers shown is not the only arrangement that can be employed it is preferred in this embodiment of the invention that a third heat exchanger 3 be used to further cool the incoming gas stream with the coldest stream of nitrogen and remnant oxygen from the refrigeration system.
  • The refrigeration process employs a thermo-acoustic refrigerator system 10. The energy to drive each thermo-acoustic refrigerator 30 is provided by an external pulse combustion system 15. The use of pulse combustion enables the thermal efficiency to be markedly increased over current systems used to add heat to a Thermo-Acoustic Driver, (TAD) 41, without incurring the penalty of increased emissions of environmentally damaging gases such as the various oxides of nitrogen.
  • The exhaust gases from the pulse combustion system are heat exchanged with the incoming combustion air which enables the temperature at the hot end of the TAD to be maintained at the highest possible temperature, commensurate with the materials of construction.
  • In the invention one or more thermo-acoustic refrigerators 30 can be used when linked together as shown in FIG. 2. This coupling method is applicable to both the thermo-acoustic driver (TAD) and thermo-acoustic Stirling Hybrid engine (TASHE) of orifice pulse tube refrigerators.
  • This practice is desirable as a TASHER can have the drawback of being very high. However it is possible to bend the TASHER into a “U” shape and further benefits can arise from two TASHER units being combined in a “U” shape, preferably with the join being at the cold end and the heat engine at the top end. The TASHER can then be tuned to reduce noise and to mutually assist another TASHER with which it is joined. The tuning can be achieved by conventional loud speakers placed along the TASHER.
  • The basis of this method is to form a U tube 35 with two TAD or TASHER units with the join 36 being at the coldest end of the refrigerator part where the orifice sits. There being a common orifice 38 between two of the TAD or TASHER units.
  • By this means each TAD or TASHER unit drives the other unit. Both units will automatically go into 180° out of phase resonance when started. Should this not occur the phasing can be achieved by placing suitably tuned closed ended tubes to each TAD or TASHER unit as shown in FIG. 2. Within each side tube resides a conventional loud speaker 40 which is driven at the resonant frequency of the main TAD or TASHER unit shells but with the voltage applied at 180° out of phase to each of the loud speakers.
  • The resulting U tube thermo-acoustic driver UTAD or UTASHER units require less energy to drive themselves than they would in total on their own. It should be noted however that the position of the side arm closed ended tubes with the loud speakers is not critical and may be placed at any suitable location.
  • The refrigeration process removes the various gases such as CO2 (26), SOx (27) and NOx (28) from the incoming hot gas stream in a cascade process except for the nitrogen and remnant oxygen from the main combustion process or, in the case of methane sources such as gas wells, coal mine ventilation exit shafts or bio-processes that produce methane, the methane itself which is valuable.
  • The remnant cold stream of nitrogen and oxygen gases is now used to cool the incoming hot gas stream in the first heat exchanger, while itself being heated up to be put 20 into the stack.
  • The methane recovery process is dictated by whether the methane is required as a gas or is itself to be liquefied. If just methane gas is required, the now cool methane is used in the first heat exchanger to cool down the incoming raw methane steam containing water vapour, CO2 and other minor quantities of different gases which are to be separated from the methane.
  • Carbon Dioxide Storage
  • The CO2 (26) is now in a liquid state at high pressure or in a solid state. The long term removal of CO2 can be achieved in a variety of ways and is based on the fact that CO2 remains in a liquid state provided the repository temperature is below 30° C. and the pressure is above 7150 kPa. The repository temperature has to be below −45° C. and the pressure has to be above 7150 kPa, if the CO2 is to be deposited in the solid state for it to remain solid. The lower the available pressure in the repository, the lower the temperature has to be to keep the CO2 in the desired state.
  • The disposal methods (shown in FIG. 3) all involve depositing the CO2 using pumping means 50 below the ocean surface 70 into a deep water based environment such as the ocean or an aquifer.
  • The first method 51 involves piping liquid CO2at pressure to a point in the ocean where the depth is sufficient to keep the CO2 in its liquid form and the density differences between the CO2 and the sea water cause the CO2 to sink to the bottom of the ocean floor which can be well away from the point of discharge.
  • The second method 52 is an extension of the first method, whereby the CO2 is kept in a pipe 55 until it reaches the maximum depth of the ocean floor. The pipe work from the point of discharge in the first method can be made of a flexible high density film allowing the CO2 to take the pipe down to the maximum depth of the ocean floor.
  • The third method 53 involves encapsulating the liquid CO2 in a suitable material such as high density plastic to form a “sausage” 56 like structure or a package, to which heavy solid material may be added to increase the density well above that of ocean or saline aquifer so that any currents present do not carry the “sausage” or package away from the intended drop zone.
  • The “sausages” or packages can be pumped along a pipe in a similar fashion to “pigs” for oil and chemical pipelines. The “sausage” like structure or package is forced along the pipe to the point of discharge as in method 51 at which point density differences take over and the “sausage” or package travels down to the ocean floor. The liquid CO2 can be used as a lubricant in the pipe for the sausage like structure.
  • Methods 52 and 53 can be combined in which the flexible plastic pipe becomes a very long “pig” or “sausage” up to several kilometers long. Once filled the pipe is sealed off and dropped to the ocean floor and a new flexible plastic pipe is placed on the pipe to recommence the filling.
  • These methods of encapsulating the CO2 and keeping it contained stop any interaction with the surrounding marine life and also make it easy to recover should it be needed at a future time.
  • The last method 54 involves using a drag plough 57 on a chain which contains the opening of a pipe 58 which is connected to the ship 60 at the surface which is pumping the carbon dioxide down. The drag plough is pulled through silts on the sea floor such that CO2 is deposited underneath 59 where it can remain undisturbed.
  • A mixture of solid and liquid CO2 slush can be used in the above disposal methods.
  • This invention described here provides an improved method of removing gases selectively from a gas stream and while we have described here one specific embodiment of the invention it is to be understood that variations and modifications in this can be made without departing from the spirit and scope of the invention.

Claims (17)

1-23. (canceled)
24. A method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means, comprising the steps of:
cooling a gas stream using at least one heat exchanger;
passing the gas stream to a thermo-acoustic refrigeration process; and,
removing a gas in a cascade process.
25. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 24, further comprising the step of:
capturing the gas removed in said removing step.
26. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 25, wherein the gas captured in said capturing step is carbon dioxide, and further comprising the step of:
cooling the carbon dioxide to either a liquid state under pressure or to a solid state.
27. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 24, wherein the gas stream contains methane.
28. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 24, wherein oxygen and nitrogen act as a heat exchange medium for said at least one heat exchanger for the gas stream that is an incoming gas stream.
29. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 28, wherein the incoming gas stream contains carbon dioxide and further comprising the step of:
cooling the incoming gas stream by passing the incoming gas stream through said at least one heat exchanger.
30. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 29, further comprising the step of:
further cooling the incoming gas stream by passing the incoming gas stream through an additional heat exchanger, or second heat exchanger, via a coolant, said at least one heat exchanger being a first heat exchanger.
31. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 30, wherein said first heat exchanger and said second heat exchanger have pulsating flow for reducing size of said first heat exchanger and said second heat exchanger are able to be decreased and thermal efficiency is increased.
32. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 30, further comprising the step of:
further cooling the incoming gas stream by passing the incoming gas stream through at least one thermo-acoustic refrigerator.
33. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 32, further comprising the step of:
further cooling the incoming gas stream via a third heat exchanger using a cold stream of nitrogen and remnant oxygen from the at least one thermo-acoustic refrigerator.
34. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 32, wherein said at least one thermo-acoustic refrigerator is a plurality of thermo-acoustic refrigerators linked to one another.
35. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 34, wherein said plurality of thermo-acoustic refrigerators are linked via bending a plurality of TASHERs into a “U” shape, so that a plurality of TASHERs are combined in the “U” shape.
36. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 32, wherein said at least one thermo-acoustic refrigerator removes gases from the incoming gas stream in a cascade process, except for nitrogen and remnant oxygen.
37. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 26, further comprising the steps of:
piping carbon dioxide captured in said capturing step as liquid carbon dioxide at pressure to a point in an ocean where ocean depth is sufficient for keeping the CO2 in its liquid phase and density differences between the CO2 and ocean water causes the CO2 to sink to a floor of the ocean.
38. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 37, further comprising the step of:
maintaining the carbon dioxide in a pipe until the carbon dioxide reaches a maximum depth.
39. The method for the selective capture and removal of gases and vapors from a gas stream using thermo-acoustic means according to claim 26, further comprising the step of:
pumping carbon dioxide captured in said capturing step as liquid carbon dioxide to, or near, a floor of an ocean.
US12/440,281 2006-09-07 2007-09-07 Capture and removal of gases from other gases in a gas stream Abandoned US20100037627A1 (en)

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PCT/AU2007/001312 WO2008028238A1 (en) 2006-09-07 2007-09-07 The capture and removal of gases from other gases in a gas stream

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US20170307261A1 (en) * 2014-10-02 2017-10-26 David Proctor Thermoacoustic refrigerator
CN108870801A (en) * 2018-08-09 2018-11-23 江苏热声机电科技有限公司 Refrigeration motor conduction structure
CN108954903A (en) * 2018-08-09 2018-12-07 江苏热声机电科技有限公司 The cold bridge structure of refrigeration motor
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US20170307261A1 (en) * 2014-10-02 2017-10-26 David Proctor Thermoacoustic refrigerator
US10591187B2 (en) * 2014-10-02 2020-03-17 Siddons Enertec Pty Ltd Thermoacoustic refrigerator
CN108870801A (en) * 2018-08-09 2018-11-23 江苏热声机电科技有限公司 Refrigeration motor conduction structure
CN108954903A (en) * 2018-08-09 2018-12-07 江苏热声机电科技有限公司 The cold bridge structure of refrigeration motor
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IT202300002766A1 (en) * 2023-02-17 2024-08-17 Snf Envirotech Srl SYSTEM FOR HEAT REMOVAL FROM A FLUID TO BE COOLED

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CA2662882A1 (en) 2008-03-13
CA2662882C (en) 2015-04-14

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