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.
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.
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:
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
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
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
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
It should be further noted that in
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
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
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
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
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
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
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
In some other embodiments, as indicated in
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
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
In some embodiments, the method further includes increasing a pressure of the condensed CO2 stream 302 using a pump 300, as indicated in
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
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
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
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
In some embodiments, the method further includes increasing a pressure of the condensed CO2 stream 302 using a pump 300, as indicated in
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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.