The removal of carbon dioxide from closed environments such as spacecraft and submersible craft is necessary to maintain carbon dioxide levels within accepted respirable limits. Currently, carbon dioxide removal is typically accomplished through non-reversible chemical fixation sorbents (lithium hydroxide, potassium superoxide), reversible chemical fixation adsorbents (liquid amines) or reversible physical adsorption (molecular sieve). Each of these removal systems has one or more drawbacks. For example, non-reversible sorbents do not allow captured carbon dioxide to be used in Sabatier reactions for the generation of water and oxygen. Oxygen generation via a Sabatier reaction can reduce resupply requirements for spacecraft. The carbon dioxide is not available for additional reactions and the used sorbents must be stored on the spacecraft or submersible for later disposal, taking up space and adding weight to the craft. Chemical fixation by liquid amines such as monoethanolamine (MEA) requires high temperatures (120° C.) and, therefore, large amounts of energy, to reverse the carbon dioxide capture reaction. MEA also degrades at elevated temperatures and can potentially contaminate closed environments due to its relatively low vapor pressure. Molecular sieves require very dry air streams. Water vapor must be removed from air streams before they are delivered to molecular sieves. Regeneration cycles of molecular sieves also require temperatures on the order of 200° C. (400° F.) and large amounts of energy.
In view of the disadvantages of existing technology, an alternative carbon dioxide removal method and system that is regenerative and allows for downstream processing (i.e. Sabatier reaction) is desirable.
A carbon dioxide (CO2) removal system includes first and second sorbent beds, a heat exchange system and means for reducing a partial pressure of CO2. The first and second sorbent beds each have a solid amine sorbent for adsorbing and desorbing CO2. At a given time, one of the sorbent beds adsorbs CO2 and the other sorbent bed desorbs CO2. The heat exchange system cools the sorbent bed adsorbing CO2 and heats the sorbent bed desorbing CO2 so that the temperature of the sorbent bed desorbing CO2 is greater than the temperature of the sorbent bed adsorbing CO2. The means for reducing a partial pressure of CO2 reduces partial pressure of CO2 at the sorbent bed desorbing CO2.
A method for removing CO2 from a gas stream includes supplying the gas stream to a first sorbent bed containing a solid amine sorbent and a second sorbent bed containing a solid amine sorbent to cause CO2 to be adsorbed and removed from the process air stream. Pressure is reduced at one of the first and second sorbent beds to cause CO2 to be desorbed and removed from the first and second sorbent beds so that one of the first and second sorbent beds is adsorbing CO2 and the other sorbent bed is desorbing CO2. The sorbent bed that is desorbing CO2 is heated and the sorbent bed that is adsorbing CO2 is cooled so that a temperature of the sorbent bed desorbing CO2 is greater than a temperature of the sorbent bed adsorbing CO2. CO2 is removed from the sorbent bed desorbing CO2 as a CO2 gas stream.
The present invention provides a system and method for carbon dioxide removal. The carbon dioxide removal system utilizes thermally linked sorbent beds. Minimal additional energy is used to heat and cool the desorbing and adsorbing beds, respectively. A pump or vacuum is used to reduce carbon dioxide partial pressure at the desorbing bed. The removed carbon dioxide can be removed from the system or routed for other uses such as Sabatier reactions. The carbon dioxide removal method and system of the present invention enables the use of a range of bed sizes that can be cycled at various frequencies between adsorption and desorption without incurring significant power penalties because the temperatures of the adsorbing and desorbing beds are kept low.
According to the carbon dioxide removal systems and methods described herein, process streams include any gaseous stream. Process streams generally include gas streams circulating within closed environments including, but not limited to, spacecraft, submersible craft, aircraft and other closed air environments. Exemplary process streams include air streams in spacecraft and submersible craft, such as cabin air. These process streams contain carbon dioxide that can be removed from the process stream and reintroduced into another stream for use in other reactions or removed from the spacecraft, submersible craft, aircraft or other closed air environment.
First sorbent assembly 14A includes a solid amine sorbent. Solid amine sorbent 26 is contained within first sorbent assembly 14A. Solid amine sorbent 26 is a regenerable CO2 sorbent. In one exemplary embodiment, solid amine sorbent 26 constitutes one of the amine sorbents described in U.S. Pat. No. 6,364,938, which is hereby incorporated by reference in its entirety. Under certain conditions, solid amine sorbent 26 adsorbs CO2 from a process stream flowing through first sorbent assembly 14A and in contact with solid amine sorbent 26. In this case, CO2 is removed from the process stream flowing through first sorbent assembly 14A when it is adsorbed by solid amine sorbent 26. Under other conditions, solid amine sorbent 26 desorbs CO2 to a process stream flowing through first sorbent assembly 14A and in contact with solid amine sorbent 26. Here, CO2 from solid amine sorbent 26 is taken up by the process stream and carried away from first sorbent assembly 14A. The temperature of and pressure surrounding solid amine sorbent 26 determines whether solid amine sorbent 26 adsorbs CO2 or desorbs CO2. Second sorbent assembly 14B is generally located near and can have identical or similar size and dimensions to first sorbent assembly 14A. Second sorbent assembly 14B also includes solid amine sorbent 26. First sorbent assembly 14A and second sorbent assembly 14B are designed to generally operate in opposing sorption modes. That is, when first sorbent assembly 14A is adsorbing CO2, second sorbent assembly 14B is desorbing CO2. When first sorbent assembly 14A is desorbing CO2, second sorbent assembly 14B is adsorbing CO2.
First sorbent assembly 14A and second sorbent assembly 14B are thermally linked by a heat exchange system. In the embodiment illustrated in
Gas stream outlet valve 18 communicates with first sorbent assembly 14A and second sorbent assembly 14B. Gas stream outlet valve 18 allows a process stream that has passed through a CO2 adsorbing bed (first sorbent assembly 14A or second sorbent assembly 14B) to exit CO2 removal system 10 and return to the spacecraft, submersible craft or other closed environment with a lower amount of CO2 than the process stream contained when it entered CO2 removal system 10 through inlet valve 12. At a given time, gas stream outlet valve 18 communicates with the CO2 adsorbing bed but not the CO2 desorbing bed.
CO2 outlet valve 20 also communicates with first sorbent assembly 14A and second sorbent assembly 14B. CO2 outlet valve 20 allows a process stream that has passed through a CO2 desorbing bed (first sorbent assembly 14A or second sorbent assembly 14B) to exit CO2 removal system 10. The process stream exiting CO2 removal system 10 through CO2 outlet valve 20 generally has a higher concentration than the process stream entering CO2 removal system 10 through inlet valve 12.
In one embodiment of CO2 removal system 10, CO2 outlet valve 20 is positioned between first sorbent assembly 14A and second sorbent assembly 14B and pump 22. Pump 22 is a fluid pump that is capable of reducing the pressure within CO2 removal system 10 at and “downstream” from first sorbent assembly 14A and second sorbent assembly 14B. Pump 22 pumps fluid out of and away from CO2 removal system 10. Pump 22 essentially reduces pressure on the outlet side of first sorbent assembly 14A and second sorbent assembly 14B to increase the rate of CO2 removal (desorption) from the desorbing bed. As discussed in greater detail below, pump 22 allows CO2 removal system 10 to produce an exiting process stream rich in CO2. In spacecraft applications, pump 22 can be replaced by a space vacuum.
The process stream flowing through CO2 outlet valve 20 can be disposed of or collected. When a space vacuum is used in place of pump 22, the process stream removed from CO2 removal system 10 through CO2 outlet valve 20 is disposed of as it is vented to space (i.e. dumped overboard). When CO2 removal system 10 includes pump 22, the process stream removed through CO2 outlet valve 20 can be disposed of (i.e. dumped overboard) or collected for additional use. Some regulations discourage the terrestrial disposal of CO2. Other applications can use process streams rich in CO2 in Sabatier reactions to form water and/or oxygen.
In the embodiment of CO2 removal system 10 shown in
As shown in
As shown in
At the same time that first sorbent assembly 14A is adsorbing CO2, second sorbent assembly 14B is desorbing CO2. Second sorbent assembly 14B includes solid amine sorbent 26 that contains adsorbed CO2 from an earlier CO2 adsorption cycle. The desorption of CO2 by solid amine sorbent 26 is endothermic. As noted above, as the temperature of solid amine sorbent 26 decreases, the loading capacity for CO2 adsorption increases. Thus, as CO2 is desorbed by solid amine sorbent 26, the temperature of solid amine sorbent 26 decreases, making it more difficult to desorb CO2 until it reaches an equilibrium state where the temperature of solid amine sorbent 26 prevents further CO2 desorption. At the same time that thermoelectric device 16 operates to cool first sorbent assembly 14A, thermoelectric device 16 heats second sorbent assembly 14B. By actively heating second sorbent assembly 14B, the CO2 loading capacity of solid amine sorbent 26 is decreased making it easier to desorb CO2 from solid amine sorbent 26 within second sorbent assembly 14B.
Pump 22 operates to reduce the partial pressure of CO2 at second sorbent assembly 14B. As noted above, as the partial pressure of CO2 within second sorbent assembly 14B increases, the loading capacity for CO2 adsorption also increases. Pump 22 communicates with the CO2 desorbing bed—second sorbent assembly 14B in the system shown in
The descriptions of the CO2 adsorbing bed (first sorbent assembly 14A) and the CO2 desorbing bed (second sorbent assembly 14B) in
The transitional states described above can be isolated from the adsorbing and desorbing operations or integrated within the adsorbing and desorbing operations. For example, first sorbent assembly 14A can be isolated from CO2 removal system 10 using valves 12, 18 and 20 to prevent process stream flow through first sorbent assembly 14A. First sorbent assembly 14A can then be heated to increase the pressure within first sorbent assembly 14A. Once first sorbent assembly 14A has been heated to an appropriate temperature, valves 12, 18 and 20 can be positioned to allow first sorbent assembly 14A to transition to the desorption mode. Alternatively, first sorbent assembly 14A can transition to the desorption mode followed by heating and application of negative pressure to increase the rate of CO2 desorption. Whether the transitional states are isolated or integrated within CO2 removal system 10 will depend on application or efficiency requirements and design considerations for CO2 removal system 10.
A wide range of temperatures are suitable for first sorbent assembly 14A and second sorbent assembly 14B during the CO2 removal process. CO2 removal system 10 generally operates most effectively at temperatures between about 15° C. and about 80° C. In an exemplary embodiment, the desorbing bed is heated to a temperature between about 35° C. and about 80° C. while the adsorbing bed is cooled to a temperature between about 15° C. and about 25° C. In one exemplary embodiment, the desorbing bed is heated to a temperature between about 55° C. and about 80° C. Due to the energy required to actively heat and cool first sorbent assembly 14A and second sorbent assembly 14B, keeping the temperature difference between the desorbing bed and the adsorbing bed small is desirable. Determination of ideal temperature differences depends upon the particular application CO2 removal system 10 is designed for in addition to CO2 removal rate requirements. In exemplary embodiments, the temperature difference between the desorbing bed and the adsorbing bed is between about 10° C. and about 65° C. In one exemplary embodiment, the temperature difference between the desorbing bed and the adsorbing bed is between about 10° C. and about 35° C. The low temperature difference between the desorbing and adsorbing beds generally allows CO2 removal system 10 to operate with much greater efficiency than liquid amine and molecular sieve systems. Generally speaking, lower temperature differentials are not necessarily required on submersible craft where energy sources are not limited; however, lower temperature differentials can be preferred for some spacecraft applications where energy sources are limited.
A wide range of pressures can be drawn on the desorbing bed. CO2 removal system 10 generally operates most effectively where pump 22 or space vacuum 36 generates a negative pressure on the desorbing bed between about 3.5 kPa (0.5 psi) and about 100 kPa (14.5 psi). In an exemplary embodiment, a negative pressure of between about 40 kPa (5.8 psi) and about 80 kPa (11.6 psi) is drawn on the desorbing bed.
CO2 removal system 10 can employ a wide range of cycle times between bed transitions from CO2 adsorption to CO2 desorption and vice versa. As is the case with the temperature difference between the adsorbing bed and the desorbing bed, determination of ideal cycle times depends upon the particular application CO2 removal system 10 is designed for in addition to CO2 removal rate requirements. In exemplary embodiments, the adsorbing and desorbing beds cycle at an interval no greater than about 30 minutes. In one exemplary embodiment, the adsorbing and desorbing beds cycle at an interval no greater than about 20 minutes.
In addition to the CO2 removal system described above, the present invention provides a method for removing CO2 from a gas stream. Taken from the above description of CO2 removal system 10,
While the invention has been described with reference to exemplary embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiments disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.