The present application relates to reactors for gas absorption, purification, and/or reaction and more particularly to composite 3-D printed reactors for gas absorption, purification, and/or reaction.
This section provides background information related to the present disclosure which is not necessarily prior art.
The exchange of gas into or out of a liquid is a common problem in the absorption of gases into a solvent for industrial chemical processes, gas purification, and water purification. The potentially largest scale application is for the absorption of CO2 for carbon capture and storage from power plants. Other applications include purification of natural gas, purification of biogas, and various industrial gas-to-liquid reactions. The most common method for gas absorption is the use of a “packed tower” absorption column. The absorption column is typically a cylindrical reactor filled with a packing material, Liquid solvent is pumped to the top of the tower and allowed to flow down over the packing while gas is blown from the bottom of the tower in the opposite direction. The liquid solvent forms a film over the wetted parts of the packing material, resulting in a gas-liquid interface where the exchange between CO2 and solvent takes place.
A major limitation of these tower packings is that the surface-area to volume ratio of the liquid is limited by the thickness of the liquid film. This thickness is determined by the properties of the solvent, but is typically around 1 mm. Additional area can be put into the tower using finer packings, but this leads to higher holdup of liquid, and impeded gas flow.
Solid sorbents are an alternative to liquid solvents in many applications, including large-scale CO2 capture. Solid sorbents are preferred for air purification for, e.g. small submarines and personal underwater rebreathers and removal of volatile organic compounds emitted from certain industrial processes, Solid sorbents include mineral CO2 sorbents like soda-lime, designer gas sorbents like metal-organic frameworks (MOFs), zeolites, and activated carbons. Solid sorbents are typically prepared in a powder, and must be pelletized or formed into monoliths with a binder, reducing accessible surface area and yielding sub-optimal gas flow.
Features and advantages of the disclosed apparatus, systems, and methods will become apparent from the following description. Applicant is providing this description, which includes drawings and examples of specific embodiments, to give a broad representation of the apparatus, systems, and methods. Various changes and modifications within the spirit and scope of the application will become apparent to those skilled in the art from this description and by practice of the apparatus, systems, and methods. The scope of the apparatus, systems, and methods is not intended to be limited to the particular forms disclosed and the application covers all modifications, equivalents, and alternatives falling within the spirit and scope of the apparatus, systems, and, methods as defined by the claims.
The inventor's apparatus, systems, and methods provide a composite material for gas capture, notably CO2 capture and storage. The composite material includes a mixture of a solid or liquid reactive filler and a gas-permeable polymer (e.g. silicone), such that the reactive filler forms micron-scale domains in the polymer matrix. In contrast to typical absorption schemes based on liquid solvents or solid sorbent powders, the composite materials can be fabricated into arbitrary fixed shapes via additive or conventional manufacturing. The gas-permeable polymer matrix acts as a gas-permeable support while the reactive filler acts as a gas sorbent or catalyst for chemical reactions. Control over the material shape allows for the patterning of high surface-area-to-volume ratio structures for fast reactivity while minimizing pressure drops typically associated with high surface area materials and packings. The inventor's apparatus, systems, and methods can be used for the absorption of gases or catalyzing chemical reactions involving a gas. This use can be tailored for specific applications such as CO2 capture from power plants, CO2 utilization, natural gas purification, biogas purification, and underwater rebreather applications. Specific gases and reactions can be targeted using different reactive fillers.
The apparatus, systems, and methods are susceptible to modifications and alternative forms. Specific embodiments are shown by way of example. It is to be understood that the apparatus, systems, and methods are not limited to the particular forms disclosed. The apparatus, systems, and methods cover all modifications, equivalents, and alternatives falling within the spirit and scope of the application as defined by the claims.
The accompanying drawings, which are incorporated into and constitute a part of the specification, illustrate specific embodiments of the apparatus, systems, and methods and, together with the general description given above, and the detailed description of the specific embodiments, serve to explain the principles of the apparatus, systems, and methods.
Referring to the drawings, to the following detailed description, and to incorporated materials, detailed information about the apparatus, systems, and methods is provided including the description of specific embodiments. The detailed description serves to explain the principles of the apparatus, systems, and methods. The apparatus, systems, and methods are susceptible to modifications and alternative forms. The application is not limited to the forms disclosed. The application covers all modifications, equivalents, and alternatives falling within the spirit and scope of the apparatus, systems, and methods as defined by the claims.
The inventor's apparatus, systems, and methods provide a high-surface-area, hierarchically-structured, reactive composite material for energy-efficient gas purification and the techniques to fabricate this material. The hierarchy consists of, on the one hand, micron-scale domains of solvent or sorbent particles embedded within a gas-permeable polymer to form the composite material and, on the other hand, the submillimeter-scale structures that the composite materials form to create a monolith reactor. The reactor has channels for optimal gas flow and features sized for fast reaction with the gas. The structure optionally consists of hollow tubes where a second solvent, for heat exchange or additional chemical reaction, is flowed through the tube cores.
The reactor is fabricated by dispersing solid sorbents, solid precursors to liquid solvents, or microencapsulated liquid solvents within a 3D printable, gas-permeable polymer, and then printing or otherwise shaping the mixture into reactor structures. The composite material may contain other reactive components, such as a pH-indicator dye to give visual indication of CO2 absorption. Various structures can be printed that have desired properties for gas flow, fit into desired reactor housings, or provide other benefits. Features at the centimeter or larger scale can be incorporated into the printed structure, such as a hierarchy of gas channel sizes. The inventors have shown that the resulting structures absorb CO2 much faster than comparable films of the liquid solvent, indicating much smaller and more efficient reactors are possible using the printed composite concept than with conventional technology. The CO2 absorption rates are higher for smaller filament sizes (which have higher surface area-to-volume ratios) and they approach or exceed the absorption rates for the microencapsulated solvents we have previously developed. Though the inventors' research focus is on CO2 capture and early demonstrations use sodium carbonate. This invention is widely applicable to other solvents, other reactions, and other applications involving gas purification or heterogeneous reactions involving a gas.
Several key innovations underpin the inventor's apparatus, systems, and methods:
1. The method of preparing a gas-absorbing composite material, i.e. by mixing solid precursors to liquid solvents with a gas-permeable polymer precursor, cross-linking the polymer, and then hydrating the solid particles to form micro-scale solvent domains. This innovation is not specific to 3-D printing (it can be achieved by extrusion or other conventional manufacturing techniques), but it is specific to solvents that can be dispersed as solid powders and then re-hydrated, solid sorbents, or microencapsulated solvents.
2. The concept of preparing and 3-D printing a gas-absorptive ink into a monolith reactor with beneficial gas-flow features. This innovation is not specific to liquid solvents and can be applied to absorptive or reactive powders that remain solid, such as metal-organic frameworks.
3. The formation of a composite material as in concepts 1 or 2 into hollow-tube structures, where a second liquid is flowed through the center of the tubes for the purpose of heat exchange. The tubes can be printed with a Direct Ink Write 3-D printing system equipped with core-shell nozzles for printing hollow or liquid-filled tubes.
Referring now to the drawings, and in particular to
A flow chart illustrates the inventor's apparatus, systems, and methods 100. The flow chart illustrates a number of individual steps that encompass the inventor's apparatus, systems, and methods 100.
Step 102 comprises selecting the sorbents. For example, the sorbents can be mixing solid precursors to liquid solvents with a gas-permeable polymer precursor, cross-linking the polymer, and then hydrating the solid particles to form micro-scale solvent domains.
Step 104 comprises dispersing the sorbent material within a 3D printable gas permeable polymer. The inventor's apparatus, systems, and methods are not specific to liquid solvents and can be applied to absorptive or reactive powders that remain solid, such as metal-organic frameworks.
Step 106 comprises 3-D printing and shaping the sorbent material within a 3D printable gas permeable polymer into a monolith reactor with beneficial gas-flow features. The inventor's apparatus, systems, and methods are limited to specific to 3-D printing (it can be achieved by extrusion or other conventional manufacturing techniques), but it is specific to solvents that can be dispersed as solid powders and then re-hydrated, solid sorbents, or microencapsulated solvents.
Step 108 comprises curing the monolith reactor by thermal treatment.
Referring now to
Referring now to
The print head 302 extrudes the material 304 onto the surface 310. Movement of the print head 302 is controlled by computer controller 308 which provides freedom of movement along all axes as indicated by the arrows 309. The instructions for creating the reactor 312 is fed to the computer controller 308. The computer controller 308 uses the instructions to move the print head 302 through a series of moments along the surface 310 forming the reactor 312.
Referring now to
As illustrated in
The inventors' ink that is used to create a monolith reactor includes solid or liquid reactive filler and a gas-permeable polymer, such that the reactive filler forms micron-scale domains in the polymer matrix. The solid particle reactive filler is illustrated in
Referring now to
Referring now to
One specific example of a system for making the spheres is shown in
In operation, the inner fluid 610 (Monoethanolamine/H2O) with a viscosity of 10-50 (cP) and a flow rate of 200-800 (uLh-1) flows in the injection tube 602 in the direction indicated by the inner fluid arrow. As this fluid proceeds it passes thru a droplet forming nozzle 624. The formed droplet 626 is released from the nozzle 602 and becomes encased in the middle fluid 612 (Norland Optical Adhesive Pre-polymer) with a viscosity of 10-50 (cP) and flow rate of 200-800 (uLh-1), the middle fluid 612 is flowing in the direction indicated by arrow 616. The inner fluid droplet 626 becomes encased in the middle fluid 612 forming encapsulated microcapsules 618 that have a CO2 capturing solvent core with a thin CO2, permeable outer shell. The outer fluid (Polyvinyl Alcohol Stabilizer) with a viscosity of 10-50 (cP) and a flow rate of 200-800 (uLh-1) flowing in the outer tube 606 in the direction indicated by arrow 622. This outer fluid 620 carries the fabricated microcapsules 618 into the collection tube 604. There is a boundary layer 614 that prevents the middle fluid 612 and outer fluid 620 from mixing as they have a large difference in both their viscosity and flow rates. The above described method will produce Microcapsules of a controlled size with an inner fluid (solvent/catalyst) enclosed in a CO2 permeable polymer shell. The fabricated microcapsules 618 move out of the system as indicated by arrow 628.
Referring now to
Referring now to
The print head 802 extrudes the material 804 onto the surface 810. Movement of the print head 802 is controlled by computer controller 808 which provides freedom of movement along all axes as indicated by the arrows 809. The instructions for creating the reactor 812 is fed to the computer controller 808. The computer controller 808 uses the instructions to move the print head 802 through a series of moments along the surface 810 forming the reactor 812.
Referring now to
The system 900 uses a stack 904 of reactors in cylindrical rector vessels 902a and 902b for removing the target gas from a fluid or mixture. An example of using the reactor for removing a target gas from a fluid or mixture include use in the capture of carbon dioxide from gas mixtures containing carbon dioxide (examples: fossil fuel plants, natural gas streams, air). Also, the system 900 can be used for removing and/or capturing other gases including nitrous oxides (NOx), sulphates (SOx), hydrogen sulfide, or other trace gases.
The target gas in a fluid or mixture 906 is directed to one of the reactor vessels 902a or 902b. This is accomplished by selectively using the valves 908a and 908b to channel the target gas in a fluid or mixture to the selected reactor vessel. The target gas in a fluid or mixture passes through the selected reactor stack and the reactive material in the reactor removes the gas. The fluid or mixture exits the system through valve 914a or 904b.
The reactors in the stack 904 of reactors needs to be purged of the trapped target gas. This can be accomplished using the temperature control system 912a and/or 912b and the purge system 910a and/or 910b. Once the reactors in the stack 904 of reactors have been purged of the trapped target gas they are ready for reuse. This is accomplished by selectively using the valves 908a and 908b to channel another target gas in a fluid or mixture to the reactor vessel with the purged reactors.
As illustrated in
Referring now to
Although the description above contains many details and specifics, these should not be construed as limiting the scope of the application but as merely providing illustrations of some of the presently preferred embodiments of the apparatus, systems, and methods. Other implementations, enhancements and variations can be made based on what is described and illustrated in this patent document. The features of the embodiments described herein may be combined in all possible combinations of methods, apparatus, modules, systems, and computer program products. Certain features that are described in this patent document in the context of separate embodiments can also be implemented in combination in a single embodiment. Conversely, various features that are described in the context of a single embodiment can also be implemented in multiple embodiments separately or in any suitable subcombination. Moreover, although features may be described above as acting in certain combinations and even initially claimed as such, one or more features from a claimed combination can in some cases be excised from the combination, and the claimed combination may be directed to a subcombination or variation of a subcombination. Similarly, while operations are depicted the drawings in a particular order, this should not be understood as requiring that such operations be performed in the particular order shown or in sequential order, or that all illustrated operations be performed, to achieve desirable results. Moreover, the separation of various system components in the embodiments described above should not be understood as requiring such separation in all embodiments.
Therefore, it will be appreciated that the scope of the present application fully encompasses other embodiments which may become obvious to those skilled in the art. In the claims, reference to an element in the singular is not intended to mean “one and only one” unless explicitly so stated, but rather “one or more.” All structural and functional equivalents to the elements of the above-described preferred embodiment that are known to those of ordinary skill in the art are expressly incorporated herein by reference and are intended to be encompassed by the present claims. Moreover, it is not necessary for a device to address each and every problem sought to be solved by the present apparatus, systems, and methods, for it to be encompassed by the present claims. Furthermore, no element or component in the present disclosure is intended to be dedicated to the public regardless of whether the element or component is explicitly recited in the claims. No claim element herein is to be construed under the provisions of 35 U.S.C. 112, sixth paragraph, unless the element is expressly recited using the phrase “means for.”
While the apparatus, systems, and methods may be susceptible to various modifications and alternative forms, specific embodiments have been shown by way of example in the drawings and have been described in detail herein. However, it should be understood that the application is not intended to be limited to the particular forms disclosed. Rather, the application is to cover all modifications, equivalents, and alternatives failing within the spirit and scope of the application as defined by the following appended claims.
The present application is a Division of application Ser. No. 15/468,297 filed Mar. 24, 2017, the disclosure of which is hereby incorporated by reference in its entirety for all purposes.
The United States Government has rights in this application pursuant to Contract No, DE-AC52-07NA27344 between the United States Department of Energy and Lawrence Livermore National Security, LLC for the operation of Lawrence Livermore National Laboratory.
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Number | Date | Country | |
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20190232247 A1 | Aug 2019 | US |
Number | Date | Country | |
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Parent | 15468297 | Mar 2017 | US |
Child | 16380648 | US |