The present disclosure relates generally to a method for making a carbon formation reactor, and a method for using the same.
For manned space flights (and other applications requiring life-support systems) it is desirable to recover oxygen from the carbon dioxide exhaled by the crew. This can be partially achieved with electrolysis (water or carbon dioxide electrolysis) and/or reverse water gas shift reactors, which convert carbon dioxide to carbon monoxide. However, an additional “carbon formation” process step is required to convert carbon monoxide to solid carbon, allowing the system to recover all of the oxygen. For example, carbon monoxide can be reduced to solid carbon via the Boudouard reaction shown below:
CO+COCO2+C(s)
The following disclosure reveals a reactor design based on a catalyst coatings approach that can significantly reduce the size, mass, and/or catalyst consumption costs of carbon formation reactors compared to previous approaches, for example, as reported in Holmes, R. F., E. E. Keller, and C. D. Kilzg, A Carbon Dioxide Reduction Unit Using Bosch Reaction and Expendable Catalyst Cartridges, NASA Report, Contract NAS 1-8217. For a one Crew Member (CM) reactor (272 g/day of carbon), the disclosed reactor core is <8 kg mass with and <10 L volume. The reactor resupply is <1 kg/year/CM, with regeneration frequency >24 hours. For a possible 1-CM CFR design of 20 cm OD by 30 cm L, the size and mass would be 9.4 L, <4 kg. Based on 2,200 cm2 available coating area in the design, catalyst activity of at least 5 mgcarbon/cm2/hr is required to make sufficient carbon for 1 CM (272 g/day). This provides an activity target for catalyst testing. Further based on a target 5 mg/cm2 of catalyst loading, the catalyst must last 97 hours before replacement for resupply to be <1 kg/year. Catalyst testing examples described below reveal examples of catalysts that can meet these requirements. In some examples catalyst coatings were deposited on light-weight woven carbon cloth. However, as will be discussed, catalyst can be coated on a number of other substrate surfaces, including steel, copper, or quartz. Additionally, carbon cloth can be used as a “filter” media at the reactor exit to retain the formed carbon and catalyst. The disclosed invention may also find use in terrestrial applications including carbon sequestration systems and manufacturing of carbon nano-materials. Further, it is expected that the catalysts and reactor design could generate carbon from nearly any non-oxidizing gas stream that contains carbon.
The following disclosure reveals a reactor design based on a catalyst coatings approach that can significantly reduce the size, mass, and/or catalyst consumption costs of carbon formation reactors compared to previous approaches. The carbon formation process as described refers to the formation of solid carbon from a gaseous stream, however, one skilled in the art will realize that the reactor and method could be applicable to any fluidic stream.
Without limiting the scope of the carbon formation reactor as disclosed herein and referring now to the drawings and figures:
These illustrations are provided to assist in the understanding of the exemplary embodiments of a carbon formation reactor, and a method for using the same, as described in more detail below, and should not be construed as unduly limiting the specification. In particular, the relative spacing, positioning, sizing and dimensions of the various elements illustrated in the drawings may not be drawn to scale and may have been exaggerated, reduced or otherwise modified for the purpose of improved clarity. Those of ordinary skill in the art will also appreciate that a range of alternative configurations have been omitted simply to improve the clarity and reduce the number of drawings.
Examples of CFR Test Results
2.5-cm Test Results.
A 2.5-cm OD reactor was set-up to test 5-cm2 catalyst-coated carbon cloth discs mounted perpendicular to the gas flow (see
1) Tests ran 18 hours with GC injections every 20 minutes;
2) Feed gas of 44% CO, 44% H2, 12% CO2, flow rate of 10 sccm unless otherwise specified;
3) Operating temperature of 475° C., unless otherwise specified; and
4) A solution of 10:10:1 by mass mixture of iron nitrate:cobalt nitrate: Sekisui BL-1 binder dissolved in water was used to coat the samples prior to testing unless otherwise specified.
A number of variables were tested, including:
1) Catalyst composition and loading;
2) Catalyst support (type of cloth and microporous carbon coating);
3) Flow rate;
4) Gas composition;
5) Temperature; and
6) Pre-treatment conditions.
An overview of test results is shown in
Experimental test runs 18-26 to 18-113 (shown in
1) Optimal temperature was identified as 475° C.;
2) High performance was obtained in humidified gas streams (18-80, 18-82);
3) The best-performing catalysts have some methane selectivity. It is not believed that methane would build up in a closed system with a recycle loop because its product composition is equilibrium limited;
4) Based on GC analysis (data not shown) the product gas composition was fairly stable once the operating temperature is reached, and the product gas clears out the downstream part of the system. This indicates that the growth rate is not aided by initial high activity, and can continue to produce carbon for a longer time;
5) Some increase in CO product is observed as the test proceeds, likely indicating one of two phenomena: (1) the catalyst may have a slow degradation mechanism, or (2) as the pressure drop across the cloth increases with increases carbon deposits, a higher percentage of the gas circumvents the cloth around the edges, which are not sealed to the reactor walls;
6) The catalyst can be supported effectively either directly on the carbon cloth, or on cloth that is pre-coated with microporous carbon nanofibers. Directly on the cloth has an advantage of being easier to ship and store. However, the direct cloth approach requires reduction using the gas feed at 550° C. that can be done either in situ or externally to obtain higher catalytic performance. It is believed that the reduction step may convert the catalyst component from a nitrate to a more active alloy and/or carbide phase;
7) Fe/Co consistently has about 2× higher growth rates than iron. Both make 5-10% methane (dry composition). The nitrate form worked better than pre-reduced metallic particles; and
8) Carbon yield of 15-17% was repeatedly obtained under standard test conditions at the target growth rate. Higher carbon yield of 30.3% was obtained at lower flow rate (see
A number of gas compositions were examined in testing. As the CFR could be integrated into systems with various design approaches. Consequently, catalyst-coated cloths were tested under a range of gas compositions. For example, the standard gas composition consisting of 40% CO, 40% H2, 10% CO2 and 10% N2 is representative of the predicted dry product stream from a Solid-Oxide Co-Electrolysis (SOCE) unit with 80% carbon dioxide conversion. A gas composition of 35% CO, 51% H2 and 15% CO2, more closely representing 70% SOCE conversion was tested and demonstrated above target carbon formation (see
Accordingly, tests were also run to evaluate performance when water is present in the gas stream. Humidification of the gas stream was completed using a simple water bubbler immediately adjacent to the reactor inlet. The extent of humidification was controlled via bubbler temperature and a benchtop controller. Tests were run at 10% humidification, corresponding to 80% SOCE conversion up to 19% humidification, corresponding to 70% SOCE conversion. The results of the testing are shown in
Maximizing the catalyst lifetime and minimizing operator time will greatly reduce the equivalent system mass (ESM). Accordingly, tests were conducted on the 2.5 cm platform investigating the life of the carbon fiber cloth and catalyst. Testing demonstrated performance stability over 100 hours while operating at 10 sccm (see
A series of tests also examined the effect of temperature. At temperatures below 425° C. the target carbon formation rate was not achieved; however, the loss in performance is mild until below about 350° C. (see
7.5-cm Test Results.
A 7.5-cm OD CFR test bed was constructed to test three-dimensional catalyst substrates. Three configurations were used for this testing: (1) woven carbon fiber cloth bags with a fixed collar, (2) woven carbon cloth bags strapped to the outside of an inlet tube, and (3) flat stainless steel sheets. A drawing of the copper collar configuration is shown in
Beyond just sample activity, tests at this scale examined long-term performance, regeneration tests, and mechanical durability of the support. Variables that were examined included:
1) Type of substrate (carbon cloth, stainless sheet, etc.);
2) Shape of the substrate (L:D ratios, flat plate);
3) Painting versus spraying of the catalyst coating; and
4) Hydroxide versus nitrate catalyst precursor.
1) Using 3:2 dimension ratio improved performance of cloth bags;
2) High activity could be obtained with either painting or spraying of the catalyst coating;
3) Flat steel sheets performed as well as cloth bags;
4) Regenerations worked better if catalyst was added after carbon removal; and
5) Mechanical problems with coated carbon cloth bags or steel cloth bags after several cycles were observed, but no mechanical problems were observed with stainless steel plates.
Testing began with a focus on matching the activity of the 2.5-cm tests. All tests incorporated about 100 square centimeters of coated material, an area increase of >20× compared to the 2.5-cm test examples. Most tests were run by strapping carbon cloth tubes around a 2.5-cm steel tube fitting. The furnace design was updated for test 18-106 (
Thicker catalyst coating formulations were also examined. These thicker formulations allow the catalyst to be painted with a roller onto a single side of the cloth. Both formulations yielded good results, with test 18-135 (
Next, testing switched to a focus on regeneration, and matching the activity target over multiple runs. Tests incorporated 50 to 150 square centimeters (depending on geometry) of coated carbon fiber cloth. Most regeneration tests were run by strapping carbon cloth tubes around a 3.8-cm OD steel fitting, with a coated cloth area that was ˜3.8 cm OD by 5.7 cm long, matching the 2:3 ratio of the target design reported above. In some testing, a flat 100-cm2 cloth (14.3 cm by 7.0 cm) coated on one side and laid parallel to the gas flow on a quartz plate was tested. In these tests, carbon was removed from the cloth with gentle brushing and reloaded and run again. In one case, aqueous catalyst solution was used to regenerate the cloth activity. In the first regeneration run, using the cloth from 18-135 (
Since a larger full-scale design would have more volume for carbon growth, it was decided to test a flat carbon sheet that allows more volume for carbon growth. In this test (18-149) (
Within the regeneration testing, observations were also made regarding the cloth mechanical durability. The cloths were removed from the reactor and weighed for each run. The cloths held together well after one run, even for the long 48 hour runs; however, they became brittle and more fragile after 2 cycles or more. Based on this result, testing switched focus to alternative supports, such as silicon carbide fabric, woven stainless steel fiber cloth, and stainless steel sheet (see Tests 18-157 through 18-170)(
Overall it was found that all of the catalyst supports performed roughly the same, with activity above the target. However, the woven non-carbon supports suffered the same fate as the carbon cloth, and became brittle during carbon growth. The steel sheet was not affected by the testing other than a change to the surface color. Consequently, the stainless steel sheet catalyst support was used in further testing, and eventually was incorporated into a prototype reactor design, as discussed in the following subsections.
In the final three standard 7.5-cm tests the use of hydroxide catalyst suspension was examined (
The hydroxide catalyst was of interest because it contains more metal by mass than nitrate or acetate salts. In each test, a catalyst loading of 5 mg/cm2 (dry solids and binder weight) was targeted on 100-cm2 stainless steel sheets. Identical activation procedures of 1 hours at 550° C. were used for each sample. The first three runs (
Tests were also run to examine hydroxide catalyst that was sprayed through a nozzle. In order to spray the catalyst suspension through a nozzle, the catalyst had to be milled using an attrition mill to break up agglomerates, then passed through a fine mesh. There was some concern that the milling step may affect performance. Additionally, the sensitivity of performance to catalyst loading was tested. Run 31-019 (
Durability Test Results.
There is uncertainty that the desired life of a stainless steel reactor may exceed thousands of hours. It is possible that as carbon grows on the steel walls, small amounts of the steel may be mechanically eroded. The steel may be subject to corrosion, although no evidence during current testing has yet supported this. An attempt was made to determine the rate the steel liner (or CFR wall) will degrade during operation, particularly during carbon removal, heating and cooling, and subsequent sheet infiltration. For this testing a 316 stainless steel sheet, 5 cm×20 cm, was cut from the same stainless steel feedstock used in prototype liners. The sheet was spray-coated with the 5 mg/cm2 target loading of Fe/Co hydroxide catalyst and 30% corn starch as the binder. The sheet was then placed in the 7.5 cm reactor for subsequent testing under standard operating conditions. However, >100 hour long tests would require an extensive amount of time to allow for the number of cycles desired (at least 10). Accordingly, the test procedure was modified so that the sheets could be cycled daily, by reducing the operating time to 18 hours. As a result, sheets were treated at 550° C. for 1 hour followed by 18 hours at 475° C. The gas composition was 40% CO, 40% H2, 10% CO2, and 10% N2 and was run at 200 sccm. Tests were also run with copper sheets for comparison. Copper may be a more appropriate reactor material to avoid long-term degradation. After each cycle, any carbon on the sheets was collected and weighed. The sheet was then wiped cleaned, dried and weighed. A total of 10 cycles were run for each sheet.
Adhesion Test Results.
In an effort to improve catalyst adhesion and optimize binder loading, a study was performed to test adhesion of the catalyst to the steel liner. Accordingly, several different adhesion agents at different loading levels were assessed on stainless steel coupons. In particular, binders, including cornstarch at 10, 20, 30 and 40% by wt. levels, polyacrylic acid at 10 and 40%, and methyl cellulose at 30%, were evaluated for adhesion. In addition, ferrous acetate, due to its sticky behavior upon drying, was also evaluated as an adhesive agent and as a raw material for the Fe portion of the catalyst. Slurry compositions of each formulation were prepared and sprayed onto metal coupons. Sprays of slurry were applied until the dried coat weight reached the target catalyst loading. The coated coupons were placed vertically into alumina crucibles, held up by steel clips, and placed into the 7.5 cm quartz reactor used previously on this project. The samples were purged with the mixed CFR feed gas for 1 hour before being heat treated to 550° C. for 1 hr, i.e. the standard activation/reduction condition. After firing, the steel sheets were collected, imaged, and weighed to determine the carbon loading on the sheets. The results of this study are summarized in
The amount of carbon adhered to the steel sheet with 40% cornstarch is much greater than the 10% case. Data from
Optimization of the adhesive agent is critical to reducing the weight of the final catalyst composite needed. Accordingly, other agents, polyacrylic acid and methyl cellulose, were also assessed for performance. Ideally, the best agent would function well at the lowest loading and lead to extensive carbon growth. However, these alternative adhesive agents, according to the results in
15-cm Test Results
Alpha-Prototype Testing. The “alpha-prototype” CFR test bed was initially designed and used to demonstrate activity and regeneration of 0.5 CM carbon cloth catalyst supports. The prototype, as seen in
The goals of the alpha-prototype testing included:
1) Demonstrate that the target activity can be achieved at the 15-cm OD (˜0.5 CM) scale;
2) Demonstrate activity targets for 100 hours of operation;
3) Test carbon removal procedures after 100 hours of operation;
4) Determine design changes for the next generation beta-prototype reactor; and
5) Perform tests to assist in failure mode analysis.
For each test, 900 to 1,200-cm2 supports (carbon fiber cloths or stainless steel sheets/reactor liners) were coated with catalyst, then rolled up and activated in the 7.5-cm reactor. In some cases, the cloths were formed into a bag before activation. Unlike previous 7.5-cm testing, catalyst adhesion was more challenging at the larger scale due to a vertical orientation and the handling required to load the samples. Approximately 10% Sekisui BL-1 binder was used in the catalyst coatings unless otherwise specified. Tests were run with a gas composition of 40% CO, 40% H2, 10% CO2, 10% N2, at the indicated flow rate. An overview of the tests completed is shown in
The following important points from alpha-prototype testing are as follows, and details are discussed in the following paragraphs.
1) Steel sheets lining the reactor, with a carbon cloth disk covering the exit, held up better mechanically during long-term operation and through regeneration; no loss of catalyst activity was observed compared to carbon cloth in this configuration;
2) An Fe/Co hydroxide catalyst would enable resupply mass targets <1 kg/CM/yr to be achieved;
3) Activity above the target over 100 hours straight of operation was proven; and 4) The carbon product was soft and could be removed via vacuum.
In the initial test (
Next, long-term tests were run with carbon cloths. The first test (
After demonstration at the 7.5-cm (100-cm2) scale, a 900-cm2 stainless steel sheet was also examined as the catalyst substrate in the alpha-prototype (
In the next long-term 15-cm OD test, a stainless steel sheet was examined with a multi-layer base (steel mesh followed by carbon cloth, followed by alumina felt) that acts as a filter. The multi-layer base was added to keep as much carbon as possible inside of the reactor. The inlet tube was also replaced with a copper-lined inlet. In this test, carbon was not removed from the reactor until after completion. Additional catalyst was added every 20 hours in an attempt to maintain elevated activity by frequently introducing fresh catalyst. The catalyst loading over the entire run was consistent with the 1 kg/yr/CM target, assuming iron (III) nitrate basis. Over 100 hours the reactor operated without clogging; however, the performance did not match the activity targets. The final iron nitrate test (
In the final alpha-prototype test, a stainless steel sheet coated with hydroxide-based catalyst with 30% cornstarch as binder was examined. The catalyst and cornstarch were mixed in water to form a viscous liquid, brush-coated on the steel sheet, then dried at 70° C. in an oven before loading in the reactor. The test ran for 100 hours with no reinfiltration of new catalyst. The catalyst loading was consistent with the target of less than 1 kg/yr/CM target. Over 100 hours the reactor achieved area-based activity of 6.52 mg/cm2/hr, easily exceeding the target of 5 mg/cm2/hr.
Beta-Prototype Testing.
Based on the results from alpha-prototype testing, a beta-prototype CFR was built for testing.
1) A longer feed line (including coil) was included to pre-heat gases. The line was entirely copper-clad. A thermocouple was added to the gas inlet for monitoring inlet temperature;
2) A ¼″ Swagelok port with graphite ferrule was added to the lid to allow an agitator arm to be inserted into the reactor;
3) Addition of a 1.5″ OD port with Swagelok cap for vacuum carbon removal;
4) A larger exit port with copper cladding to reduce risk of copper clogging; and
5) Bolted lid to reduce leaking.
For the beta-prototype, hydroxide catalyst and 30% cornstarch binder coated on stainless steel was used for most testing. For some tests, the stainless steel liner was initially spray-coated with aqueous catalyst precursor, then loaded and activated in the reactor before the test began. In other cases, the CFR was activated by in situ spraying of the walls with the catalyst precursor. Various carbon agitation approaches were examined, as will be discussed. Goals that were a focus of the beta-prototype testing included:
1) Shakedown testing to verify the reactor design functions as expected;
2) Increase to maturity of the technology by:
a) Demonstrating >100 hours of catalyst operation before regeneration;
b) Demonstrating vacuum carbon removal via the vacuum port;
c) Demonstrating in situ catalyst spray injection regeneration;
d) Perform tests to assist in failure mode analysis;
e) Regenerate the same steel liner multiple times; and
f) Demonstrate operation in humidified gas streams and updated compositions simulating integration with various system design options.
An overview of the results is given below in
1) Activity targets were achieved over 100 hours with use of the optimized binder spray;
2) Pressure limits were reached after 130 hours (no agitation during test); 144 hours of testing was demonstrated with periodic agitation and pressure did not increase;
3) As high as 99% carbon removal through vacuum port was demonstrated with use of an agitator, and typically >97% of the carbon was removed;
4) in situ spray regeneration of the CFR was demonstrated;
5) Carbon cloth used on the reactor exit for filtering large particles demonstrated greater than 340 hours of durability;
6) Performance and regeneration was demonstrated with catalyst coating directly on the CFR wall (without using the stainless steel liner).
Initial Shakedown Testing.
An initial shakedown test (
The disk agitator consisted of a disk-shaped stainless steel mesh attached to a perpendicular steel rod that runs axially inside the reactor. The agitator allows carbon to be lifted towards the vacuum port. It remains to be determined if the disk agitator would be required in a microgravity environment. In the next test (
Table 8; Test 31-042; 100-hour Testing.
The coating process developed during the Adhesion Testing was implemented in the beta-prototype. A hydroxide slurry containing 30% cornstarch by weight was down-selected for coating. A stainless steel sheet was coated to a loading of 5 mg/cm2. The sheet was loaded into the beta prototype reactor, purged with the standard CFR feed gas mixture and then reduced at 550° C. for 1 hour as usual. The reactor was then run for 130 hours at 475° C. GC injections were performed every 20 minutes. Carbon weight was determined at the end of the run. The run accumulated over 680 grams of solid carbon. The rate at which the carbon formed was well above the target rate. Furthermore, GC analysis over the 130 hour run, summarized in
Test 31-045; Spray Nozzle Regeneration.
In this test, a spray nozzle system was used for in-situ regeneration of the reactor. The steel liner from run 31-042 (
After the run, a vacuum tube was inserted through the carbon removal port. The activity for the test, 6.86 mg/cm2/hr was the highest obtained at this scale.
Test 31-057; Hot Spray Regeneration, Improved Agitator Design.
In the next test, two modifications were made to the reactor, seen well in
The first modification was the addition of a rotating arm agitator (400). Previously, the disk agitator was moved up-and-down to dislodge carbon from the walls; however, this resulted in carbon being trapped below the disk (this trapped carbon is the primary carbon that cannot be removed through the vacuum port). With the new agitator design, the disk remains fixed to the bottom of the reactor while a rotating arm (420) removes carbon from the wall. The arm (420) is connected to a shaft (410) that extends out of the reactor, where it is sealed to a port. The shaft can be lifted or spun while the reactor is hot. Consequently, the arm (420) can move up-and-down and/or rotate, while the disk remains fixed.
Table 8; Test 31-061; Humidification Testing.
In the next test, the reactor liner was again spray-regenerated, this time while at ˜100° C. wall temperature. Next, the CFR was run for over 100 hours with 10-mol % water added to the feed. Under these conditions the activity was below the target. For this test the water was injected through the inlet thermocouple port, thus no inlet temperature measurement could be obtained. It is possible that the poor activity can partially be blamed on a colder than typical inlet temperature, as the water could cool the gas ˜150° C. After testing, the agitator arm was rotated and moved up-and-down to dislodge carbon from the walls. Next, the reactor was vacuumed out through the vacuum port. With this approach, 95% of the carbon formed was removed through the vacuum port. The remaining carbon was removed via vacuum from the walls after the lid was taken off for inspection and spray regeneration. Carbon that fell below the disk was left in the reactor again.
Table 8; Test 31-061; Reactor Demonstration.
The improved agitator was used in a 50-hour test with a dry feed so the carbon removal process and spray regeneration could be demonstrated. The reactor was not agitated, by spinning and lifting the agitator arm, until after the run was complete. With this approach, 99% of the carbon was removed through the vacuum port. The additional carbon was removed from the reactor walls after the CFR was opened, but before it was spray-regenerated. Carbon that fell below the disk was left in the reactor again.
Table 8; Test 31-075; Humidification Testing.
Humidification of the CFR feed was improved by the addition of a heater to the gas inlet (as opposed to the direct injection of water approach used in test 31-061 (
Table 8; Test 31-081; Updated Conservative Composition for 144 Hours.
A long-term test was run using a composition based on integrated CFR-SOCE projections. The composition used was 41% CO, 18% H2, 33% CO2, 3% H2O, and 5% N2. This composition is also similar to the expected composition from a system that integrates with water electrolysis to hydrogen with a reverse water-gas-shift reactor as a means to generate carbon monoxide. As shown in
Table 8; Test 31-084; Conservative Composition, Higher Flow.
In the next test, the same gas composition as the previous test (
Table 8; Test 31-088; Ideal Composition.
In the final test with the beta-prototype, the integrated CFR-SOCE system stream composition was re-evaluated assuming more aggressive SOCE operation. The design subsection discusses the assumptions for that composition. By operating the SOCE under lower CO2 concentration, the CFR inlet composition would be 51% CO, 16% H2, 16% CO2, 7% H2O, and 10% N2. With this inlet composition for the CFR, activity exceeded target performance.
System Design Concepts
CFR Concept of Operation
The concept of operation for an automated 4-CM flight system was created. For a 4-CM flight system, four CFR's could be packaged in parallel, as shown in the top-down view of
Conceptual procedures, including valve switching, to operate the CFR during the various states are outlined below:
Start-up Operation (see
Based on test results with the 0.5 CM beta-prototype CFR, a third-generation (Gen3) CFR design capable of nearly complete automation was created. To minimize crew interaction, there are three main processes that needed to be automated: spray reinfiltration, carbon agitation, and carbon removal. The Gen3 reactor was designed to combine all of these actions into one simplified reactor. For spray reinifiltration, a spray nozzle sits in the middle of the reactor as seen in
Consumables
The largest replacement mass for the CFR is the catalyst and binder. Based on the concept of operation demonstrated in prototype testing, 790 g/CM/year of catalyst and binder will be consumed. With a density of 1.2 g/cc, this will store in 0.66 L/CM/year. Due to the powder nature of the catalyst, it can be stored in irregular shapes if a soft container is used.
The above disclosure provides examples of a CFR design with exceptionally low resupply mass and the ability to operate in an automated fashion. A number of variations to the design could be envisioned by on skilled in the art. Such variations could include, but are not limited to, the following:
1) Integration of the CFR with other various means of generating a reducing gas containing carbon, such as reverse water gas shift, Sabatier reactor, plasma reactor, pyrolysis reactor, or electrolysis;
2) Alternative methods for delivering catalyst into the reactor, such as dry catalyst particles, coated particles (i.e. beads, grains, or other high surface area shapes), coated reactor liners, or catalyst cartridges;
3) Alternative mechanical methods and designs for agitating the carbon so that it can be vacuumed and/or entrained in gas flow that carries it out of the reactor; and
4) Alternative catalyst compositions for formation of carbon, such as Fe, Co, Ni, Mn, Al, other transition metals, and mixtures thereof.
5) Alternative catalyst support materials that can withstand the operating conditions of the CFR 6) Alternative catalyst precursors such as metal nano-particles or materials that would decompose to catalytically active particles, such as various transition metal compounds including salts, organo-metallic compounds, oxides, hydroxides, metal alloys, carbides, and metal organic framework structures.
As used in this specification, a “transition metal compound” includes any compound that contains a transition metal, such as metal nitrates, metal acetates, metal oxides, metal hydroxides, elemental transition metals, metal carbides, metal hydrides, alloys, and mixtures thereof, while a transition metal is defined as one or more of the transitional metals as given in the Periodic Table and as well-known to one skilled in the art.
Further, the above disclosure provides examples of a CFR design for use in a spacecraft life-support system. The reactor design could also be used in a number of other applications, including:
1) Manufacturing of carbon nano-materials;
2) Oxygen recovery and/or sequestration of carbon in industrial and/or environmental applications;
3) Other life-support systems, including submarines.
What is claimed, then, includes a chemical composition bearing a mixture suitable for use in forming solid carbon from carbon-containing fluid in a non-oxidizing atmosphere. The composition further may include an organic binder; and a solid catalyst precursor component that includes a transition metal compound. In some embodiments, the transition metal compound may be selected from the group of compounds consisting of hydroxides, oxides, carbides, alloys, hydrides and mixtures thereof. In other embodiments, the transition metal component of the transition metal compound may be selected from the group of transition metals consisting of iron, cobalt, nickel, manganese, and mixtures thereof.
In other embodiments, the binder may be water soluble, and in others, the transition metal compound may equal to or more than 25-wt % of a solids mass of the composition, while in yet others, the transition metal compound may equal to or more than 10-wt % of a solids mass of the composition. The composition is an aqueous suspension.
Also claimed is a chemical reactor (10), seen well in
In further embodiments, the reactor (10) may include a valve system suitable for use in automated carbon removal from the reactor (10), a vacuum port (170) in fluid communication with the reaction chamber (105), and/or a spray nozzle (430) suitable for use in delivery of a catalyst coating into the reaction chamber (105). In yet other embodiments, wherein the reaction chamber (105) further comprises a filter media (210) suitable for use in retaining catalyst in the heated zone of the reaction chamber (105). In yet other embodiments, the reactor (10) further comprises a mechanical means for periodically loosening carbon from the filter media (210). In others, the reusable substrate further comprises a portion of a reaction chamber wall (110).
Together, the composition and the reactor (10) may be used in a method for producing carbon that includes the steps of; a) coating a substrate with a mixture comprising binder and a predetermined mass of catalyst precursor particles selected from the group of particles consisting of forms of iron, cobalt, nickel, manganese and mixtures thereof; b) heating the catalyst coated precursor; c) exposing the catalyst-coated precursor to a non-oxidizing fluid stream containing carbon, thereby; d) forming a mass of carbon equal to or greater than ten (10) times the mass of catalyst precursor; and e) separating the carbon from the substrate. Steps (b) through (e) may be repeated in a cyclic function.
In some embodiments, the substrate may be coated by spraying with at least one catalyst precursor. The catalyst precursor particles may include metal hydroxide particles, and the mixture may be an aqueous suspension
In other embodiments, the catalyst precursor particles further include transition metal compounds such that the transition metal compounds m equal to or greater than 25-wt % of a solid mass of the catalyst and binder; while in others, the catalyst precursor particles further comprise transition metal compounds such that the transition metal compounds may be equal to or greater than 10-wt % of a solid mass of the catalyst and binder.
In other embodiments of the method, the step of heating the catalyst-coated precursor may include a step of heating the catalyst-coated precursor to between about 350° C. and 650° C. In yet other embodiments, the step of forming a mass of carbon equal to or greater than ten (10) times the mass of catalyst precursor further comprises a step of forming a mass of carbon equal to or greater than one hundred (100) times the mass of the catalyst precursor.
In certain embodiment's, the step of separating the carbon from the substrate may include a step of using gas flow to separate the carbon from the substrate.
Numerous alterations, modifications, and variations of the preferred embodiments disclosed herein will be apparent to those skilled in the art and they are all anticipated and contemplated to be within the spirit and scope of the disclosed specification. For example, although specific embodiments have been described in detail, those with skill in the art will understand that the preceding embodiments and variations can be modified to incorporate various types of substitute and or additional or alternative materials, relative arrangement of elements, order of steps and additional steps, and dimensional configurations. Accordingly, even though only few variations of the method and products are described herein, it is to be understood that the practice of such additional modifications and variations and the equivalents thereof, are within the spirit and scope of the method and products as defined in the following claims. The corresponding structures, materials, acts, and equivalents of all means or step plus function elements in the claims below are intended to include any structure, material, or acts for performing the functions in combination with other claimed elements as specifically claimed.
This application claims the benefit of U.S. Provisional Patent Application 62/364,468 filed Jul. 20, 2016.
This invention was made with government support under National Aeronautics and Space Administration Contract Number NASA NNC15CA03C. The government may have certain rights in the invention.
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Number | Date | Country | |
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20180023200 A1 | Jan 2018 | US |
Number | Date | Country | |
---|---|---|---|
62364468 | Jul 2016 | US |