SUPPORTED PEROVSKITE-OXIDE COMPOSITES FOR ENHANCED LOW TEMPERATURE THERMOCHEMICAL CONVERSION OF C0 ₂ TO CO

CROSS-REFERENCE TO RELATED APPLICATION(S)

[0001] This application claims the benefit of and priority to U.S. Provisional Patent Application No. 62/512,475, filed on May 30, 2017 and U.S. Provisional Patent Application No. 62/672,999, filed on May 17, 2018, the contents of which are incorporated by reference herein in their entirety, and priority to which is hereby claimed.

STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT

[0002] This invention was made with government support under CBET1335817, IIP 1743623, CHE1531590 and EEC 1560303 awarded by the National Science Foundation. The government has certain rights in the invention.

TECHNICAL FIELD

[0003] The invention relates to a catalyst composite containing a perovskite-oxide and an oxide support, and the use thereof for C0 ₂ conversion by reverse water gas shift chemical looping (RWGS-CL) process.

BACKGROUND

[0004] Throughout preceding decades, global environmental concerns instigated a major shift of research focus and investment in renewable energy generation. However, the need for fossil fuels remains on the rise due to demand for transportation fuels and electricity, resulting in vast emissions of carbon dioxide, a major greenhouse gas. Efficient conversion of C0 ₂ to valuable hydrocarbons is crucial for energy security and a balanced carbon cycle.

[0005] Carbon capture and storage (CCS) is aimed at mitigating this C0 ₂ emission problem and promote carbon neutrality. However, annual emissions (-35 GT in 2015) continue to relentlessly outweigh the scale of reutilization (estimated -35 MT in early 2017). This scenario demands several processes that are capable of converting C0 ₂ to CO to valuable hydrocarbons. The extreme conditions required for natural C0 ₂ dissociation, over 2000°C in vacuum, underscore the need for catalytic reinforcements and more energy-efficient processes. Amongst the proposed techniques, solar thermochemical approach (STC), for instance, is particularly attractive. It presents the novelty of harvesting solar energy towards repurposing waste C0 ₂ emissions to hydrocarbons. Corresponding CO selectivity and C0 ₂ conversion rates are much higher than those of photocatalytic methodologies which struggle to achieve even 1 μιηοΐ g _C a _t ^_1 min ^"1 .

However, STC processes are typically accompanied by extreme operation temperatures (> 1000 °C), thereby limiting implementation due to a narrow range of stable materials.

[0006] A feasible alternative is reverse water gas shift chemical looping (RWGS-CL). RWGS- CL uses mixed metal oxides to convert C0 ₂ to CO at much lower temperatures (450 - 700 °C). However, development of an oxide material that is capable of balancing formation of numerous oxygen vacancies, kinetics for C0 ₂ activation and oxygen exchange, and lasting through numerous reaction cycles required for an industrial catalyst has been challenging. Therefore, there remains an unmet need for catalytic materials with structural stability and long-term activity of C0 ₂ conversion for industrial scale RWGS-CL processes.

SUMMARY

[0007] In an aspect, the disclosure relates to a catalyst composite comprising a perovskite-oxide of formula AB0 ₃ , wherein A is an alkaline earth element, a rare-earth element, an alkali metal element, a metal element, or a combination thereof, and B is a transitional metal element, metal element, or a combination thereof; and an oxide support having a formula different from the perovskite-oxide.

[0008] In another aspect, the disclosure relates to a method for forming a catalyst composite comprising mixing a perovskite-oxide of formula AB0 ₃ with an oxide support having a formula different from the perovskite-oxide to form a mixture, wherein A is an alkaline earth element, a rare-earth element, an alkali metal element, a metal element, or a combination thereof, B is a transitional metal element, a metal element, or a combination thereof; and heating the mixture to a temperature of between 600 °C and 1300 °C. In some embodiments, the perovskite-oxide used in the present preparation method has a cubic crystal structure, the O atoms being at the edge centers. In some embodiments of the disclosed preparation method, the perovskite-oxide adheres to the oxide support, and the oxide support induces strain in the crystal structure, causes surface reconstruction/termination, and/or regulates crystallite growth of active surfaces of the perovskite-oxide.

[0009] The disclosed perovskite-oxide may have a formula of AB0 ₃ In some embodiments, A is selected from the group consisting of Pb, Ca, Mg, Be, Sr, Ba, La, K, and Na or a combination thereof. In some embodiments, A has a formula of A^A^, wherein A ¹ and A ² are independently Pb, Ca, Mg, Be, Sr, Ba, La, K, or Na, x is 0-1, y is 0-1, and the sum of x and y is 1. In some embodiments, A has a formula of A ^x _x A ² _y and is Lao.75Sro.25· In some embodiments, B is selected from the group consisting of Fe, Ti, Y, Mn, Al, Cr, Co, Ta, Ni, and Ce, or a combination thereof. In some embodiments, the perovskite-oxide is Lao.75Sr _0.2 5Fe0 ₃ .

[0010] In some embodiments, the oxide support is Ce0 ₂ , Zr0 ₂ , A1 ₂ 0 ₃ , Si0 ₂ , Ti0 ₂ , or a combination thereof. In some embodiments, a weight ratio of the perovskite-oxide to the oxide support is from 10:90 to 90: 10.

[0011] In a further aspect, the disclosure relates to a method for converting C0 ₂ to CO comprising contacting H ₂ with the catalyst composite comprising a perovskite-oxide and an oxide support, whereby the perovskite-oxide is reduced, and whereby H ₂ is oxidized to produce H ₂ 0 and contacting C0 ₂ with the catalyst composite, whereby the reduced perovskite-oxide is oxidized, and whereby C0 ₂ is reduced to produce CO.

[0012] In some embodiments, the temperature of the method for converting C0 ₂ to CO is isothermal between 450 °C and 800 °C. In some embodiments, the perovskite-oxide reduction is at a different temperature than the perovskite-oxide oxidation. In some embodiments the perovskite-oxide reduction is between 400 °C and 850 °C. In some embodiments, the perovskite- oxide oxidation is between 450 °C and 900 °C.

[0013] In some embodiments, CO is produced by the disclosed method at a rate greater than a process using the perovskite-oxide without the oxide support. In some embodiments, CO is produced at a rate of 0.5 to 1 mmol CO/g perovskite-oxide/min.

[0014] In some embodiments, the disclosed method includes repeating the perovskite reduction and the perovskite oxidation in succession.

[0015] The disclosure provides for other aspects and embodiments that will be apparent in light of the following detailed description and accompanying figures.

BRIEF DESCRIPTION OF THE DRAWINGS

[0016] The features, objects and advantages other than those set forth above will become more readily apparent when consideration is given to the detailed description below. Such detailed description makes reference to the following drawings.

[0017] FIG. 1 shows the reverse water gas shift-chemical looping (RWGS-CL) process. [0018] FIG. 2A shows the X-ray diffraction patterns of fresh and post Temperature Programmed Oxidation (TPO) of C0 ₂ LSF ₂₅ /Si0 ₂ with constituents and closer inspection of 25-40 2Θ range to show the emergence of secondary phases.

[0019] FIG. 2B shows the X-ray diffraction patterns of fresh and post TPO-C0 ₂ LSF ₂₅ /SiC with constituents and closer inspection of the aforementioned range to show the absence of secondary phases.

[0020] FIG. 2C shows the X-ray diffraction patterns of LSF _x /Si0 ₂ (X = 25, 50, 75) in which each show a presence of secondary phases.

[0021] FIG. 2D shows the Fourier transform infrared spectra of LSF _x /Si0 ₂ (X = 25, 50, 75) in which each illustrate the consistent decrease in silica content at 1080 cm ^"1 with increasing LSF content.

[0022] FIG. 3 A shows the temperature-programmed experimental data for H ₂ 0. Temperature Programmed Reduction (TPR) spectra show 600 °C is an adequate temperature for partial reduction of the materials.

[0023] FIG. 3B the temperature-programmed experimental data for CO. TPO-C0 ₂ reveals the changes in CO production with each support and mass ratio.

[0024] FIG. 3C shows the temperature-programmed quantifications for H ₂ 0 and CO.

[0025] FIG. 4A shows the DFT calculations for Oxygen vacancy formation energies for each oxide species identified in the composite materials, δ represents the extent of oxygen vacancy formation. A value of 0.125 was chosen for consistent comparison.

[0026] FIG. 4B shows the variation of oxygen vacancy formation energy with lattice strain.

[0027] FIG. 5 shows RWGS-CL experiment results for LSF, LSF ₂₅ /Si0 ₂ , and LSF ₂₅ /SiC over eight cycles at 600 °C. The top graph shows H ₂ 0 production yields and peak rates. The bottom graph shows CO production yields and peak rates.

[0028] FIG. 6A shows a visual schematic of LSF particle size modification by supporting materials during RWGS-CL.

[0029] FIG. 6B shows a TEM image of LSF indicating particle size.

[0030] FIG. 6C shows a TEM image of LSF indicating interplanar spacing.

[0031] FIG. 6D shows a TEM image of Fresh LSF ₂₅ /Si0 ₂ interface.

[0032] FIG. 6E shows a TEM image of Fresh LSF ₂₅ /Si0 ₂ interplanar spacing. [0033] FIG. 6F shows a TEM image of LSF ₂₅ /Si0 ₂ after 8 RWGS-CL cycles illustrating a significant decrease in LSF particle size and formation of nanoparticles.

[0034] FIG. 6G shows a TEM image of LSF ₂₅ /Si0 ₂ after 8 RWGS-CL cycles illustrating a significant decrease in LSF particle size and formation of nanoparticles.

[0035] FIG. 6H shows a TEM image of LSF ₂₅ /Si0 ₂ after 8 RWGS-CL cycles illustrating a significant decrease in LSF particle size and formation of nanoparticles.

[0036] FIG. 7 shows the change in nonstoichiometric LSF mass over time with different particle sizes. The time required for vacancies to replenish decreases with particle size as calculated by Equation 1 (D = 2 x 10 ^"7 cm ² /s).

[0037] FIG. 8 shows the results from temperature-programmed reductions with H ₂ (left panel) and temperature-programmed oxidations with C0 ₂ for LSF and affiliated composites (right panel).

[0038] FIG. 9A shows diffraction patterns of LSF and a close inspection of identified secondary phases witnessed in fresh LSF ₂₅ /Si0 ₂ (red, top) and post TPO-C0 ₂ LSF ₂₅ /Ti0 ₂ (green, bottom).

[0039] FIG. 9B shows post heat treatment at 950 °C and post TPO-C0 ₂ diffraction patterns of LSF ₂₅ /Ce0 ₂ , demonstrating structural stability throughout material lifetime.

[0040] FIG. 9C shows post heat treatment at 950 °C and post TPO-C0 ₂ diffraction patterns of LSF ₂₅ /Zr0 ₂ , demonstrating structural stability throughout material lifetime.

[0041] FIG. 9D shows post heat treatment at 950 °C and post TPO-C0 ₂ diffraction patterns of LSF ₂₅ /A1 ₂ 0 ₃ (with corundum), demonstrating structural stability throughout material lifetime.

[0042] FIG. 9E shows post heat treatment at 950 °C and post TPO-C0 ₂ diffraction patterns of LSF ₂₅ /Si0 ₂ (with quartz), demonstrating structural stability throughout material lifetime.

[0043] FIG. 9F shows post heat treatment at 950 °C and post TPO-C0 ₂ diffraction patterns of LSF ₂₅ /Ti0 ₂ (with rutile), demonstrating structural stability throughout material lifetime.

[0044] FIG. 10 shows DFT-calculated oxygen vacancy formation energies of LSF, supporting materials, and detected secondary phases, δ represents the extent of oxygen nonstoichiometry for each support.

[0045] FIG. 11 A shows an SEM image of LSF ₂₅ /Ce0 ₂

[0046] FIG. 1 IB shows a TEM image of LSF ₂₅ /Ce0 ₂

[0047] FIG. l lC shows an SEM image of LSF ₂₅ /Zr0 _2.

[0048] FIG. 1 ID shows a TEM image of LSF ₂₅ /Zr0 ₂ [0049] FIG. HE shows an SEM image of LSF ₂₅ /AI ₂ O _3.

[0050] FIG. 11F shows an TEM image of LSF ₂₅ /A1 ₂ 0 ₃

[0051] FIG. 11G shows an SEM image of LSF ₂₅ /Si0 _2.

[0052] FIG. 11H shows a TEM image of LSF ₂₅ /Si0 ₂

[0053] FIG. I ll shows an SEM image of LSF ₂₅ /Ti0 _2.

[0054] FIG. 11 J shows a TEM image of LSF ₂₅ /Ti0 ₂

[0055] FIG. 12 shows the X-ray diffraction pattern for LSF post-TPR (10% v/v H ₂ in He up to 950 °C). Major diffraction lines are identified as La ₂ 0 ₃ (blue), Sr0 ₂ (green), Fe ₂ 0 ₃ (red), and FeO (dark red).

[0056] FIG. 13 shows the Rietveld refinement results for the LSF XRD pattern with a Rwp value of 3.7% and RBragg of 1.0%.

[0057] FIG. 14 shows the X-ray photoelectron spectrometry (XPS) spectra of LSF and all supported samples following 8 cycles of reverse water-gas shift chemical looping at 600 °C.

[0058] While the present invention is susceptible to various modifications and alternative forms, exemplary embodiments thereof are shown by way of example in the drawings and are herein described in detail. It should be understood, however, that the description of exemplary embodiments is not intended to limit the invention to the particular forms disclosed, but on the contrary, the intention is to cover all modifications, equivalents and alternatives falling within the spirit and scope of the invention as defined by the embodiments above and the claims below. Reference should therefore be made to the embodiments above and claims below for interpreting the scope of the invention.

[0059] The patent or application file contains at least one drawing executed in color. Copies of this patent or patent application publication with color drawing(s) will be provided by the Office upon request and payment of the necessary fee.

DETAILED DESCRIPTION

[0060] The present disclosure relates to a catalyst composite containing a perovskite-oxide and an oxide support, and the use of such catalyst composite for converting carbon dioxide (C0 ₂ ) to carbon monoxide (CO) in an industrial scale process. Various aspects of suitable perovskite- oxides and their uses as catalysts for the thermochemical conversion of C0 ₂ to CO are described in U.S. Patent Application Ser. No. 15/903,196 to Kuhn et al. ("PEROVSKITE-OXIDES FOR THERMOCHEMICAL CONVERSION OF CARBON DIOXIDE," filed February 23, 2018, Attorney Docket No. 292105-1520), which is herein incorporated by reference in its entirety.

[0061] In some aspects, the perovskite-oxide and the oxide support forms the disclosed composite catalyst inducing strain in the crystal structure of the perovskite-oxide and increasing the exposed surface area.

[0062] Surprisingly, the advantages of utilizing the composite catalyst in the disclosed method include the high rates of conversion of C0 ₂ to CO and increased long-term stability for repeated catalytic oxidation-reduction cycles, allowing this technique to be useful, for example, for providing a stable catalyst platform for industrial low temperature C0 ₂ thermochemical conversion. The increased stability of the composite catalyst allows repetitive cycles of the disclosed method, thereby generating large quantities of CO, which can be subsequently converted to hydrocarbons via Fischer-Tropsch synthesis.

1. Definitions

[0063] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art. In case of conflict, the present document, including definitions, will control. Preferred methods and materials are described below, although methods and materials similar or equivalent to those described herein can be used in practice or testing of the present invention. All publications, patent applications, patents and other references mentioned herein are incorporated by reference in their entirety. The materials, methods, and examples disclosed herein are illustrative only and not intended to be limiting.

[0064] The terms "comprise(s)," "include(s)," "having," "has," "can," "contain(s)," and variants thereof, as used herein, are intended to be open-ended transitional phrases, terms, or words that do not preclude the possibility of additional acts or structures. The singular forms "a," "an" and "the" include plural references unless the context clearly dictates otherwise. The present disclosure also contemplates other embodiments "comprising," "consisting of and "consisting essentially of," the embodiments or elements presented herein, whether explicitly set forth or not.

[0065] The modifier "about" used in connection with a quantity is inclusive of the stated value and has the meaning dictated by the context (for example, it includes at least the degree of error associated with the measurement of the particular quantity). The modifier "about" should also be considered as disclosing the range defined by the absolute values of the two endpoints. For example, the expression "from about 2 to about 4" also discloses the range "from 2 to 4." The term "about" may refer to plus or minus 10% of the indicated number. For example, "about 10%" may indicate a range of 9% to 11%, and "about 1" may mean from 0.9-1.1. Other meanings of "about" may be apparent from the context, such as rounding off, so, for example "about 1" may also mean from 0.5 to 1.4.

[0066] Definitions of specific functional groups and chemical terms are described in more detail below. For purposes of this disclosure, the chemical elements are identified in accordance with the Periodic Table of the Elements, CAS version, Handbook of Chemistry and Physics, 75 ^th Ed., inside cover, and specific functional groups are generally defined as described therein.

Additionally, general principles of organic chemistry, as well as specific functional moieties and reactivity, are described in Organic Chemistry, Thomas Sorrell, University Science Books, Sausalito, 1999; Smith and March March 's Advanced Organic Chemistry, 5 ^th Edition, John Wiley & Sons, Inc., New York, 2001; Larock, Comprehensive Organic Transformations, VCH Publishers, Inc., New York, 1989; Carruthers, Some Modern Methods of Organic Synthesis, 3 ^rd Edition, Cambridge University Press, Cambridge, 1987; the entire contents of each of which are incorporated herein by reference.

[0067] For the recitation of numeric ranges herein, each intervening number there between with the same degree of precision is explicitly contemplated. For example, for the range of 6-9, the numbers 7 and 8 are contemplated in addition to 6 and 9, and for the range 6.0-7.0, the number

6.0, 6.1, 6.2, 6.3, 6.4, 6.5, 6.6, 6.7, 6.8, 6.9, and 7.0 are explicitly contemplated.

[0068] An "active surface" is those surface terminations, or elements at the crystal surface facets, in the perovskite oxide that participate in the redox reactions during the RWGS-CL process.

[0069] An "alkali metal element" is a group of elements consisting of lithium (Li), sodium (Na), potassium (K), rubidium (Rb), cesium (Cs), and francium (Fr).

[0070] An "alkaline earth element" is one of the six chemical elements in group 2 of the periodic table including beryllium (Be), magnesium (Mg), calcium (Ca), strontium (Sr), barium (Ba), and radium (Ra).

[0071] "Catalyst" as used herein refers to a substance that increases the rate of a chemical reaction without itself undergoing any permanent chemical change. [0072] "Composite" as used herein refers to a material made from two or more constituent materials that, when combined, produce a material with different physical and/or chemical characteristics different from the individual starting materials.

[0073] The term "crystallite size" as used herein refers to the measurement that encompasses all the lattices in a repetitive structure, or repeating unit cells, until a defect occurs or the repetitive structure ends at the boundary of the crystal. In some embodiments, the crystallite size of the crystalline structures as disclosed herein is between 5 nm to 100 nm, such as between 10 nm and 90 nm, between 20 nm and 80 nm, between 30 nm and 70 nm, or between 40 nm and 60 nm.

[0074] A "metal element" includes any of the alkali metals, alkaline earth metals, transition metals, post-transition metals, lanthanides and actinide series of elements.

[0075] "Oxide support" as used herein refers to any conventional refractory oxide supports well known in the art. These include, for example, alumina, silica, magnesia, thoria, titania, zirconia, silica-aluminas, silica-zirconias, magnesia-aluminas and the like. Other suitable supports include the naturally occurring clays such as diatomaceous earth. The oxide support as used herein has a molecular formula different from the perovskite-oxide as disclosed herein.

[0076] "Perovskite" and "perovskite-oxide" as used interchangeably herein to refer

to compositions nominally designated as ABO ₃ , in which A is an alkaline earth element, a rare- earth element, an alkali metal element, a metal element or a combination thereof, and B is a transitional metal element, metal element, or a combination thereof. Representative elements for the A component include, but are not limited to, rare earth metal elements such as lanthanum, strontium, cerium, calcium, yttrium, erbium, praseodymium, neodymium, samarium, europium, silicon, magnesium, barium, niobium, lead, bismuth, and antimony or the like. Representative elements for the B component include, but are not limited to, transition metal elements such as iron, cobalt, manganese, copper, titanium, chromium, nickel, and molybdenum or the like. In some embodiments, A has a formula of A^A^, wherein x is 0-1, y is 0-1, and the sum of x and y is 1. In some embodiments, the A and B components of the perovskite-oxide as used herein are represented by A ¹ _x A ² _y B ¹ _w B ² _z , wherein x, y, w, and z are independently between 0-1 and the sum of x and y is 1 and the sum of w and z is 1. In some embodiments, the perovskite-oxide as used herein is represented by the formula A _a-X B _x MO _b , in which A is a mixture of elements originally in the form of single phase mixed lanthanides collected from bastnasite; B is a divalent or monovalent cation; M is at least one element selected from the group consisting of elements of an atomic number of from 22 to 30, 40 to 51, and 73 to 80; a is 1 or 2; b is 3 when a is 1 or b is 4 when a is 2; and x is a number defined by 0≤x<0.7.

[0077] A "rare earth element" is one of seventeen chemical elements including the fifteen lanthanides, cerium (Ce), dysprosium (Dy), erbium (Er), europium (Eu), gadolinium (Gd), holmium (Ho), lanthanum (La), lutetium (Lu), neodymium (Nd), praseodymium (Pr), promethium (Pm), samarium (Sm), terbium (Tb), thulium (Tm) and ytterbium (Yb), as well as scandium (Sc) and yttrium (Y).

[0078] "Surface termination" refers to the crystal surface facets of the perovskite oxide materials terminating in different elemental compositions, or alternatively, the surface facts are comprised of different elements. Based on reaction conditions or growth conditions, these surface terminations can relax, or change in bond distance, and often restructure themselves for better stability in a process called "surface reconstruction."

[0079] A "transition metal element" includes any element in groups 3-12 on the periodic table, as well as, the f-block lanthanide and actinide series.

2. Catalyst Composite Compositions

[0080] A first aspect of the invention provides a catalyst composition comprising a perovskite- oxide of formula AB0 ₃ , wherein A is an alkaline earth element, a rare-earth element, an alkali metal element, a metal element, or a combination thereof, and B is a transitional metal element, metal element, or a combination thereof and an oxide support having a formula different from the perovskite-oxide.

a) The perovskite-oxide

[0081] Perovskite-oxide generally refers to a structural class of mixed metal oxides, e.g.

ABO ₃ as defined herein, which are structurally analogous to the naturally occurring

mineral perovskite (CaTi0 ₃ ). In a representative perovskite-oxide structure, the cations possess the appropriate relative sizes and coordination properties to form a cubic crystalline structure in which the smaller B site cations occupy the corners of unit cubes and the larger A site cations occupy the centers of the cubes. Oxygen ions are located at lattice sites which provide octahedral coordinations with B ions and dodecahedral coordination with A ions. Strained or distorted cubic crystal structures can result from variations in the sizes of the metal ions as well as variations in the valence of the metal ions. [0082] Any thermodynamically stable perovskite-oxide capable of sustaining vacancies without deterioration may be suitable for the catalyst composite. In some embodiments, the perovskite- oxide has a formula of ABO3, in which A is an alkaline earth element, a rare-earth element, an alkali metal element, a metal element, or a combination thereof. In some embodiments, A is Pb, Ca, Mg, Be, Sr, Ba, La, K, or Na, or a combination thereof. In other embodiments, A has the formula of A ^l _x A ² _y , wherein A ¹ and A ² are independently Pb, Ca, Mg, Be, Sr, Ba, La, K, and Na, x is 0-1, y is 0-1, and the sum of x and y are 1. In some embodiments, x is about 0.2 to 0.8, 0.3 to 0.7, or 0.4 to 0.6. In some embodiments, y is about 0.2 to 0.8, 0.3 to 0.7, or 0.4 to 0.6. In certain embodiments, x is 0.75 and y is 0.25. In certain embodiments, A ¹ is La and A ² is Sr. In some embodiments, A has the formula of A ^x _x A ² _y and is Lao.75Sro.25.

[0083] In some embodiments, the perovskite-oxide has a formula of ABO3, in which B is a transitional metal element, metal element, or a combination thereof. In some embodiments, B is selected from the group consisting of Fe, Ti, Y, Mn, Al, Cr, Co, Ta, Ni, and Ce, or a combination thereof. In some embodiments, B is Fe.

[0084] In some embodiments, the perovskite-oxide has a formula of ABO3, in which A has a formula of A ^l _x A ² _y , wherein A ¹ is La, A ² is Sr, and B is Fe. In certain embodiments, the perovskite-oxide is Lao _. 75Sr _0.2 5Fe0 ₃ .

[0085] In certain embodiments, the perovskite-oxide has a formula of Α ¹ Β ¹ _γ Β ² _(ΐ . _Υ) 0 ₃ , in which y is 0.1 to 0.9, including 0.2 to 0.8, 0.3 to 0.7, or 0.4 to 0.6. In certain embodiments, the perovskite-oxide has a formula of A ¹ _x A ² (i _-X )B ¹ _y B ² (i _-y )0 ₃ , in which x is 0.1 to 0.9, including 0.2 to 0.8, 0.3 to 0.7, or 0.4 to 0.6; and y is 0.1 to 0.9, including 0.2 to 0.8, 0.3 to 0.7, or 0.4 to 0.6.

[0086] In some embodiments, the perovskite-oxide has a cubic crystal structure wherein the oxygen atoms are at the edge centers,

b) The oxide support

[0087] Oxide supports may be any conventional refractory oxide supports. These include, for example, alumina, silica, magnesia, thoria, titania, zirconia, silica-aluminas, silica-zirconias, magnesia-aluminas and the like. Other suitable supports include the naturally occurring clays such as diatomaceous earth. In some embodiments, the oxide support as used herein may include M ² , which is a non-oxygen element, such as silica, zirconium, aluminum, titanium, or cerium.

[0088] In some embodiments, the oxide support is Ce0 ₂ , Zr0 ₂ , A1 ₂ 0 ₃ , Si0 _2, Ti0 ₂ , or a combination thereof. In other embodiments, the oxide support is Ce0 ₂ , Zr0 ₂ , or Si0 ₂ . In certain embodiments, the oxide support is Si0 ₂ . Suitable Si0 ₂ materials include various forms of Si0 ₂ known in the art (for example, SBA-15, which is a mesoporous form of Si0 ₂ ).

[0089] In some embodiments, the weight ratio of the perovskite-oxide to the oxide support is from 10:90 to 90: 10. The weight ratio of the perovskite-oxide to the oxide support may be 10:90, 20:80, 30:70, 40:60, 50:50, 60:40, 70:30, 80:20 or 90: 10. The weight ratio of the perovskite-oxide to the oxide support may be 25:75, 35:65, 45:55, 55:45, 65:35 or 75:25. In certain embodiments, the weight ratio of the perovskite-oxide to the oxide support is 25:75.

[0090] Upon forming a composite as disclosed herein, the oxide support may affect the physical crystal structure of the perovskite-oxide. In some embodiments, the oxide support induces strain in the crystal structure. In some embodiments, the oxide support may cause surface

reconstruction and/or termination in the crystal structure of the perovskite-oxide. In some embodiments, the oxide support may regulate crystallite growth of active surfaces of the perovskite-oxide. The effects of surface reconstruction and/or termination, as well as regulation of crystallite growth of active surfaces, may be demonstrated by analytical methods known in the art, including for example XPS, XRD, and surface areas measurements.

c) The catalyst composite

[0091] Industrial-scale pellets are often shaped as spheres, cylinders, Raschig rings and other common variations with an extruded substrate serving as a catalyst support. The true potential of the use of a perovskite-oxide catalyst remains unrecognized due to a considerable lack of specific surface area.

[0092] In some embodiments, the surface area of the perovskite-oxide of the disclosed catalyst composite is between 1 and 1000 m ² /g. The surface area of the perovskite-oxides may be between 1 and 2 m ² /g, 1 and 5 m ² /g, 1 and 10 m ² /g, 1 and 100 m ² /g, 1 and 500 m ² /g, 1 and 750 m ² /g, 10 and 100 m ² /g, 10 and 500 m ² /g, 10 and 1000 m ² /g, 50 and 100 m ² /g, 50 and 500 m ² /g, 50 and 1000 m ² /g, 100 and 500 m ² /g, 100 and 100 m ² /g or 500 and 1000 m ² /g.

[0093] In some embodiments, the oxide support increases the surface area of the perovskite- oxide upon forming the disclosed catalyst composite. In some embodiments, the oxide support does not affect the surface area of the perovskite-oxide upon forming the disclosed catalyst composite.

[0094] In some embodiments, the oxide support increases the cell volume of the perovskite- oxide upon forming the disclosed catalyst composite. In some embodiments, the increased cell volume is due to increased strain in the perovskite structure. For example, as shown in Table 5, the oxide support (such as Ce0 ₂ , Zr0 ₂ , A1 ₂ 0 ₃ , Si0 ₂ or Ti0 ₂ ) may enlarge the cell volume of the perovskite-oxide (such as LSF) as measured by the geometrical characteristics of the (020) diffraction line.

[0095] The size of the crystal structure can be measured as a lattice parameter or a crystallite size. A lattice parameter is the spacing of individual atoms comprising a repeating unit of the crystal. Crystallite size is a measurement that encompasses all the lattices in a repetitive structure, or repeating unit cells, until a defect or boundary ends the crystal. In some

embodiments, the perovskite-oxide of the disclosed catalyst composite has a crystallite size of between 5 and 100 nm, including, but not limited to, between 5 and 10 nm, between 5 and 20 nm, between 5 and 30 nm, between 5 and 40 nm, between 5 and 50 nm, between 5 and 60 nm, between 5 and 70 nm, between 5 and 80 nm, between 5 and 90 nm, between 10 and 100 nm, between 20 and 100 nm, between 30 and 100 nm, between 40 and 100 nm, between 50 and 100 nm, between 60 and 100 nm, between 70 and 100 nm, between 80 and 100 nm, between 90 and 100 nm, between 10 and 90 nm, between 20 and 80 nm, between 30 and 70 nm, and between 40 and 60 nm.

3. Methods of Preparing the Catalyst Composite Compositions

[0096] Another aspect of the invention provides a method for preparing a catalyst composite comprising (a) mixing a perovskite-oxide of formula AB0 ₃ with an oxide support having a formula different from the perovskite-oxide to form a mixture, wherein A is an alkaline earth element, a rare-earth element, an alkali metal element, a metal element, or a combination thereof, B is a transitional metal element, a metal element, or a combination thereof; and (b) heating the mixture to a temperature of 600 °C to 1300 °C. In some embodiments, the perovskite-oxide of step (a) has a cubic crystal structure, the O atoms being at the edge centers. In some

embodiments, the perovskite-oxide adheres to the oxide support in step (b), and the oxide support induces strain in the crystal structure, causes surface reconstruction/termination, and/or regulates crystallite growth of active surfaces of the perovskite-oxide in step (b).

[0097] In some embodiments, disclosed is a method for preparing a catalyst composite comprising: (a) mixing a perovskite-oxide of formula AB0 ₃ with an oxide support having a formula different from the perovskite-oxide to form a mixture, wherein A is an alkaline earth element, a rare-earth element, an alkali metal element, a metal element, or a combination thereof, B is a transitional metal element, a metal element, or a combination thereof, and wherein the perovskite-oxide has a cubic crystal structure, the O atoms being at the edge centers; and (b) heating the mixture to a temperature of 600 °C to 1300 °C, whereby the perovskite-oxide adheres to the oxide support, and the oxide support induces strain in the crystal structure, causes surface reconstruction/termination, and/or regulates crystallite growth of active surfaces of the perovskite-oxide.

[0098] In some embodiments, the perovskite-oxide used in the disclosed method has a formula of ABO3, in which A is Pb, Ca, Mg, Be, Sr, Ba, La, K, or Na, or a combination thereof. In other embodiments, A has the formula of A ^l _x A ² _y , wherein A ¹ and A ² are independently Pb, Ca, Mg, Be, Sr, Ba, La, K, and Na, x is 0-1, y is 0-1, and the sum of x and y are 1. In some embodiments, A is A ^l _x A ² _y , in which x is 0.1-0.9, such as 0.2 to 0.8, 0.3 to 0.7, or 0.4 to 0.6. In some

embodiments, y is 0.1 to 0.9, such as 0.2 to 0.8, 0.3 to 0.7, or 0.4 to 0.6. In certain embodiments, A is A^A^, in which x is 0.75 and y is 0.25. In certain embodiments, A is A ^l _x A ² _y , in which A ¹ is La and A ² is Sr. In some embodiments, A has the formula of A ^x _x A ² y and is Lao.75Sro.25·

[0099] In some embodiments, the perovskite-oxide used in the disclosed method has a formula of ABO3, in which B is selected from the group consisting of Fe, Ti, Y, Mn, Al, Cr, Co, Ta, Ni, and Ce, or a combination thereof. In some embodiments, B is Fe.

[00100] In some embodiments, the perovskite-oxide used in the disclosed method has a formula of ABO3, in which A is A ^l _x A ² _y , A ¹ is La, A ² is Sr, and B is Fe. In certain embodiments, the perovskite-oxide is

[00101] The disclosed perovskite-oxides can be made by any method know in the art, including, for example, a modified Pechini method, a sol gel method, precipitation, a hydrothermal method or a solid state method. In some embodiments, the perovskite-oxide is calcined before mixing with the oxide support.

[00102] In some embodiments, the oxide support is Ce0 ₂ , Zr0 ₂ , AI2O3, Si0 ₂ , Ti0 ₂ , or combinations thereof. In other embodiments, the oxide support is Ce0 ₂ , Zr0 ₂ or Si0 ₂ . In certain embodiments, the oxide support is Si0 ₂ .

[00103] In some embodiments, the weight ratio of the perovskite-oxide to the oxide support is from 10:90 to 90: 10. The weight ratio of the perovskite-oxide to the oxide support may be 10:90, 20:80, 30:70, 40:60, 50:50, 60:40, 70:30, 80:20 or 90: 10. The weight ratio of the perovskite-oxide to the oxide support may be 25:75, 35:65, 45:55, 55:45, 65:35 or 75:25. In certain embodiments, the weight ratio of the perovskite-oxide to the oxide support is 25:75.

[00104] Any mixing methods known in the art may be used to combine the perovskite- oxide with the oxide support. In some embodiments, the mixing may be accomplished by grinding, ball milling, drum tumbling, or solution based methods.

[00105] The mixture may be heated to a temperature of 600 °C to 1300 °C as needed to ensure that the perovskite-oxide adheres to the oxide support. In some embodiments the mixture is heated to a temperature of about 600 °C, about 650 °C, about 700 °C, about 750 °C, about 800 °C, about 850 °C, about 900 °C, about 950 °C, about 1000 °C, about 1050 °C, about 1100 °C, about 1150 °C, about 1200 °C, about 1250 °C, or about 1300 °C.

[00106] The mixture of the oxide support and perovskite-oxide disclosed herein may lead to the spontaneous formation of one or more secondary phases at elevated temperatures. These secondary phases may be the result of the conversion of the perovskite-oxide into a non- stoichiometric form. In some embodiments, heating the mixture causes the formation of secondary phases due to solid state reactions between the perovskite-oxide and the oxide support. In some embodiments, the secondary phases are of formula of M ¹ _p M ² _q O _v , wherein M ¹ is A or B component of the disclosed perovskite-oxide (having a formula of AB0 ₃ ), M ² is the non-oxygen element of the oxide support, p is 1-3, q is 1-3, and v is 2-7.

[00107] In general, M ¹ in the secondary phases is the A or B element of the perovskite- oxide used herein to form the composite catalyst. In some embodiments, M ¹ is A, which is selected from group consisting of Pb, Ca, Mg, Be, Sr, Ba, La, K, and Na. In some embodiments, M ¹ is B, which is from group consisting of Fe, Ti, Y, Mn, Al, Cr, Co, Ta, Ni and Ce.

[00108] In general, M ² in the secondary phases is a non-oxygen element of the oxide support used herein to form the composite catalyst. In some embodiments, M ² is Ce, Zr, Al, Si _; or Ti. In certain embodiments, the secondary phases are FeSi0 ₃ and La ₂ Si0 ₅ .

[00109] The secondary phases may be produced in minor to trace amounts in comparison to the stoichiometric form of the perovskite-oxide. In some embodiments, the secondary phases comprise less than 2% by weight of the catalyst composite. In some embodiments, the secondary phases comprise less than 1.5% by weight of the catalyst composite. In some embodiments, the secondary phases comprise less than 1% by weight of the catalyst composite. In some embodiments, the secondary phases comprise less than 0.5% by weight of the catalyst composite. In some embodiments, the secondary phases comprise between 0.5 and 1% by weight of the catalyst composite.

[00110] In some embodiments, the perovskite-oxide catalyst is LSF ₂₅ , the oxide support is Si0 ₂ , and the catalyst composite is characterized by an X-ray diffraction pattern shown in FIG. 2A. In some embodiments, the perovskite-oxide catalyst is LSF _X (X is 25, 50, or 75), the oxide support is Si0 ₂ , and the catalyst composite is characterized by the corresponding X-ray diffraction patterns shown in FIG. 2C. In some embodiments, the perovskite-oxide catalyst is LSF ₂₅ , the oxide support is Ce0 ₂ , Zr0 ₂ , A1 ₂ 0 ₃ or Ti0 ₂ and the catalyst composite is

characterized by an X-ray diffraction pattern shown in FIG. 9B, FIG. 9C, FIG. 9D, or FIG. 9E, respectively.

4. Methods of Use

[00111] Another aspect of the invention provides a method for converting C0 ₂ to CO comprising (a) contacting H ₂ with the catalyst composite of claim 1, whereby the perovskite- oxide is reduced, and whereby H ₂ is oxidized to produce H ₂ 0 and (b) contacting C0 ₂ with the catalyst composite, whereby the reduced perovskite-oxide is oxidized, and whereby C0 ₂ is reduced to produce CO.

[00112] Without being limited by any theory, the reverse water gas shift chemical looping

(RWGS-CL) process as disclosed herein may include a two-step process that simultaneously reduces net C0 ₂ emissions and provides a pathway for renewable hydrocarbon production from synthesis gas. As described herein and shown in FIG. 1, mixed metal oxides such as perovskite- oxides (ABO3) may be used for generation of 100% selective CO from C0 ₂ . The first step may result in the partial reduction of perovskite-oxides to their oxygen deficient forms (ΑΒ0 _3-δ ) under exposure to hydrogen. The second step is the platform for converting C0 ₂ to CO over these oxygen vacant perovskites, allowing the oxides to regain their original stoichiometric forms (AB0 ₃ ). This cyclic operation converts C0 ₂ to CO, which can be subsequently converted to hydrocarbons via Fischer- Tropsch synthesis.

[00113] In some embodiments, the method for converting C0 ₂ to CO is carried out isothermally at a temperature between 450 °C and 800 °C, including, but not limited to, between 500 °C and 800 °C, between 550 °C and 800 °C, between 600 °C and 800 °C, between 650 °C and 800 °C, between 700 °C and 800 °C, between 750 °C and 800 °C, between 450 °C and 500 °C, between 450 °C and 550 °C, between 450 °C and 600 °C, between 450 °C and 650 °C, between 450 °C and 700 °C, between 450 °C and 750 °C, between 500 °C and 550°C, between 500 °C and 600 °C, between 500 °C and 650 °C, between 500 °C and 700 °C, between 500 °C and 750 °C, between 550 °C and 600 °C, between 550 °C and 650 °C, between 550 °C and 700 °C, between 550 °C and 750 °C, between 600 °C and 650 °C, between 600 °C and 700 °C, between 600 °C and 750 °C, between 650 °C and 700 °C, between 650 °C and 750 °C, and between 700°C and 750 °C. In certain embodiments, the disclosed method of converting C0 ₂ to CO is carried out isothermally at a temperature of between 500 °C and 700 °C, such as between 550 °C and 650 °C, and between 580 °C and 620 °C. In certain embodiments, the disclosed method of converting C0 ₂ to CO is carried out isothermally at 600 °C.

[00114] In some embodiments, the method for converting C0 ₂ to CO is carried out at two different temperatures, one temperature for step (a) and one temperature for step (b).

[00115] In some embodiments, the temperature of step (a) is between 400 °C and 850 °C. The temperature of step (a) may be about 400 °C, about 450 °C, about 500 °C, about 550 °C, about 600 °C, about 650 °C, about 700 °C, about 750 °C, about 800 °C or about 850 °C.

[00116] In some embodiments, the temperature of step (b) is between 450 °C and 900 °C. The temperature of step (a) may be about 450 °C, about 500 °C, about 550 °C, about 600 °C, about 650 °C, about 700 °C, about 750 °C, about 800 °C, about 850 °C or about 900 °C.

[00117] Oxygen vacancy formation energies (Ev _ac ) serve as descriptors for the ability of an oxide material to convert C0 ₂ . In some embodiments, the oxygen vacancy formation energy for the supporting materials in the disclosed catalyst composite may have a value of at least 4 eV, such as a value between 4 eV and 8 eV, as calculated at δ=0.125 (δ represents the extent of oxygen vacancy formation), as shown in FIG. 10. In some embodiments, the oxygen vacancy formation energy for the perovskite oxide in the disclosed catalyst composite may have a value of at less than 4 eV, such as a value between 2 eV and 4 eV, as calculated at 5=0.125, as shown in FIG. 4B.

[00118] In some embodiments, the CO is produced at a rate of 0.5 to 1 mmol CO/g perovskite-oxide/min. the CO may be produced at a rate of about 0.5 mmol CO/g perovskite- oxide/min, about 0.6 mmol CO/g perovskite-oxide/min, about 0.7 mmol CO/g perovskite- oxide/min, about 0.8 mmol CO/g perovskite-oxide/min, about 0.9 mmol CO/g perovskite- oxide/min or about 1 mmol CO/g perovskite-oxide/min. [00119] In some embodiments, CO is produced at a rate greater using the process with the catalyst composite than the process using a perovskite-oxide without the oxide support. In some embodiments, there is up to a 200% increase in CO production. In some embodiments, there is up to a 150%) increase in CO production. In some embodiments, there is up to a 100% increase in CO production. In some embodiments, there is up to a 50% increase in CO production.

[00120] In some embodiments, step (a) and step (b) are repeated in succession. Step (a) and step (b) may be repeated in succession as many times as needed until a certain quantity of CO is produced. Step (a) and step (b) may be repeated at least 5 times in succession, at least 10 times in succession, at least 20 times in succession, at least 25 times in succession, at least 30 times in succession, at least 40 times in succession, at least 50 times in succession

[00121] In some embodiments, the process further reduces the perovskite-oxide surface area. The perovskite-oxide surface area may be reduced by up to 25%. The perovskite-oxide surface area may be reduced by up to 20%. The perovskite-oxide surface area may be reduced by up to 15%). The perovskite-oxide surface area may be reduced by up to 10%>. The perovskite- oxide surface area may be reduced by up to 5%.

[00122] In some embodiments, the process further comprises wetting of the catalyst composite.

5. Examples

[00123] Example 1. Materials & Methods

[00124] Material Synthesis: A sol gel-based Pechini method was used to synthesize the Lao _. 75Sr _0.2 5Fe03 (LSF) perovskite-oxide similar to that proposed by Popa and Kakihana (Solid State Ionics 2002, 151, 251-257). Using citric acid (CA) (Aldrich >99.5%) as a chelating agent, a 2 M aqueous solution was made with deionized water. Metal precursors La(N0 ₃ ) ₃ (Aldrich 99.9%), SrC0 ₃ (Aesar 99.994%), and Fe(N0 ₃ ) ₃ (Aldrich ACS grade +98%) were each dissolved into the CA solution followed by 2 hr of stirring (200 rpm) at 60°C to minimize mixture variations. Ethylene glycol (EG) (Aldrich >99%) was then added to induce polyesterification as the solution was stirred for 7 hr at 90°C. All reagents were measured to achieve a

La:Sr:Fe:CA:EG molar ratio of 0.75 :0.25 : 1.0: 10:40. The resulting dark red viscous gel was immediately charred at 450°C (25°C/min) for 2 hr. The solidified residue was crushed into powder and further calcined in air at 950°C (25°C/min) for 6 hr to finalize the crystallization of LSF. The perovskite was then combined with silica (quartz, Sigma-Aldrich purum) to obtain a composite material of mass ratios 25%, 50%, and 75% LSF. In some cases, the resulting catalyst was then combined with Ce0 ₂ , Zr0 ₂ , A1 ₂ 0 ₃ (Sigma-Aldrich puriss corundum), Si0 ₂ (Sigma- Aldrich purum quartz) and Ti0 ₂ (Alfa Aesar 99.5% rutile) at 25 % by mass. Black silicon carbide 70 grit (Panadyne Abrasives) was also included as a support but was first subjected to thermal pretreatment at 1000°C for 2 hr to achieve crystalline phases that would remain stable throughout high-temperature TPO-C0 ₂ experiments. LSF and the respective materials (X% w/w LSF/support) were grinded together by hand in a mortar and pestle for about 15 min and then heated in air at 950°C for 10 hr to achieve aggregation of constituents and to ensure strong adhesion of the perovskite phase to the support particles. Ce0 ₂ and Zr0 ₂ in particular were acquired by thermolysis of Ce(N0 ₃ ) ₃ (Alfa Aesar 99.5%) and ZrO(N0 ₃ ) ₂ respectively at 600 °C.

[00125] Temperature-programmed experiments: About 75 mg of each sample was positioned between glass wool within a quartz U-tube. The quartz reactor was then placed within a Thermo Scientific furnace in which the heating ramp was held constant at 10°C/min for all temperature-programmed experiments. The total flow rate was maintained at 50 seem using Alicat mass flow controllers and consisted of ultra-high purity (UUP) grade gases supplied by Airgas. A MKS Cirrus mass spectrometer (MS) was used to monitor changes in gas flow composition over time. For temperature-programmed reductions (TPR), gas signals were permitted to stabilize at ambient temperature once the initial flow was adjusted to 10% H ₂ in Helium (He) (v/v). The temperature was then increased to 950°C (10 °C/min) and held constant until the m/z = 18 signal, representing H ₂ 0, was steady. The TPR profiles revealed a generalized peak reduction temperature for the material set. For temperature-programmed oxidations (TPO- C0 ₂ ), each sample was heated under 10% H ₂ in He (v/v) flow at 600 °C for 30 min. The oxygen- deficient perovskite material was allowed to cool naturally under He to about 100°C to maintain vacancies. The material was then exposed to a 10% C0 ₂ in He (v/v) flow and heated to 950°C (10 °C/min) and CO generation was represented by peak formation in the m/z = 28 signal.

Quantitative analysis of the resulting data followed procedures previously described.

[00126] Structural Characterization: X-ray diffraction was used to probe fresh and post- experimental samples. Main interests included changes in crystalline structure or secondary phases concomitant with solid-state reactions. A Bruker X-Ray Diffractometer with Cu Κα (λ = 0.154 nm) provided patterns at ambient conditions from 20 to 80° (2Θ°) with a step size of 0.0102 (2Θ°) and 1.2 seconds per step. Raw data and literature patterns from X'Pert Highscore Plus software were juxtaposed for reference when calculating lattice parameters and LSF

orthorhombic cell dimensions in pre-calcination, post-calcination and post-experiment samples. This assay consisted of indexing using Bragg' s Law and unique geometrical and interplanar distance equations. Library reference codes are provided when necessary. A Scherrer analysis was also done with a shape factor of 0.9, an acceptable approximation, across the width of the primary LSF (020) diffraction line, given the assumption of spherical perovskite particles. This permitted the comparison of crystalline sizes and surface areas of supported and unsupported LSF and the estimation of the change in LSF crystallite size throughout the material lifetime.

[00127] Rietveld refinement using Topas 5 software was performed on the LSF control sample diffraction pattern to ensure the accuracy of the raw data and numerical calculations with atomic coordinates provided by Dann et al. (J. Solid State Chem. 1994). A PV peak type was chosen in Topas 5 software. The profile shape functions for the full width half maximum (FWHM) and PV mixing parameter (η) are shown as Equations SI and S2 respectively. They consist of refinable FWHM parameters (a^ bh, ¾) and Lorentzian mix parameters (ai _or , bi _or , ci _or )

■ £ i ia^C^ ^'^ζ,, (Ml)

[00128] FTIR spectroscopy (attenuated total reflectance (ATR)) was performed on all the perovskite-support samples in the Nicolet IS50 instrument from Thermo-Scientific. All the spectra comprised of 50 scans, taken at a resolution of 0.241 cm ^"1 having a data spacing of 0.482 cm ^"1 .

[00129] X-ray photoelectron spectrometry (XPS) data was acquired with a Thermo

Scientific K- Alpha spectrometer. The instrument utilized Ka radiation and a dwell time of 0.5 s. The Cls peak was identified at 285.18 eV.

[00130] Microscopy: A Tecnai F20 transmission electron microscope (TEM) was used for high resolution imaging of LSF particle development after composite synthesis and reaction testing. A Schottky Field emitter sufficed as the electron source with minimal energy spread (< 0.7 eV) and a point resolution of 0.24 nm. With a line resolution of 0.102 nm, the (020) plane of LSF was probed to calculate the interplanar spacing which remained consistent with crystallographic data.

[00131] A Field Emission Scanning electron microscope (SEM), accompanied with energy-dispersive spectroscopy (EDS), was used for precise imaging and elemental analysis of the post-calcination and post-experiment perovskite phases. The Hitachi S800 SEM with EDS attachment was operated with 2 nm resolution at a working distance of 5 mm.

[00132] Physisorption: Specific surface areas were obtained using Quantachrome

Autosorb IQ analyzer. After degassing at 300 °C. Adsorption-desorption isotherms were obtained by measuring volume adsorbed by the sample at a set interval of partial pressures (P/Po) using N ₂ as the adsorbate at 77 K. Specific surface area was calculated using Brunauer-Emmet- Teller (BET) method using adsorption data points inside the P/Po range of 0.05 to 0.3.

[00133] Chemical Looping: LSF25/S1O2, LSF25/S1C, and unsupported LSF were each tested in eight consecutive isothermal cycles of reverse water gas shift chemical looping

(RWGS-CL). Maintaining a total flow rate of 50 seem throughout the entire experiment, the process began with a 20 min period of 10% H ₂ in He (v/v) to reduce the perovskite, thus instigating oxygen vacancy formation. Helium was flowed again for 20 min before changing the flow to 10%) C0 ₂ in He (v/v) to re-oxidize the perovskite material and generate CO. H ₂ 0 and CO production was quantified for each cycle using the same procedures for TPO-C0 ₂ to test reaction capability and durability over elongated use.

[00134] Density-Functional Theory (DFT): All the DFT calculations were performed using plane wave basis sets and GGA electron densities using VASP - 5.3.3. Projected augmented wave (PAW) potentials were used for treating the core electronic densities. Perdew- Burke-Ernzerhof (PBE) exchange correlation was used. For the study of LSF, a 2><2><2 supercell of 40 atoms (consisting 'n' = 8 unit cells) was used. And hence creating an oxygen vacancy extent (δ) of 0.125 involved removing only one oxygen atom. An average of oxygen vacancy formation energies over different perovskite locations has been reported. The crystal structures of these materials were based on the experimental results as obtained from XRD patterns. The atomic distribution within the crystal lattice was based on the minimum energy configuration as per DFT-calculations. A 4x4x4 k-point mesh having Monkhorst Pack grid was generated and was used throughout all calculations over LSF. For other materials like silica, FeSi0 ₃ and La ₂ Si0 ₅ , k-points were set so as to maintain to similar k-point grid spacing. Throughout the calculations, an energy cut off (ENCUT) value of 600 eV was used. In regards to oxygen vacancy formation energy calculations, oxygen over-binding has been accounted for as well. The heat of formation (¾) of the perovskite-oxide was calculated as per the equation

M _j * ⁸⁸⁵ — ¾ ¾, where ELSF IS LSF' S calculated total energy from DFT and μι is the ground state fitted elemental reference energy for each of La, Sr, Fe and O. The oxygen vacancy formation energies were calculated as per the equation jg^,— $X ^— where, is the total energy of the stoichiometric materials (LSF and the metal oxides), n is the number of unit cells in a one supercell, while ¾ _S ~ is that of the oxygen vacant material and ¾ _g is the molecular energy of oxygen. The correction factor for oxygen over-binding error (for PBE functionals) by Wang et al. (Wang, L.; Maxisch, T.; Ceder, G. Oxidation energies of transition metal oxides within the GGA + U framework. Phys. Rev. B, 2006, 73, 195107) was considered as well.

[00135] Example 2. Structural Characterization

[00136] Table 1 consists of each sample synthesized, characterized, and tested with its respective nomenclature. X-ray diffraction (XRD) patterns of Lao _. 75Sro _.2 5Fe03 (LSF) and Si0 ₂ along with that of the LSF ₂₅ /Si0 ₂ amalgam (25% by weight of LSF) are reported in FIG. 2A. The composite sample indicated the dominant presence of pure phase silica (hexagonal quartz [Ref. Code: 00-046- 1045]) and LSF phases (orthorhombic structure [Ref. Code: 00-035-1480]). Closer inspection of the 25-40 20° (FIG. 2A) range revealed formation of secondary phases FeSiC"3 and La ₂ Si0 ₅ in minor amounts. These became more prominent after H ₂ -reduction and subsequent temperature-programmed oxidation under C0 ₂ (TPO-C0 ₂ ) experiments. The LSF- Si0 ₂ interface region of the composite material was the most vulnerable to solid state reactions. Yet FeSiC"3 and La ₂ Si0 ₅ were present as traces and exhibited no adverse effects on the long-term stability of the composite. SiC was used as non-oxygen based reference support to test the effect of Si on stability, secondary phase formation, and C0 ₂ conversion performance of perovskite:SiC mixtures. The diffraction pattern of the SiC-based amalgam illustrated an absence of any secondary phases, even after H ₂ -reduction and subsequent TPO-C0 ₂ , as evident from FIG. 2B and FIG. 2C. Table 1: Sample nomenclature for perovskite composites synthesized and tested in temperature programmed experiments.

c Quartz SSA (after heat treatment at 950 °C): 1.7 m ² g ^'1

[00137] The presence of secondary phases (FeSi0 ₃ and La ₂ Si0 ₅ ) in the LSF/Si0 ₂ composites can be consequential to perovskite grain characteristics and C0 ₂ conversion performance. Therefore, different ratios of LSF and Si0 ₂ were tested, resulting in varying concentrations of these phases evident from the relative peak intensities (R.I) at 28.0, 30.6, and 35.5 20° (FIG. 2D). The R.I. of the primary diffraction pattern affiliated with orthorhombic FeSi0 ₃ (Ref. Code: 01-076-0886) changed from 1.35% to 1.74% to 0.71% with increasing LSF content (25% to 75%) as indicated in Table 1. The (-202) XRD peak of monoclinic La ₂ Si0 ₅ (Ref. Code: 00-040-0234) however, remained relatively constant between 0.76% and 0.50% possibly due to high activation energies for La ion migration in perovskites with short O-Fe-0 and 0-0 distances in the lattice. Silica phase transition from quartz to tridymite, a typically lethargic transformation even with alkali promoters, was negligible. Overall, apart from the minor formation of secondary phases, which remained stable over several C0 ₂ conversion cycles, orthorhombic LSF and hexagonal Si0 ₂ phases maintained dominancy. Fourier transform infrared spectroscopy (FTIR) results, shown in FIG. 2D, confirmed a consistent trend of decreasing silica peak at 1080 cm ^"1 with increasing LSF in the composites. A notable trend observed in the LSF:Si0 ₂ amalgams was the change in orthorhombic cell volume with different ratios as reported in Table 1. This pattern was complementary with the formation of secondary phases as shown in FIG. 2D. The generation of secondary phases along with surface wetness resulted in interfacial strain and a slight increase in the cell volume as previously witnessed in interfacial layers between Si0 ₂ and complex Sr oxides. Calculation of the LSF crystallite size via Scherrer analysis revealed the role of supports in restricting the perovskites from sintering during RWGS-CL experiments as documented in Table 2. This particular role of supports in tuning the LSF crystallite size and strain was fundamental for exploring the underlying mechanism of C0 ₂ conversion over these composites.

Table 2 - Crystallite size estimations by Scherrer analysis for fresh and post RWGS-CL experiment samples with CO formation rates on the estimated LSF surface area for the final cycle

a Based on LSF surface area when alone and estimated surface area based on changes in

crystallite size and proportions of total SSA

b Estimated on BET SSA (assumes equivalent surface areas per phase)

[00138] Example 3. Temperature-programmed C0 ₂ conversion experiments

[00139] Successful RWGS-CL is contingent on generation of oxygen vacant active sites throughout the perovskite surface and bulk during the reduction step. These active sites are then repurposed for C02 to CO conversion in the subsequent oxidation step. Under H2 flow and increasing temperature, H20 formation indicated the generation of oxygen vacancies by removal of oxygen installed in the bulk and strongly adsorbed to the surface. Consecutive disintegration of the perovskite phase into simpler, unary and oxides was also observed. These reactions are depicted in FIG. 3 A by H20 formation (m/z = 18) below 700 °C and over 750 °C, respectively. The LSF-based composites exhibited higher peak temperatures, about 600 °C, for H ₂ 0 formation than that of LSF (550 °C) alone. This phenomenon may be related to formation of cationic vacancies during the sintering of LSF and Si0 ₂ . A previous study delineated the increase in oxygen vacancy formation energy as the extent of vacancies in the lattice increases. Therefore, the slight but permanent removal of Fe and La from the perovskite lattice resulted in the formation of FeSi0 ₃ and La ₂ Si0 ₅ respectively along with the shift in the perovskite reduction temperature. Sustainable chemical looping with perovskite-oxides required the formation of oxygen deficient phases without decomposition to disparate species. The TPR profiles suggested 600 °C was an adequate temperature for achieving numerous vacancies prior to C0 ₂ conversion while retaining material intactness. CO formation was indicated by the m/z = 28 peak as displayed in FIG. 3B. Complementary to TPR experiments, CO generated over the LSF composites at about 50 °C higher than over pure LSF. Quantifications in FIG. 3C showed that H ₂ 0 production surpassed that of CO due to a few crucial factors. The entirety of perovskite surface oxygen, for instance, contributed to immense H ₂ 0 formation during first-time reduction. Yet replenishment remained highly implausible due to the gradual buildup of kinetic stagnation during C0 ₂ conversion. Moreover, the activity of oxygen vacant sites towards CO formation was closely related to the net number of oxygen vacancies present at any time. C0 ₂ adsorption strength over a perovskite-oxide increased with the extent of surface oxygen vacancies, reflecting higher probability of conversion. Thus, with progressive refilling of oxygen vacant sites via C0 ₂ to CO conversion came a gradual stagnation of surface exchange kinetics which resulted in less CO production than that of H ₂ 0 in the first cycle.

[00140] Capacities of 2.21 mmol H ₂ 0 gLSF ^-1 and 0.69 mmol CO gLSF ^-1 were produced during the control experiment with unsupported LSF. While utilization of Si0 ₂ as a supporting material with 25% LSF resulted in a 67% increase in H ₂ 0 formation capacity at 3.69 mmol gLSF~ ^l , CO production experienced a greater magnitude of improvement of 150% for a total yield of 1.70 mmol gLSF ^-1 . LSF ₂₅ /SiC also exhibited improved H ₂ 0 (2.91 mmol gLSF ^-1 ) and CO (1.20 mmol gLSF ¹ ) formation. The XRD patterns of LSF:Si0 ₂ amalgams after the experiment showed the presence of pure orthorhombic LSF and hexagonal Si0 ₂ phases along with minor concentrations of secondary phases of FeSi0 ₃ and La ₂ Si0 ₅ . Density functional theory (DFT) based calculations revealed that the LSF phase was the most favorable substrate to accommodate oxygen vacancies while all other phases (Si0 ₂ , FeSi0 ₃ and La ₂ Si0 ₅ ) demanded a higher energy input to create oxygen vacancies (FIG. 4A). C0 ₂ conversion results for LSF ₂₅ /SiC validated this hypothesis, for this composite demonstrated enhanced H ₂ 0 and CO formation without consisting of Si0 ₂ or secondary phases. Thus, the reason for better C0 ₂ conversion was attributed to more surface area of LSF exposed for gas interactions. This was corroborated by the decreased crystallite size of LSF in the composites compared to its pure phase catalyst.

[00141] Moreover, the increased cell volume of the LSF perovskite indicated the presence of a strained perovskite structure. As shown in FIG. 4B, an expanded crystal lattice enabled oxygen vacancy formation in LSF. Thus, these strained interfaces, suggested by cell volume calculations in Table 1, were found to promote oxygen vacancy creation and subsequently enhance C0 ₂ conversion. Si0 ₂ showed greater promise than SiC, as it manifested a wettability effect on the perovskite particles. Silica was previously shown to demonstrate affinity for transition metals and was capable of both reducing particle sizes and contact angles. However, there existed an optimum LSF:Si0 ₂ ratio as was evident from FIG. 3C whereby LSF ₅₀ /SiO ₂ and LSF ₇₅ /S1O ₂ showed poor C0 ₂ conversion performance. This was associated with increased formation of FeSi0 ₃ and La ₂ Si0 ₅ at the LSF:Si0 ₂ interface. These secondary phases acted as catalyst poisons, reducing the composites' ability to accommodate oxygen vacancies and CO generation capacity. As aforementioned, they were also believed to be the underlying cause of an increase in Ev _ac due to additional cationic vacancies, and therefore the reduction temperature observed in the TPR experiments. LSF ₂₅ /S1O ₂ however, simultaneously demonstrated minimal secondary phase formation and maximum wettability making the material a suitable candidate for chemical looping.

[00142] Example 4. Sustained performance in RWGS-CL

[00143] The stability and activity of the materials were demonstrated across eight consecutive RWGS-CL cycles (FIG. 5). LSF ₂₅ /S1O ₂ achieved the highest H ₂ 0 and CO yields per perovskite mass basis. By the concluding cycle, the results for LSF ₂₅ /S1O ₂ settled at about 3.10 mmol H ₂ 0 gLSF ^-1 per cycle and 2.60 mmol CO gLSF ^-1 per cycle. Overall, LSF25/S1O2 exhibited 8% and 12% decreases in H ₂ 0 and CO production, respectively, after 8 cycles. Unsupported LSF showed no decrease in H ₂ 0 production, H ₂ 0 production stabilized at about 1.10 mmol H ₂ 0 gLSF~ ^l , or CO production, which remained steady around 0.90 mmol CO gLSF ^-1 - LSF ₂₅ /S1C

demonstrated better performance than pure LSF but fell short of LSF ₂₅ /S1O ₂ . The extent of oxygen vacancy formation, δ (in ΑΒ0 _3-δ ), for LSF was calculated to be 0.26. Those of

LSF ₂₅ /S1O ₂ and LSF ₂₅ /S1C were 0.72 and 0.40 respectively. The CO production rate for pure LSF stabilized over time at 0.93 mmol CO gLSF ^-1 min ^"1 in comparison to 0.80 and 0.38 for LSF ₂₅ /S1O ₂ and LSF/SiC respectively, restrictions potentially imputed to transport limitations exhibited by the supports. Rates were estimated also on an approximated perovskite-oxide surface area basis (Table 2). In this metric, the LSF ₂₅ /S1O ₂ composite surpassed the rate of LSF alone and this was consistent with changes in exposed facets and/or strain that would enhance vacancy formation at the surface.

[00144] Perhaps the greatest significance of the chemical looping data was attributed to the escalation in the H ₂ 0 production rate using Si0 ₂ . As aforementioned, accelerated oxygen vacancy formation was concomitant with smaller average perovskite particle radii. It was also possible that water spillover to the silica support enabled faster reduction rates, but this effect was anticipated to be minimal in comparison due to the limited water adsorption at these elevated temperatures. Crystallite size reduction, resulting in increased surface area of LSF, was established to be the primary governing criteria for enhanced C0 ₂ conversion by supported perovskites. Although the average crystallite size of unsupported LSF remained unchanged throughout the 8 cycles, those of the supported samples decreased (Table 2). More in particular, LSF supported on Si0 ₂ resulted in a 55% decrease in crystallite size and complimented the loss of bulk oxygen during the course of particle separation. This notable change was illustrated and confirmed by transmission electron microscopy (TEM; FIGS. 6B-H). While the size of fresh LSF particles, unsupported and supported, remained in the micron threshold, small clusters of LSF nanoparticles formed during RWGS-CL. These nanoparticles were essentially a source of active sites for oxygen vacancy formation and C0 ₂ conversion. These nanoparticles were not seen to consist of any metallic (Fe, Sr or La) phases nor were they comprised of any binary oxides (Fe oxides, Sr oxides and La oxides). As was evident from FIG. 6H, the high-resolution image of the nanoparticle structure revealed the (020) crystal facet that matched that of the fresh samples (FIG. 6C) and post reaction samples (FIG. 6E). Strong interaction between LSF nanoparticles and silica rafts restricted their growth and agglomeration, thereby ensuring a surfeit of active sites for C0 ₂ conversion.

[00145] Although silicon carbide demonstrated the same effect according to the Scherrer analysis, it was assured that the particle size reduction magnitude remained much greater when utilizing silica to support perovskite-oxides. Because the black silicon carbide was not reduced, but rather pretreated at 1000 °C in air, there was expected to be a notable presence of oxygen due to a partially oxidized surface and iron oxide impurities. Interactions between a support and active phase are much stronger when using a bulk oxide as opposed to an inert support consisting of a few surface oxide layers. Perovskite segregation likely occurred during the second reduction step when surface oxygen was previously removed and the increase in H ₂ 0 was noted. The high presence of metallic B-site metals on the perovskite surface during reduction was perhaps the driving force for particle size reduction on silica due to the spontaneity of metals to diffuse into the top layers of the oxide bulk. The kinetic inclination of these ions perhaps pulled apart the large particles to form nanoparticles. This phenomenon was accompanied by the strong surface energy of the reduced perovskite, i.e., oxygen vacant perovskites show strong affinity for species with high oxygen content, such as C0 ₂ or even potentially Si0 ₂ regardless of its inert behavior. This surface behavior was not observed in the post TPO-C0 ₂ samples where C0 ₂ flows over these samples up to 950 °C. It was thus evident that perovskite particle aggregation was inevitable at high temperatures during synthesis and other STC processes, but may be reversed by subjection to the RWGS-CL process in the presence of appropriate supports at low thermochemical temperatures.

[00146] RWGS-CL was capable of converting C0 ₂ to CO at a low temperature of 600 °C with unprecedented rates using the Lao _. 75Sr _0.2 5Fe03 (LSF) perovskite-type oxide supported on silica. The LSF-silica composite (25% LSF by mass) promoted a greater extent of oxygen vacancies, a key parameter for C0 ₂ conversion. Throughout eight cycles of RWGS-CL, CO generation yields of LSF on silica surpassed those of LSF alone by about 200%, producing 0.8 mmol CO/gLSF/min. Average LSF crystalline size in the composite decreased by 55% over eight cycles of chemical looping. This phenomenon may be attributed to wettability by silica and controlled quantities of secondary phases formed during high temperature sintering.

[00147] Example 5. Temperature-programmed Experiments

[00148] As opposed to using bulk single-phase catalyst pellets, the inclusion of supporting material was necessary to improve perovskite surface area and accelerate oxygen self-diffusion. The speed at which oxygen is exchanged by nonstoichiometric oxides may be modeled with the one-dimensional equation

where M _t is the sample mass at time t, M _∞ is the sample mass at the experiment conclusion and 1 is the radius. D represents the effective diffusivity of the oxygen vacancy which in this case will depend on the perovskite metallic composition and a thermodynamic proportionality factor. An effective diffusivity coefficient (D) of 2 ^χ 10 ^"7 cm ² /s was obtained for LSF at 600 °C through the interpolation of data obtained by Armstrong et al (E.N. Armstrong, K.L. Duncan, E.D.

Wachsman, Effect of A and B-site cations on surface exchange coefficient for ABO ₃ perovskite materials, Phys. Chem. Chem. Phys., 15 (2013) 2298-2308). L is the dimensionless ratio lk/D where k is the surface exchange coefficient, given as 10 ^"5 cm/s. b _n is the n ^th positive root of b*tan(b) = L [38]. This phenomenon, illustrated in FIG. 7 with LSF, foreshadowed low CO yields and long cycle times if pellets were designed without supporting material able to maintain a high surface to volume ratio for the perovskite phase.

[00149] Each composite and LSF individually was subjected to TPR and TPO-C0 ₂ experiments to identify conversion temperatures and quantify H ₂ 0 and C0 ₂ yields. TPR results (FIG. 8) suggested oxygen vacancy formation occurred, an important step in initiating the RWGS-CL process. Signal elevation below 700 °C was interpreted as partial reduction of the perovskite phase (ABO ₃ to ΑΒ03- _δ ) while that above 800 °C was confirmed to be decomposition of the perovskite into binary oxides such as FeO (FIG. 12). Thus, TPR profiles suggested 600 °C is an adequate temperature for creating vacancies and thus active sites for C0 ₂ conversion. CO production temperatures following isothermal reduction at 600 °C (FIG. 8) undoubtedly complimented those of their respective TPRs, suggesting each of the materials are suitable for RWGS-CL.

[00150] Total H ₂ 0 and CO yields (Table 3) were obtained from numerical integration. Most notably, LSF ₂₅ /Si0 ₂ resulted in the highest H ₂ 0 and CO yields of 3690 and 1700 μιηοΙ/gLSF respectively. This significant 150% increase in CO production by LSF ₂₅ /Si0 ₂ even surpassed those of LSF ₂₅ /Ce0 ₂ and LSF ₂₅ /Zr0 ₂ . Due to the similarity between LSF and LSF ₂₅ /Ce0 ₂ TPR profiles below 600 °C along with the Ce0 ₂ reduction peak witnessed at about 800 °C, it was highly unlikely that this support participated in the reactions. This catalytic hindering may be alleviated by using higher redox temperatures, which contradicts the incentives for feasible C0 ₂ utilization due to a higher energy input. While Ti0 ₂ appeared to have no consequential effect on the reaction, the use of A1 ₂ 0 ₃ was evidently detrimental to the redox properties of LSF given the 29%) decrease in CO production. Nonetheless, LSF ₂₅ /Si0 ₂ remained the top composite candidate for perovskite-based syngas production.

Table 3. Quantified TPR and TPO-CQ ₂ results.

[00151] Example 6. X-ray Diffraction

[00152] XRD patterns were examined for changes in crystalline phases and the presence of secondary phases due to solid state reactions between the perovskite and support. As illustrated in FIGS. 9A-F, the overall stability of orthorhombic LSF (Ref. Code 00-035-1480) on each support was assured while (020) remained the dominant perovskite facet throughout the sample lifetime from particle sintering to the conclusion of TPO-C0 ₂ experiments. Rietveld refinement of the LSF diffraction pattern resulted in an Rwp value of 3.7% and RBragg of 1.0% (FIG. 13 and Table 4). The crystal structures of Ce0 ₂ , Zr0 ₂ , A1 ₂ 0 ₃ , Si0 ₂ , and A1 ₂ 0 ₃ were cubic, monolithic, hexagonal, hexagonal, and tetragonal, respectively.

[00153] Close examination revealed the minute presence of orthorhombic FeSi0 ₃ (Ref. Code 01-076-0886) and monoclinic La ₂ Si0 ₅ (Ref. Code 00-040-0234) at the LSF:Si0 ₂ interface following composite sintering at high temperatures. These phases had been witnessed before in iron oxide: silica composites yet were not expected to exercise notable presences as reflected by current difficulties in synthesizing bulk single-phase quantities of FeSi0 ₃ . In addition, cubic Fe ₂ .5Tio.5O4 (Ref. Code 00-051-1587) was detected at 35.6 2Θ as a result from solid state reactions during either the reduction or oxidation of LSF. These phases did not initially appear detrimental to the catalytic activity but may pose consequences of interest during the

manufacturing of large-scale pellets and monoliths.

Obtained from Dann et al. J. Solid State Chem. 1994

[00154] By utilizing the geometrical characteristics of the (020) diffraction line, LSF crystallite size was estimated before and after 8 cycles of RWGS-CL through a Scherrer analysis (Table 5). These values demonstrated the effect of each support on perovskite particles. By utilizing silica, the average LSF crystallite size decreased by 21% as opposed to an increase with every other support. These results complimented the expected increase in catalytic performance predicted with Equation 1. Although the majority of the supports resulted in further sintering of the perovskite particles, they each induced strain on the perovskite lattice and enlarged the LSF cell volume. This slight expansion of interplanar distance between atoms decreased oxygen vacancy formation energy, making it easier for more oxygen to desorb from the lattice.

Table 5. LSF cell volume, secondary phases identified in perovskite composites, and crystallite size estimations.

Calculated by Scherrer analysis of XRD data with a shape factor of 0.9

[00155] X-ray photoelectron spectra (FIG. 14) were obtained for the LSF control and all supported samples following 8 cycles of reverse water-gas shift chemical looping at 600 °C. The spectra each consisted of two major orbital peaks: Fe2pi _/2 at -723 eV and Fe2p _3/2 at -710 eV. The Fe (III) Fe2pi _/2 -731 and Fe (II) Fe2p _3/2 -717 eV satellite peaks are unique to the distinct oxidation states of Fe and suggested that the perovskite surface in LSF ₂₅ /Ce0 ₂ has a relatively even mix of Fe ³⁺ and Fe ²⁺ , that the oxide support did not pose a significant effect on the

Fe ³⁺ /Fe ²⁺ surface content ratio. The same conclusion can likely be made for perovskite surfaces in the other composites.

[00156] Example 7. DFT-based Oxygen Vacancy Formation Energies

[00157] Oxygen vacancy formation energies (E _ac ) serve as descriptors for the ability of an oxide material to convert C0 ₂ . If a material exhibited a high E _vaC , it would be unwilling to form vacancies, and therefore C0 ₂ conversion active sites, at low RWGS-CL operating temperatures. On the other hand, a low E _vac would encourage numerous vacancies that were unlikely to be replenished in an oxidation reaction. With an Ev _ac of about 3.4 eV, calculated with Equation 2, LSF resided in the optimal regime for notable catalytic activity. Each of the supporting materials however, including Ce0 ₂ , possessed Ev _ac values greater than 4.0 eV as shown in FIG. 10. These results suggested that each support remained inactive during TPO-C0 ₂ experiments and that the perovskite was the only phase to produce vacancies during reduction at 600 °C. Given that popular redox materials such as Ce0 ₂ and Zr0 ₂ themselves do not participate in the reaction, utilizing them in low temperature RWGS-CL would contradict the investigation for a more economically friendly and kinetically enhanced composite.

[00158] Secondary phases identified through XRD analysis shared unidentified roles in

C0 ₂ conversion. FIG. 10 also includes DFT-calculated Ev _ac values for FeSi0 _3; La ₂ Si0 ₅ , and Fe ₂ .5Tio.504 to provide insight regarding their own abilities to form oxygen vacancies at the composite interface. In regards to LSF ₂₅ /Si0 ₂ , FeSi0 ₃ possessed an Ev _ac of about 5.3 eV while La ₂ SiC"5 resided in the much higher energy regime with an Ev _ac of about 7.0 eV. Given that Ce0 ₂ , the oxide with the lowest Ev _ac aside from LSF, did not form its own vacancies until about 700 °C in the TPR experiments, it remained highly improbable that these secondary phases were active participants at these experimental temperatures. The same conclusion was reached for Fe ₂ .5Tio.504 due to its relatively high Ev _ac of about 6.0 eV.

[00159] Example 8. Microscopy

[00160] Detailed images of each composite following 8 cycles of RWGS-CL are arranged in FIGS. 11 A-l 1 J. TEM revealed a consistent interplanar spacing of 0.27 A for the LSF (020) facet when combined with each support. Minor amounts of strain resulted at each

perovskite: support site of contact due to both interfacial forces and cationic migration during solid state reactions at high temperatures. The interplanar spacings of the LSF (020) facet on Ce0 ₂ , Zr0 ₂ , A1 ₂ 0 ₃ , Si0 ₂ , and Ti0 ₂ were 2.86, 2.74, 2.74, 2.78, and 2.70 A respectively. The repercussions of this expanded lattice included decreased oxygen vacancy formation energy by perovskites and increased cell volume in accordance with XRD data.

[00161] The SEM images however provided valuable insight to changes in C0 ₂ conversion by LSF. The Ce0 ₂ , Zr0 ₂ , and Si0 ₂ supports formed small particles which corresponded to the high CO yields in the TPO-C0 ₂ experiments. Si0 ₂ in particular

demonstrated the greatest reduction in perovskite particle size, especially in comparison to the abundant alternatives. SEM also emphasized distinction between different oxide morphologies, e.g. orthorhombic perovskite particles and hexagonal A1 ₂ 0 ₃ plates. Not only did LSF retain its size, but hexagonal A1 ₂ 0 ₃ plates and Ti0 ₂ growth appeared to be supported on, if not masking, the perovskite (FIGS. 1 IE and 1 II, respectively). This encapsulation explained the absence of kinetic enhancement when using A1 ₂ 0 ₃ and Ti0 ₂ as supports with physical barriers hindering C0 ₂ adsorption to the perovskite surface.

***

[00162] The foregoing description of the specific aspects will so fully reveal the general nature of the invention that others can, by applying knowledge within the skill of the art, readily modify and/or adapt for various applications such specific aspects, without undue

experimentation, without departing from the general concept of the present disclosure. Therefore, such adaptations and modifications are intended to be within the meaning and range of equivalents of the disclosed aspects, based on the teaching and guidance presented herein. It is to be understood that the phraseology or terminology herein is for the purpose of description and not of limitation, such that the terminology or phraseology of the present specification is to be interpreted by the skilled artisan in light of the teachings and guidance.

[00163] The breadth and scope of the present disclosure should not be limited by any of the above-described exemplary aspects, but should be defined only in accordance with the following claims and their equivalents.

[00164] All publications, patents, patent applications, and/or other documents cited in this application are incorporated by reference in their entirety for all purposes to the same extent as if each individual publication, patent, patent application, and/or other document were individually indicated to be incorporated by reference for all purposes.

[00165] For reasons of completeness, various aspects of the invention are set out in the following numbered clauses:

[00166] Clause 1. A catalyst composite comprising: a perovskite-oxide of formula AB0 ₃ , wherein A is an alkaline earth element, a rare-earth element, an alkali metal element, a metal element, or a combination thereof, and B is a transitional metal element, metal element, or a combination thereof; and an oxide support having a formula different from the perovskite-oxide. [00167] Clause 2. The catalyst composite of clause 1, wherein the perovskite-oxide has a cubic crystal structure, the O atoms being at the edge centers.

[00168] Clause 3. The catalyst composite of any one of clauses 1-2, wherein the oxide support induces strain in the crystal structure.

[00169] Clause 4. The catalyst composite of any one of clauses 1-3, wherein the oxide support causes surface reconstruction/termination.

[00170] Clause 5. The catalyst composite of any one of clauses 1-4, wherein the oxide support regulates crystallite growth of active surfaces of the perovskite-oxide.

[00171] Clause 6. The catalyst composite of any one of clauses 1-5, wherein oxide support increases the perovskite-oxide surface area.

[00172] Clause 7. The catalyst composite of any one of clauses 1-6, wherein the perovskite-oxide surface area is between 1 and 1000 m ² /g.

[00173] Clause 8. The catalyst composite of any one of clauses 1-7, wherein the perovskite-oxide crystallite size is between 5 and 100 nm.

[00174] Clause 9. The catalyst composite of any one of clauses 1-8, wherein A is selected from the group consisting of Pb, Ca, Mg, Be, Sr, Ba, La, K, and Na or a combination thereof.

[00175] Clause 10. The catalyst composite of any one of clauses 1-9, wherein A has a formula of A^A^, wherein A ¹ and A ² are independently Pb, Ca, Mg, Be, Sr, Ba, La, K, or Na; x is 0-1; y is 0-1; and the sum of x and y is 1.

[00176] Clause 11. The catalyst composite of any one of clauses 1-10, wherein A has a formula of A^A^, and is Lao.75Sro.25·

[00177] Clause 12. The catalyst composite of any one of clauses 1-11, wherein B is selected from the group consisting of Fe, Ti, Y, Mn, Al, Cr, Co, Ta, Ni, and Ce, or a combination thereof. [00178] Clause 13. The catalyst composite of any one of clauses 1-12, wherein the perovskite-oxide is Lao.75Sro _.25 Fe0 ₃ .

[00179] Clause 14. The catalyst composite of any one of clauses 1-13, wherein the oxide support is Ce0 ₂ , Zr0 ₂ , A1 ₂ 0 ₃ , Si0 _2, Ti0 ₂ , or a combination thereof.

[00180] Clause 15. The catalyst composite of any one of clauses 1-14, wherein a weight ratio of the perovskite-oxide to the oxide support is from 10:90 to 90: 10.

[00181] Clause 16. The catalyst composite of any one of clauses 1-15, wherein a weight ratio of the perovskite-oxide to the oxide support is from 25:75 to 75:25.

[00182] Clause 17. A method for preparing a catalyst composite, comprising: (a) mixing a perovskite-oxide of formula AB0 ₃ with an oxide support having a formula different from the perovskite-oxide to form a mixture, wherein A is an alkaline earth element, a rare-earth element, an alkali metal element, a metal element, or a combination thereof, B is a transitional metal element, a metal element, or a combination thereof; and (b) heating the mixture to a temperature of between 600 °C and 1300 °C.

[00183] Clause 17.1 The method of clause 17, wherein the perovskite-oxide of step (a) has a cubic crystal structure, the O atoms being at the edge centers.

[00184] Clause 17.2 The method of clause 17 or clause 17.1, wherein the perovskite-oxide adheres to the oxide support in step (b), and wherein the oxide support induces strain in the crystal structure, causes surface reconstruction/termination, and/or regulates crystallite growth of active surfaces of the perovskite-oxide in step (b).

[00185] Clause 18. The method of clause 17, wherein the mixing is accomplished by grinding, ball milling, drum tumbling or solution based methods.

[00186] Clause 19. The method of any one of clauses 17-18, wherein A is selected from the group consisting of Pb, Ca, Mg, Be, Sr, Ba, La, K, and Na, or a combination thereof. [00187] Clause 20. The method of any one of clauses 17-19, wherein A has a formula of

A^A^, wherein A ¹ and A ² are independently Pb, Ca, Mg, Be, Sr, Ba, La, K, or Na; x is 0-1; y is 0-1; and the sum of x and y is 1.

[00188] Clause 21. The method of any one of clauses 17-20, wherein B is selected from the group consisting of Fe, Ti, Y, Mn, Al, Cr, Co, Ta, Ni, and Ce, or a combination thereof.

[00189] Clause 22. The method of any one of clauses 17-21, wherein the perovskite-oxide

[00190] Clause 23. The method of any one of clauses 17-22, wherein the oxide support is

Ce0 ₂ , Zr0 ₂ , A1 ₂ 0 ₃ , Si0 ₂ , Ti0 ₂ , or a combination thereof.

[00191] Clause 24. The method of any one of clauses 17-23, wherein the weight ratio of the perovskite-oxide to the oxide support is from 10:90 to 90: 10.

[00192] Clause 25. The method of any one of clauses 17-24, wherein the oxide support comprises M ² , wherein M ² is an element other than O; and the perovskite-oxide and the oxide support form a secondary phase of formula of M ¹ _p M ² _q O _v , wherein M ¹ is the A or B component of the perovskite-oxide; p is 1-3; q is 1-3; and v is 2-7.

[00193] Clause 26. The method of any one of clauses 17-25, further comprising calcining the perovskite-oxide before step (a).

[00194] Clause 27. A method for converting C0 ₂ to CO comprising: (a) contacting H ₂ with the catalyst composite of claim 1, whereby the perovskite-oxide is reduced, and whereby H ₂ is oxidized to produce H ₂ 0; and (b) contacting C0 ₂ with the catalyst composite, whereby the reduced perovskite-oxide is oxidized, and whereby C0 ₂ is reduced to produce CO.

[00195] Clause 28. The method of clause 27, wherein each of step (a) and step (b) is carried out isothermally at a temperature between 450 °C and 800 °C.

[00196] Clause 29. The method of any one of clauses 27-28, wherein the temperature for steps (a) and (b) is about 600 °C. [00197] Clause 30. The method of clause 27, wherein the temperature of step (a) is between 400 °C and 850 °C.

[00198] Clause 31. The method of any one of clause 27 or 30, wherein the temperature of step (b) is between 450 °C and 900 °C.

[00199] Clause 32. The method of any one of clauses 27-31, wherein CO is produced at a rate of 0.5 to 1 mmol CO/g perovskite-oxide/min.

[00200] Clause 33. The method of any one of clauses 27-32, wherein CO is produced at a rate greater than a process using the perovskite-oxide without the oxide support.

[00201] Clause 34. The method of any one of clauses 27-33, further comprising repeating step (a) and step (b) in succession.

[00202] Clause 35. The method of any one of clauses 27-34, further comprising wetting of the catalyst composite.

[00203] Clause 36. The method of any one of clauses 27-35, further comprising reducing the perovskite-oxide surface area.