Synthesis of a homogeneously porous solid oxide matrix with tunable porosity and pore size
09650301 ยท 2017-05-16
Assignee
Inventors
Cpc classification
C04B38/0051
CHEMISTRY; METALLURGY
C04B2235/549
CHEMISTRY; METALLURGY
C04B38/06
CHEMISTRY; METALLURGY
C04B2235/785
CHEMISTRY; METALLURGY
C04B2235/3229
CHEMISTRY; METALLURGY
C04B2235/5445
CHEMISTRY; METALLURGY
C04B2235/3224
CHEMISTRY; METALLURGY
C04B2235/3279
CHEMISTRY; METALLURGY
C04B2235/5436
CHEMISTRY; METALLURGY
C04B38/0051
CHEMISTRY; METALLURGY
International classification
Abstract
The present disclosure relates to a method for synthesis of a porous solid oxide matrix. The method includes synthesizing a composite by co-precipitating a porous ceramic material with a sacrificial material. The composite is sintered and the sacrificial material of the sintered composite is reduced. A porous solid oxide matrix is formed from the reduced and sintered composite. Porosity of the solid oxide matrix is controlled by a volume fraction of the sacrificial material or sintering temperature and a volume fraction of the sacrificial material. Pore size of the solid oxide matrix is controlled by sintering temperature and a volume fraction of the sacrificial material.
Claims
1. A method for synthesis of a porous solid oxide matrix comprising: synthesizing a composite by co-precipitating a ceramic material with a sacrificial material, the method of co-precipitating comprising combining stoichiometric amounts of starting materials including Ce(NO.sub.3).sub.3.6H.sub.2O, Ni(NO.sub.3).sub.2.6H.sub.2O, and Sm(NO.sub.3).sub.3.6H.sub.2O in the presence of (NH.sub.4).sub.2CO.sub.3 as mineralizer, the co-precipitation forming a samarium doped cerium (SDC)-nickel oxide (NiO) composite that includes the NiO as the sacrificial material; sintering the composite; reducing the sacrificial material of the sintered composite; removing the reduced sacrificial material from the sintered composite to form the porous solid oxide matrix; and controlling a median pore size of the porous solid oxide matrix by controlling a sintering temperature of the composite and a volume fraction of the sacrificial material; wherein an increase in the sintering temperature at a given volume fraction of the sacrificial material will increase the median pore size of the porous solid oxide matrix without an equivalent increase in porosity of the porous solid oxide matrix.
2. A method as in claim 1, wherein sintering the composite occurs at a temperature of between about 1000 and 1700 C.
3. A method as in claim 1, wherein reducing the sacrificial material occurs in the presence of H.sub.2.
4. A method as in claim 3, wherein reducing the sacrificial material occurs at a temperature of between about 500 and 1000 C.
5. The method of claim 1, wherein the SDC-NiO composite includes the NiO as the sacrificial material at a volume fraction of from 35% to 50%.
Description
BRIEF DESCRIPTION OF THE FIGURES
(1) A full and enabling disclosure of the present subject matter, including the best mode thereof, to one of ordinary skill in the art, is set forth more particularly in the remainder of the specification, including reference to the accompanying figures in which:
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DETAILED DESCRIPTION
(11) Reference will now be made in detail to embodiments of the disclosed subject matter, one or more examples of which are set forth below. Each example is provided by way of explanation of the subject matter, not limitation of the subject matter. In fact, it will be apparent to those skilled in the art that various modifications and variations can be made in the present disclosure without departing from the scope or spirit of the subject matter. For instance, features illustrated or described as part of one embodiment, can be used on another embodiment to yield a still further embodiment.
(12) Porous ceramics are a technologically important branch of functional materials for a variety of physical and chemical systems. The properties of porous ceramics depend on porosity, pore morphology, pore size and distribution. In the present disclosure, the synthesis of a homogeneously porous samarium doped cerium (Ce.sub.0.8Sm.sub.0.2O.sub.1.9, SDC) matrix with tunable porosity and pore size via a sacrificial template method is demonstrated. The present disclosure describes that the porosity and pore size of the resultant porous matrix can be controlled by the volume fraction of sacrificial material and sintering temperature, along with the mono-mode pore distribution produced by molecular-level mixing of co-precipitating SDC and sacrificial material. The demonstrated sacrificial template methodology provides an alternative means of tailoring properties of a porous ceramic for particular applications in catalysis, fuel cells and gas separation membranes.
(13) Generally, the method for synthesis of a porous solid oxide matrix includes synthesizing a composite by co-precipitating a porous ceramic material with a sacrificial material. The composite is sintered and the sacrificial material of the sintered composite is reduced. For instance, the composite can be sintered at a temperature of between about 1000 and 1700 C. The sintered composite can be reduced with H.sub.2 at a suitable temperature. For example, the sintered composite can be reduced at a temperature of between about 500 and 1000 C. A porous solid oxide matrix is formed from the reduced and sintered composite. Porosity of the solid oxide matrix is controlled by a volume fraction of the sacrificial material or sintering temperature and a volume fraction of the sacrificial material. Pore size of the solid oxide matrix is controlled by sintering temperature and a volume fraction of the sacrificial material.
(14) In accordance with the present disclosure, a samarium doped CeO.sub.2 (SDC) ceramic porous microstructure with a tunable porosity, pore size and distribution is described. NiO can be selected as the sacrificial template material because NiO is chemically inert and has a very limited solubility in SDC even at elevated temperatures. However, other suitable materials such as Fe.sub.2O.sub.3 can be utilized as a sacrificial template material in accordance with the present disclosure.
(15) For example, use of NiO allows the use of high temperatures to attain a mechanically stronger NiO-SDC ceramic, which is important for practical applications. After the reduction of NiO in reducing atmospheres, the resultant elemental Ni in the composite is then chemically removed by dissolving it into a diluted nitric acid, leaving behind a porous SDC matrix. To maximize the homogeneity, the SDC-NiO composite was prepared by co-precipitation method. The potential use of fabricated homogenous porous scaffold is to support molten carbonate as a functional membrane for application in either SOFCs or CO.sub.2 separation.
(16) The following examples are meant to illustrate the disclosure described herein and are not intended to limit the scope of this disclosure.
EXAMPLES
(17) Co-Precipitation Synthesis of SDC-NiO Composite
(18) The Ce.sub.0.8Sm.sub.0.2O.sub.1.9 and NiO composite powders were synthesized by a co-precipitation method. Starting materials Ce(NO.sub.3).sub.3.6H.sub.2O (Alfa Aesar, 99.95%), Ni(NO.sub.3).sub.2.6H.sub.2O (Alfa Aesar, 99%), and Sm(NO.sub.3).sub.3.6H.sub.2O (Alfa Aesar, 99.5%) in a stiochimetric ratio were mixed with deionized water as the precursors and (NH.sub.4).sub.2CO.sub.3 (Fisher Scientific, 95%) as the mineralizer. The volume fractions of NiO in SDC-NiO composite varied among 35, 40 and 50 vol %. After precipitation, the co-precipitate was first washed with DI-water for multiple times, and then filtered, dried and subsequently calcined at 600 C. for 4 h in air to ensure the formation of SDC-NiO composite and removal of any residues. The obtained powders were then pressed into 13 mm pellets in a thickness of 1 mm, followed by sintering at 1200-1550 C. in air for 10 h. The well-sintered pellets were then reduced in pure H.sub.2 at 800 C. for another 10 h to convert nickel oxide to nickel metal. The nickel in the reduced composite was finally removed by dissolving it into a 2.2 M nitric acid at 80 C. for 24 h. The overall synthesis steps are schematically illustrated in
(19) Characterization of the Synthesized Powders and Porous Matrix
(20) The phase evolutions of the samples at different stages were examined with X-ray diffraction (XRD). The XRD patterns were recorded by a X-ray diffractometer (Rigaku, Japan) equipped with graphite-monochromatized CuKa radiation (=1.5418 ) at a scanning rate of 10 min.sup.1 in 2 range from 20 to 80, and analyzed with JADE (MDI) software to identify phases. After powder synthesis, the particle sizes were measured by a particle size analyzer (Horiba, LA950) and the morphology was examined by transmission electron microscopy (TEM, Hitachi H-800, 200 kV). The microstructure of synthesized porous solid-oxide matrix was captured by a field emission scanning electron microscopy (FESEM, Zeiss Ultra) equipped with an energy dispersive X-ray spectroscopy (EDS). To visualize the internal microstructure in a 3-D manner, a Micro 3-D X-ray microscope (XCT-400, Xradia) was employed. The final pore size distributions, median pore sizes and porosities were quantified by a mercury porosimetry (Autopore IV, Micromeritics) at pressures ranging from 0.5-30000 psi.
(21) Results and Discussion
(22) Powder Characterization
(23) The XRD patterns of SDC60/NiO40 (40 vol % NiO) powder after calcining at 600 C. are shown in
(24) The chemical homogeneity of the formed composite is examined by EDX elemental mapping. The surface morphology of a SDC50/NiO50 (50 vol % NiO) sintered at 1400 C. for 10 h is shown in
(25) Phase Evolution Throughout Synthesis Step
(26) The phase evolution of SDC50/NiO50 ceramic in the course of synthesis is shown in
(27) Porous Microstructure
(28) The internal microstructure of a 1500 C.-sintered SDC50/NiO50 porous matrix revealed by a 3-D X-ray computed tomography imaging technique is shown in
(29) Temperature Effect on Pore Size
(30) The pore size of porous SDC matrix is expected to increase with sintering temperature as the grain size of sacrificial material NiO increases with sintering temperature. This assertion is evidently confirmed by
(31) Effect on Porosity
(32) The porosity of a porous material made from a sacrificial template method is controlled largely by the volume fraction of the sacrificial material. This premise has been indirectly verified in
(33) Selection Strategy
(34) Thus far, it has been demonstrated that with NiO as the sacrificial material, the pore size and porosity of the resultant porous SDC matrix can be, respectively, controlled by sintering temperature and volume fraction of NiO.
CONCLUSIONS
(35) The nano-sized SDC-NiO composite powders have been synthesized by the method of co-precipitation. Thus synthesized intimately mixed powders were then used as the precursor for making homogeneously porous SDC matrix by high-temperature sintering, chemical reduction of NiO to Ni and chemical leaching of Ni. It has been explicitly demonstrated that the porosity can be controlled by the volume fraction of the sacrificial phase NiO while the pore size can be affected by both the sintering temperature and volumetric fraction of NiO. The formed porous network is mechanically strong, homogeneous, interconnected and uniformly distributed across the entire sample. It is highly expected that the synthesized high-quality porous SDC ceramics can find useful applications in catalysis, fuel cells and gas separation membranes.
(36) In the interests of brevity and conciseness, any ranges of values set forth in this specification are to be construed as written description support for claims reciting any sub-ranges having endpoints which are whole number values within the specified range in question. By way of a hypothetical illustrative example, a disclosure in this specification of a range of 1-5 shall be considered to support claims to any of the following sub-ranges: 1-4; 1-3; 1-2; 2-5; 2-4; 2-3; 3-5; 3-4; and 4-5.
(37) These and other modifications and variations to the present disclosure can be practiced by those of ordinary skill in the art, without departing from the spirit and scope of the present disclosure, which is more particularly set forth in the appended claims. In addition, it should be understood that aspects of the various embodiments can be interchanged both in whole or in part. Furthermore, those of ordinary skill in the art will appreciate that the foregoing description is by way of example only, and is not intended to limit the disclosure so further described in such appended claims.