Refractory ceramics are structures processed at high temperature and designed for high-temperature applications. Among the different materials available to fabricate refractory ceramics, group IV carbides and borides are key candidates due to their high melting points, toughness, and thermal conductivity. Refractory ceramics containing this type of material can be fabricated using the following methods: chemical vapor deposition (CVD), melt infiltration (MI), and polymer infiltration and pyrolysis (PIP).
The CVD infiltration of continuous fiber matrices has been demonstrated to prepare refractory ceramics made of group IV carbides and borides. This method can generate high purity matrices but is slow, includes expensive starting materials, and generally results in highly porous matrices. The MI infiltration of fiber preform, where the preform is partially carbonized and then exposed to the molten metal to form the corresponding carbide or boride, has also been used to fabricate refractory ceramics containing group IV carbides and borides. However, this method requires special precautions to protect the fiber structure from the molten metal and generally results in mixtures of carbide and metal phases as the metal does not react completely. The PIP infiltration of fiber preform utilizes a polymer to infiltrate the preform followed by pyrolysis under controlled conditions of the polymeric fiber preform to form the desired refractory ceramic. One or more cycles of infiltration and pyrolysis can be performed to obtain refractory ceramics with specific properties, e.g., density. In addition, to allow the ready fabrication of refractory ceramics, polymers have also proven to: (i) require a lower temperature for densification; (ii) reduce impurities that can impact the ceramic properties; and (iii) provide the ability to generate mixed ceramics in a controlled fashion at shorter length scales, e.g., nanometer and micron length scales.
They are only a few polymers available for the PIP fabrication of refractory ceramics like ZrC, HfC, ZrB2, and HfB2, and most of the polymers that are used in the art lead to hybrid ceramics instead of pure ceramics, e.g., silicon containing ceramics. For instance, reduced metal oxides in the presence of boron carbide polymer has been demonstrated to produce phase pure metal borides at moderate temperatures and in good yield. The particulate metal oxide precursor, however, makes it challenging to obtain a uniform microstructure. In order to improve this process, metal (Zr, Hf) borohydrides have been reacted with borazine to obtain brittle solids that convert to the corresponding borides in good yield. While these materials show good conversion, their brittle nature, thought to be due to extensive crosslinking, makes them unsuitable for PIP processes. Similarly, an aqueous approach using a complex polymer of chitosan, metaloxychloride, and boric acid has been demonstrated to give a cross-linked gel after drying that convert to the corresponding boride in moderate yield. Another approach uses hafnocene as a building block to prepare heavily cross-linked or rigid-rod polymers. However, the resulting materials have poor solubility, which make them poor candidates for the PIP process. These materials can form the desired carbides but only in moderate yield and as a mixture with carbon.
Therefore, there is a continued need to improve polymers for fabricating refractory ceramics containing group IV carbides and borides, and thereby improve the various steps of fabricating such refractory ceramics.
Some embodiments provide a method for preparing a refractory ceramic comprising providing at least one polymer derived from a metallocene comprising a group IV element and at least one cyclopentadienyl group; infiltrating the polymer into a fiber preform to form a polymeric fiber preform; and pyrolyzing the polymeric fiber preform, wherein the refractory ceramic comprises a group IV carbide, a group IV boride, or a combination thereof.
In some embodiments, the metallocene has a Formula (I), (II), (III), (IV), or (V) with a structure:
wherein each R4 is independently H, an unsubstituted C1-C6 alkyl, a substituted C1-C6 alkyl, an unsubstituted C1-C6 heteroalkyl, or a substituted C1-C6 heteroalkyl; and
In some such embodiments, M is Hf or Zr; A is null, Si(CH3)2, or CH2; PG is an ethylene (CH3=CH2-) group; each R1 is independently BH3 or Cl; each R2 is H; and o is 0. In some embodiments, the metallocene is selected from the group consisting of:
In some embodiments, the polymer has a Formula (VI), (VII), (VIII), (IX), or (X) with a structure:
In some embodiments, the fiber preform is selected from the group consisting of carbon fiber, SiC, HfC, ZrC, or combinations thereof. In some embodiments, the fiber preform is a carbon fiber. In some embodiments, the carbon fiber is coated with pyrolytic carbon. In some embodiments, the carbon fiber is coated with a layer of SiC. In some embodiments, the layer of SiC is deposited by chemical vapor infiltration.
In some embodiments, the polymeric fiber preform is pyrolyzed at a temperature of at least about 1000° C. In some embodiments, the polymeric fiber preform is pyrolyzed at a temperature from about 1000° C. to about 2000° C. In some embodiments, the polymeric fiber preform is pyrolyzed at a temperature from 1200° C. to about 2000° C. In some embodiments, the polymeric fiber preform is pyrolyzed at a temperature from 1400° C. to about 2000° C.
In some embodiments, the polymeric fiber preform is pyrolyzed for at least about 0.5 hour. In some embodiments, the polymeric fiber preform is pyrolyzed for about 0.5 hour to about 5 hours. In some embodiments, the polymeric fiber preform is pyrolyzed for about 1.0 hour to about 5 hours. In some embodiments, the polymeric fiber preform is pyrolyzed for about 2.0 hours to about 5 hours.
In some embodiments, the polymeric fiber preform is pyrolyzed under inert atmosphere. In some embodiments, the inert atmosphere is selected from the group consisting of nitrogen, argon, helium, and any combinations thereof.
In some embodiments, the polymer is a polymer mixture comprising a solvent. In some embodiments, the solvent is selected from the group consisting of ethers, ketones, aromatics or esters, any derivatives thereof, and any mixtures thereof.
In some embodiments, the polymer is a polymer mixture comprising a reactive additive. In some embodiments, the reactive additive is selected from the group consisting of ZrO2, HfO2, SiO2, B2O3, or any carbide forming metal oxide, boron, any derivatives thereof, or any combinations thereof.
In some embodiments, the polymer is a polymer mixture comprising a dispersant. In some embodiments, the dispersant is selected from the group consisting of aprotic anionic, cationic or nonionic surfactants, any derivatives thereof, or any combinations thereof.
In some embodiments, the ceramic composition comprises at least about 30 wt. % of group IV carbide. In some embodiments, the ceramic composition comprises about 30 wt. % to about 90 wt. % of group IV carbide. In some embodiments, the ceramic composition comprises about 45 wt. % to about 90 wt. % of group IV carbide. In some embodiments, the ceramic composition comprises about 60 wt. % to about 90 wt. % of group IV carbide.
In some embodiments, the ceramic composition comprises at least about 30 wt. % of group IV boride. In some embodiments, the ceramic composition comprises about 30 wt. % to about 90 wt. % of group IV boride. In some embodiments, the ceramic composition comprises about 45 wt. % to about 90 wt. % of group IV boride. In some embodiments, the ceramic composition comprises about 60 wt. % to about 90 wt. % of group IV boride.
Some embodiments provide a polymer of Formula (VI), (VII), (VIII), (IX), or (X) with a structure:
wherein each R4 is independently H, an unsubstituted C1-C6 alkyl, a substituted C1-C6 alkyl, an unsubstituted C1-C6 heteroalkyl, or a substituted C1-C6 heteroalkyl;
In some embodiments, M is Zr or Hf; A is null, Si(CH3)2, or CH2; each R1 is independently BH3 or Cl; each R2 is independently H or CH3; and o is 0. In some embodiments, the polymer is selected from the group consisting of:
A detailed description of various embodiments is provided herein below with reference, by way of example, to the following drawings. The skilled person in the art will understand that the drawings, described below, are for illustration purposes only. The drawings are not intended to limit the scope of the applicant's teachings in any way.
In the figures:
Before the present compounds, compositions, and methods are described, it is to be understood that this invention is not limited to the particular processes, compositions, or methodologies described, as these may vary. It is also to be understood that the terminology used in the description is for the purpose of describing the particular versions or embodiments only, and is not intended to limit the scope of the present invention, which will be limited only by the appended claims. Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art. Although any methods and materials similar or equivalent to those described herein can be used in the practice or testing of embodiments of the present invention, the preferred methods, devices, and materials are now described. All publications mentioned herein are incorporated by reference in their entirety. Nothing herein is to be construed as an admission that the invention is not entitled to antedate such disclosure by virtue of prior invention.
It must be noted that as used herein and in the appended claims, the singular forms “a”, “an”, and “the” include plural reference unless the context clearly dictates otherwise. Thus, for example, reference to “a polymer” is a reference to “one or more polymers” and equivalents thereof known to those skilled in the art, and so forth.
As used herein, the term “about” means plus or minus 10% of the numerical value of the number with which it is being used. Therefore, “about 50” means in the range of 45%-55%.
As used herein, the term “group IV” or “group IV element” refers to a chemical element belonging to the fourth group in the Periodic Table of the Elements and may include a titanium, zirconium, or hafnium atom.
As used herein, the term “C1-C6-alkyl” refers to a linear or branched, saturated or unsaturated, monovalent hydrocarbon group having 1, 2, 3, 4, 5, or 6 carbon atoms.
As used herein, the term “C1-C6-alkylene” refers to a linear or branched, saturated or unsaturated, bivalent hydrocarbon group having 1, 2, 3, 4, 5, or 6 carbon atoms.
As used herein, the term “heteroalkyl” refers to an alkyl group, which further includes at least one heteroatom selected from oxygen, nitrogen, or sulfur within (i.e., inserted between adjacent carbon atoms of) and/or placed at one or more terminal position(s) of the parent chain.
As used herein, the term “heteroalkylene” refers to an alkylene group, which further includes at least one heteroatom selected from oxygen, nitrogen, or sulfur within (i.e., inserted between adjacent carbon atoms of) and/or placed at one or more terminal position(s) of the parent chain.
As used herein, the term “Cp” refers to a cyclopentadienyl group, a substituted cyclopentadienyl group, or any derivatives thereof. For instance, Cp can refer to Cp*, the methyl substituted cyclopentadienyl group 1,2,3,4,5-pentamethylcyclopentadienyl.
As used herein, the term “substituted” means that one or more hydrogen atoms on the designated atom or group are replaced with a substituent, provided that the designated atom's normal valency under the existing circumstances is not exceeded. Combinations of substituents and/or variables are permissible. Unless otherwise indicated, it is possible that substituted groups are substituted with as many optional substituents as can be accommodated. The substituent can be any aprotic substituent, including, but not limited to, alkyl, alkenyl, and halide.
As used herein, the term “halogen” refers to a fluorine, chlorine, bromine, or iodine atom, particularly a fluorine, chlorine, or bromine atom.
As used herein, the term “polymerizable group” means any polymerizable group that is known in the art. The “polymerizable group” can be an alkene group, an aldehyde group, an acid group, an amine group, a phosphate group, thiol group, derivatives thereof, or combinations thereof. The “polymerizable group” can be a vinyl (CH3═CH2—) group, substituted vinyl groups, methylvinyl, vinyl ethers, acrylic and methacrylic esters, vinyl halides.
Compounds and polymers disclosed herein include diastereomers, racemates, tautomers, N-oxides, hydrates, solvates, salt, and mixtures of same.
It will be understood that the description of compounds and polymers herein is limited by principles of chemical bonding known to those skilled in the art. Accordingly, where a group may be substituted by one or more of a number of substituents, such substitutions are selected so as to comply with principles of chemical bonding with regard to valencies, etc., and to give compounds which are not inherently unstable. For example, any carbon atom will be bonded to two, three, or four other atoms, consistent with the four valence electrons of carbon.
In accordance with certain embodiments, the present disclosure provides a method for preparing a refractory ceramic. The method may include for example the following steps (
The metallocene comprising a group IV element and at least one cyclopentadienyl group of the embodiments of this disclosure is not limited and can be any metallocene known in the art. The metallocene can include one cyclopentadienyl group, two cyclopentadienyl groups, or more cyclopentadienyl groups. The metallocene can include Ti, Zr, or Hf, any derivatives thereof, or any combinations thereof. The metallocene can have a Formula (I), (II), (III), (IV), (V) or (VI) with a structure:
wherein:
wherein each R4 is independently H, an unsubstituted C1-C6 alkyl, a substituted C1-C6 alkyl, an unsubstituted C1-C6 heteroalkyl; or a substituted C1-C6 heteroalkyl and
The metallocene can have the Formula (I), (II), (III), (IV), or (V) wherein:
The metallocene can be selected from the group consisting of:
any derivatives thereof, and any combinations thereof.
Without being bound to any theory, varying the degree and type of functional group, e.g., R1, R2, R3, and PG group, attached to a compound, a monomer, a polymer, or a group attached to a compound, a monomer, or a polymer, e.g., a metallocene or a cyclopentadienyl group attached to a metallocene, can vary the solubility of the compound, polymer, or monomer. For example, increasing the degree of methylation on a cyclopentadienyl group that is attached to a metallocene can increase the solubility of the metallocene.
The polymer derived from the metallocene comprising a group IV element and at least one cyclopentadienyl group of the embodiments of this disclosure is not limited and can be any polymer known in the art. The polymer can be an oligomer, a polymer, a linear polymer, a branched polymer, a hyper-branched polymer, a random copolymer, or a block copolymer. The polymer can have a Formula (VI), (VII), (VIII), (IX), or (X) with a structure:
wherein:
wherein each R4 is independently H, an unsubstituted C1-C6 alkyl, a substituted C1-C6 alkyl, an unsubstituted C1-C6 heteroalkyl, or a substituted C1-C6 heteroalkyl;
The polymer can have the Formula (VI), (VII), (VIII), (IX), or (X) wherein:
The polymer can be selected from the group consisting of:
any derivatives thereof, and any combinations thereof.
The polymer from the invention can be polymerized in various ways. These include chain-growth polymerization, step-growth polymerization, acyclic diene metathesis (ADMET) polymerization, radical polymerization, and any derivatives thereof.
One of ordinary skill in the art will appreciate that the copolymer disclosed herein can be used to control the composition and doping of the refractory ceramic. For example, the level of Si in the copolymer can be varied to control the amount of Si in the resulting refractory ceramic. This can be a valuable tool for tuning the oxidation resistance of the ceramic. Different group IV elements within the copolymer can also be used to obtain refractory ceramic with different proportions of group IV elements.
The fiber preform of the embodiments of this disclosure is not limited and is any fiber preform known in the art. The fiber preform relates generally to preform having strips of material that are woven, knitted, braided, stitched, or any combinations thereof. The fiber preform is used to reinforce refractive ceramic materials to produce structural components. One skilled in the art would appreciate that the use of such components is widespread. For instance, the reinforced materials find applications where materials that are light in weight, strong, tough, thermally resistant, self-supporting, and/or adaptable to being formed and shaped are needed. Such components are used, for example, in aeronautic, aerospace, satellite, automobile, nautical, and other applications.
In some embodiments, the fiber preform can include a carbon fiber preform, SiC, HfC, ZrC, mixed systems (ZrC/SiC), any derivatives thereof, or any combinations thereof. The fiber preform can be coated with any of those common in the art, including but not limited to, pyrolytic carbon, a layer of SiC, BN, any derivatives thereof, or any combinations thereof. The fiber preform can be coated using chemical vapor infiltration, chemical vapor deposition, laser CVD, liquid processing, etc., any derivatives thereof, or any combinations thereof.
The step of infiltrating a polymer into a fiber preform to form the polymeric fiber preform disclosed herein can include infiltrating the preform using standard resin infiltration techniques (e.g., vacuum infiltration, wet layup), drying the infiltrated fiber preform, and low-temperature curing of the infiltrated preform. This step can also be combined with other infiltration methods such as melt infiltration and chemical vapor deposition infiltration.
The pyrolysis of the polymeric fiber preform can be performed at controlled parameters to obtain specific properties. The pyrolysis of the polymeric fiber preform can be performed in a furnace. In some embodiments, the pyrolysis of the polymeric fiber preform can be performed at a temperature of at least about 800° C., or about 1000° C., or about 1200° C., or about 1400° C., or about 1600° C., or about 1800° C., or about 2000° C., or about 2200° C., or about 2400° C., or about 2600° C., or about 2800° C., or about 3000° C., or any ranges that is formed from any two of those values as endpoints. In some embodiments, the pyrolysis of the polymeric fiber preform can be performed for at least about 0.2 hour, or about 0.5 hour, or about 1.0 hour, or about 1.5 hour, or about 2.0 hour, or about 2.5 hour, or about 3.0 hour, or about 3.5 hour, or about 4.0 hour, or about 4.5 hour, or about 5.0 hour, or any range that is formed from any two of those values as endpoints. In some embodiments, the pyrolysis of the polymeric fiber preform yields group IV carbide at about 0 wt. %, or at about 10 wt. %, or at about 20 wt. %, or at about 30 wt. %, or at about 40 wt. %, or at about 50 wt. %, or at about 60 wt. %, or at about 70 wt. %, or at about 80 wt. %, or at about 90 wt. %, or at about 100 wt. %, or any ranges that is formed from any two of those values as endpoints. In some embodiments, the pyrolysis of the polymeric fiber preform yields group IV boride at about 0 wt. %, or at about 10 wt. %, or at about 20 wt. %, or at about 30 wt. %, or at about 40 wt. %, or at about 50 wt. %, or at about 60 wt. %, or at about 70 wt. %, or at about 80 wt. %, or at about 90 wt. %, or at about 100 wt. %, or any ranges that is formed from any two of those values as endpoints. In some embodiments, the pyrolysis of the polymeric fiber preform yields a ratio of group IV carbide:group IV boride at about 0:100, or at about 10:90, or at about 20:80, or at about 30:70, or at about 40:60: or at about 50:50, or at about 60:40, or at about 70:30, or at about 80:20, or at about 90:10, or at about 100:0.
The steps disclosed herein, such as the steps to form the refractory ceramic, can include an inert atmosphere. The inert atmosphere of the embodiments of this disclosure is not limited and is any material known in the art. The inert atmosphere can include nitrogen, helium, argon, neon, krypton, xenon, radon, any derivatives thereof, or any combinations thereof. The inert atmosphere could also be at a vacuum or at a partial pressure of any of the inert gases.
The polymer disclosed herein can be a polymer or a polymer mixture comprising a solvent and one or more additives such as a reactive additive, a non-reactive additive, a dispersant, a surfactant, a stabilizer, a dopant, a catalyst, a filler, and any derivatives thereof.
The solvent of the embodiments of this disclosure is not limited and is any solvent known in the art. The solvent can be an organic solvent, an inorganic solvent, or a mixture thereof. The solvent can have the ability to dissolve and/or suspend the polymer, additive, and other solvent. In some embodiments, the solvent can dissolve the polymer at high concentration. In some embodiments, the solvent is a high evaporation solvent that requires less time and energy to remove and therefore can speed fabrication cycles. In some embodiments, the solvent is compatible with use in a production environment. The solvent can include, but is not limited to, THF, toluene, dimethoxyethane, N-methylpyrrole anisole, benzene, any derivatives thereof, or any mixtures thereof.
The additive of the embodiments of this disclosure is not limited and is any additive known in the art. The additive can be an organic additive, an inorganic additive, or a combination thereof, can be a particle, a molecule, or a combination thereof, and can have a millimeter size, a micron size, a nanometer size, an angstrom size, or any combinations thereof.
One skilled in the art would appreciate that reactive and non-reactive additives can be used to increase the overall yield of the system and reach a target yield of carbide, boride, or combination thereof of about 30 vol. %, or about 40 vol. %, or about 50 vol. %, or about 60 vol. %, or about 70 vol. %, or about 80 vol. %, or about 90 vol. %, or about 100 vol. %, or any ranges that is formed from any two of those values as endpoints. Reactive additives can consume extra material produced as byproducts of the ceramitization process, like oxides that undergo carbothermal reduction to consume excesses of carbon and to produce additional carbides. Non-reactive additives, in addition to be able to simply increase the yield, can also act as nucleation centers to improve the conversion of the preceramic materials to the target ceramic. Reactive additives include ZrO2, HfO2, SiO2, B2O3, or any carbide forming metal oxide, boron, any derivatives thereof, or any combinations thereof.
In some embodiments, for both reactive and non-reactive additives, nanometer size materials are favored because they have a higher surface area for reaction and nucleation and they can more easily infiltrate fiber structures, e.g., fiber preform. Nanometer size materials are also favored because they can be more easily suspended to generate well-dispersed and stable suspension, which can improve processability.
In some embodiments, a surfactant is added to the polymer or polymer mixture as dispersant and/or stabilizer. The surfactant can have a concentration of about 0.1 wt. %, or about 0.5 wt. %, or about 1.0 wt. %, or about 1.5 wt. %, or about 2.0 wt. %, or about 2.5 wt. %, or about 3.0 wt. %, or about 3.5 wt. %, or about 4.0 wt. %, or about 4.5 wt. %, or about 5.0 wt. %, or about 5.5 wt. %, or about 6.0 wt. %, or about 6.5 wt. %, or about 7.0 wt. %, or about 7.5 wt. %, or about 8.0 wt. %, or about 8.5 wt. %, or about 9.0 wt. %, or about 9.5 wt. %, or about 10.0 wt. %, or any ranges that is formed from any two of those values as endpoints. The surfactant can include a polyurethane and/or polyacrylate with a polar functionality that binds to the particles and a hydrophobic backbone that keeps particles from aggregating through steric hindrance and keeps them suspended by improving compatibility with the solvent. In some embodiments, the surfactant is a positively charged polymer such as a positively charged polymer available from BASF (e.g., Efka® and Dispex® brands) or Dow (TAMOL® brand). Other surfactants that are aprotic and non-reactive to borohydrides may be used, including but not limited to alkyl quaternary ammonium halides, alkyl sulfonates, alkyl sulfates, and any derivatives thereof.
Although the present invention has been described in considerable detail with reference to certain preferred embodiments thereof, other versions are possible. Therefore, the spirit and scope of the appended claims should not be limited to the description and the preferred versions contained within this specification. Various aspects of the present invention will be illustrated with reference to the following non-limiting examples.
Borohydride derivatives of zirconocene and hafnocene are prepared from the corresponding chlorides by salt metathesis with lithium borohydride and analyzed by Simultaneous Thermal Analysis (STA).
Cp2Zr(BH4)2
Cp2Zr(BH4)2 is subject to a STA treatment up to 1500° C. (
Cp2Zr(BH4)2+ZrO2
Cp2Zr(BH4)2 with the reactive additive ZrO2 at a 1:2 Cp2Zr(BH4)2:ZrO2 molar ratio is subject to a STA treatment up to 1500° C. (
The stoichiometry of the STA analysis is chosen based on a Thermogravimetric Analysis (TGA) at 1000° C. Given that the weight loss observed in the STA analysis at about 1300° C. for the pure compound is significantly lower than that seen in the TGA analysis, it suggests that too much zirconia for the available carbon is added and this would result in residual oxide contamination. Matching the addition of reactive additive to available reactants is a key part of developing preceramic systems such as high-yield preceramic systems.
CpZr(BH4)3
CpZr(BH4)3 is subject to a STA treatment up to 1500° C. (
The XRD analysis of the residues from the STA treatment shows that the product comprises about 96% of ZrB2, about 4% of ZrO2 contaminant, and no carbide (
A polymerizable cyclopentadienyl halide compound (
Ansa-bridged zirconocene dichloride is subject to a TGA analysis. An initial 65 wt. % loss between 250-300° C. is observed and followed by a second loss starting at around 475° C. The total residual material is 19 wt. %, which is close to the lower end of the theoretical 28-39 wt. % yield. Note that the range is calculated using pure ZrC for the low end and ZrC+SiC for the high end. The presence of the silyl bridge creates the possibility of making a mixed carbide of Zr and Si, which may be desirable for improved oxidation resistance of the resulting material.
Ansa-bridged zirconocene diborohydride is subject to a STA treatment (
Ansa-bridged hafnocene diborohydride is subject to a STA treatment. A small loss of 2.8 wt. % at around 100° C. is observed and followed by another small loss of 8.4 wt. % between around 250 and 500° C. One final loss of 5.7 wt. % at above 1000° C. is observed. The total yield, therefore, is 83.1 wt. %, relative to the 45-57 wt. % theoretical yield.
The borohydride versions of the ansa-compounds show much improved yield relative to the original chloride system. The powder X-ray diffraction analysis of the resulting solids also show that the desired phases are made. For example,
Polymeric zirconocenes are polymerized via three different polymerization mechanisms. First, step-growth reactions between lithium diacetylide and a difunctional zirconocene compound (e.g., Li2C2 and Cp2ZrCl2) are performed (
A polymeric zirconocene is polymerized via a radical chain addition polymerization of an ansa-zirconocene compound to make the pendant polymer (
Cp2M(BH4)2 (M=Zr, Hf) are pyrolyzed in covered Mo crucibles in a graphite furnace. The furnace is heated to 200° C. under vacuum, backfilled to 500 Torr with Ar, and subject to a continuous flow of Ar. The temperature is ramped to 1500° C. at 10° C./min and then held at 1500° C. for 2 h. After cooling, the samples are removed for analysis. The results are summarized in Table 3, and the XRD, SEM, and EDS analysis of the resulting ceramics are shown in
During pyrolysis, the Cp2Zr(BH4)2 is converted from an off-white powder to a black powder at 39 wt. % yield, which is close to the theoretical yield. The Cp2Hf(BH4)2 is converted from an off-white powder to a chunky aggregate at only 17 wt. % yield. The other two samples are zirconocene or hafnocene borohydrides mixed with the corresponding oxide at a ratio calculated to consume excess carbon via carbothermal reduction based on the STA results. From the furnace yields of the pure compounds, however, it appears unlikely that any carbon material remained after 2 h at 1500° C. to react with the oxide by carbothermal reduction.
The Cp2Zr(BH4)2 converts to 60% ZrC and 17% ZrB2 with about 23% ZrO2 contamination. The peaks observed by XRD analysis are narrow and therefore indicate a certain degree of crystallization (
The Cp2Zr(BH4)2 and ZrO2 mixture is converted during pyrolysis to primarily ZrC (42%) with residual ZrO2 (58%), and no boride is observed (
The hafnium version follows a similar pattern. During pyrolysis, the Cp2Hf(BH4)2 converts to a mixture of HfB2 (53%) and HfC (57%) with only traces of HfO2 (<1%), and all phases show a certain degree of crystallinity by XRD analysis. The SEM/EDS analysis shows crystalline materials with an elemental composition of Hf, C, and O, and no boron is observed.
The hafnium version with the related oxide follows a similar pattern. During pyrolysis, the mixture of Cp2Hf(BH4)2 and HfO2 converts to primarily HfC (67%) with residual HfO2 (33%), and no boride is observed. The peaks observed by XRD analysis are sharp and therefore indicate a certain degree of crystallization. The SEM/EDS analysis shows the mixture of oxide as larger crystallites and carbide as smaller crystallites.
The amount of oxide contamination observed in the furnace runs is substantially lower than that seen in STA runs, which may be due to the more tightly controlled atmosphere in the furnace. The STA treatment of samples likely leads to some level of air contamination. Furthermore, the combination of oxide with these preceramic materials appears to inhibit the formation of the boride. The boron may react with the oxygen released during carbothermal reduction of the oxide, before reacting with the zirconium, to form a volatile species.
CpM(BH4)3 (M=Zr, Hf) are pyrolyzed and the results are summarized in Table 4.
The XRD pattern of the pyrolyzed CpZr(BH4)3, shows a complete conversion to highly crystalline ZrC (
The pyrolysis of the Cp*Zr(BH4)3 is similar to the plain-Cp version. The XRD analysis shows that the compound is predominantly composed of ZrC (96%) with a small amount of ZrO2 contamination (4%). The SEM analysis shows that the compound has a lacey crystalline structure with submicron size crystallites. The Cp*Hf(BH4)3, in contrast to the Zr analogs, retained significantly more material and shows a mixture of HfC (70%) and HfB2 (30%) without oxide contamination by XRD analysis. The SEM analysis shows a similar open crystalline structure with submicron size crystallites, just like the Zr analogs.
Cp2Zr(BH4)2/ZrC disks are pyrolyzed. First, a mixture of Cp2Zr(BH4)2 and ZrC in toluene is formulated. The zirconocene diborohydride is dissolved in toluene at 0.8 g/mL and 325 mesh ZrC is suspended in the solution (
This application claims the benefit of priority to U.S. Provisional Application No. 63/349,498, filed Jun. 6, 2022, which are incorporated herein by reference in their entirety.
This invention was made with Government support under Contracts No. FA8650-26-M-5028 and FA8650-17-C-5076 awarded by the US Air Force. The Government has certain rights in this invention.
Number | Date | Country | |
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63349498 | Jun 2022 | US |