EP4157806A1 - Formulations de monomères et de polymères d'impression 3d précéramique - Google Patents

Formulations de monomères et de polymères d'impression 3d précéramique

Info

Publication number
EP4157806A1
EP4157806A1 EP20938855.2A EP20938855A EP4157806A1 EP 4157806 A1 EP4157806 A1 EP 4157806A1 EP 20938855 A EP20938855 A EP 20938855A EP 4157806 A1 EP4157806 A1 EP 4157806A1
Authority
EP
European Patent Office
Prior art keywords
group
vinyl
preceramic
polymer composition
thiol
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
EP20938855.2A
Other languages
German (de)
English (en)
Other versions
EP4157806A4 (fr
Inventor
Zak Eckel
Andrew Nowak
Ashley DUSTIN
April RODRIGUEZ
Phuong BUI
Tobias SCHAEDLER
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
HRL Laboratories LLC
Original Assignee
HRL Laboratories LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US16/888,724 external-priority patent/US11891341B2/en
Application filed by HRL Laboratories LLC filed Critical HRL Laboratories LLC
Publication of EP4157806A1 publication Critical patent/EP4157806A1/fr
Publication of EP4157806A4 publication Critical patent/EP4157806A4/fr
Pending legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y70/00—Materials specially adapted for additive manufacturing
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    • C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
    • C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
    • C04B35/5603—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides with a well-defined oxygen content, e.g. oxycarbides
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    • C08G77/60—Macromolecular compounds obtained by reactions forming a linkage containing silicon with or without sulfur, nitrogen, oxygen or carbon in the main chain of the macromolecule in which all the silicon atoms are connected by linkages other than oxygen atoms

Definitions

  • the present invention generally relates to monomer formulations suitable for making preceramic polymers, which can be converted into ceramic matrix composites and other ceramic structures.
  • Ceramic matrix composite (CMC) materials overcome many disadvantages of conventional ceramics, such as brittle failure, low fracture toughness, and limited thermal shock resistance. Applications of ceramic matrix composites include those requiring reliability at high temperatures (beyond the capability of metals or polymers) and resistance to corrosion and wear.
  • 3D-printed ceramics in fields including industrial filtration (molten metal filters, flow separators); metal processing (casting molds/blanks); implantable dental and medical devices; and semiconductor processing. Additive manufacturing of ceramic materials is also of interest for propulsion components, thermal protection systems, porous burners, microelectromechanical systems, and electronic device packaging, for example. [0005] No mature method for 3D printing ceramic matrix composites exists.
  • CMC materials are limited to manual lay-up, molding, or thermoforming.
  • techniques for sintering ceramic particles or using ceramic particles printed in a binder both of which typically produce porous ceramics which have lower strength than the parent material.
  • Ceramic structures are typically sintered as compacted porous materials, severely limiting the manufacturable geometries.
  • Formulations have been described for creating ceramic materials, which can be printed (additively manufactured) with various methods such as stereolithography techniques and laser sintering. These are typically unreinforced ceramics that do not contain a second phase and suffer from low fracture toughness. These methods are described in Zocca et al., “Additive Manufacturing of Ceramics: Issues, Potentialities, and Opportunities”, J Am. Ceram. Soc., 98 [7] 1983-2001 (2015).
  • ceramics are difficult to process, particularly into complex shapes. Because they cannot be cast or machined easily, ceramics are typically consolidated from powders by sintering or deposited in thin films. Flaws, such as porosity and inhomogeneity introduced during processing, govern the strength because the flaws initiate cracks, and — in contrast to metals — brittle ceramics have little ability to resist fracture. This processing challenge has limited the ability to take advantage of ceramics’ impressive properties, including high-temperature capability, environmental resistance, and high strength. Recent advances in additive manufacturing have led to a multitude of different techniques, but all additive manufacturing techniques developed for ceramic materials only process unreinforced ceramics and not ceramic matrix composites.
  • Preceramic polymers are a class of polymers which allow, via a thermal treatment, a conversion of a polymer part to a ceramic material.
  • these preceramic polymers contain silicon (Si) in the molecular backbone, with the resulting material containing Si.
  • Si silicon
  • preceramic polymers There are a wide variety of known preceramic polymers. Examples include polysilazanes, borazine-modified hydridopolysilazanes, polysilanes, polycarbosilanes, silicone resins, polyvinylborazine, polyborazylene, and decaborane-based polymers. These preceramic polymers have been used to form specific polymer-based structures that can be subsequently heat-treated (pyrolyzed or sintered) to create near net-shape ceramic structures.
  • a stereolithography technique provides a method to build a 3D polymer microstructure in a layer-by-layer process.
  • This process usually involves a platform (e.g., substrate) that is lowered into a photomonomer bath in discrete steps.
  • a laser is used to scan over the area of the photomonomer that is to be cured (i.e., polymerized) for that particular layer.
  • the platform is lowered by a specific amount, determined by the processing parameters and desired feature/surface resolution, and the process is repeated until the complete 3D structure is created.
  • a stereolithography technique is disclosed in U.S. Patent No. 4,575,330 issued March 11, 1986 to Hull et al.
  • 3D printing for engineering and other applications.
  • Lower-cost structures that are lightweight, strong, and stiff, but can withstand a high-temperature oxidizing environment, are sought.
  • preceramic resin formulation for 3D- printing and free-radical or cationic polymerization, the preceramic resin formulation comprising:
  • R 1 is selected from the group consisting of hydrogen, a vinyl group, an allyl group, an ethynyl group, a Ci-Cig unsubstituted or substituted alkyl group, an ester group, an amine group, a hydroxyl group, a vinyl ether group, a vinyl ester group, a glycidyl group, a glycidyl ether group, a vinyl glycidyl ether group, a vinyl amide group, a vinyl triazine group, a vinyl isocyanurate group, an acrylate group, an alkacrylate group, an alkyl alkacrylate group, a phenyl group, a halide group, a thiol group, a thiol-containing group, a cyano group, a cyanate group, a thiocyanate group, and combinations thereof;
  • R 2 is selected from the group consisting of hydrogen (except when R 1 is hydrogen), a vinyl group, an allyl group, an ethynyl group, a C
  • - Cix unsubstituted or substituted alkyl group, an ester group, an amine group, a hydroxyl group, a vinyl ether group, a vinyl ester group, a glycidyl group, a glycidyl ether group, a vinyl glycidyl ether group, a vinyl amide group, a vinyl triazine group, a vinyl isocyanurate group, an acrylate group, an alkacrylate group, an alkyl alkacrylate group, a phenyl group, a halide group, a thiol group, a thiol-containing group, a cyano group, a cyanate group, a thiocyanate group, and combinations thereof; and n 1 to 100;
  • R 2 is hydrogen. In some embodiments, at least one of R 1 or R 2 is a vinyl group or an allyl group. In some embodiments, at least one of R 1 or R 2 is an acrylate group or a methacrylate group (or other alkacrylate group). In some embodiments, at least one of R 1 or R 2 is a thiol group or a thiol-containing group.
  • the preceramic resin formulation may contain at least two distinct functionalized carbosilanes that are each in accordance with the chemical structure above, wherein R 1 , R 2 , and n are independently selected for the distinct functionalized carbosilanes.
  • the photoinitiator may be present in a concentration from about 0.001 wt% to about 10 wt% in the preceramic monomer formulation, for example.
  • the photoinitiator generates free radicals by intramolecular bond cleavage or intermolecular hydrogen abstraction when exposed to light having a wavelength from about 200 nm to about 500 nm.
  • the photoinitiator may be selected from the group consisting of 2,2- dimethoxy-2-phenylacetophenone, 2-hydroxy -2-methylpropiophenone, camphorquinone, bis(2,4,6-trimethylbenzoyl)-phenylphosphineoxide, benzophenone, benzoyl peroxide, and combinations thereof, for example.
  • the free-radical inhibitor may be present in a concentration from about
  • the free-radical inhibitor may be selected from the group consisting of hydroquinone, methylhydroquinone, ethylhydroquinone, methoxyhydroquinone, ethoxyhydroquinone, monomethylether hydroquinone, propylhydroquinone, propoxyhydroquinone, tert-butylhydroquinone, n-butylhydroquinone, and combinations thereof, for example.
  • the 3D-printing resolution agent may be present in a concentration from about 0.001 wt% to about 10 wt% in the preceramic resin formulation, for example.
  • the 3D-printing resolution agent may be selected from the group consisting of 2-(2-hydroxyphenyl)-benzotriazole, 2-hydroxyphenyl-benzophenones, 2-hydroxyphenyl-s-triazines, 2,2'-(2,5-thiophenediyl)bis(5-tert-butylbenzoxazole), 2,2'-(l,2-ethenediyl)bis(4,l-phenylene)bisbenzoxazole, and combinations thereof, for example.
  • the preceramic monomer formulation further comprises a thermal free-radical initiator, such as (but not limited to) a thermal free- radical initiator selected from the group consisting of benzoyl peroxide, dicumyl peroxide, 2,2'-azobisisobutyronitrile, and combinations thereof.
  • a thermal free-radical initiator such as (but not limited to) a thermal free- radical initiator selected from the group consisting of benzoyl peroxide, dicumyl peroxide, 2,2'-azobisisobutyronitrile, and combinations thereof.
  • the preceramic monomer formulation further comprises a radiation-trigger free-radical initiator active at a second wavelength that is substantially different from a first wavelength for which the photoinitiator is active.
  • the preceramic resin formulation may further contain a crosslinking agent, such as (but not limited to) a silazane.
  • the preceramic monomer formulation further comprises from about 0.1 vol% to about 70 vol% of solid-phase fillers.
  • solid-phase fillers include, but are not limited to, Si, SiC, SiOC, SiCN, SiCBN, SiOCN, SiAlON, S13N4, S1O2, silicate glasses, zirconium hydride, and combinations thereof.
  • Some variations of the invention provide a preceramic polymer composition comprising functionalized polycarbosilane having the polymer structure: wherein:
  • R 1 is selected from the group consisting of hydrogen, a vinyl group, an allyl group, an ethynyl group, a Ci-Cis unsubstituted or substituted alkyl group, an ester group, an amine group, a hydroxyl group, a vinyl ether group, a vinyl ester group, a glycidyl group, a glycidyl ether group, a vinyl glycidyl ether group, a vinyl amide group, a vinyl triazine group, a vinyl isocyanurate group, an acrylate group, an alkacrylate group, an alkyl alkacrylate group, a phenyl group, a halide group, a thiol group, a thiol-containing group, a cyano group, a cyanate group, a thiocyanate group, and combinations thereof;
  • R 1 or R 2 is hydrogen.
  • the preceramic polymer composition may contain at least two distinct functionalized polycarbosilanes that are each in accordance with the above polymer structure, wherein R 1 , R 2 , and n are independently selected for the distinct functionalized polycarbosilanes.
  • the preceramic polymer composition comprises a functionalized polycarbosilane copolymer having the copolymer structure: wherein:
  • R 1 , R 2 , R 3 , and R 4 are independently selected from the group consisting of hydrogen, a vinyl group, an allyl group, an ethynyl group, a C
  • the preceramic polymer composition comprises a functionalized polycarbosilane copolymer having the copolymer structure: wherein R 1 is hydrogen, R 2 is an allyl group, R 3 is hydrogen, and R 4 is a vinyl group.
  • the ratio of m to n may be from about 2 to about 20, for example.
  • the preceramic polymer composition comprises a functionalized polycarbosilane copolymer having the copolymer structure: wherein R 1 is hydrogen, R 2 is an allyl group, R 3 is an acrylate group, and R 4 is hydrogen.
  • the ratio of m to n may be from about 0.1 to about 10, for example.
  • the preceramic polymer composition comprises a functionalized polycarbosilane copolymer having the copolymer structure: wherein R 3 may be selected from Ci-Cis unsubstituted or substituted alkyl groups.
  • R 3 may be selected from Ci-Cis unsubstituted or substituted alkyl groups.
  • the ratio of m to n may be from about 0.1 to about 10, for example.
  • the preceramic polymer composition comprises a functionalized polycarbosilane copolymer having the copolymer structure:
  • R 3 may be selected from Ci-Cig unsubstituted or substituted alkyl groups.
  • the ratio of m to n may be from about 0.1 to about 10, for example.
  • the preceramic polymer composition comprises a functionalized polycarbosilane copolymer having the copolymer structure: wherein R 3 may be selected from Ci-Cis unsubstituted or substituted alkyl groups.
  • R 3 may be selected from Ci-Cis unsubstituted or substituted alkyl groups.
  • the ratio of m to n may be from about 0.1 to about 10, for example.
  • the preceramic polymer composition may further contain a crosslinking agent, such as (but not limited to) a silazane.
  • crosslinking agents may be monomers or oligomers of silanes with UV-reactive functional groups, such as vinyl, vinyl ether, acrylate, methacrylate, glycidyl, and/or glycidyl ether.
  • Crosslinking agents may be used to improve the crosslink density of the polymers. In some cases, crosslinking agents reduce the resin viscosity.
  • the preceramic polymer composition comprises copolymer repeat units that are different from the polycarbosilane repeat units.
  • the copolymer repeat units may be polycarbonitrosilane repeat units containing nitrogen bonded to silicon and/or carbon.
  • the nitrogen is bonded to a functional group selected from the group consisting of hydrogen, a vinyl group, an allyl group, an ethynyl group, a C
  • the preceramic polymer composition further comprises from about 0.1 vol% to about 70 vol% of solid-phase fillers.
  • solid-phase fillers may be selected from the group consisting of Si, SiC, SiOC, SiCN, SiCBN, SiOCN, SiAlON, Si 3 N , Si0 2 , silicate glasses, zirconium hydride, and combinations thereof.
  • the preceramic polymer composition may be a 3D-printed polymer, which may be thermally treated to fabricate a 3D-printed ceramic part.
  • FIG. 1 A is an optical microscope image of SiC solid-phase fillers dispersed in a preceramic silicone monomer (scale bar 500 pm), in Example 1.
  • FIG. IB is an optical microscope image of SiC solid-phase fillers dispersed in a preceramic silicone monomer (scale bar 200 pm), in Example 1.
  • FIG. 2 is a photograph of a preceramic polymer (right-hand side) and a pyrolyzed ceramic part (left-hand side), in Example 2.
  • FIG. 3 is a graph of thermogravimetric analysis for the pyrolysis of a
  • UV-cured preceramic polymer into a pyrolyzed ceramic material measuring the loss of sample mass over time as the pyrolysis temperature increases, in Example 2.
  • FIG. 4 is a photograph of a 3D-printed polymer plate and 3D-printed polymer bars, in Example 9.
  • FIG. 5 is a photograph of an amorphous SiC plate and amorphous SiC bars, in Example 9.
  • FIG. 6 is a photograph of a 3D-printed polymer bar, an amorphous SiC bar, and SiC bars crystallized at 1500°C and 1600°C, in Example 9.
  • FIG. 7 is a graph of thermogravimetric weight loss associated with a preceramic polymer as it is pyrolyzed up to 1000°C, in Example 9.
  • FIG. 8 is a graph of thermogravimetric (TG) weight loss and differential scanning calorimetry (DSC) associated with a preceramic polymer as it is pyrolyzed up to 1000°C and then further thermally treated to 1500°C, in Example 9.
  • FIG. 9 shows an X-ray powder diffraction pattern of the ceramic material obtained from high-temperature treatment at 1600°C for 4 hours in argon, revealing the b-SiC phase in the crystallized ceramic material, in Example 9.
  • compositions also referred to as formulations
  • structures, systems, and methods of the present invention will be described in detail by reference to various non-limiting embodiments.
  • Variations of this invention provide resin formulations which may be used for 3D printing (e.g., by stereolithography) of an intermediate structure followed by thermally treating (e.g., by firing or pyrolyzing) to convert the 3D intermediate structure into a 3D ceramic structure.
  • the monomers and polymeric systems can be printed into potentially complex 3D shapes with high thermal stability and mechanical strength.
  • Preceramic in this disclosure simply refers to the capability to be ultimately converted to a ceramic material. It is noted that the disclosed preceramic resin formulations are precursors to preceramic polymers, which themselves are precursors to ceramic materials.
  • a “resin” means a composition capable of being polymerized or cured, further polymerized or cured, or crosslinked. Resins may include monomers, oligomers, prepolymers, or mixtures thereof.
  • Some variations of the invention are premised on direct, free-form 3D printing of a preceramic polymer optionally loaded with a solid-phase filler, followed by converting the preceramic polymer to a 3D-printed ceramic matrix composite.
  • the monomers and polymeric systems are selected with specific properties so that they can be printed using 3D-printing methods including stereolithography into complex 3D shapes.
  • Some embodiments provide free-form ceramic matrix composite parts containing UV-cured, 3D-printed (e.g., stereolithographically), solid-filled preceramic Si-containing polymer resins, or related monomer formulations.
  • polymer resin means monomer, oligomer, prepolymer, or other molecule that is converted to a polymer.
  • the preceramic monomer formulations are designed to allow the ceramic structures to be formed with preferably high thermal stability (such as chemical and physical stability at temperatures greater than 1200°C) and good mechanical strength (including stiffness, flexural strength, hardness, and/or fracture toughness).
  • the solid solid-phase filler can improve mechanical properties, especially the fracture toughness of the (otherwise) brittle ceramic material.
  • the invention in various embodiments applies to additively manufactured components, such as to reduce part count, scrap, or non-recurring engineering. Some embodiments apply to high-wear or high-temperature applications that would necessitate ceramic materials. Specific applications of interest include, for example, propulsion structures (vanes, impellors, nacelles, and thrusters), control surfaces (fins and leading edges), hypersonic structures (thermal protection systems and heat shields), high-wear components (brakes, clutches, and rotors), catalyst support structures (such as catalytic converters), pump components, filters, brakes, clutches, and space-exploration probes and vehicles.
  • propulsion structures vanes, impellors, nacelles, and thrusters
  • control surfaces fins and leading edges
  • hypersonic structures thermal protection systems and heat shields
  • high-wear components brakes, clutches, and rotors
  • catalyst support structures such as catalytic converters
  • pump components filters, brakes, clutches, and space-exploration probes and vehicles.
  • preceramic polymer parts with optional solid solid-phase fillers, and then firing or pyrolyzing the part into a ceramic.
  • the ceramic materials may be prepared from a wide variety of preceramic monomer formulations that can be used in UV-cure-based 3D printing. Stereolithography, laser rastering, digital light processing, liquid crystal device projection, two-photon lithography, or other techniques may be employed to 3D print the monomer formulations.
  • a monomer formulation is a mixture of a liquid preceramic monomer resin and a solid solid-phase filler.
  • the liquid resin is preferably UV-curable to enable definition of three-dimensional shapes via a 3D- printing process.
  • UV-cure-based shall include reference not only to ultraviolet radiation but also other electromagnetic radiation bands that can be effective in various embodiments, including microwave radiation, terahertz radiation, infrared radiation, visible radiation (light), ultraviolet radiation, and X-rays.
  • preceramic resin formulation for 3D- printing and free-radical or cationic polymerization, the preceramic resin formulation comprising:
  • R 1 is selected from the group consisting of hydrogen, a vinyl group, an allyl group, an ethynyl group, a Ci-Cis unsubstituted or substituted alkyl group, an ester group, an amine group, a hydroxyl group, a vinyl ether group, a vinyl ester group, a glycidyl group, a glycidyl ether group, a vinyl glycidyl ether group, a vinyl amide group, a vinyl triazine group, a vinyl isocyanurate group, an acrylate group, a methacrylate group, an alkacrylate group, an alkyl alkacrylate group, a phenyl group, a halide group, a thiol group, an alkylthiol group, a thiol-containing group, a cyano group, a cyanate group, a cyanate group, a cyanate group, a cyanate group,
  • R 2 is selected from the group consisting of hydrogen (except when R 1 is hydrogen), a vinyl group, an allyl group, an ethynyl group, a Ci-Cis unsubstituted or substituted alkyl group, an ester group, an amine group, a hydroxyl group, a vinyl ether group, a vinyl ester group, a glycidyl group, a glycidyl ether group, a vinyl glycidyl ether group, a vinyl amide group, a vinyl triazine group, a vinyl isocyanurate group, an acrylate group, a methacrylate group, an alkacrylate group, an alkyl alkacrylate group, a phenyl group, a halide group, a thiol group, an alkylthiol group, a thiol-containing group, a cyano group, a cyanate group, a thiocyanate group, a mercapto
  • a photoinitiator e.g., a photoinitiator that generates free radicals when exposed to light and/or a cationic photoinitiator
  • R 1 and R 2 are not hydrogen, in which case the carbosilane is referred to as “functionalized carbosilane.” In preferred embodiments, neither R 1 nor R 2 is hydrogen. In some embodiments of the preceramic resin formulation, one of R 1 or R 2 is hydrogen. In some embodiments, at least one of R 1 or R 2 is a vinyl group or an allyl group. In some embodiments, at least one of R 1 or R 2 is an acrylate group or a methacrylate group (or other alkacrylate group). In some embodiments, at least one of R 1 or R 2 is a thiol group or a thiol-containing group.
  • the fraction of repeat units that contain R 1 and R 2 may be at least 50%, 60%, 70%, 80%, 90%, 95%, 99%, or 100%.
  • a propargyl group may be present when R 1 or R 2 is a C3-C18 unsubstituted or substituted group, in which there is a terminal CoC bond.
  • Aromatic portions may be present, e.g.
  • the R group may be or include a phenyl group (e.g., phenyl ethenyl, phenyl allyl, etc.).
  • a Ci or C 2 unsubstituted or substituted group is structurally linear, while a C3-C18 unsubstituted or substituted group may be linear, cyclic, or branched.
  • the repeat units of the carbosilane above may be arranged as linear repeat units, cyclic repeat units, branched repeat units, or a combination thereof. Branched repeat units themselves may be linear or cyclic.
  • the molecule is depicted in a linear arrangement for convenience, without limitation.
  • the n repeat units are all connected linearly.
  • the n repeat units are connected within a cyclic molecule.
  • a “cyclic molecule” is a molecule within which there is at least one atomic ring that contains at least two Si-C bonds.
  • some of the n repeat units are connected within a cyclic portion of the molecule, while other of the n repeat units are connected within a linear portion of the molecule.
  • At least one of R 1 or R 2 is a UV-active functional group.
  • a “UV-active functional group” is a chemical group in the form of multiple atoms bonded together in a functional group that has absorption in the UV or visible region of electromagnetic radiation (wavelengths from about 100 nm to about 700 nm). Absorption (UV activity) occurs when a UV-active molecule absorbs ultraviolet or visible light that excites valence electrons, causing an electronic transition from a ground state to an excited state. UV absorption can be measured by a UV-visible spectrophotometer, which provides a spectrum of absorption versus wavelength.
  • a UV-active functional group selected from the group consisting of ethynyl, vinyl, allyl, acrylate, methacrylate, vinyl ether, epoxide, oxetane, thiol, thioketone, isothiocyanate, and combinations, analogues, or derivatives thereof that maintain UV activity.
  • the preceramic resin formulation may contain at least two distinct carbosilanes that are each in accordance with the chemical structure above, wherein R 1 , R 2 , and n are independently selected for the distinct carbosilanes.
  • the photoinitiator may be present in a concentration from about 0.001 wt% to about 10 wt% in the preceramic monomer formulation, for example.
  • the photoinitiator generates free radicals by intramolecular bond cleavage or intermolecular hydrogen abstraction when exposed to light having a wavelength from about 200 nm to about 500 nm.
  • the photoinitiator may be selected from the group consisting of 2,2- dimethoxy-2-phenylacetophenone, 2-hydroxy -2-methylpropiophenone, camphorquinone, bis(2,4,6-trimethylbenzoyl)-phenylphosphineoxide, benzophenone, benzoyl peroxide, and combinations thereof, for example.
  • the photoinitiator is a cationic photoinitiator, such as (but not limited to) sulphonium, iodonium, and/or ferrocenium cation paired with a non-nucleophilic anion.
  • the UV-curable resin may contain a salt which under light exposure creates acids (e.g., Bronsted acids) by cleavage of the sulphonium, iodonium, and/or ferrocenium cation of the onium salt, paired with a proton donor.
  • Cationic photoinitiators are typically active under light wavelengths from 200 nm to 350 nm.
  • Cationic photoinitiators may be used when the polymerization is, or includes, cationic polymerization. Different cationic photoinitiators or photoacid generators will generally result in different reaction rates for polymerization. A combination of different types of cationic photoinitiators (including ionic and non-ionic photoacid generators) may be used in the polymerization process.
  • Exemplary cationic photoinitiators include, but are not limited to, sulfonium, iodonium, and ferrocenium salts; cyclopentacienylcumene-iron hexafluoro phosphate; diphenyliodonium phosphate; triarylsulfonium hexafluoroantimonate; or a combination thereof.
  • the cationic photoinitiator when present, may be up to about 10 wt% of the monomer formulation. In various embodiments, the cationic photoinitiator is about 0.001, 0.005, 0.01, 0.05, 0.1, 0.5, 1, 2, 5, or 10 wt% of the monomer formulation.
  • a free-radical inhibitor may be present in a concentration from about
  • the free-radical inhibitor may be selected from the group consisting of hydroquinone, methylhydroquinone, ethylhydroquinone, methoxyhydroquinone, ethoxyhydroquinone, monomethylether hydroquinone, propylhydroquinone, propoxyhydroquinone, tert-butylhydroquinone, n-butylhydroquinone, and combinations thereof, for example.
  • the 3D-printing resolution agent may be present in a concentration from about 0.001 wt% to about 10 wt% in the preceramic resin formulation, for example.
  • the 3D-printing resolution agent may be selected from the group consisting of 2-(2-hydroxyphenyl)-benzotriazole, 2-hydroxyphenyl-benzophenones, 2-hydroxyphenyl-s-triazines, 2,2'-(2,5-thiophenediyl)bis(5-tert-butylbenzoxazole), 2,2'-(l,2-ethenediyl)bis(4,l-phenylene)bisbenzoxazole, and combinations thereof, for example.
  • the preceramic monomer formulation further comprises a thermal free-radical initiator, such as (but not limited to) a thermal free- radical initiator selected from the group consisting of benzoyl peroxide, dicumyl peroxide, 2,2'-azobisisobutyronitrile, and combinations thereof.
  • a thermal free-radical initiator such as (but not limited to) a thermal free- radical initiator selected from the group consisting of benzoyl peroxide, dicumyl peroxide, 2,2'-azobisisobutyronitrile, and combinations thereof.
  • the preceramic monomer formulation further comprises a radiation-trigger free-radical initiator active at a second wavelength that is substantially different from a first wavelength for which the photoinitiator is active.
  • the preceramic resin formulation may further contain a crosslinking agent, such as (but not limited to) a silazane.
  • a crosslinking agent may be selected from the group consisting of monovinyl silanes, divinylsilanes, trivinyl silanes, tetravinyl silanes, (meth)acryloxypropyldimethyl methoxy silane, (meth)acryloxypropylmethyldimethoxy silane, dimethyldivinylsilane, 1,3-divinyl- 1,1,3,3-tetramethyldisilazane, l,3,5,7-tetravinyl-l,3,5,7-tetramethylcyclotetrasilazane, 1,2,3,4,5,6,7,8-octamethylcyclotetrasilazane, and combinations thereof.
  • crosslinking agents are monomers or oligomers of silanes and/or hydrocarbons with UV-reactive functional groups (e.g., vinyl, vinyl ether, (meth)acrylate, glycidyl, or glycidyl ether).
  • UV-reactive functional groups e.g., vinyl, vinyl ether, (meth)acrylate, glycidyl, or glycidyl ether.
  • the preceramic monomer formulations may be loaded with a dissimilar solid material, or multiple solid materials, as solid-phase fillers to form polymer composite parts that can be directly converted to ceramic matrix composites (CMCs) via pyrolysis or other thermal treatment.
  • the solid-phase fillers may include fibers, whiskers, platelets, particles, nanoparticles, nanotubes, or other forms of materials which can at least partially survive the pyrolysis conditions.
  • Exemplary solid-phase fillers include, but are not limited to, carbides, oxides, nitrides, or carbon (such as diamond).
  • Certain exemplary solid-phase fillers include, but are not limited to, Si, SiC, C, A1 2 0 3 , Si0 2 , mullite (Al 2 0 3- Si0 2 ), Si 3 N 4 , SiAlON, BN, and/or YAG (Y 3 AI 5 O ).
  • the preceramic monomer formulation comprises from about 0.1 vol% to about 70 vol% of solid-phase fillers.
  • solid-phase fillers include, but are not limited to, Si, SiC, SiOC, SiCN, SiCBN, SiOCN, SiAlON, Si 3 N 4, Si0 2 , silicate glasses, zirconium hydride, and combinations thereof.
  • the preceramic monomer formulation may further comprise one or more surface-active agents in the form of surfactants, such as dispersants, emulsifiers, or wetting agents that decrease the interfacial tension between the optional solid fillers and the liquid resin, facilitating mixing and dispersing the solids within the resin matrix.
  • surfactants may reduce settling and agglomeration of (optional) solid fillers to improve the uniformity, stability, and shelf life of the UV-curable resin.
  • Surfactants contain a mixture of hydrophobic and hydrophilic functional groups that provide simultaneous adsorption onto multiple types of surfaces.
  • the hydrophobic functional groups may include, but are not limited to, hydrocarbon chains, fluorocarbon chains, siloxanes, or carbosilanes.
  • the hydrophilic functional groups may have a range of compositions based on the polarity (e.g., nonionic, anionic, cationic, or zwitterionic).
  • surfactants include, but are not limited to, carboxylates, sulfate esters, sulfonate esters, phosphates, quaternary ammonium salts, betaines, sultaines, ethoxylates, methoxysilanes, or a combination thereof. Multiple types of surfactants may be present.
  • the surfactant when included in the preceramic monomer formulation, may be present in a concentration from about 0.001 wt% to about 15 wt% in the preceramic monomer formulation. In various embodiments, the surfactant is in a concentration of about 0.005, 0.01, 0.1, 0.5, 1, 2, 5, or 10 wt% of the preceramic monomer formulation.
  • Some variations of the invention provide a preceramic polymer composition comprising functionalized polycarbosilane having the polymer structure: wherein:
  • R 1 is selected from the group consisting of hydrogen, a vinyl group, an allyl group, an ethynyl group, a Ci-Cis unsubstituted or substituted alkyl group, an ester group, an amine group, a hydroxyl group, a vinyl ether group, a vinyl ester group, a glycidyl group, a glycidyl ether group, a vinyl glycidyl ether group, a vinyl amide group, a vinyl triazine group, a vinyl isocyanurate group, an acrylate group, an alkacrylate group (e.g., methacrylate, ethacrylate, etc.), an alkyl alkacrylate group, a phenyl group, a halide group, a thiol group, an alkylthiol group, a thiol-containing group, a cyano group, a cyanate group, a thiocyanate group, a
  • R 2 is selected from the group consisting of hydrogen (except when R 1 is hydrogen), a vinyl group, an allyl group, an ethynyl group, a Ci-Cig unsubstituted or substituted alkyl group, an ester group, an amine group, a hydroxyl group, a vinyl ether group, a vinyl ester group, a glycidyl group, a glycidyl ether group, a vinyl glycidyl ether group, a vinyl amide group, a vinyl triazine group, a vinyl isocyanurate group, an acrylate group, a methacrylate group, an alkacrylate group, an alkyl alkacrylate group, a phenyl group, a halide group, a thiol group, an alkylthiol group, a thiol-containing group, a cyano group, a cyanate group, a thiocyanate group, a mercap
  • the repeat units of the polycarbosilane above may be arranged as linear repeat units, cyclic repeat units, branched repeat units, or a combination thereof. Branched repeat units themselves may be linear or cyclic.
  • the polymer is depicted in a linear arrangement for convenience, without limitation.
  • the n repeat units are all connected linearly.
  • the n repeat units are connected within a cyclic polymer.
  • some of the n repeat units are connected within a cyclic portion of the polymer, while other of the n repeat units are connected within a linear portion of the polymer.
  • R 1 and R 2 are not hydrogen. In preferred embodiments, neither R 1 nor R 2 is hydrogen. In some embodiments of the preceramic polymer composition, one of R 1 or R 2 is hydrogen.
  • the fraction of repeat units that contain R 1 and R 2 may be at least 50%, 60%, 70%, 80%, 90%, 95%, 99%, or 100%.
  • the preceramic polymer composition may contain at least two distinct polycarbosilane repeat units that are each in accordance with the above polymer structure, wherein R 1 , R 2 , and n are independently selected for the distinct polycarbosilane repeat units.
  • the preceramic polymer composition comprises a polycarbosilane copolymer having the copolymer structure: wherein: R 1 , R 2 , R 3 , and R 4 are independently selected from the group consisting of hydrogen, a vinyl group, an allyl group, an ethynyl group, a C
  • the copolymer is depicted in a linear arrangement for convenience, without limitation.
  • the n repeat units and m repeat units are all connected linearly.
  • some of the repeat units are connected within a cyclic portion of the copolymer, while other repeat units are connected within a linear portion of the copolymer.
  • the copolymer is depicted as a block copolymer; it will be understood that the copolymer may be an alternating copolymer or a random copolymer, for example.
  • An alternating copolymer may contain single repeat units with R 1 and R 2 alternating with single repeat units containing R 3 and R 4 , or may contain short blocks of repeat units containing R 1 and R 2 alternating with short blocks of repeat units containing R 3 and R 4 , for example.
  • the preceramic polymer composition comprises a functionalized polycarbosilane copolymer having the copolymer structure: wherein R 1 is hydrogen, R 2 is an allyl group, R 3 is hydrogen, and R 4 is a vinyl group.
  • R 1 is hydrogen
  • R 2 is an allyl group
  • R 3 is hydrogen
  • R 4 is a vinyl group.
  • the ratio of m to n may be from about 2 to about 20, for example.
  • an allyl group is a vinyl-containing group
  • a carbosilane polymer that is modified with vinyl groups and/or allyl groups may be referred to as a vinyl-functionalized polycarbosilane.
  • a carbosilane molecule that is modified with vinyl groups and/or allyl groups may be referred to as a vinyl- functionalized carbosilane.
  • An exemplary synthesis route for producing a vinyl- functionalized carbosilane or polycarbosilane includes reaction of halogenated silanes with vinyl Grignard reagents, allyl Grignard reagents, or a blend thereof, followed by reduction. See U.S. Patent No. 5,153,295, issued to Whitmarsh et al. on October 6, 1992, which is incorporated by reference herein.
  • the preceramic polymer composition comprises a functionalized polycarbosilane copolymer having the copolymer structure: wherein R 1 is hydrogen, R 2 is an allyl group, R 3 is an acrylate group, and R 4 is hydrogen.
  • the ratio of m to n may be from about 0.1 to about 10, for example.
  • a carbosilane polymer that is modified with acrylate groups and/or alkacrylate groups may be referred to as an acrylate-functionalized polycarbosilane.
  • the preceramic polymer composition comprises a functionalized polycarbosilane copolymer having the copolymer structure: wherein R 3 may be selected from Ci-Cig unsubstituted or substituted alkyl groups.
  • the ratio of m to n may be from about 0.1 to about 10, for example.
  • the preceramic polymer composition comprises a functionalized polycarbosilane copolymer having the copolymer structure: wherein R 3 may be selected from Ci-Cig unsubstituted or substituted alkyl groups.
  • R 3 may be selected from Ci-Cig unsubstituted or substituted alkyl groups.
  • the ratio of m to n may be from about 0.1 to about 10, for example.
  • the preceramic polymer composition comprises a functionalized polycarbosilane copolymer having the copolymer structure: wherein R 3 may be selected from Ci-Cig unsubstituted or substituted alkyl groups.
  • R 3 may be selected from Ci-Cig unsubstituted or substituted alkyl groups.
  • the ratio of m to n may be from about 0.1 to about 10, for example.
  • a carbosilane polymer that is modified with thiol groups may be referred to as a thiol-functionalized polycarbosilane.
  • a carbosilane molecule that is modified with thiol groups may be referred to as a thiol- functionalized carbosilane.
  • An exemplary synthesis route for producing a thiol- functionalized carbosilane or polycarbosilane involves reacting halogenated silanes with thiourea in aqueous base.
  • the preceramic polymer composition may further contain a crosslinking agent, such as (but not limited to) a silazane.
  • a crosslinking agent may be selected from the group consisting of monovinylsilanes, divinylsilanes, trivinylsilanes, tetravinyl silanes, (meth)acryloxypropyldimethyl methoxy silane, (meth)acryloxypropylmethyldimethoxy silane, dimethyldivinylsilane, 1 , 3 -di viny 1 - 1 , 1 , 3 , 3 -tetramethy 1 di sil azane, 1 , 3 , 5 , 7 -tetravinyl - 1 , 3 , 5 , 7- tetramethylcyclotetrasilazane, 1,2,3,4,5,6,7,8-octamethylcyclotetrasilazane, and combinations thereof
  • the preceramic polymer composition comprises copolymer repeat units that are different from the polycarbosilane repeat units.
  • the copolymer repeat units may be polycarbonitrosilane repeat units containing nitrogen bonded to silicon and/or carbon.
  • the nitrogen is bonded to a functional group selected from the group consisting of hydrogen, a vinyl group, an allyl group, an ethynyl group, a Ci-Cig unsubstituted or substituted alkyl group, an ester group, an amine group, a hydroxyl group, a vinyl ether group, a vinyl ester group, a glycidyl group, a glycidyl ether group, a vinyl glycidyl ether group, a vinyl amide group, a vinyl triazine group, a vinyl isocyanurate group, an acrylate group, an alkacrylate group, an alkyl alkacrylate group, a phenyl group, a halide group, a thiol group, a cyano group, a cyanate group, a thiocyanate group, and combinations thereof.
  • a functional group selected from the group consisting of hydrogen, a vinyl group, an allyl group, an
  • the preceramic polymer composition further contains a photoinitiator that was present in the starting preceramic resin formulation and remains in the final polymer, in original or reacted form.
  • the preceramic polymer composition further contains a free-radical inhibitor that was present in the starting preceramic resin formulation and remains in the final polymer, in original or reacted form.
  • the preceramic polymer composition further contains a 3D-printing resolution agent that was present in the starting preceramic resin formulation and remains in the final polymer, in original or reacted form.
  • the preceramic polymer composition further comprises from about 0.1 vol% to about 70 vol% of solid-phase fillers.
  • Exemplary solid-phase fillers may be selected from the group consisting of Si, SiC, SiOC, SiCN, SiCBN, SiOCN, SiAlON, S13N4, S1O2, silicate glasses, zirconium hydride, and combinations thereof.
  • rheology modifiers e.g., thickening or thinning agents
  • exemplary rheology modifiers include silica, alumina, kaolin clay, carbon black, and polyphosphates.
  • the ceramic material comprises interconnected three-dimensional ceramic matrix materials such as, but not limited to, silicon oxycarbide (SiOC), silicon carbide (SiC), silicon nitride (S1 3 N 4 ), silicon oxynitride (SiON), silicon oxycarbonitride (SiOCN), silicon carbonitride (SiCN), silicon boronitride (SiBN), silicon boron carbonitride (SiBCN), boron nitride (BN), and/or silicon carbide-zirconium oxide composites (SiC/ZrCE).
  • SiOC silicon oxycarbide
  • SiC silicon carbide
  • SiN silicon nitride
  • SiON silicon oxycarbonitride
  • SiCN silicon carbonitride
  • SiBN silicon boronitride
  • SiBCN silicon boron carbonitride
  • BN boron nitride
  • BN silicon carbide-zirconium oxide composites
  • the preceramic polymer composition may be a 3D-printed polymer, which may be thermally treated to fabricate a 3D-printed ceramic part, as will be described in further detail later in this specification.
  • the first molecule may contain different combinations of these different unsaturated bonds.
  • the first molecule also contains at least one non carbon atom in the main chain or side chains of the first molecule.
  • non carbon atoms examples include, but are not limited to, Si, B, Al, Ti, Zn, O, N, P, S, Ge, and combinations thereof.
  • the non-carbon atoms may be a part of cyclic or acyclic groups or structures within the first molecule.
  • the non-carbon atoms are preferably not merely single non-carbon atoms ionically bonded at the end(s) of the first molecule.
  • Examples of the first molecules include, but are not limited to, trivinylborazine; 2,4,6-trimethyl-2,4,6-trivinylcyclotrisilazane; 1,3,5,7-tetravinyl-
  • the first molecule when present, may be up to about 100 wt% of the monomer formulation. In various embodiments, the first molecule is about 5, 10, 20, 30, 40, 50, 60, 70, 80, 90, or 95 wt% of the monomer formulation.
  • the molecules R-Y-H can provide two or more YH groups for polymerization, and can be part of cyclic or acyclic structures.
  • Typical YH groups are SH groups, e.g. thiol or mercapto groups.
  • the R groups can be organic groups such as alkyl groups, ester groups, amine groups, or hydroxyl groups, or inorganic non- carbon-containing atoms or groups.
  • inorganic non-carbon atoms or groups in the second molecule include, but are not limited to, Si, B, Al, Ti, Zn, P, Ge, S, O, N, or combinations thereof.
  • the reaction rate varies depending on the different molecules utilized.
  • a thiol is employed with at least half of the main chain made of inorganic atoms, such as silicon.
  • Other atoms in the main chain may include oxygen, nitrogen, and/or carbon.
  • the second molecule when present, may be up to about 97 wt% of the monomer formulation. In various embodiments, the second molecule is about 0, 5,
  • the second molecule may be present whether or not the first molecule is present.
  • Exemplary second molecule include, but are not limited to, pentaerythritol tetrakis(3-mercaptopropionate); trimethylolpropanetris(2- mercaptoacetate); trimethylolpropane tris(3-mercaptopropionate); tetrakis(dimethyl-3- mercaptopropylsiloxy)silane; tetrakis(dimethyl-2-mercaptoacetate siloxy)silane; (mercaptopropyl)methylsiloxane-dimethylsiloxane copolymer; (mercaptopropyl)methylsiloxane homopolymer; pentaerythritol tetrakis(2- mercaptoacetate), thiol-functionalized polycarbosilane; or a combination thereof.
  • the UV-curable monomer formulation comprises a third molecule with a structure R-Y, wherein Y is selected from an aliphatic ether, a cyclic ether, a vinyl ether, an epoxy, a cycloaliphatic epoxy, an oxetane group, or a combination thereof.
  • the R groups may be selected from organic groups such as alkyl groups, ester groups, amine groups, or hydroxyl groups, or inorganic non-carbon containing atoms or groups. Examples of inorganic non-carbon atoms or groups in the second molecule include, but are not limited to, Si, B, Al, Ti, Zn, P, Ge, S, O, N, or combinations thereof.
  • the inorganic non-carbon atoms or groups may be a part of cyclic or acyclic structures.
  • Exemplary third molecules include, but are not limited to, epoxy functional dimethylpolysiloxane and/or epoxycyclohexylethyl methylsiloxane/dimethylsiloxane. These monomers can be any portion of the monomer formulation.
  • the third molecule when present, may be up to about 100 wt% of the monomer formulation. In various embodiments, the third molecule is about 5, 10, 20, 30, 40, 50, 60, 70, 80, 90, or 95 wt% of the monomer formulation.
  • the third molecule may be present whether or not the first or second molecules are present.
  • the UV-curable monomer formulation comprises a photoinitiator that generates free radicals under light exposure by intramolecular bond cleavage or intermolecular hydrogen abstraction.
  • the photoinitiator may be active in the presence of light having a wavelength from about 200 nm to about 500 nm, for example.
  • Photoinitiators may be used when the polymerization is, or includes, free-radical polymerization. Photoinitiators may be used to initiate polymerization when exposed to other wavelengths, such as in the visible spectrum.
  • light exposure is produced from light having one or more wavelengths selected from about 200 nm to about 700 nm, such as about 250, 300, 350, 400, 500, or 600 nm.
  • photoinitiators will generally result in different reaction rates for polymerization.
  • a combination of different types of photoinitiators may be used in the polymerization process. More than one photoinitiator may be included to allow multi -wavelength curing, for example.
  • photoinitiators include, but are not limited to, 2,2- dimethoxy-2-phenylacetophenone; 2-hydroxy-2-methylpropiophenone; camphorquinone; bis(2,4,6-trimethylbenzoyl)-phenylphosphineoxide; benzophenone; benzoyl peroxide; thioxanones; dicumyl peroxide; 2,2'-azobisisobutyronitrile; camphorquinone; oxygen; nitrogen dioxide; or a combination thereof.
  • the photoinitiator when present, may be up to about 10 wt% of the monomer formulation. In various embodiments, the photoinitiator is about 0.001, 0.005, 0.01, 0.05, 0.1, 0.5, 1, 2, 5, or 10 wt% of the monomer formulation.
  • the UV-curable monomer formulation comprises a free-radical inhibitor added in a sufficient amount to the monomer formulation to inhibit unwanted polymerization of regions outside the desired printing area.
  • a free-radical inhibitor can improve resolution to the desired part in embodiments that employ free-radical polymerization.
  • a free-radical inhibitor can also deter shadow curing, which is normally not desired. Additionally, a free-radical inhibitor can improve long-term stability of the formulation and keep reaction kinetic parameters constant over time.
  • Exemplary free-radical inhibitors include, but are not limited to, hydroquinone, methylhydroquinone, ethylhydroquinone, methoxyhydroquinone, ethoxyhydroquinone, monomethyl ether hydroquinone, propylhydroquinone, propoxyhydroquinone, tert-butylhydroquinone, n-butylhydroquinone, or a combination thereof.
  • the free-radical inhibitor may be up to about 5 wt% of the monomer formulation, such as about 0.001, 0.005, 0.01, 0.05, 0.1, 0.2, 0.5, 1, or 2 wt% of the monomer formulation.
  • the formulation further includes a radiation-trigger free- radical initiator that is active at a wavelength substantially different from the photoinitiator.
  • the preceramic resin formulation includes a thermal free-radical initiator
  • the formulation further includes a radiation-trigger free-radical initiator.
  • the UV-curable monomer formulation comprises a free-radical thermal initiator that generates free radicals under elevated temperature conditions.
  • a free-radical thermal initiator allows for multiple-mechanism curing in the formulation, i.e., both UV curing and thermal curing, or allows for a different polymerization reaction rate.
  • One or a combination of different types of thermal initiators may be used in the polymerization process.
  • a thermal initiator may be used to crosslink unreacted vinyl groups remaining which have not reacted with the thiol group or to react the vinyl group with other available functional groups such as methyl or hydro groups on the first or second molecule, creating a second type of reaction mechanism.
  • a thermal post-cure after 3D printing may be done, such as by heating the polymer structure up to 300°C.
  • exemplary free-radical thermal initiators include, but are not limited to, benzoyl peroxide, dicumyl peroxide, 2,2'-azobisisobutyronitrile, or a combination thereof. When present, the free-radical thermal initiator may be up to about 10 wt% of the monomer formulation, such as about 0.001, 0.01, 0.1, 1, 2, or 5 wt% of the monomer formulation.
  • the UV-curable monomer formulation comprises a photoinitiator that is a cationic photoinitiator or photoacid generator, such as (but not limited to) sulphonium, iodonium, and/or ferrocenium cation paired with a non-nucleophilic anion.
  • the UV-curable resin may contain a salt which under light exposure creates acids (e.g., Bronsted acids) by cleavage of the sulphonium, iodonium, and/or ferrocenium cation of the onium salt, paired with a proton donor.
  • Cationic photoinitiators are typically active under light wavelengths from 200 nm to 350 nm.
  • Ionic photoacid generators may be used when the polymerization is, or includes, cationic polymerization. Different cationic photoinitiators or photoacid generators will generally result in different reaction rates for polymerization. A combination of different types of cationic photoinitiators (including ionic and non-ionic photoacid generators) may be used in the polymerization process.
  • Exemplary cationic photoinitiators include, but are not limited to, sulfonium, iodonium, and ferrocenium salts; cyclopentacienylcumene-iron hexafluoro phosphate; diphenyliodonium phosphate; triarylsulfonium hexafluoroantimonate; or a combination thereof.
  • the cationic photoinitiator when present, may be up to about 10 wt% of the monomer formulation. In various embodiments, the cationic photoinitiator is about 0.001, 0.005, 0.01, 0.05, 0.1, 0.5, 1, 2, 5, or 10 wt% of the monomer formulation.
  • the UV-curable monomer formulation comprises a hydrogen donor that may be used to assist in the generation of a Bronsted acid in the cation or in acceleration of anionic photoinitiator reactions, for example.
  • Exemplary hydrogen donors include, but are not limited to, tertiary amines, alcohols, ethers, esters, water, or a combination thereof. When present, the hydrogen donor may be up to about 2 wt% of the monomer formulation, such as about 0.001, 0.005, 0.01, 0.05, 0.1, 0.5, 1, or 1.5 wt% of the monomer formulation.
  • the UV-curable monomer formulation comprises a UV sensitizer that may be used to enable the long-UV-wavelength reaction of UV systems with photoinitiators which typically absorb at lower wavelengths. This is typically the case with cationic photoinitiators, which are generally limited to absorption up to about 325-375 nm, for example.
  • UV sensitizers interact with UV light at higher wavelengths, generally into the 375-425 nm range, and then interact with the photoinitiator to create either free radicals and/or Bronsted acids.
  • a UV sensitizer forms an excited triplet state under UV light absorption, and then via electron or energy transfer, reacts with a photoinitiator to generate free radicals and/or Bronsted acids. This initiates photopolymerizaton.
  • UV sensitizers may be selected from dibutoxyantracene, diethoxyanthracene, l-chloro-4-propoxythioxanthone, 2-isopropylthioxanthone, 4- isopropylthioxanthone, or a combination thereof, for example.
  • the UV sensitizer may be up to about 5 wt% of the monomer formulation, such as about 0.001, 0.005, 0.01, 0.05, 0.1, 0.5, 1, 2, 3, or 4 wt% of the monomer formulation.
  • the UV-curable monomer formulation comprises one or more 3D-printing resolution agents selected from UV absorbers, fluorescents, optical brighteners, or a combination thereof.
  • a “3D-printing resolution agent” is a compound that improves print quality and resolution by containing the curing to a desired region of the laser or light exposure.
  • the 3D-printing resolution agent functions by absorbing light (e.g., UV or visible light) at a desired wavelength and converting the energy either into thermal energy or radiation at a higher wavelength.
  • the use of 3D- printing resolution agents improves print quality and resolution by containing the curing by the laser or light exposure to the desired region laterally and/or vertically in the print bath.
  • Exemplary 3D-printing resolution agents include, but are not limited to, 2-(2-hydroxyphenyl)-benzotriazole; 2-hydroxyphenyl-benzophenones; 2- hydroxyphenyl-s-triazines; 2,2'-(2,5-thiophenediyl)bis(5-tert-butylbenzoxazole); 2,2'- (l,2-ethenediyl)bis(4,l-phenylene)bisbenzoxazole; or a combination thereof.
  • the 3D-printing resolution agent may be up to about 10 wt% of the monomer formulation, such as about 0.001, 0.01, 0.1, 0.5, 1, 2, 3, 4, 5, 6, 7, 8, or 9 wt% of the monomer formulation.
  • R-Y-H optionally a second molecule comprising R-Y-H, wherein R is an organic group or an inorganic group, and wherein Y is selected from the group consisting of S, N, O, and combinations thereof (Y is not yttrium in this specification);
  • the first molecule is present from about 3 wt% to about 97 wt% of the formulation, such as about 4, 5, 10, 15, 20, 25, 30, 35, 40, 45, 50, 55, 60, 65, 70, 75, 80, 85, 90, or 95 wt%, for example.
  • the non-carbon atom may be present in the main chain, in side chains, or in both of these.
  • the first molecule may include one or more functional groups selected from the group consisting of vinyl, ethynyl, vinyl ether, vinyl ester, vinyl amide, vinyl triazine, vinyl isocyanurate, acrylate, methacrylate, diene, triene, and analogues thereof.
  • the first molecule includes two or more of such functional groups.
  • An “analogue” herein means that the functional group has similar chemical and reactive properties, with respect to the polymerization of the preceramic resin formulation.
  • the second molecule is included in the preceramic resin formulation, the second molecule is present from about 0.1 wt% to about 97 wt% of the formulation, such as about 0.2, 0.5, 1, 2, 3, 4, 5, 10, 15, 20, 25,
  • the second molecule may include one or more functional groups selected from the group consisting of thiol, alkyl, ester, amine, hydroxyl, and functional analogs thereof. Alternatively, or additionally, the second molecule may be chemically contained within one or more functional groups selected from the group consisting of thiol, alkyl, ester, amine, hydroxyl, and analogues thereof.
  • the R group may be, or include, an inorganic group containing an element selected from the group consisting of Si, B, Al, Ti, Zn, P, Ge, S, N, O, and combinations thereof.
  • At least 5%, 10%, 15%, 20%, 25%, 30%, 35%, 40%, 45%, or 50% (mole percent) of the R group is inorganic, i.e. not carbon. In certain embodiments, at least 5%, 10%, 15%, 20%, 25%, 30%, 35%, 40%, 45%, or 50% (mole percent) of the R group is specifically Si.
  • the R group may be present in the main chain, in side chains, or in both of these.
  • the non-carbon atom of the R group when it is inorganic, may be the same as or different than the non-carbon atom in the first molecule.
  • the weight ratio of the second molecule to the first molecule may vary from about 0 to about 32, such as about 0.5, 1, 2, 3, 5, 10, 15, 20, 25, or 30. In some embodiments, the weight ratio of second molecule to first molecule is dependent on the ratio of thiol to vinyl. For example, in certain embodiments there is at least one thiol functional group available per vinyl group.
  • a preceramic monomer formulation compatible with stereolithography or UV-cure 3D printing leverages both cationic and free-radical polymerization mechanisms, wherein the formulation comprises:
  • a second molecule comprising two or more thiol or mercapto (SH) groups, wherein the second molecule further comprises at least one non-carbon atom in the main chain or side chains selected from the group consisting of Si, B, Al, Ti,
  • Zn, P, S Ge, and combinations thereof preferably at least 10 wt%, more preferably at least 40 wt%, of the non-carbon atoms being inorganic, such as Si
  • the second molecule may be a part of an alkyl group, ester group, amine group, or hydroxy group;
  • a third molecule comprising two or more functional groups selected from aliphatic ether, cyclic ether, vinyl ether, epoxy, cycloaliphatic epoxy, oxcetane, or a combination thereof, wherein the third molecule further contains at least one non carbon atom in the main chain or side chains selected from the group consisting of Si, B, Al, Ti, Zn, P, S, Ge, and combinations thereof;
  • UV absorbers, fluorescents, and/or optical brighteners added in a sufficient amount to the monomer formulation to improve print quality and resolution by containing the curing to the region of the laser or light exposure to the desired region;
  • the UV-curable monomer formulation further comprises one or more solid-phase fillers.
  • a “solid-phase filler” as meant herein is a material that (a) forms at least one solid phase at 25°C and 1 bar, and (b) enhances at least one chemical, physical, mechanical, or electrical property within the UV-curable monomer formulation or a reaction product thereof.
  • a solid-phase filler is not merely a low-cost, diluent material (known also as extenders) but rather an important component of some formulations disclosed herein.
  • the solid-phase filler may be from about 0.1 vol% or about 1 vol% to about 70 vol% of the monomer formulation, with the majority of the remainder typically being liquid-phase UV-curable monomer.
  • the geometric shape of the solid-phase filler may be fibers including short fibers (1-100 micrometers in length) or long fibers (>100 micrometers in length), whiskers, nanotubes, nanorods, flat platelets, microparticles with diameters between 1 and 100 micrometers, nanoparticles with diameters between 1 and 1000 nanometers, or a combination thereof.
  • Particle sizes may be measured by a variety of techniques, including dynamic light scattering, laser diffraction, image analysis, or sieve separation, for example.
  • Dynamic light scattering is a non-invasive, well-established technique for measuring the size and size distribution of particles typically in the submicron region, and with the latest technology down to 1 nanometer.
  • Laser diffraction is a widely used particle-sizing technique for materials ranging from hundreds of nanometers up to several millimeters in size.
  • Exemplary dynamic light scattering instruments and laser diffraction instruments for measuring particle sizes are available from Malvern Instruments Ltd., Worcestershire, UK.
  • Image analysis to estimate particle sizes and distributions can be done directly on photomicrographs, scanning electron micrographs, or other images.
  • sieving is a conventional technique of identifying particles by size.
  • solid-phase fillers with aspect ratios of at least 2 are preferred, such as fibers, whiskers, nanotubes, and nanorods.
  • aspect ratio is the ratio of average length to average width, or in the case of an arbitrary shape, the ratio of average maximum length scale to average minimum length scale.
  • the solid-phase filler aspect ratio is preferably at least 5, more preferably at least 10, in certain embodiments.
  • the solid-phase filler composition is preferably stable at a pyrolysis temperature of at least 800°C, so as not to disintegrate, melt, or vaporize during later conversion of a preceramic polymer to a ceramic material.
  • the solid-phase filler may react at pyrolysis temperatures with other components present in the monomer formulation or its reaction products (e.g., polymer) or with furnace atmosphere gases. It is possible for a portion of the solid-phase filler to react away into the vapor phase, or into a liquid phase, during high-temperature processing.
  • a solid-phase filler precursor is introduced to the monomer formulation, wherein the precursor is in a liquid phase or is a gel, for example. The solid-phase filler precursor may then react or undergo a phase change, such as during polymerization, to convert the solid-phase filler precursor into a solid- phase filler.
  • the solid-phase filler may have a wide range of compositions.
  • solid-phase filler compositions may include, but are not limited to, silicon- based ceramics such as SiOC, Si0 2 , SiCN, SiC, SiCBN, SiOCN, Si 3 N 4 , silicate glasses, etc.
  • Solid-phase filler compositions may include non-silicon-based ceramics such as metal oxides, e.g. A1 2 0 3 , Zr0 2 , Ti0 2 , or Y 3 A1 5 0 I2.
  • Solid-phase filler compositions may include carbon-based, high-temperature materials such as carbon, graphene, diamond, and metal carbides, e.g. TiC, ZrC, HfC, or B C.
  • Solid-phase filler compositions may include nitride-based ceramics, e.g. BN, TiN, ZrN, or AIN.
  • Solid-phase fillers interact with UV light according to Snell’s law and the well-known Fresnel equations. These laws of physics determine the fractions of the light that are reflected, transmitted, or absorbed when UV light passes from resin to filler. For a UV-based 3D printing process, it is preferred that the fillers do not absorb too much UV light which would hinder complete UV curing of the resin. To avoid absorption of too much UV light, a low level of solid-phase filler may be employed, such as less than 10 vol% of relatively small (e.g., 10 micron or smaller) particles.
  • a solid-phase filler that is somewhat transparent to UV light and lets UV light pass through, may be employed.
  • Another approach to ensure that UV light is not excessively absorbed by the filler particles is to employ particles with a surface that reflects UV light.
  • a surface that reflects UV light For example, aluminum reflects UV light well. For maximum reflection, the surface of such particle should be smooth. Surface treatments or coatings may be applied to render the surface of filler particles reflective — such as a thin coating of aluminum or silver.
  • Preferred solid-phase filler materials are short fibers of alumina (AI2O3), quartz (S1O2), glass, silicon nitride (S13N4), yttrium aluminum garnet (YAG), or boron nitride (BN) because these materials transmit at least some UV light.
  • SiC or C fibers absorb too much UV light and therefore should to be coated with a reflective coating, to enable efficient 3D printing.
  • the solid-phase filler may be treated to increase its compatibility with and wetting of the resin, the solubility and dispersion of the filler in the resin, and/or the bonding between the filler and the resin.
  • dispersion aides may be chosen to match the isoelectric point of the solid-phase filler particle and the chemistry and functionality of the monomer resin.
  • Some embodiments employ surfactants with a component which bonds to the surface of the filler and a component which solvates in the resin system.
  • Surface functionality may be added to the surface of the solid-phase filler by covalently bonding a functional group to the surface of the filler.
  • Examples include the use of silane surface modifiers with active groups that can either react with the chemistry of the resin or increase the wettability and dispersability in the solid-phase filler. These include the addition of mercapto trimethoxy silane, vinyl trimethoxy silane, 3-glycidyl oxypropyl trimethoxy silane, or a combination thereof, for example.
  • the surface may also be modified through other chemical means, such as vapor-solid reactions or liquid-solid reactions, e.g. oxidation in a furnace or acid or base treatments.
  • the solid-phase filler itself is coated or surface-treated with a chemical that contains a functional group that aids in polymerization or crosslinking of the resin on UV and/or thermal exposure.
  • a functional group that aids in polymerization or crosslinking of the resin on UV and/or thermal exposure.
  • Such functional groups include unsaturated ethers, vinyls, acrylates, methacrylates, cyclic ethers, epoxies, oxetanes, amines, hydroxyls, isocyanates, hydrides, or combinations thereof.
  • functional groups introduced to the surface of the solid-phase filler particles may enable a thermal cure after initial UV curing during 3D printing.
  • the solid-phase filler may be coated to protect it from environmental degradation during pyrolysis.
  • Reactive species such as oxygen free radicals, and other free radicals, may be generated during the pyrolysis.
  • free radicals can react with the fillers and degrade their properties.
  • the fillers may be coated with a thin layer of a protective material such as BN or a sacrificial material such as pyrolytic carbon that preferentially decomposes during pyrolysis.
  • a high-aspect-ratio filler such as a fiber
  • a filler/matrix interfacial coating may be coated with a filler/matrix interfacial coating.
  • the purpose of this coating is to provide a weak filler-matrix interface that prevents matrix cracks from penetrating the fillers — thus providing damage tolerance (toughness) to the composite.
  • the interfacial coating is preferably chemically and mechanically stable during processing and pyrolysis. Examples of interfacial coatings include BN, C, AIN, or a combination thereof.
  • the formulations disclosed herein may be 3D printed using many different methods.
  • the formulations may be directly 3D printed and converted to tree-form ceramic matrix composite structures.
  • a 3D-printed preceramic polymer material may be prepared directly from preceramic monomer formulations, with no intervening steps being necessary.
  • a 3D-printed ceramic material may then be prepared directly from the 3D-printed preceramic polymer material, with no intervening steps being necessary.
  • Preferred methods may include stereolithography, binder jetting, resin jetting with fiber placement, polyjetting, extrusion printing, or a combination thereof.
  • stereolithography the solid-phase filler is dispersed in the liquid resin (monomer formulation). Layers are cured from the top or bottom using UV- laser rastering, projection micro-stereolithography, digital light projection, or liquid crystal device projection, for example. Smaller filler sizes are preferred since the filler size often limits the resolution, depending on material choice.
  • jetting of a material means that droplets of a build material are selectively deposited onto a build bed to develop a three- dimensional object. Jetting can be carried out by liquid deposition, vapor deposition, or liquid-vapor mist deposition, for example, via spraying (such as via a nozzle in communication with a material under pressure), impingement (such as via a tube or pipe in communication with a material that is pumped), or other means.
  • binder jetting a layer of the solid-phase filler is spread out and resin (monomer formulation) is jetted on selected locations and cured such as via UV light or thermally.
  • resin monomer formulation
  • This process is similar to conventional binder jetting methods, but instead of a binder, a preceramic monomer formulation is used.
  • the solid-phase filler may initially be spread out on a substrate or on a region of polymer based on the selected monomer, for example. After an initial step of binder jetting, another layer of the solid-phase filler may be spread out on a 3D-printed polymer layer, followed by resin jetting and curing. This process may be repeated many times for large parts.
  • resin jetting with fiber placement solid-phase fillers in the form of long or short fibers are placed in the preferred location and aligned in the preferred direction. Subsequently, preceramic resin (monomer formulation) is jetted in selected locations and cured. The process is repeated layer-by-layer to build a part. Resin jetting with fiber placement enables printing of parts with high volume fraction (such as 30-60 vol%) of aligned fibers, resulting in improved mechanical properties for the final ceramic structure (following pyrolysis).
  • the resin and filler mixture is squeezed through a micro-nozzle, or multiple micro-nozzles, and cured via UV light.
  • One advantage is that high-aspect-ratio fillers can be aligned with the extrusion process. Alignment generally improves mechanical properties in the aligned direction.
  • the part may be post-cured.
  • An optional thermal post-cure of the 3D polymer is performed after the 3D printing but prior to the pyrolysis to produce the ceramic structure.
  • a post-cure step may be employed to crosslink unreacted functional groups, for example.
  • Post-curing may be accomplished by additional UV exposure and/or a thermal post-cure at elevated temperatures (such as 60-500°C) in an oven for about 10 minutes to about 8 hours.
  • elevated temperatures such as 60-500°C
  • a monomer formulation is conveyed (printed) to a region of interest, such as via stereolithography, binder jetting, resin jetting with fiber placement, polyjetting, or extrusion printing, either followed by polymerization or with polymerization taking place simultaneously with the printing.
  • the polymerizing and 3D printing steps are performed simultaneously, at a desired location (e.g., a layer) within a part.
  • the polymerizing and 3D printing steps are performed semi-simultaneously, in which multiple steps are performed overall while at each step, some amount of polymerizing and some amount of 3D printing takes place. It is also possible, in some embodiments, to first polymerize a preceramic resin formulation, followed by 3D printing of the already- made polymer — especially when the polymer is a thermoplastic material.
  • the curing or conversion of preceramic resin formulation to preceramic polymer includes crosslinking.
  • a crosslink is a bond that links one polymer chain to another.
  • Crosslink bonds can be covalent bonds or ionic bonds. When polymer chains are linked together by crosslinks, they lose some of their ability to move as individual polymer chains.
  • Crosslinks are the characteristic property of thermosetting plastic materials. In most cases, crosslinking is irreversible, unless ionic bonds are employed in reversible crosslinks (see, for example, commonly owned U.S. Patent App. No. 15/391,749, filed December 27, 2016, which is hereby incorporated by reference herein).
  • a gel is formed first. Gel formation is followed by formation of a solid material as the monomer conversion is further increased, to crosslink chains together.
  • a “gel” is a solid, jelly-like material that can have properties ranging from soft and weak to hard and tough. Gels exhibit no flow when in the steady-state. By weight, gels are mostly liquid, yet they behave like solids due to a three-dimensional crosslinked network within the liquid.
  • Some variations of the invention utilize a self-propagating polymer waveguide, as described in commonly owned U.S. Patent No. 7,687,132 issued March 30, 2010 to Gross et ah; U.S. Patent No. 9,341,775 issued May 17, 2016 to Eckel et ah; U.S. Patent No. 9,377,567 issued June 28, 2016 to Jacobsen et ah; and U.S. Patent No. 9,528,776 issued December 27, 2016 to Roper et ah, which are hereby incorporated by reference herein. Without being limited by speculation or theory, it is hypothesized that initial exposure of monomer to a collimated beam can initiate microgel sites within the liquid monomer layer.
  • microgel sites have a higher crosslink density than the surrounding monomer/polymer, which leads to a higher localized refractive index.
  • the higher refractive index at the microgel site may act as a lens.
  • the focused energy from the incident beam leads to initial “waveguide” formation in the direction of the incident (primary) beam, where the refractive index of the waveguide is higher than the surrounding monomer/polymer.
  • U.S. Patent No. 7,382,959 issued June 3, 2008 to Jacobsen is hereby incorporated by reference herein for its description of mechanisms involving self-propagating polymer waveguide formation.
  • sufficient polymerization inhibitor and UV absorber are added to the resin formulation to confine the polymerization to the laser exposure point and to minimize scatter, thus maintaining fidelity in the features of the printed part. UV light is then scanned across the resin surface to expose a cross section and build up a thin slice of the part to be manufactured.
  • any geometry can be fabricated with this approach, the process can be slow, because every thin layer has to be exposed separately.
  • Structures with linear features extending from the exposure surface can be formed much more rapidly when utilizing the self-propagating photopolymer waveguide technology.
  • Monomers are selected to promote a change in the index of refraction upon polymerization, which causes internal reflection of the UV light, trapping it in the already -formed polymer. This exploits a self-focusing effect that forms a polymer waveguide, tunneling the light toward the tip of the waveguide and causing it to polymerize further. There is a reduced need for additives that control scatter and UV absorption.
  • the architecture of the material or structure can then be defined by a patterned mask that defines the areas exposed to a collimated UV light source, for example.
  • the polymer crosslink density depends on exposure parameters and can be increased by thermal treatments or additional UV exposure. Unpolymerized resin may be recycled and reused.
  • the direct, near-net-shape conversion of a preceramic 3D-printed polymer to a ceramic structure may be achieved by pyrolysis or other thermal treatment, such as (but not limited to) sintering, annealing, or calcination.
  • the thermal treatment is based on heating the 3D-printed structure for an extended period of time (such as from 10 minutes to 1 week) under various inert or reactive atmospheres.
  • Thermal treatment may be done for an extended period of time under various atmospheres, including but not limited to N 2 , Ar, He, air, C0 2 , CH 4 , C 2 H 6 , C 2 H 4 , N3 ⁇ 4, or a combination thereof.
  • Treatment pressures may vary from about 1 atm to about 20 atm, for example.
  • Vacuum pyrolysis may also be employed, in which the treatment pressure is less than 1 atm, again under various atmospheres as noted above.
  • the pyrolysis or other thermal treatment may include heating at a heating rate of 0.1-20°C/min from ambient temperature to an elevated temperature from about 500°C to about 1500°C, such as from about 800°C to about 1100°C.
  • the pyrolysis or other thermal treatment may also include dwelling at the elevated temperature (e.g., 950°C) for at least 1, 5, 10, 15, 30, or 60 minutes.
  • the material may be cooled at a cooling rate (magnitude) of 0. l-20°C/min back to ambient temperature.
  • faster cooling e.g., higher than 20°C/min in magnitude
  • the thermal treatment is preferably performed following polymerization and any (optional) thermal post-cure of the 3D polymer.
  • the thermal treatment is combined (i.e., overlaps in time and/or temperature) with polymerization, thermal post-cure, or both. It will also be recognized that even when a sequential operation is intended, some amount of ceramic formation may occur prior to a planned step of thermal treatment, as a result of the intrinsic kinetics and thermodynamics of the reaction system.
  • a reactive thermal treatment is performed, in which the gas that is initially present is reactive toward the initial polymer, the final ceramic material, or both of these.
  • the gas When the gas is reactive, it may react with a component and cause it to leave the material. Alternatively, or additionally, the gas may react with a component and remain with the base material. It is also possible for the gas to react and form products, some of which depart from the material while the rest remains with the material.
  • Reactive gases may be selected from O2, O3, air, CO, CO2, H 2 , H 2 0, CH4, SO2, H 2 S, NH3, NO, NO2, and N2O, and so on.
  • the maximum temperature for reactive thermal treatment may be, for example, about 300°C to about 1500°C.
  • the system pressure may also be adjusted to influence the gas atmosphere.
  • the pyrolysis or other thermal treatment process produces a ceramic part or ceramic matrix composite which may include various ceramic materials such as, but not limited to, SiC, SiOC, Si 3 N 4 , SiON, SiCN, SiOCN, SiBN, SiBCN, BN, or a combination thereof.
  • the composition of the ceramic part or ceramic matrix composite obviously is directly dependent on the composition of the starting 3D- printing monomer formulation as provided in this disclosure.
  • the fraction of carbon may be tailored, for example, by adding phenyl groups on the side chain of the polymer or by using a carbon-based crosslinking agent such as divinyl benzene.
  • final ceramic structures are lightweight, strong, and stiff — but can withstand a high-temperature oxidizing environment.
  • the configuration and microstructure of the preceramic polymer determine the composition, microstructure, and yield of the ceramic material after thermal treatment.
  • a high crosslink density is preferred to prevent the fragmentation and loss of low-molecular-mass species, which have not fully converted to either ceramic or escaping gases, during thermal treatment.
  • the escaping gases or vapors may include (but are by no means limited to) CH 4 , 3 ⁇ 4, CO, C0 2 , H 2 0, S0 2 , H 2 S, CH 3 S, etc.
  • the concentration of the solid-phase filler will typically be higher in the final ceramic material, compared to the starting 3D-printing monomer formulation. This is because the solid-phase filler is typically very stable during thermal treatment and does not lose much, if any, mass, while the polymer typically loses a significant amount of mass in pyrolysis (for example, see FIG. 3). Therefore, the concentration of solid-phase filler may be greater than 70 vol% in the final ceramic structure.
  • the concentration of solid-phase filler is from about 0.1 vol% to about 90 vol%, such as about 0.5, 1, 5, 10, 20, 30, 40, 50, 60, 70, or 80 vol% on the basis of the total ceramic structure following thermal treatment and any post processing (e.g., washing).
  • solid-phase functional additives are employed as the solid-phase fillers.
  • solid-phase functional additives it is meant a material that (a) forms at least one solid phase at 25°C and 1 atm, and (b) performs or enhances at least one chemical, physical, mechanical, electrical, or magnetic function within the ceramic structure as it is being formed and in the final structure.
  • solid-phase functional additives are distinguished from the solid-phase fillers disclosed above. Compared to solid-phase fillers , solid-phase functional additives actively improve the final ceramic structure through one or more changes explicitly induced by the additives during pyrolysis or other thermal treatment, as will now be described.
  • the solid-phase functional additives may be present from about 0.1 vol% and 70 vol% of the monomer formulation, with the majority of the remainder being liquid UV-curable resin.
  • the solid-phase functional additive geometry varies.
  • the solid-phase functional additives are small particles with average sizes (length or effective diameter) from 5 nanometers to 5 micrometers. [00208] In some embodiments, the solid-phase functional additives actively expand in volume and counteract the shrinkage of the resin, eliminating or reducing the overall shrinkage during conversion of the polymer to ceramic. This addresses a significant shortcoming in the art.
  • the overall shrinkage during conversion of the polymer to ceramic can be reduced or even eliminated.
  • the solid-phase functional additives are not necessarily stable (unreactive) at pyrolysis temperatures. In many case, it is desired that the functional additives are reactive.
  • the solid-phase functional additives may react with the preceramic resin directly on heat treatment.
  • the solid- phase functional additives may react with species (e.g., oxygen, nitrogen or carbon) generated from decomposition of the polymer during pyrolysis.
  • the solid-phase functional additives may react with the pyrolysis atmosphere during the pyrolysis, for example a nitrogen, methane, or ammonia atmosphere. To counteract the detrimental effects of shrinkage, it is preferred that these reactions happen at the same time as the preceramic resin shrinks, or are effective to reverse the volume reduction.
  • solid-phase functional additives for counteracting the shrinkage of the resin include, but are not limited to, scandium, yttrium, titanium, zirconium, zirconium hydride, hafnium, vanadium, niobium, tantalum, chromium, molybdenum, tungsten, manganese, iron, cobalt, nickel, zinc, boron, aluminum, gallium, silicon, germanium, phosphorus, or combinations thereof. Combinations of these elements such as titanium silicide, chromium silicide, magnesium silicide, zirconium silicide, or molybdenum silicide may be used as the solid-phase functional additives.
  • Preferred solid-phase functional additives in this category include aluminum, titanium, zirconium, titanium silicide, chromium silicide, magnesium silicide, and zirconium silicide.
  • the solid-phase functional additives actively bind sulfur.
  • the solid-phase functional additives may react with sulfur from thiol groups in the resin and bind the sulfur into stable compounds.
  • One class of preferred UV-curable preceramic resins for 3D printing is based on the thiol-ene reaction (alkene hydrothiolation).
  • the thiol groups contain sulfur which can partially remain in the ceramic after pyrolysis, causing an unpleasant smell. Residual sulfur can also corrode metals.
  • active solid-phase functional additives may be added that react with the sulfur and bind the sulfur in stable compounds that are neutral in smell and neutral with respect to corrosion of metals.
  • solid-phase functional additives for binding with sulfur include, but are not limited to, Ti, Zr, Hf, Si, Al, Cr, Nb, CrSri, TiSri, or a combination thereof.
  • Preferred sulfur gathering/scavenging solid-phase functional additives are Ti, Zr, and Hf which react to form the stable compounds T12S3, ZrS2, and HfS2, respectively.
  • the ceramic structure contains from about 0.01 wt% to about 20 wt% sulfur, such as from about 0.1 wt% to about 10 wt% sulfur. In various embodiments, the ceramic structure contains about 0.1, 0.2, 0.5, 1, 2, 3, 4, 5,
  • sulfur 6, 7, 8, 9, 10, 11, 12, 13, 14, or 15 wt% sulfur.
  • sulfur that is present, from about 10 wt% to about 100 wt%, such as about 20, 30, 40, 50, 60, 70, 80, or 90 wt%, may be bound to solid-phase functional additives in stable compounds containing sulfur.
  • the solid-phase functional additives actively seed crystallization of a preferred ceramic phase by enabling epitaxial growth of the preferred phase without a nucleation barrier.
  • an amorphous ceramic is usually obtained.
  • the amorphous ceramic material needs to then be crystallized into a preferred ceramic phase. This is typically achieved by a long (many hours) heat treatment at temperatures above the pyrolysis temperature, performed right after the pyrolysis or as a distinct second heat treatment.
  • crystallization may be facilitated by seeding crystallization.
  • the mechanism may include providing a surface for epitaxial growth of the preferred phase or multiple ceramic phases.
  • the crystallization of b-SiC in an amorphous SiC or SiCN ceramic derived from a polycarbosilane-based or polysilazane-based resin can be facilitated by small (e.g., 1 nanometer to 5 microns) b-SiC crystals. Crystallization of such a resin may be performed at temperatures between 1300°C and 2800°C over the course of 5 to 50 hours.
  • the crystallization of the a phase or b phase of S13N4 in an amorphous Si 3 N or SiCN ceramic derived from a polysilazane-based resin can be facilitated by small (e.g., 50 nanometers to 5 microns) a-Si 3 N 4 or b-8 ⁇ 3 N 4 crystals, respectively.
  • Other crystals may be chosen to facilitate crystallization, with the typical constraint of epitaxial growth on one crystal facet with low lattice strain.
  • the ceramic structure may be characterized by at least 50% theoretical density, preferably at least 75% theoretical density, and more preferably at least 95% theoretical density.
  • theoretical density it is meant the actual density of the ceramic structure as a percentage of theoretical density of the material itself, calculated in the absence of porous voids.
  • the ceramic structure is characterized by a theoretical density of about (or at least about) 50%, 60%, 70%, 75%, 80%, 85%, 90%, or 95%.
  • the ceramic structure is a fully dense monolith, which means that the ceramic structure has at least 99% (e.g., essentially 100%) theoretical density associated with a part or continuous region of material (also referred to as a “monolith”).
  • the absolute density in g/cm 3 will vary, depending on the selection of base materials; an exemplary range is about 1 g/cm 3 to about 4 g/cm 3 .
  • the overall mass loss associated with the conversion of preceramic polymer to the ceramic structure may vary widely, such as from about 1 wt% to about 90 wt%, e.g. about 5, 10, 20, 30, 40, 50, 60, 70, or 80 wt%.
  • the overall mass loss will be dictated by the starting formulation (e.g., fraction organic versus inorganic) as well as by process parameters. In principle, the lost mass may be recovered separately and used for other purposes.
  • Associated with mass loss may be shrinkage of the preceramic polymer as it converts to the ceramic structure.
  • the linear shrinkage (calculated in a single dimension, such as height of part) may be from 0% to about 60%, for example. Note that the mass loss and shrinkage are not necessarily correlated. In some embodiments with high mass loss, there is not much (if any) shrinkage. These embodiments tend to produce higher porosity and therefore lower densities. In some embodiments with high mass loss, there is substantial shrinkage, unless certain solid-phase fillers are utilized as described above and/or solid-phase functional additives are utilized as described below. These embodiments tend to produce lower porosity, or no porosity, and therefore higher densities (e.g., fully dense ceramic materials). Finally, in some embodiments, there is little mass loss but shrinkage associated with chemical reactions taking place. These embodiments also tend to produce relatively high densities.
  • the bulk shape (relative geometry) of the preceramic 3D-printed polymer may be preserved in the final ceramic structure. That is, when shrinkage is uniform in all dimensions, the geometrical features are retained in the part: it is a scaled-down version, in all three dimensions. In some embodiments, shrinkage is approximately uniform, which means the geometrical features are basically maintained, with slight deviations. Uniform shrinkage is possible when there is no random fragmentation during conversion of the preceramic polymer to the ceramic structure, and when the reactions and gas escape are isotropic within the material. Note that very small features, such as at the nanoscale, may not be preserved during otherwise uniform shrinkage.
  • net shape means that the geometrical features are retained, so that manufactured parts allow final fabrication matching the intended design with little or no post-processing.
  • Near net shape means that the geometrical features are not perfectly retained but require only minimal post processing or hand-work. Both net-shape parts and near-net-shape parts require little or no machining, polishing, bonding, surface finishing, or assembly.
  • the density of the final ceramic part may vary, as explained above. In general (without limitation), absolute densities ranging from about 0.1 g/cm 3 to about 5 g/cm 3 may be produced. A fully dense ceramic may have a density from about 1 g/cm 3 to about 4 g/cm 3 , for example.
  • the strength of the final ceramic material will vary, depending on the initial preceramic resin formulation, as well as the processing parameters.
  • the final ceramic material is characterized by a Young’s Modulus of at least about 200 GPa, 300 GPa, 400 GPa, 500 GPa, or more, measured at 25°C.
  • the final ceramic material is characterized by a flexural strength of at least about 300 GPa, 400 GPa, 500 GPa, or more, measured at 25°C.
  • the final ceramic material is characterized by a hardness of at least about 10 GPa, 20 GPa, 30 GPa, or more, measured at 25°C.
  • the engineering strength of a ceramic part also will depend on the geometry — such as a microtruss produced by some embodiments employing a self- propagating polymer waveguide technique. It is noted that, for instance, silicon oxycarbide microlattice and honeycomb cellular materials fabricated with the present methods exhibit higher strength than ceramic foams of similar density.
  • the thermal stability of the final ceramic material will vary, depending primarily on the initial preceramic resin formulation, as well as the processing parameters.
  • the final ceramic material is thermally stable at a temperature of at least 1500°C, 1600°C, 1700°C, 1800°C, 1900°C, or 2000°C.
  • Thermal stability means at least that the ceramic material does melt at these temperatures, and preferably also that the ceramic material does not react (e.g., by oxidation or reduction), undergo thermal shock, or physically decompose (introducing defects) at these temperatures.
  • the ceramic structure is characterized by being stable in the presence of air at a temperature of about 1000°C, 1100°C, 1200°C, 1300°C, 1400°C, 1500°C, 1600°C, 1700°C, 1800°C, or higher.
  • the final ceramic structure even when no machining, polishing, bonding, surface finishing, or assembly is required, may be subjected to coloring (e.g., with inks or dyes), stamping, or other non-functional features, if desired.
  • coloring e.g., with inks or dyes
  • stamping e.g., stamping, or other non-functional features
  • Example 1 Preparation of 3D-Printing Composition for SiC/SiOC UV-Cured Ceramic Matrix Composite.
  • This resin is capable of forming a silicon oxycarbide (SiOC) ceramic phase when polymerized and thermally treated.
  • SiC silicon carbide
  • Example 2 Production of 3D-Printed, UV-Cured SiC/SiOC Ceramic Matrix Composite.
  • Example 1 The monomer formulation of Example 1 is 3D-printed and UV-cured, followed by thermal treatment to form a ceramic matrix composite. Bulk parts are demonstrated by curing layers at 385 nm with LED-UV to form a preceramic polymer, and then pyrolyzing the preceramic polymer at 1000°C in inert atmosphere to form a pyrolyzed ceramic material.
  • FIG. 2 shows a photograph of the preceramic polymer (right-hand side) and the darker pyrolyzed ceramic part (left-hand side).
  • FIG. 3 is a graph of thermogravimetric analysis for the pyrolysis of the UV-cured preceramic polymer into a pyrolyzed ceramic material, measuring the loss of sample mass over time as the pyrolysis temperature increases.
  • Example 3 Production of Preceramic Polymer Composition Comprising Acrylate-Functionalized Polycarbosilane.
  • the reaction mixture is stirred under argon at a reaction temperature from 20°C to 80°C for a reaction time from 1 hour to 48 hours (with an inverse correlation between reaction temperature and reaction time).
  • the result of the reaction is a UV-reactive, acrylate-functionalized polycarbosilane preceramic polymer.
  • a polymerization initiator such as benzophenone
  • a free-radical inhibitor such as hydroquinone
  • hydroquinone may be added to the initial reaction mixture or to the acrylate-functionalized polycarbosilane, in a concentration of about 0.001 wt% to 1 wt%, and stirred until dissolved or suspended.
  • a 3D-printing resolution agent such as 2-(2-hydroxyphenyl)- benzotriazole, may be added to the initial reaction mixture or to the acrylate- functionalized polycarbosilane, in a concentration of about 0.001 wt% to 1 wt%, and stirred until dissolved or suspended.
  • the UV-reactive, acrylate-functionalized polycarbosilane preceramic polymer may be 3D-printed (e.g., by stereolithography) and thermally treated (e.g., by pyrolysis) to form a 3D ceramic structure containing SiC (and possibly SiOC).
  • Example 4 Production of Preceramic Polymer Composition Comprising Acrylate-Functionalized Polycarbosilane.
  • the mixing temperature may be from about 20°C to 80°C for a mixing time from about 1 minute to 4 hours.
  • the initial mixture is combined with acrylic acid, 30 grams, to form a reaction mixture in a container.
  • the reaction mixture is stirred under argon at a reaction temperature from 20°C to 80°C for a reaction time from 1 hour to 48 hours (with an inverse correlation between reaction temperature and reaction time).
  • the result of the reaction is a UV-reactive, acrylate- functionalized polycarbosilane preceramic polymer.
  • a polymerization initiator such as 2,2-dimethoxy-2- phenylacetophenone, may be added to the initial reaction mixture or to the acrylate- functionalized polycarbosilane, in a concentration of about 1 wt% to 2 wt%, and stirred until dissolved or suspended.
  • a free-radical inhibitor such as methylhydroquinone
  • a free-radical inhibitor such as methylhydroquinone
  • a 3D-printing resolution agent such as 2-(2-hydroxyphenyl)- benzotriazole
  • 2-(2-hydroxyphenyl)- benzotriazole may be added to the initial reaction mixture or to the acrylate- functionalized polycarbosilane, in a concentration of about 0.001 wt% to 1 wt%, and stirred until dissolved or suspended.
  • the UV-reactive, acrylate-functionalized polycarbosilane preceramic polymer may be 3D-printed (e.g., by stereolithography) and thermally treated (e.g., by pyrolysis) to form a 3D ceramic structure containing SiC (and possibly SiOC).
  • Example 5 Production of Preceramic Polymer Composition Comprising Acrylate-Functionalized Polycarbosilane.
  • Dry tetrahydrofuran (THF), 300 g, is added to a container and purged with argon. Allylhydridopolycarbosilane, 35 grams, is combined with allylphenylhydridopolycarbosilane, 35 grams, in the container and stirred to achieve a homogenous initial mixture in the container.
  • the mixing temperature may be from about 20°C to 75°C for a mixing time from about 1 minute to 4 hours.
  • the initial mixture is combined with acrylic acid, 30 grams, to form a reaction mixture in the container (or transferred to a separate reactor).
  • the reaction mixture is refluxed under argon at 75°C for a reaction time from 1 hour to 24 hours (with an inverse correlation between reaction temperature and reaction time), with condensation and return of vapors to the reacting mixture.
  • the result of the reflux reaction is a UV-reactive, acrylate-functionalized polycarbosilane preceramic polymer, which may be vacuum- dried.
  • a polymerization initiator such as camphorquinone
  • camphorquinone may be added to the initial reaction mixture or to the acrylate-functionalized polycarbosilane, in a concentration of about 1 wt% to 2 wt%, and stirred until dissolved or suspended.
  • a free-radical inhibitor such as ethylhydroquinone, may be added to the initial reaction mixture or to the acrylate-functionalized polycarbosilane, in a concentration of about 0.001 wt% to 1 wt%, and stirred until dissolved or suspended.
  • a 3D-printing resolution agent such as 2-hydroxyphenyl- benzophenone, may be added to the initial reaction mixture or to the acrylate- functionalized polycarbosilane, in a concentration of about 0.001 wt% to 1 wt%, and stirred until dissolved or suspended.
  • the UV-reactive, acrylate-functionalized polycarbosilane preceramic polymer may be 3D-printed (e.g., by stereolithography) and thermally treated (e.g., by pyrolysis) to form a 3D ceramic structure containing SiC (and possibly SiOC).
  • Example 6 Production of Preceramic Polymer Composition Comprising Acrylate-Functionalized Polycarbosilane.
  • a crosslinking agent divinyl dimethyl silane, 15 grams, is added to the container and stirred to dissolve.
  • reaction mixture is stirred under argon at a reaction temperature from 20°C to 80°C for a reaction time from 1 hour to 48 hours (with an inverse correlation between reaction temperature and reaction time).
  • the result of the reaction is a UV-reactive, acrylate-functionalized polycarbosilane preceramic polymer.
  • a polymerization initiator such as bis(2,4,6-trimethylbenzoyl)- phenylphosphineoxide, may be added to the initial reaction mixture or to the acrylate- functionalized polycarbosilane, in a concentration of about 1 wt% to 2 wt%, and stirred until dissolved or suspended.
  • a free-radical inhibitor such as methoxyhydroquinone
  • a free-radical inhibitor such as methoxyhydroquinone
  • a 3D-printing resolution agent such as 2-hydroxyphenyl-s-triazine
  • 2-hydroxyphenyl-s-triazine may be added to the initial reaction mixture or to the acrylate-functionalized polycarbosilane, in a concentration of about 0.001 wt% to 1 wt%, and stirred until dissolved or suspended.
  • the UV-reactive, acrylate-functionalized polycarbosilane preceramic polymer may be 3D-printed (e.g., by stereolithography) and thermally treated (e.g., by pyrolysis) to form a 3D ceramic structure containing SiC (and possibly SiOC).
  • Example 7 Production of Preceramic Polymer Composition Comprising Acrylate-Functionalized Polycarbonitrosilane.
  • Allylhydridopolycarbosilane 77 grams, is combined with acrylic acid, 23 grams, to form a reaction mixture in a container.
  • reaction mixture is stirred under argon at a reaction temperature from 20°C to 80°C for a reaction time from 1 hour to 48 hours (with an inverse correlation between reaction temperature and reaction time).
  • the result of the reaction is a UV-reactive, acrylate-functionalized polycarbonitrosilane preceramic polymer.
  • a polymerization initiator such as benzophenone
  • a free-radical inhibitor such as hydroquinone
  • hydroquinone may be added to the initial reaction mixture or to the acrylate-functionalized polycarbonitrosilane, in a concentration of about 0.001 wt% to 1 wt%, and stirred until dissolved or suspended.
  • a 3D-printing resolution agent such as 2-(2-hydroxyphenyl)- benzotriazole, may be added to the initial reaction mixture or to the acrylate- functionalized polycarbonitrosilane, in a concentration of about 0.001 wt% to 1 wt%, and stirred until dissolved or suspended.
  • the UV-reactive, acrylate-functionalized polycarbonitrosilane preceramic polymer may be 3D-printed (e.g., by stereolithography) and thermally treated (e.g., by pyrolysis) to form a 3D ceramic structure containing SiCN (and possibly SiOCN).
  • Example 8 Production of Preceramic Polymer Composition Comprising Acrylate-Functionalized Polycarbonitrosilane.
  • the first reaction mixture is stirred under argon at a first-container reaction temperature from 20°C to 80°C for a first-container reaction time from 1 hour to 48 hours (with an inverse correlation between reaction temperature and reaction time).
  • polycarbosilazane is stirred under argon.
  • 2-isocyanatoethylacrylate is added and the second mixture is stirred under argon.
  • the second-container reaction temperature may be from about 0°C to 50°C for a second-container reaction time from about 1 hour to 48 hours.
  • the contents of the second containers are added to the first container, and stirred until dissolved.
  • An additional reaction time may be provided, from about 1 hour to 24 hours, at a reaction temperature may be from about 0°C to 80°C.
  • the result of the reaction is a UV-reactive, acrylate-functionalized polycarbonitrosilane preceramic polymer.
  • a polymerization initiator such as benzophenone
  • a free-radical inhibitor such as hydroquinone
  • hydroquinone may be added to the initial reaction mixture or to the acrylate-functionalized polycarbonitrosilane, in a concentration of about 0.001 wt% to 1 wt%, and stirred until dissolved or suspended.
  • a 3D-printing resolution agent such as 2-(2-hydroxyphenyl)- benzotriazole, may be added to the initial reaction mixture or to the acrylate- functionalized polycarbonitrosilane, in a concentration of about 0.001 wt% to 1 wt%, and stirred until dissolved or suspended.
  • the UV-reactive, acrylate-functionalized polycarbonitrosilane preceramic polymer may be 3D-printed (e.g., by stereolithography) and thermally treated (e.g., by pyrolysis) to form a 3D ceramic structure containing SiCN (and possibly SiOCN).
  • Example 9 Production of 3D-Printed SiC from Acrylate- Functionalized Polycarbosilane.
  • the UV-reactive, acrylate-functionalized polycarbosilane preceramic polymer of Example 4 is 3D-printed into a plate and bars using a UV-based digital light projection 3D printer, Prodways L5000, following a top-down printing technique.
  • the resin is filled into a vat.
  • a mobile print platform is initially set at one- print-layer thickness, about 50 micron, below the resin surface.
  • Via a scanning mirror a UV beam is selectively projected onto the resin.
  • the final 3D part is printed layer by layer of cross-section images as the print platform moves downward.
  • FIG. 4 is a photograph of the 3D-printed polymer plate and bars.
  • FIG. 6 also shows a 3D- printed polymer bar (image on left-hand side).
  • the 3D-printed preceramic polymer is then converted to an amorphous SiC ceramic material via pyrolysis at a temperature of 1000°C for 1 hour under an atmosphere of argon.
  • FIG. 5 is a photograph of the amorphous SiC plate and bars.
  • FIG. 6 also shows an amorphous ceramic bar (second image from left).
  • the amorphous SiC ceramic material is subjected to high-temperature crystallization at a temperature of 1500°C for 4 hours.
  • the amorphous SiC ceramic material is subjected to high-temperature crystallization at a temperature of 1600°C for 4 hours.
  • FIG. 6 is a photograph of the crystallized SiC bars at 1500°C (third image from left) and 1600°C (image on right- hand side). It is observed that the 3D-printed and pyrolyzed bars survive high- temperature crystallization.
  • FIG. 9 shows the X-ray powder diffraction pattern of the ceramic material obtained from high-temperature treatment at 1600°C for 4 hours in argon.
  • the X-ray powder diffraction pattern reveals the b-SiC phase present in the crystallized ceramic material.

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Abstract

L'invention concerne des formulations de résine qui peuvent être utilisées pour une impression 3D et un traitement thermique pour produire un matériau céramique. L'invention concerne l'impression 3D directe à forme libre d'un polymère précéramique, suivie par la conversion du polymère précéramique en un composite céramique imprimé en 3D ayant des formes 3D potentiellement complexes. Une large variété de compositions chimiques est décrite et plusieurs exemples expérimentaux sont inclus pour démontrer la mise en œuvre. Par exemple, des formulations de résine précéramique peuvent contenir un carbosilane dans lequel il y a au moins un groupe fonctionnel sélectionné parmi les groupes vinyle, allyle, éthynyle, alkyle non substitué ou substitué, un groupe ester, amine, hydroxyle, vinyl éther, vinyl ester, glycidyle, glycidyl éther, vinyl glycidyl éther, vinyl amide, vinyl triazine, vinyl isocyanurate, acrylate, méthacrylate, alkacrylate, alkyl alkacrylate, phényle, halogénure, thiol, cyano, cyanate ou thiocyanate. Les formulations de résine peuvent contenir une charge en phase solide, pour fournir une stabilité thermique et une résistance mécanique élevées (par exemple, une ténacité à la rupture) au matériau céramique final.
EP20938855.2A 2020-05-30 2020-05-31 Formulations de monomères et de polymères d'impression 3d précéramique Pending EP4157806A4 (fr)

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