METHOD OF FABRICATING METAL-CERAMIC COMPOSITES, AND METAL-CERAMIC COMPOSITES MADE THEREBY

Abstract: A chemical pretreatment method is used to produce boron carbide-, boron-, and boride-reactive metal composites by an infiltration process. The boron carbide or other starting constituents, in powder form, are immersed in various alcohols, or other chemical agents, to change the surface chemistry of the starting constituents. The chemically treated starting constituents are consoli­ dated into a porous ceramic precursor which is then infil­ trated by molten aluminum or other metal by heating to wetting conditions. Chemical treatment of the starting constituents allows infiltration to full density. The infiltrated precursor is further heat treated to produce a tailorable microstructure. The process at low cost pro­ duces composites with improved characteristics, including increased toughness and strength.

Description: The present invention relates to methods of making metal-ceramic composites, and more particularly to infiltration methods, and metal-ceramic composites made thereby. U.S. Patent No. 4,605,440 is directed to boron carbide-reactive metal composites, particularly B₄C-Al, and methods for making same. Fully dense composites with tailorable microstructures can be produced. However, it is desirable to find alternative methods for producing these composites. It is also desirable to form composites of reactive metals and boron or borides. The concept of infiltrating a molten metal into a ceramic sponge is known and has been carried out by various different methods. U. S. Patent No. 3,864,154 by Gazza et al shows a method of infiltrating metal into a porous ceramic compact without any treatment of the compact. A compact of silicon boride, aluminum boride or boron is positioned between powdered aluminum in a vacuum furnace. Full density is not achieved. To infiltrate Al into B₄C, Si must be added to the Al as a wetting agent; Al alone could not be infiltrated into B₄C. U. S. Patent No. 3,725,015 by weaver shows an infiltration method in which a precursor is formed with a carbon containing substance and the precursor is heated to decompose the carbon containing substance to form a carbon residue. U. S. Patent No. 3,718,441 by Landingham shows an infiltration method in which the metal is treated by heating at low pressure to remove an oxide film and facilitate wetting. Other related art includes U. S. Patent No. 2,612,443, Goetzel et al, which shows an infiltration method in which a skeleton body is formed in a mold by heat treating/sintering and molten metal is forced into the pores by fluid pressure; U. S. Patent No. 2,581,252, Goetzel et al, and U. S. Patent No. 2,581,253, Ellis et al, which are directed to infiltrating a skeleton in a mold by applying pressure to the infiltrant; and U. S. Patent No. 2,672,426, Grubel, which shows a method of making and sintering a metal compact and impregnating with a molten ceramic. None of these patents show the infiltration of aluminum into a porous boron carbide (B₄C) sponge; Gazza shows that silicon must be added. Previous attempts to infiltrate aluminum into a B₄C sponge were unsuccessful since these methods were not based on the chemical reaction kinetics and the mechanisms of liquid rearrangement which are the basis of the present invention. Recently Pyzik and Aksay have shown that, by thermal modification of the as-received B₄C starting constituent, it is possible to infiltrate aluminum and aluminum alloys into a porous B₄C sponge. The thermal modification process requires heating to high temperatures, about 2000°C, in a controlled atmosphere, thereby sintering the ceramic grains. The process of the present invention is superior to the prior art for the following reasons: 1. It is more economical than previously described infiltration processes. 2. It results in a microstructure that offers improved properties over other processes. 3. It is possible to achieve tailorable properties in a fully dense composite body. 4. It is less costly than current commercial processes (hot pressing, hot-isostatic pressing, etc). Accordingly, it is an object of the invention to provide an infiltration method for producing B₄C-reactive metal, and particularly B₄C-Al, composites. It is another object to provide fully dense composites by an infiltration process. It is also an object to provide a method of producing boron- and boride- reactive metal composites by infiltration. The invention is a process for the infiltration of molten reactive metals into chemically pre-treated boron carbide, boron, or boride starting constituents (powders, fibers, etc.) that have been consolidated into a ceramic precursor or sponge via conventional or colloidal-chemical-casting techniques, or by injection molding processes. The process includes the steps of chemical pretreatment of the starting constituents, consolidation of the chemically pretreated starting constituents into a precursor, and infiltration of the reactive metal into the precursor. The infiltrated precursor can then be further heat treated to produce desired reaction products in a tailored microstructure. This invention is superior to the prior art in that it is more economical than conventional processing methods, such as hot-isostatic pressing and hot pressing. The process also costs considerably less than the recently developed method of infiltration using thermally-modified precursors. The invention not only offers cost savings but results in a product with increased toughness, strength, and thermal and electrical conductivity in these materials over the same processed by other methods. The key to this process is controlling the surface chemistry of the starting constituents. When the mechanisms of infiltration are inhibited by undesirable phases (such as oxides and/or stoichiometric deficiencies) at the surface of these starting constituents, it is possible to chemically convert or chemically convert and then subsequently pyrolyze them at low temperatures into phases which are conducive to the process. By chemically controlling the surface of the starting constituents, full density, i.e., greater than 99% of theoretical density, can be achieved by infiltration. Additional advantages of the new process include the ability to fabricate gradient microstructures with properties that can be tailored to meet use demands which vary along the finished part. The invention could also be incorporated with injection molding in a two-step process. Here, small highly-configured geometries can be molded using binders containing the appropriate chemical pre-treatment agents as the first step. Then the binder is volatilized from the precursor making it ready for subsequent infiltration in the second step. This new process is particularly applicable to the fabrication of boron carbide-aluminum cermets. However, the process can also be used with boron and boride starting constituents, and other reactive metals, or alloys, or compounds which reduce to the metal or alloy during the process. In the accompanying drawings: Figures 1A,B show two B₄C precursor (sponge) morphologies produced by the thermal modification process; Figures 2A,B show two infiltrated microstructures of titanium carbide (TiC) cermet having continuous and discontinuous carbide networks, respectively; Figures 3A,B,C are schematic diagrams of the infiltration of a metal into a precursor; and Figure 4 shows the infiltrant-precursor interface in an Al-B₄C composite. The infiltration process of the present invention is a chemical modification method. The process is more economical than thermal modification methods because chemical treatments can be done at room temperatures with relatively inexpensive chemicals, whereas thermal treatments require costly furnace equipment to obtain temperatures between 1800°C and 2250°C in controlled atmospheres (i.e., with minimal oxygen contamination, etc). The chemical modification process of the invention results in microstructures that have improved properties over those produced by thermal modification processes. The microstructure characteristics of concern can be illustrated by examining Figs. 1A,B and 2A,B; these Figures do not show composites made by the process of the invention but serve to illustrate important features. Figures 1A,B show two different B₄C sponge morphologies, both obtained by thermal processes. The 27 vol% porosity sponge was achieved by heating previously cold-pressed B₄C powders to 2100°C for 30 min. in an argon atmosphere.The 39 vol% porosity sponge was fabricated in a similar manner but at 1900°C for 30 min. The key difference in the sponge morphologies of Figures 1A,B is the degree of interconnecting of the B₄C grains. The 2100°C microstructure has been partially sintered to a greater extent than the 1900°C microstructure. Both of these microstructures can be infiltrated with aluminum or aluminum alloys because thermal treatments result in a compositional modification of the B₄C surface. This allows the kinetics of densification to proceed faster than the kinetics of interfacial chemical reactions resulting in dense final bodies. Figures 2A,B show two infiltrated microstructures of prior art TiC cermets. There is a greater degree of interconnected grains in Figure 2A over that of Figure 2B. The continuous and the discontinuous carbide networks result in microstructures that have widely differing properties. The process of the present invention includes control of the porosity and degree of interconnection. It is an object of the invention to produce a disconnected morphology, i.e., wherein the ceramic grains are not fused together and are preferably surrounded by metal. The thermal modification process produces a connected morphology as a result of the high temperature sintering. These property differences of composites prepared according to the invention compared to composites prepared by thermal processes are qualitatively outlined in Table 1. MECHANICAL AND PHYSICAL PROPERTY BEHAVIOR RELATIONSHIP OF CERMETS TO CARBIDE SPONGE MORPHOLOGY Equal weight Carbide Morphology Property Connected (Thermal Process) Disconnected (Chemical Process) Hardness increases decreases Toughness decreases increases Brittleness increases decreases Ductility decreases increases Modulus of Rupture decreases increases Elastic Modulus increases decreases Impact Resistance decreases increases Thermal Conductivity decreases increases Electrical Conductivity decreases increases Neutron Absorption unchanged unchanged The infiltration step of the process is schematically shown in Figures 3A,B,C. The chemical modification process is performed on the B₄C starting constituents prior to preparation of the porous B₄C precursor or sponge 10. Once the chemically modified precursor 10 is prepared, aluminum metal 12 is placed on the precursor 10. The metal and precursor are heated to achieve the wetting condition so that molten metal 14 flows or infiltrates into the pore space 16 of the precursor. By filling the pore volume with metal, a fully dense composite 18 is produced. One major advantage of the infiltration process of the invention is that it allows the fabrication of "graded" or gradient microstructures. The term "graded" means that the metal content in the cermet component varies along one or more directions so the physical and mechanical properties of any given section can accommodate the imposed conditions which could also vary in these directions. The fabrication of graded components can be accomplished by controlled colloidal consolidation of the B₄C precursor after chemical modifications have been made to the B₄C starting constituents. Colloidal consolidation is a method whereby the B₄C starting particulates are suspended temporarily in a liquid medium. Then by selecting an electrostatic, steric, or combined electrostatic and steric (electrosteric) means of controlling the sol, it is possible to control the forces between particulates (which may also be classified into controlled size distributions) to cause them to remain dispersed or allow them to flocculate. This control results in a desired sponge morphology upon consolidating the green body by gravitational settling filtration casting (pressure or pressureless), centrifugal casting, or injection molding technologies. The colloidal consolidation approach combined with controlled polymodal size distributions of B₄C starting constituents allows the fabrication of B₄C precursors with controlled porosities from less than 10 vol% to over 80 vol%. These pores are subsequently infiltrated with liquid aluminum, aluminum alloys or compounds which are reduced to aluminum or aluminum alloys during the process, thereby offering a wide range of properties in the "as-infiltrated" cermet. A colloidal consolidation method is described in U. S. Patent No. 4,605,440 which is herein incorporated by reference. Other, more conventional, means can also be used to fabricate the B₄C precursor after chemical modification of the starting constituents. These include cold pressing, warm pressing, (e.g., injection molding with a binder phase), plasma jet coating, combustion synthesis, hot pressing, hot-isostatic pressing etc. By selectively loading (either with different powder densities or with different pressures) the pressing dies, cavities, or molds it is also possible to obtain gradient B₄C sponge morphologies, but with less control than with the colloidal consolidation method previously described. With either method, however, the gradient morphology will be maintained after infiltration. The graded precursor can also be achieved on a shaped product, even when the starting sponge morphology is of uniform density, i.e., not graded. With a selected B₄C starting size distribution, proper control of the infiltration process, and/or non-isothermal heat treatments, selected areas of the shaped product can be preferentially altered. Another important effect that can be achieved by the infiltration process is the integral attachment of a metallic aluminum or aluminum alloy surface to the B₄C precursor. This metal-enriched surface film is merely an extension of the aluminum or aluminum alloy phase of the infiltrated structure and it may or may not be saturated with phases typical to B₄C-Al or B₄C-Al-alloy cermets depending on the processing conditions employed. This concept can be extended to the idea of attaching a bulk metal phase to the infiltrated cermet thereby creating a gradient microstructure. This is especially observed along the edge of the precursor-infiltrant interface where a dispersion and separation of the carbide grains is preponderant. This phenomenon is illustrated in Figure 4 for an Al infiltrant and B₄C precursor. This type of product could have completely different properties at the surface or surfaces of the part compared to its bulk properties. It is also possible to coinfiltrate the B₄C precursor with different metals or other infiltratable materials to even further enhance the multiproperty character of the products obtained. The chemical modification of B₄C starting constituents involves immersing of the starting constituents in selected chemical solutions. The exposure of the B₄C surfaces to these chemical solutions results in a chemical reaction at the B₄C-solution interface. The reaction products that form at the B₄C-solution interface have stoichiometrically different boron to carbon ratios than that of the initial B₄C starting constituent. It is primarily this difference in B:C ratios at the surface that inhibits the reaction kinetics and/or promotes the densification kinetics during the infiltration process. Boron carbide (B₄C) is typically prepared by a carbothermic reduction of boric anhydride (B₂O₃, also called boron oxide, boron trioxide, boric oxide, or boron sesquioxide) with carbon by the following chemical reaction: Other, more sophisticated, manufacturing processes have been developed which also result in the production of boron carbide. Boron carbide as discussed herein is not limited to the stoichiometry of B₄C, but can exist as a homogeneous range of boron and carbon atoms with carbon contents between less than 1 atom% and 25 atom%. Other boron carbides outside of this homogeneity range have also been reported. Therefore, this invention is applicable to all types of boron carbide starting constituents, amorphous or crystalline, regardless of stoichiometries. This invention is also applicable to boron or other boride starting constituents. The key to this invention is not the control of the bulk chemistry of the B₄C starting constituents but rather the control of their surface chemistry. These starting constituents are typically in the form of powders from as large as several millimeters to as small as tens of angstroms in size. The smaller the size the larger the surface area per unit volume of B₄C, hence the greater effect surface properties play on processing behavior. Any B₄C starting constituent, either through incomplete reactions during manufacture or by the mere contact with an atmosphere that contains oxygen, will have a surface layer of B₂O₃ or other boron oxide stoichiometry at its surface as a contaminant. Other contaminants or impurities may also be present in the surface as well as in the bulk (e.g., Fe, Ti, Al, Si, Ca, Mg, Ni, Cr, Mn, Cu, Ag, Be, etc.). The level of these other impurities depends on the manufacturing process and is usually on the order of a few parts per million up to as much as a few tenths of a weight percent in the bulk and even less at the surface. The levels of these other contaminants at the surface are insignificant compared to the amount of boron oxides (herein referred to as just B₂O₃ for brevity. In addition to the B₂O₃ at the surface of the B₄C starting constituents, the presence of moisture in the atmosphere will cause some or all of the B₂O₃ surface to convert to boric acid (BH₃O₃, also called boracic acid or orthoboric acid). Sometimes the B₂O₃ can exist in a hydrated state (B₂O₃·H₂O). When B₂O₃ and/or BH₃O₃ "contaminated" B₄C starting constituents are used to prepare the B₄C precursor prior to infiltration, the surface chemistry at the infiltrant-precursor interface will not be conducive to the infiltration process for two reasons: (1) a large concentration of B₂O₃ and/or BH₃O₃ at the surface will, upon heating past 450°C, form a liquid phase which fills the pores of the precursor and inhibits infiltration of the molten metal; or (2) a small concentration of B₂O₃ and/or BH₃O₃ at the surface will, upon heating past 450°C, form a liquid phase which acts as a flux causing an increase in the reaction rates of the chemical reactions at the B₄C-Al interface. This later condition will cause the reaction kinetics to be accelerated faster than the kinetics of densification (infiltration) thereby "locking up" the microstructure with residual porosity before full density is achieved. In either case the presence of an undesired B:C ratio at the surface of the precursor is established. When the precursor undergoes the previously described thermal modification process two results occur: First, the B₂O₃ and/or BH₃O₃ is volatilized at temperatures near 2000°C in an argon atmosphere. Second, the free boron present at the interface will form boron-nitrogen phases and/or a change in B₄C stoichiometry. The nitrogen is made available via the argon gas which can typically contain up to or more than 100 ppm N₂. The formation of BN is thermodynamically favored over that of B₄C at temperatures near 2000°C (-12 kcal/mole versus -6 kcal/mole for BN and B₄C, respectively at 2000°C). Because we are dealing with surface chemistry, these effects do not have to be large in extent and usually occur within the first 30-50A of the surface. The removal of B₂O₃ and/or BH₃O₃ plus the presence of BN and/or B₄C stoichiometry changes at the surface alters the B:C ratio such that the surface chemistry of the infiltrant-precursor interface is conducive to the infiltration process. That is, the kinetics of reaction are slowed down while the system is in a condition which is thermodynamically favorable for wetting to occur; or the kinetics of densification (infiltration) are faster than the kinetics of chemical reactions at the B₄C-Al interfaces. In this invention, the B:C ratio is adjusted chemically rather than thermally. This is accomplished by immersing or washing the B₄C starting constituents in a chemical substance which reacts with the B₂O₃ and/or BH₂O₃ to form trimethyl borate (C₃H₉BO₃, also called boric acid, trimethyl ester) and/or any other boron-carbon-hydrogen-oxygen chemical complex that will pyrolyze upon heating prior to or during the infiltration process to the required B:C ratio or ratios. The starting constituents are immersed for as long as necessary to change the surface chemistry, typically a few hours to a few days or longer. Some of the preferred chemical substances that react with B₂O₃ and/or BH₃O₃ to form C₃H₉BO₃ and/or any other boron-carbon-hydrogen-oxygen chemical complex include, but are not limited to the following: 1. Methanol (CH₄O or CH₃OH, also called methyl alcohol, carbinol, wood spirit, or wood alcohol). 2. Anhydrous alcohol (C₂H₆OH to which has been added some substance or substances which renders it entirely unfit for consumption as a beverage; e.g., methanol, camphor, aldehol, amylalcohol, gasoline, isopropanol terpineol, benzene, caster oil, acetone, nicotine, aniline dyes, ether, cadmium iodide, pyridine bases, sulfuric acid, kerosene, diethyl phthαlate, etc.). 3. n-Propyl alcohol (C₃H₈O or CH₃CH₂CH₂OH, also called 1-propanol or propylic alcohol). 4. Isopropyl alcohol (C₃H₈O or CH₃HOHCH₃, also called 2-propanol, isopropanol, secondary propyl alcohol, dimethyl carbinol, or petrohol). 5. n-Butyl alcohol (C₄H₁₀O or CH₃CH₂CH₂CH₂OH, also called 1-butanol, butyl alcohol, or propyl carbinol). 6. sec-Butyl alcohol (C₄H₁₀O or CH₃CH₂CH(OH)CH₃, also called 2-butanol, butylene hydrate, 2-hydroxy butane, or methyl ethyl carbinol). 7. tert-butyl alcohol (C₄H₁₀O or (CH₃)₃COH, also called 2-methyl-2-propanol, or trimethyl carbinol). 8. Any azeotrope of the above. 9. Any dilution of the the above. 10. Any higher alcohol (C n H m O), where n ≧ 4 and m ≧ 10), or azeotrope or dilution thereof. 11. Glycerol (C₃H₈O₃ or CH₂OHCHOHCH₂OH, also called 1, 2, 3-propanetriol, glycerin, or trihydroxypropane). 12. Any glycerol derivative (C n H m O p , where n ≧ 3, m ≧ 6, and p ≧ 2), including glyceraldehyde (C₃H₆O₃), glyceric acid (C₃H₆O₄ or CH₂OHCH(OH)COOH), glycerol formal (C₄H₈O₃), and glycidol (C₃H₆O₂). 13. Any methyl- abietate (C₂₁H₃₂O₂), acetate (C₃H₆O₂ or CH₃COOCH₃), acetoacetate (C₃H₈O₃ or CH₃COCH₂COOCH₃), acetylsalicylate (C₁₀H₁₀O₄), acrylate (C₄H₆O₂ or CH₂ = CHCOOCH₃, benzoate (C₈H₈O₂ or C₆H₅COOCH₃), benzoylsalicylate (C₁₅H₁₂O₄), butyl ketone (C₆H₁₂O or CH₃COC₄H₉), butyrate (C₅H₁₀O₂ or CH₃(CH₂)₂COOCH₃), carbitol (C₅H₁₂O₃ or CH₃OCH₂CH₂OCH₂CH₂OH), carbonate (C₃H₆O₃ or CO(OCH₃)₂), cellosolve (C₃H₈O₂ or HOCH₂CH₂OCH₃), cellosolve acetate (C₅H₁₀O₃ or CH₃OCH₂CH₂OOCCH₃), or methylcellulose, or methylal (C₃H₈O₂ or CH₂(OCH₃)₂). 14. Any combination of the above, in part or whole. 15. Any binder, for the purpose of injection molding, containing any of the above, in part or whole. The infiltration process according to the invention can be summarized as follows: Step 1 Precursor starting constituents, typically in powder form, are immersed in a chemical substance as previously described. The surface chemistry is altered to facilitate wetting. Step 2 The chemically treated starting constituents are then consolidated or packed into a porous "sponge" or compact by colloidal chemical means followed by a selected casting method as previously explained to form the consolidated precursor. Alternatively, other consolidation methods can be used. Step 3 The metal phase is placed adjacent to the consolidated precursor and the assembly is placed in a vacuum or inert atmosphere furnace. Step 4 The assembly is heated to conditions which promote wetting. Step 5 The assembly can also be further heated to conditions which promote microstructural enhancement and/or gradiation as previously described. Step 6 The final part is removed from the furnace and machined to its final dimensions (if not already processed to its desired configuration). The infiltration process of the invention is carried out in accordance with the wetting and reaction conditions described in U.S. Patent No. 4,605,440, filed May 6, 1985, which is herein incorporated by reference. By controlling the reaction conditions, e.g., temperature and time, the relative proportion of various phases in the composite microstructure is controlled. Example 1 Start with 1 micron average diameter B₄C powders. Soak these starting constituents in methanol for 10 days with continuous stirring. Filter cast this slurry into a mold of desired configuration. Remove casted precursor (sponge) from mold and place an amount of aluminum equivalent to the calculated pore volume of the precursor on the sponge. Heat in a vacuum furnace to 500°C and hold for one hour (to remove volatiles), then increase temperature to 1180°C for a long enough time to allow for complete infiltration of aluminum into the precursor, then cool under vacuum. Remove fired part. Final machine if necessary. Example 2 Start with a polymodal distribution of 0.2 micron and 0.8 micron diameter B₄C powders. Soak these starting constituents in methanol with a 3 wt.% polyethylene glycol binder addition for 10 days with continuous stirring. Filter cast this slurry through a filtration-funnel system and catch all starting constituents on filter paper. Scrape these starting constituents into a cold pressing die and press to 10,000 psi. Remove precursor from die and place in a crucible containing a bed of powdered aluminum equivalent to or greater than the calculated pore volume of the precursor. Heat assembly in a vacuum furnace to 500°C and hold for one hour, then increase temperature to 1050°C for a long enough time to allow for complete infiltration of aluminum into the sponge, then drop temperature to 800°C for 24 hours to enhance the microstructure, then cool under vacuum. Remove assembly and machine to final dimensions. Example 3 Start with 10 micron average diameter B₄C. Soak these starting constituents in isopropanol for 10 days with continuous stirring. Filter cast this slurry through a filtration-funnel system and catch all starting constituents on filter paper. Scrape off these starting constituents and mix them with a thermoplastic injection molding resin containing methylcellulose (binder). Injection mold the mix into a desired mold configuration. Remove the consolidated B₄C-resin mix and place in a vacuum oven and "burn out" the binder leaving only the B₄C sponge. Place an amount of aluminum alloy (e.g., 7075-T6) equivalent to the calculated pore volume of the precursor on top of the sponge. Heat the assembly in a vacuum furnace to 1100°C for 2 hours (to cause both infiltration and microstructural enhancement). Remove fired part and finish machine if necessary. The invention has been described with respect to the treatment of B₄C starting constituents for the formation of B₄C-Al composites. However, boron and boride, e.g., AlB₁₂, AlB₂, TiB₂, starting constituents can similarly be treated prior to the formation of the porous precursor. Reactive metals, or alloys thereof, or compounds which reduce to the metal or alloy, can then be infiltrated by heating to the wetting condition, and the infiltrated precursor can be further heat treated to promote reactions to tailor the microstructure of the composite.

Claims: A method of fabricating metal-ceramic composites from previously formed ceramic precursor-starting constituents which are boron-carbide, boron and borides which are infiltrated with metals reacted therewith, said metal being a reactive metal, an alloy of a reactive metal or a compound of a reactive metal which compound reduces to provide the required reactive metal or alloy thereof, the said method comprising: chemically pretreating the previously formed starting constituents from which a porous ceramic precursor is produced; consolidating the chemically pretreated starting constituents into the porous ceramic precursor; and infiltrating molten reactive metal into the chemically pretreated ceramic precursor, said method being characterised in that the step of chemically pretreating the starting constituents for the porous ceramic precursor comprises immersing or washing the boron-carbide starting constituents in a chemical substance which reacts with boric acid to yield boric acid esters or any other boron-carbon-hydrogen-oxygen chemical complex that will pyrolyse to the required B:C ratio such as to alter the surface chemistry of the starting constituents thereby to enhance infiltration of the porous precursor by the molten reactive metal by slowing the kinetics of reaction of the reactive metal with the ceramic precursor relative to the kinetics of densification so as to produce a metal-ceramic composite with a disconnected morphology wherein the ceramic grains are not fused together and the composite has a density greater than 99% of the theoretical density. A method as claimed in claim 1 wherein the step of chemically pretreating the starting constituents comprises chemically altering the surface chemistry of the starting constituents to eliminate phases which inhibit infiltration. A method as claimed in claim 2 wherein the step of chemically pretreating the starting constituents comprises chemically converting phases which inhibit infiltration to phases which promote infiltration. A method as claimed in claim 3 further including pyrolyzing the chemically converted phases at low temperature. A method as claimed in any one of the preceding claims further comprising forming the starting constituents into particles prior to chemically pretreating. A method as claimed in claim 5 further comprising forming the particles with a controlled polymodal size distribution. A method as claimed in any one of the preceding claims wherein the step of consolidating the starting constituents is performed by colloidal consolidation. A method as claimed in any one of claims 1 to 6 wherein the steps of pretreating and consolidating the starting constituents are performed by injection molding the starting constituents using a binder containing chemical pretreatment agents. A method as claimed in any one of the preceding claims comprising immersing the starting constituents in any one of the following: a. methanol (CH₄O or CH₃OH); b. anhydrous alcohol (C₂H₆OH); c. n-propyl alcohol (C₃H₈O or CH₃CH₂CH₂OH); d. isopropyl alcohol (C₃H₈O or CH₃HOHCH₃); e. n-butyl alcohol (C₄H₁₀O or CH₃CH₂CH₂CH₂OH); f. sec-butyl alcohol (C₄H₁₀O or CH₃CH₂CH(OH)CH₃); g. tert-butyl alcohol (C₄H₁₀O or (CH₃)₃COH); h. any azeotrope of the above; i. any dilution of the above; j. any higher alcohol (C n H m O), where n ≧ 4 and m ≧ 10), or azeotrope or dilution thereof; k. glycerol (C₃H₈O₃ or CH₂OHCHOHCH₂OH); l. any glycerol derivative (C n H m O p , where n ≧ 3, m ≧ 6, and p ≧ 2), including glyceraldehyde (C₃H₆O₃), glyceric acid (C₃H₆O₄ or CH₂OHCH(OH)COOH), glycerol formal (C₄H₈O₃), and glycidol (C₃H₆O₂); m. any of - methyl abietate (C₂₁H₃₂O₂), acetate (C₃H₆O₂ or CH₃COOCH₃), methylacetoacetate (C₅H₈O₃ or CH₃COCH₂COOCH₃), methyl acetylsalicylate (C₁₀H₁₀O₄), acrylate (C₄H₆O₂ or CH₂ = CHCOOCN₃), methyl benzoate (C₈H₈O₂ or C₆H₅COOCH₃), O - benzoyl-salicylic acid methyl ester (C₁₅H₁₂O₄), methyl butylketone (C₆H₁₂O or CH₃COC₄H₉), methyl butyrate (C₅H₁₀O₂ or CH₃(CH₂)₂COOCH₃), carbitol (C₅H₁₂O₃ or CH₃OCH₂CH₂OCH₂CH₂OH), dimethyl carbonate (C₃H₆O₃ or CO(OCH₃)₂), cellosolve (C₃H₈O₂ or HOCH₂CH₂OCH₃), cellosolve acetate (C₅H₁₀O₃ or CH₃OCH₂CH₂OOCCH₃), or methylcellulose, or methylal (C₃H₈O₂ or CH₂(OCH₃)₂); n. any combination of the above, in part or whole; o. any binder, for the purpose of injection molding, containing any of the above, in part or whole. A method as claimed in any one of the preceding claims wherein the step of infiltrating the metal into the percursor comprises: placing the metal adjacent to the precursor; and heating the metal and precursor to a temperature which promotes wetting of the precursor by the metal. A method as claimed in claim 10 wherein the heating step is performed in a vacuum. A method as claimed in claim 10 wherein the heating step is performed in an inert atmosphere. A method as claimed in any one of claims 10 to 12 further comprising further heating to a temperature which promotes microstructural enhancement of the composite. A method as claimed in any one of the preceding claims further comprising forming a graded microstructure. A method as claimed in any one of the preceding claims further comprising consolidating the starting constituents into a precursor having a substantially disconnected microstructure.

Inventors: HALVERSON, DANNY C., LANDINGHAM, RICHARD L.
Applicants: THE REGENTS OF THE UNIVERSITY OF CALIFORNIA
Application year: 1987
Main classification: C04B41
IPC codes: C04B35, C22C29, C04B38, C22C32, C04B41, B22D19, C22C1