EP0217946A1 - High density reinforced ceramic bodies and method of making same - Google Patents

High density reinforced ceramic bodies and method of making same

Info

Publication number
EP0217946A1
EP0217946A1 EP86902963A EP86902963A EP0217946A1 EP 0217946 A1 EP0217946 A1 EP 0217946A1 EP 86902963 A EP86902963 A EP 86902963A EP 86902963 A EP86902963 A EP 86902963A EP 0217946 A1 EP0217946 A1 EP 0217946A1
Authority
EP
European Patent Office
Prior art keywords
density
ceramic
mixture
sintering
sintered
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.)
Withdrawn
Application number
EP86902963A
Other languages
German (de)
French (fr)
Inventor
James F. Rhodes
Hillar M. Rootare
Chester J. Dziedzic
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.)
Atlantic Richfield Co
Original Assignee
Atlantic Richfield Co
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
Application filed by Atlantic Richfield Co filed Critical Atlantic Richfield Co
Publication of EP0217946A1 publication Critical patent/EP0217946A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/01Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
    • C04B35/10Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on aluminium oxide
    • C04B35/111Fine ceramics
    • C04B35/117Composites
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/622Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/64Burning or sintering processes
    • C04B35/645Pressure sintering
    • C04B35/6455Hot isostatic pressing
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/71Ceramic products containing macroscopic reinforcing agents
    • C04B35/78Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
    • C04B35/80Fibres, filaments, whiskers, platelets, or the like
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/32Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
    • C04B2235/3205Alkaline earth oxides or oxide forming salts thereof, e.g. beryllium oxide
    • C04B2235/3206Magnesium oxides or oxide-forming salts thereof
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/32Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
    • C04B2235/3217Aluminum oxide or oxide forming salts thereof, e.g. bauxite, alpha-alumina
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/32Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
    • C04B2235/3224Rare earth oxide or oxide forming salts thereof, e.g. scandium oxide
    • C04B2235/3225Yttrium oxide or oxide-forming salts thereof
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5216Inorganic
    • C04B2235/524Non-oxidic, e.g. borides, carbides, silicides or nitrides
    • C04B2235/5244Silicon carbide
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/526Fibers characterised by the length of the fibers
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5264Fibers characterised by the diameter of the fibers
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5276Whiskers, spindles, needles or pins
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/54Particle size related information
    • C04B2235/5418Particle size related information expressed by the size of the particles or aggregates thereof
    • C04B2235/5445Particle size related information expressed by the size of the particles or aggregates thereof submicron sized, i.e. from 0,1 to 1 micron
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/60Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
    • C04B2235/604Pressing at temperatures other than sintering temperatures
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/60Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
    • C04B2235/608Green bodies or pre-forms with well-defined density
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/66Specific sintering techniques, e.g. centrifugal sintering
    • C04B2235/668Pressureless sintering
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/74Physical characteristics
    • C04B2235/77Density

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)
  • Composite Materials (AREA)
  • Inorganic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Ceramic Products (AREA)

Abstract

Procédé de frittage sans pression de corps céramiques renforcés par des cristaux filiformes. Des mélanges contenant des cristaux filiformes de carbure de silicium et des poudres de matrice céramique finement divisées sont formés dans lesquels la teneur en cristaux filiformes se situe dans la plage de 0,5 à 21% en volume du mélange. Le mélange est ensuite compacté sans chauffage externe pour former un corps façonné dont la densité est comprise entre 55 et 70% de la densité du produit fritté final désiré. Le corps brut ainsi formé est ensuite fritté dans des conditions de frittage sans pression dans une atmosphère non oxydante pour former un corps céramique renforcé, de dureté et densité élevées. Dans un mode de réalisation, le corps brut est fritté sans pression pour former un corps céramique à pores fermés, lequel est ensuite soumis à un pressage isostatique à chaud en dehors d'un récipient afin de porter sa densité à au moins 98% environ de la densité théorique maximale du corps.Pressure-free sintering process of ceramic bodies reinforced with filiform crystals. Mixtures containing filiform crystals of silicon carbide and finely divided ceramic matrix powders are formed in which the content of filiform crystals is in the range of 0.5 to 21% by volume of the mixture. The mixture is then compacted without external heating to form a shaped body whose density is between 55 and 70% of the density of the desired final sintered product. The raw body thus formed is then sintered under pressureless sintering conditions in a non-oxidizing atmosphere to form a reinforced ceramic body of high hardness and density. In one embodiment, the raw body is pressureless sintered to form a closed pore ceramic body, which is then subjected to hot isostatic pressing out of a container to bring its density to at least about 98% of the maximum theoretical density of the body.

Description

HIGH DENSITY REINFORCED CERAMIC BODIES AND METHOD OF MAKING SAME
TECHNICAL FIELD The invention herein relates to ceramic bodies. More particularly it relates to ceramic bodies reinforced by single crystal or monocrystal- line silicon carbide whiskers, BACKGROUND ART The desirable properties of ceramic bodies, including strength, low porosity and heat resistance, have been known for some time to make ceramics highly valuable in many industrial applications. These pro¬ perties should serve to make the ceramics directly competitive with metals in many such applications. It has been found, however, that the ceramics' lack of "toughness" often prevents them from successfully competing with metals. Toughness, for the purposes of this invention, refers to the ability of a body to "resist crack propagation through the body; the tougher a materia*!, the more it is able to slow the rate of crack propagation through it. Materials which are brittle possess little toughness, and cracks which are started in such materials propagate rapidly so that such materials can fracture catastro- phically.
It has been known that the degree of tough¬ ness of a body can be significantly increased by incorporation of fibrous reinforcement into the body. if the material of the body matrix and the fibers are sufficiently bound together, the fibers will hold the matrix pieces together.and prevent a crack from propagating beyond the location of the rein¬ forcement. Such types of reinforcements have been used in coarse-grained materials such as cements and bricks for many years.
The process of forming intricately shaped dense ceramic bodies by sintering of ceramic powders is well known. In sintering the mass of powder is molded into the desired shape and heated to an ele¬ vated temperature, usually 70-90% of the melting point of the material. The body is held at that temperature while the individual particles fuse together into a coherent unitary body. In hot pressing and hot isostatic pressing, the shaped powders are subjected to high pressure, either in a press mold or by a surrounding gas, while at tempera¬ ture. In "pressureless" sintering, the powder mass is first consolidated at near ambient temperature. The molded body is then separately heated at ambient or moderate positive pressure or' under vacuum. From a commercial and industrial point of view, the pres¬ sureless sintering operation is much more desirable since it eliminates the necessity of maintaining high temperatures and high pressures simultaneously. The operator can use common low temperature molding equipment and the heating can be conducted in open- ended continuous furnaces.
In the past it has been found possible to make reinforced ceramic composites from ceramic powders (such as alumina powder) and silicon carbide whiskers by hot pressing or hot isostatic pressing. See, for example Wei U.S. Patent 4,543,345. Such composites exhibit both high strength and high tough- ness. However, efforts to form such composites by the more desirable pressureless sintering method have been unsuccessful. It would therefore be desirable to have a process which would permit silicon carbide whisker reinforced ceramic composites to be formed by pressureless sintering. DISCLOSURE OF THE INVENTION
We have now discovered that high strength, high toughness whisker-reinforced ceramic composites can be formed by pressureless sintering, if the whisker content is maintained in the range of 0.5-21.0% by volume of the composite and the fiber/ ceramic powder blend is first molded to a density of 55-70% of the maximum theoretical density of the final body. (All compositional percentages are volume percents unless otherwise noted. )
In its broadest form, therefore, this invention is a method for the formation of high density reinforced ceramic bodies which comprises (a) forming* a mixture containing 0.5-21.0 volume percent silicon carbide whiskers' and the balance ceramic matrix powder; (b) compacting the mixture to form a shaped body having a density of 55-70% of the theoretical maximum density of the body; and (c) heating the body at a sintering temperature of 70-90% of the melting temperature of the ceramic matrix for a period of time sufficient to sinter the powder and whisker mixture into a high-strength, high-toughness, monolithic, shaped ceramic composite having a density of at least 85% of the theoretical maximum density of the body.'
The invention also comprises the high den¬ sity, tough reinforced ceramic composite bodies formed by the method of this invention. MODES FOR CARRYING OUT THE INVENTION
The ceramic matrix materials of the present invention can be any type of ceramic which is capable of being sintered to form coherent bodies. These may include oxides, carbides, borides and nitrides. Typi¬ cal examples include alumina, silica, aluminum sili¬ cates, silicon nitride, aluminum nitride, titanium diboride, zirconia and titanium carbide. Of these the ceramic of most interest because of its wide variety of applications is alumina. The ceramic mixture may also contain small amounts of other ceramic or doping materials to modify or enhance sin- terability or physical properties; typical of such additive materials are yttria and magnesia.
The ceramic matrix material is used in finely divided powdered form. The particle sizes involved will be dependent on the specific ceramic being used and the desired density of the ultimate product, as well as on the degree of reinforcement to be obtained from the Whiskers. Normally, the higher-density finished products are obtained from ceramic powders having the smaller particles sizes. Particle sizes may range from as high as approxi- mately 3 mm (6 mesh) down to approximately 0.01 urn in size. Most frequently the particle sizes will be in the range of 0.1-100 um.
The silicon carbide whiskers used as rein¬ forcement in the present invention are high strength materials which are usually formed by the high temperature reaction of silica and a carbonaceous material. The whiskers commonly have lengths in the range from about 10-100 um and average diameters on the order of 1 um or less. The crystalline structure is normally alpha or beta silicon carbide. The fibers are 98-99% silicon carbide whisker with the impurities being a variety of metals, primarily calcium, manganese and aluminum. Silicon carbide whiskers and methods for their formation are shown in Handbook of Fillers and Reinforcements for Plastics, Chapter 25, pages 446-464 ("Whiskers", by J. V. Milewski and H. S. Katz) (Von Nostrand Reinhold Co., N.Y. 1978). Particularly preferred are the whiskers manufactured by the Advanced
Materials Group of ARCO Chemical Company, Silag, now an operating unit of Atlantic Richfield Company, a whisker source mentioned on page 447 of that reference. These silicon carbide whiskers are single crystal or monocrystalline materials manufactured from rice hulls. The silicon carbide whiskers typically have average diameters on the order 0.6 um and aspect ratios on the order of 15-150. Strengths are typically on the order of 1 million psi (70,000 'kg/cn_2) and tensile moduli .on the order of 60-100. million psi (4-7 million kg/cπ.2). The silicon carbide whiskers are thermally stable to 3200°F (1760°C).
Short fiber materials of the polycrystal- line type are to be distinguished from the single crystal whiskers used in this invention. The poly- crystalline filaments or chopped fibers are much larger in diameter e.g., 10 microns or larger. As taught in the Wei patent referred to above, the polycrystalline fibers
"suffer considerable degradation due to grain growth at temperatures above about 1250°C which severely limited their use in high temperature fabrication processes such as hot pressing for producing ceramic composites of nearly theoretical density. Further, during high pressure loadings such as encountered during hot pressing, the polycrystalline fibers undergo fragmen¬ tation which detracts from the reinforcing properties of the fibers in the ceramic composite. Also, these polycrystalline fibers provided insufficient resistance to cracking of the ceramic composite since the fibers extending across the crack line or fracture plane possess insufficient tensile strength to inhibit crack growth through the composite especially after the composite has been fabricated by being exposed to elevated pressures and tempera¬ tures in hot pressing." Also see Milewski, J. V. "Short-Fiber Reinforcements: Where The Action Is", Plastics Compounding, November/ December 1979, pages 17-37. A clear distinction -is drawn between single crystal "whiskers" and polycry¬ stalline "Microfibers" on pages 17-19.
In the present invention the ceramic powder and the silicon carbide whiskers are mechanically blended to produce a thorough mixture of the fibrous and particulate components. If desired, conventional organic forming binders may be added to the mixture. There are a number of commercial mixing devices which will provide adequate blending of these compo- nents. These devices are well described in engi¬ neering handbooks and textbooks on mixing of solids. The whiskers component of the mixture will comprise 0.5-21%, preferably 2-18% of the blend. Composites containing less than 0.5% of fibers do not have a sufficient whisker content to provide significant reinforcement and improvement of proper¬ ties over the unreinforced ceramics. Composities containing more than 21% whiskers cannot be suffi- ciently densified upon pressureless sintering to provide high strength composites.
Following blending of the components, the blended mass of particles and whiskers is densified (consolidated) in a mold or by isostatic pressing to form a shaped body having a density in the range of about 55-70%, preferably about 55-65%, and more preferably about 58-62%, of the theoretical density of the final sintered body. This densification is critical to the success of the subsequent sintering operation. If the components are not densified to this level prior to sintering the high density rein¬ forced product cannot be obtained from the subsequent sintering operation. It is preferred to densify to less than the 70% upper limit in order to avoid practical problems of binder outgasing which may be encountered at the higher levels.
The densification is performed by conven¬ tional techniques such as extrusion, injection- molding, slip casting, cold pressing or cold isostatic techniques. Mold pressures are generally in the range of from about 10-50 tons/in2 (1400-7000 kg/cm2), although pressures may be greater or lesser depending on the particular molding technique used and the desired shape of the end product. Generally speaking, ambient temperatures are appropriate and preferred for carrying out this initial densification. In cases where procedures such as extrusion and injec¬ tion molding are used, mild heating sufficient to soften organic binder materials, e.g. to about 300°C, can be employed. After consolidating the components to the 55-70% of theoretical density and obtaining the "green" shape, the green body is sintered at a temperature in the range of 70-90% of the melting temperature of the matrix materials. This will normally be in the range of 1500-3200°F (800-1750°C) . More refractory materials will require sintering at higher temperatures. The green bodies are usually maintained at sintering temperature for a period of from 15 minutes to 2 hours.
The sintering is conducted in an atmosphere which will not adversely react with the component particles and whiskers. Because of the small particle and whisker size, the green bodies contain very large surface areas. Such large surface areas make oxidizable components highly reactive to oxidation in the presence of an oxidizing atmosphere at high temperatures. Consequently, the atmosphere in the sintering furnace must be of an inert or nonoxidizing - gas such as hydrogen, carbon monoxide, nitrogen or the noble gases such as argon and helium. The atmos¬ phere will normally be maintained at approximately ambient pressure. Alternatively, one can conduct the sintering under vacuum or moderate positive pressure. Vacuum sintering is normally performed at pressures on the order of 0.5 inch (12mm) of of mercury. Positive pressure sintering (distinguished from hot isostatic pressing) is normally performed at a very slight positive pressure. The pressureless sintering is carried out until the shaped body has a density which is at least about 85% of the theoretical density.
In especially advantageous practice the pressure-less sintering is carried out until the shaped body has reached closed porosity, a state usually corresponding to a density which is at least 94% of the theoretical density. Closed porosity bodies are characterized by the substantial absence of pores or void spaces communicating with the surface - i.e., such pores or void spaces which occur in the shaped bodies do not communicate with the surface of the body but rather are contained within the interior volume of the body. It is of considerable importance that the shaped bodies which have been brought to the condi¬ tion of closed porosity as above indicated, can by containerless hot isostatic pressing procedures be brought to nearly 100% of the theoretical density thus resulting in a product which has greatly enhanced properties of strength, hardness, etc. Unless the shaped body is first brought to the closed porosity state, containerless hot isostatic pressing will not achieve the optimum benefits. " Thus, in an especially .advantageous prac¬ tice of the invention, appropriate amounts of the monocrystalline silicon carbide whiskers and powdered ceramic matrix material are blended to homogeneously distribute the whiskers throughout the mixture. The blended materials are cold pressed to form the green bodies which have a density which is 55-70% of the theoretical maximum. These green shapes are then subjected to pressureless sintering to the extent necessary to achieve closed porosity. This is typically achieved by raising the density of the article by sintering to 94% or higher of the theore¬ tical maximum. The closed porosity sintered articles are then subjected to containerless hot isostatic pressing to bring the density to at least about 98% of the theoretical maximum. In this way products having outstanding properties of toughness and strength are formed while avoiding costly procedures which were heretofore deemed necessary. The hot isostatic pressing to which the closed porosity sintered composite can be subjected is preferably carried out in a gas autoclave employ¬ ing nitrogen or argon atmosphere. Since the sintered composites are characterized by closed porosity, the hot isostatic pressing is containerless - i.e., the sintered composites need not be placed in a container to accomplish the isostatic pressing. In this pres¬ sing, pressures generally ranging from about 10,000 psi up to 30,000 psi or higher are appropriate. Temperatures generally ranging from about 1500°C to about 1800°C are suitable for pressing times of about 15 minutes to about 2 hours.
* EXAMPLE 1 The following example will illustrate the present invention. Several component blends composed of finely divided commercial alumina powder- (average particle size 0.4 um) and silicon carbide whiskers (80% 10-80 um length, 0.6 um average diameter) were made up containing various ratios of the two compo- nents. The components of each sample were thoroughly blended and then cold pressed to form green bodies having densities in the range of 60-70% of theoretical density. Each green sample was then sintered at 2867°F (1575°C) for 1 hour. The following Table 1 presents the results of the experiments.
TABLE 1 .
Sample Whisker Green Density Sintered Density Number Content, % Theoretical % Theoretical
Volume %
1 6.1 68 97 2 16.1 68 97 3 12.1 61 97 4 12.1 62 97 5 18.0 65 93 6 23.7 65 79 7 29.2 65 76
It will be evident from these data that the samples with the lower whisker contents could be quite successfully sintered to high density products while the samples containing higher whisker contents were not significantly improved over the green products. The other properties of the final products, including toughness and strength, correspond in improvements to the improved densities. Thus, under the conditions of this invention pressureless sintering is found to produce highly satisfactory reinforced sintered products which have the improved toughness expected of whisker reinforced bodies.
EXAMPLE 2 Composites were formed which contained
7-1/2 volume % silicon carbide whiskers in an alumina matrix using the materials described above in Example 1; also a minor amount (5%) of organic binder (poly- vinyl alcohol and Carbowax) was included. The powders were thoroughly blended and cold pressed to form various given shapes. Shape A, a cuttingtool insert, was formed by axial pressing at 20,000 psi. Shapes B and C, nozzle and plug shapes, were formed by cold isopressing for 1 minute at 12,500 psi. In this latter procedure the blends were placed in a flexible container and isopressed in liquid as indicated at ambient temperature.
The green shapes formed as above indicated were heated in air to about 550°C to effectively remove organic binder. Shape A had a density in the range 58-62% of maximum theoretical while shapes B and C had densities in the range 58-60% of maximum theoretical.
The green shape composites were subjected to pressureless sintering at ambient pressure under a nitrogen atmosphere". Sintering was accomplished by heating the green shapes to 1595°C, maintaining the temperature for 1 hour, cooling to 1250°C, maintain- ing this temperature for 1 hour and then cooling to room temperature. In each case the density of the pressureless sintered composite was in excess of 94% of the theoretical maximum and each composite was characterized by closed porosity. The closed porosity sintered composites were subjected to containerless hot isostatic pres¬ sing in a argon gas autoclave. Over a period of 4 hours the composites were heated to 1575°C and then maintained at that temperature for 1 hour, the pres- sure being 20,000 psi. Thereafter the pressed com¬ posites were cooled over a 4 hour period.
The following Table 2 shows the change in percentage of theoretical maximum density which resulted after each of the above steps.
TABLE 2 Percentage of Maximum Theoretical Density After Pressureless Sintering After HIP*
Shape A 97.96 98. .99 Shape B 96.1 98. .9
96.0 98, .7
95.8 98. .7
95.8 98, .8
I
95.6 98. .7 I— '
Shape C 96.9 98, .6 I
96.7 98, .7
97.0 98, .7
*Hot Isostatic Press
As shown by the above, the closed porosity pressureless sintered composites are brought to well in excess of 98% of the theoretical density by hot isostatic pressing thus resulting in a composite characterized by exceedingly high strength and tough¬ ness. INDUSTRIAL APPLICABILITY
The process and products of this invention have applicability in a wide variety of industrial areas. Among these are production of sintered mate¬ rials for use as high strength cutting tools and other ceramic applications where toughness of a ceramic body or coating is of importance. It will be understood that the above description is intended to be exemplary and that there will be other embodiments which are not described but which are clearly within the scope and spirit of the present invention. The scope of the invention is therefore to be limited solely by the appended claims.

Claims

WHAT IS CLAIMED IS;
1. A method for the formation of high density reinforced ceramic bodies which comprises: a. Forming a mixture of 0.5-21 volume percent silicon carbide whiskers and the balance ceramic matrix powder; b. compacting said mixture to form a shaped body having a density of
55-70% of the theoretical maximum density of said body; and c. heating said body at a temperature and for a time sufficient to sinter said body into a unitary shaped structure having a density of at least 85% of the theoretical maximum density of the sintered body under pressureless .sintering conditions.
2. The method as in Claim 1 wherein said compaction in Step b. compacts the mixture to a den¬ sity in the range of 58-62% of the theoretical maximum density of the body.
3. The method as in Claim 1 wherein the sintering in Step c. is conducted at a temperature in the range of 70-90% of the melting temperature of the ceramic material comprising the ceramic matrix powder.
4. The method as in Claim 1 wherein the whisker content is in the range of 2-18 volume per¬ cent of the mixture.
5. The method as in Claim 1 wherein the ceramic matrix powder comprises alumina.
6. The method as in Claim 5 wherein the alumina powder further contains small quantities of magnesia or yttria.
7. A high density reinforced ceramic body formed by the pressureless sintering method of Claim 1.
8. A high density reinforced ceramic body formed by the pressureless sintering method of Claim 5.
9. The method of Claim 1 wherein said body is sintered into a closed porosity unitary shaped structure under pressureless sintering conditions.
10. The method of Claim 9 wherein the ceramic matrix powder comprises alumina.
11. The method of Claim 9 characterized by the further step of subjecting the said closed porosity unitary shaped article to a containerless hot isostatic pressing until the density of the shaped article is increased to at least 98% of the theoretical maximum density.
12. The densified shaped article formed by the method of Claim 11.
EP86902963A 1985-03-14 1986-03-13 High density reinforced ceramic bodies and method of making same Withdrawn EP0217946A1 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US71169685A 1985-03-14 1985-03-14
US711696 1985-03-14
US83124286A 1986-02-19 1986-02-19
US831242 1986-02-19

Publications (1)

Publication Number Publication Date
EP0217946A1 true EP0217946A1 (en) 1987-04-15

Family

ID=27108685

Family Applications (1)

Application Number Title Priority Date Filing Date
EP86902963A Withdrawn EP0217946A1 (en) 1985-03-14 1986-03-13 High density reinforced ceramic bodies and method of making same

Country Status (3)

Country Link
EP (1) EP0217946A1 (en)
AU (1) AU5868386A (en)
WO (1) WO1986005480A1 (en)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0816028B2 (en) * 1986-07-31 1996-02-21 日本特殊陶業株式会社 Highly tough ceramic sintered body, ceramic tool and method for manufacturing sintered body
US4946807A (en) * 1986-08-18 1990-08-07 Ngk Spark Plug Co., Ltd. Composite ceramic material reinforced with silicon carbide whiskers
FR2604702B1 (en) * 1986-10-02 1992-07-24 Desmarquest Ceramiques Tech PROCESS FOR THE MANUFACTURE OF COMPOSITE PARTS COMPRISING A MATRIX OF CERAMIC MATERIAL REINFORCED WITH ZIRCONIA PARTICLES AND POSSIBLY MONOCRYSTALLINE FIBERS OF SILICON CARBIDE
DE3706000A1 (en) * 1987-02-25 1988-09-08 Feldmuehle Ag Cutting tip (cutting insert, cutting tool)
DE3708689A1 (en) * 1987-03-17 1988-10-20 Max Planck Gesellschaft METHOD FOR HOT ISOSTATIC PRESSING OF CARBIDE FIBER AND CARBIDE WHISKER REINFORCED SILICON NITRIDE BODIES
JPS63265864A (en) * 1987-04-22 1988-11-02 Yoshida Kogyo Kk <Ykk> High-strength si3n4-sic whisker composite and its production
US4820663A (en) * 1987-09-02 1989-04-11 Kennametal Inc. Whisker reinforced ceramic and a method of clad/hot isostatic pressing same
US4956315A (en) * 1987-09-02 1990-09-11 Kennametal Inc. Whisker reinforced ceramics and a method of clad/hot isostatic pressing same
JPH01103205A (en) * 1987-10-15 1989-04-20 Toshiba Ceramics Co Ltd Tool for working carbon
JPH029777A (en) * 1988-03-02 1990-01-12 Honda Motor Co Ltd Fiber reinforced ceramic molded body and production thereof
US5024976A (en) * 1988-11-03 1991-06-18 Kennametal Inc. Alumina-zirconia-silicon carbide-magnesia ceramic cutting tools
US4959332A (en) * 1988-11-03 1990-09-25 Kennametal Inc. Alumina-zirconia-carbide whisker reinforced cutting tools
US4965231A (en) * 1988-11-03 1990-10-23 Kennametal Inc. Alumina-zirconia-silicon carbide-magnesia compositions and articles made therefrom
US4959331A (en) * 1988-11-03 1990-09-25 Kennametal Inc. Alumina-zirconia-silicon carbide-magnesia cutting tools
US4960735A (en) * 1988-11-03 1990-10-02 Kennametal Inc. Alumina-zirconia-silicon carbide-magnesia ceramics
US5227344A (en) * 1988-12-28 1993-07-13 Japan Metals & Chemicals Co., Ltd. Ceramics composite article and method for making same
US5059564A (en) * 1989-06-05 1991-10-22 Kennametal Inc. Alumina-titanium carbide-silicon carbide composition
US5009822A (en) * 1989-07-17 1991-04-23 University Of Florida Alumina-or alumina/zirconia-silicon carbide whisker ceramic composites and methods of manufacture
WO1991008992A1 (en) * 1989-12-13 1991-06-27 The Dow Chemical Company Silicon carbide whisker reinforced ceramic composites and method for making the same
SE469075B (en) * 1991-01-21 1993-05-10 Sandvik Ab WHISKER-STRENGTH OXID-BASED CERAMIC CUTTER
SE9100675D0 (en) * 1991-03-06 1991-03-06 Sandvik Ab CERAMIC WHISKER-REINFORCED CUTTING TOOL WITH PRE-FORMED CHIPBREAKERS FOR MACHINING
ES2099429T3 (en) * 1991-12-03 1997-05-16 Advanced Composite Materials PRESSURE-FREE SINTERING OF MATERIALS COMPOSED OF ALUMINA REINFORCED WITH MONOCRISTALS.
JPH07232959A (en) * 1993-12-21 1995-09-05 Kobe Steel Ltd Alumina-based ceramics and its production
ES2121714T3 (en) * 1995-11-13 2002-09-16 Kennametal Inc CERAMIC CUTTING TOOL REINFORCED WITH TRICKS AND COMPOSITION OF THE SAME.
US6204213B1 (en) 1999-09-18 2001-03-20 Kennametal Pc Inc. Whisker reinforced ceramic cutting tool and composition thereof
US6905992B2 (en) 2002-07-30 2005-06-14 Kennametal Inc. Ceramic body reinforced with coarse silicon carbide whiskers and method for making the same
CN102952542B (en) * 2012-10-24 2014-07-23 江苏博睿光电有限公司 Nitride or nitrogen oxide fluorescent powder and preparation method thereof

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB954285A (en) * 1959-01-15 1964-04-02 Ti Group Services Ltd Reinforced refractory materials
US3575789A (en) * 1966-12-27 1971-04-20 Owens Corning Fiberglass Corp Fiber ceramic composites and method of producing same
GB1377487A (en) * 1970-12-23 1974-12-18 Tokyo Shibaura Electric Co Heat resistant composite materials
JPS5833196B2 (en) * 1975-10-27 1983-07-18 トウホクダイガクキンゾクザイリヨウケンキユウシヨチヨウ Tainetsei Ceramics
US4410635A (en) * 1982-02-05 1983-10-18 United Technologies Corporation Discontinuous silicon carbide fiber reinforced ceramic composites
US4464192A (en) * 1982-05-25 1984-08-07 United Technologies Corporation Molding process for fiber reinforced glass matrix composite articles
US4507224A (en) * 1982-12-03 1985-03-26 Agency Of Industrial Science & Technology Ceramics containing fibers of silicon carbide
JPS59137366A (en) * 1983-01-24 1984-08-07 住友電気工業株式会社 Manufacture of ceramics
FR2555933A2 (en) * 1983-12-01 1985-06-07 Ceraver PROCESS FOR PRODUCING A COMPOSITE STRUCTURE REINFORCED WITH CERAMIC MATERIAL
US4543345A (en) * 1984-02-09 1985-09-24 The United States Of America As Represented By The Department Of Energy Silicon carbide whisker reinforced ceramic composites and method for making same

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO8605480A1 *

Also Published As

Publication number Publication date
AU5868386A (en) 1986-10-13
WO1986005480A1 (en) 1986-09-25

Similar Documents

Publication Publication Date Title
EP0217946A1 (en) High density reinforced ceramic bodies and method of making same
RU1830056C (en) Process for preparing composite material
US5053367A (en) Composite ceramic structures
US4891338A (en) Production of metal carbide articles
EP0378499B1 (en) A process for preparing selfsupporting bodies and products produced thereby
Greil et al. Sintering and HIPping of silicon nitride-silicon carbide composite materials
US5017334A (en) Process for preparing self-supporting bodies and products produced thereby
US4657876A (en) Composite by infiltration
EP0246610A2 (en) Composite by infiltration
US4636480A (en) Composite by infiltration
JPH06505225A (en) High-density, self-strengthening silicon nitride ceramic produced by pressureless or low-pressure gas sintering
EP0299905B1 (en) Process for preparing self-supporting bodies and products made thereby
CA2138662A1 (en) Method for in situ tailoring the component of ceramic articles and articles made thereby
US5464583A (en) Method for manufacturing whisker preforms and composites
US4833110A (en) Method for producing composite ceramic structures
Lee et al. Fabrication of TiB 2/TiC composites by the directional reaction of titanium with boron carbide
US5296417A (en) Self-supporting bodies
US5633213A (en) Method for in situ tailoring the component of ceramic articles
EP0754659A1 (en) Porous inorganic material and metal-matrix composite material containing the same and process therefor
EP0334577A1 (en) Carbon-coated silicon carbide whiskers for controlling the formation of an oxide coating
US5180697A (en) Process for preparing self-supporting bodies and products produced thereby
JPH0157075B2 (en)
US5047186A (en) Process for producing silicon nitride based articles of high fracture toughness and strength
EP0517449A2 (en) Infiltration forming composites of silicon carbide and molybdenum silicide free of silicon
WO1991011407A1 (en) Method of making large cross-section injection molded or slip cast ceramics shapes

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH DE FR GB IT LI LU NL SE

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19861216

RIN1 Information on inventor provided before grant (corrected)

Inventor name: RHODES, JAMES, F.

Inventor name: ROOTARE, HILLAR, M.

Inventor name: DZIEDZIC, CHESTER, J.