WO2011005808A2 - Hard non-oxide or oxide ceramic / hard non-oxide or oxide ceramic composite hybrid article - Google Patents
Hard non-oxide or oxide ceramic / hard non-oxide or oxide ceramic composite hybrid article Download PDFInfo
- Publication number
- WO2011005808A2 WO2011005808A2 PCT/US2010/041131 US2010041131W WO2011005808A2 WO 2011005808 A2 WO2011005808 A2 WO 2011005808A2 US 2010041131 W US2010041131 W US 2010041131W WO 2011005808 A2 WO2011005808 A2 WO 2011005808A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- oxide
- hard non
- oxide ceramic
- ceramic composite
- silicon carbide
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- 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
- C04B35/565—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 based on silicon carbide
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
- C04B35/628—Coating the powders or the macroscopic reinforcing agents
- C04B35/62802—Powder coating materials
- C04B35/62828—Non-oxide ceramics
- C04B35/62839—Carbon
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/001—Joining burned ceramic articles with other burned ceramic articles or other articles by heating directly with other burned ceramic articles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/043—Sliding surface consisting mainly of ceramics, cermets or hard carbon, e.g. diamond like carbon [DLC]
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/14—Special methods of manufacture; Running-in
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3205—Alkaline earth oxides or oxide forming salts thereof, e.g. beryllium oxide
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3817—Carbides
- C04B2235/3821—Boron carbides
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/40—Metallic constituents or additives not added as binding phase
- C04B2235/402—Aluminium
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/42—Non metallic elements added as constituents or additives, e.g. sulfur, phosphor, selenium or tellurium
- C04B2235/421—Boron
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/42—Non metallic elements added as constituents or additives, e.g. sulfur, phosphor, selenium or tellurium
- C04B2235/422—Carbon
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/42—Non metallic elements added as constituents or additives, e.g. sulfur, phosphor, selenium or tellurium
- C04B2235/422—Carbon
- C04B2235/425—Graphite
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
- C04B2237/343—Alumina or aluminates
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/36—Non-oxidic
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/36—Non-oxidic
- C04B2237/363—Carbon
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/36—Non-oxidic
- C04B2237/365—Silicon carbide
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/36—Non-oxidic
- C04B2237/368—Silicon nitride
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2220/00—Shaping
- F16C2220/60—Shaping by removing material, e.g. machining
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2220/00—Shaping
- F16C2220/60—Shaping by removing material, e.g. machining
- F16C2220/70—Shaping by removing material, e.g. machining by grinding
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12576—Boride, carbide or nitride component
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249967—Inorganic matrix in void-containing component
- Y10T428/249969—Of silicon-containing material [e.g., glass, etc.]
Definitions
- This invention relates to the field of articles formed from components of hard non-oxide or oxide ceramic materials and composites of these same materials.
- Hard non-oxide or oxide ceramic materials are commonly used in applications requiring materials with a high hardness, superior strength, good corrosion resistance, and high thermal conductivity, such as the materials used in acidic, caustic, corrosive, abrasive, high speed, or high temperature environments. These types of applications include rotating equipment, pump seals and bearings, gas turbine
- hard non-oxide or oxide ceramic materials include but are not limited to silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride.
- a drawback to these hard non-oxide or oxide ceramic materials is the lack of self-lubricity when used alone.
- a self-lubricating solid is one having low friction in the absence of an adequate lubricant.
- parts, such as seals or bearings having a hard non-oxide or oxide ceramic material surface adjoining with relative motion against another surface made of the same or other hard non-oxide or oxide ceramic material, other silicon carbide materials, other ceramics, or steel will wear excessively due to the forces generated by the high friction.
- special wear surfaces must be provided on at least one of the bodies.
- Graphite is a known lubricant and has been incorporated into carbon and silicon carbide materials to impart a self-lubricating property to the material.
- U.S. Patent Nos. 5,580,834, 5,656,563, and 5,968,653, the contents of which are incorporated herein by reference teach the use of a carbon graphite/silicon carbide composite material.
- Other inclusions, such as tribology enhancing additives, porosity, boron carbide, etc., can also improve the tribology of the material.
- the composite materials have wear resistance superior to hard non-oxide or oxide ceramic materials, in that the material of the present invention can run against itself or other hard non-oxide or oxide ceramic, non-self-lubricating materials in sliding face applications, such as for mechanical seals and pump bearings, in marginal lubrication conditions.
- Composite materials also have thermal shock resistance superior to hard non-oxide or oxide ceramic materials. In catastrophic failure or dry run conditions, such as when fluid is lost in pump applications, seals and bearings made of the composite material have enhanced survivability and can maintain their integrity, while seals and bearings made of hard non- oxide or oxide ceramic materials can fail almost immediately.
- a drawback to the use of composite materials alone is that the composite material does not exhibit the same level of superior hardness, corrosion resistance, thermal conductivity, and strength that are enhanced physical properties of hard non-oxide or oxide ceramic materials.
- Embodiments of the invention include a hybrid article comprising at least one hard non-oxide or oxide ceramic component of at least 95% of theoretical density directly bonded to, and different from, a hard non-oxide or oxide ceramic composite component comprising a tribology enhancing component.
- the at least one hard non-oxide or oxide ceramic component comprises a member of the group consisting of silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride.
- the at least one hard non-oxide or oxide ceramic composite component comprises a member of the group consisting of silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride.
- the tribology enhancing additive may be selected from the group consisting of but not limited to porosity, carbon graphite, graphite, and boron carbide.
- the hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article comprises a hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid seal component comprising a wall having a thickness at least in part greater than 2.5 mm.
- the hybrid article is formed by preparing at least one hard non-oxide or oxide ceramic body of at least 95% of theoretical density, preparing at least one hard non-oxide or oxide ceramic composite body comprising a tribology enhancing component, placing the bodies into contact with one another to form a hybrid article, and treating the hybrid article to directly bond the bodies.
- treating the hybrid article comprises hot isostatic pressing. In other embodiments, treating the hybrid article comprises pressureless sintering. In yet other embodiments, treating the hybrid article comprises liquid phase sintering. In still other embodiments, treating the hybrid article comprises reaction bonding.
- Figure 1 is a front view of a hybrid article according to one embodiment of the present invention.
- Figure 2 is a cross-sectional view of the hybrid article of Figure 1 taken along line 2-2.
- Figure 3 is a side view of a portion of the surface of the hybrid article of
- Figure 4 is another side view of a portion of the surface of the hybrid article of Figure 1.
- Figure 5 is a front view of a hybrid article according to another
- Figure 6 is a cross-sectional view of the hybrid article of Figure 5 taken along line 6-6.
- Figure 7 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1.
- Figure 8 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1.
- Figure 9 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1.
- Figure 10 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1.
- Figure 11 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1 taken from an alternate orientation.
- Figure 12 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1 taken from an alternate orientation.
- Embodiments of the invention provide a hybrid article comprising at least one hard non-oxide or oxide ceramic component coupled to at least hard non-oxide or oxide ceramic composite component to create a hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article.
- FIGs 1-12 illustrate embodiments of a hybrid article 10.
- the hybrid article 10 comprises at least one hard non-oxide or oxide ceramic component 12 and at least one hard non-oxide or oxide ceramic composite component 14. As shown in Figures 7-12, an interface 16 is formed between the components 12 and 14. The interface 16 demonstrates a clear transition from the at least one hard non-oxide or oxide ceramic component 12 to the at least one hard non-oxide or oxide ceramic composite component 14.
- the hybrid article 10 comprises at least one hard non-oxide or oxide ceramic component 12 coupled to a plurality of hard non-oxide or oxide ceramic composite components 14.
- the hybrid material comprises a plurality of hard non-oxide or oxide ceramic components 12 coupled to a plurality of hard non-oxide or oxide ceramic composite components 14.
- the combination of the components 12 and 14 in the hybrid article 10 is configured so that at least one hard non-oxide or oxide ceramic composite component 14 is positioned adjacent surfaces of the hybrid article 10 requiring enhanced tribological capability.
- the interface 16 comprises a robust bond between the at least hard non-oxide or oxide ceramic component 12 and the at least one hard non- oxide or oxide ceramic composite component 14.
- the resultant hybrid article 10 is a stiff and strong article with enhanced tribological capability, particularly suitable for seal components, axial bearing components, and radial bearing components, although the hybrid article 10 may be used in any suitable application.
- the hybrid article 10 may comprise a cylindrical shape 18, although one of ordinary skill in the relevant art will understand that the hybrid article may have any suitable shape including but not limited to rectilinear, spherical, frusto-conical, or other similar shapes.
- the embodiment of the hybrid article 10 shown in Figures 1-4 comprises a plurality of inner diameters along its length so that an inner surface 24 includes a plurality of cross-sectional shapes.
- the embodiment of the hybrid article 10 shown in Figures 1-4 also comprises a plurality of outer diameters along its length so that an outer surface 26 includes a plurality of cross-sectional shapes.
- an alternative embodiment of the hybrid article 10 shown in Figures 5 and 6 comprises a uniform inner diameter and a uniform outer diameter along its length so that the inner surface 24 and the outer surface 26 each have a uniform cross-sectional shape.
- any suitable shape for the hybrid article 10 may be used.
- the at least one hard non-oxide or oxide ceramic composite component 14 is located on a seal face 20 of the hybrid article 10.
- the at least one hard non-oxide or oxide ceramic composite component 14 has a thickness at least in part greater than 2.5 mm.
- the at least one hard non-oxide or oxide ceramic composite component 14 may be located on an opposing end 22 of the hybrid article 10, on both the seal face 20 and the opposing end 22, the inner surface 24, the outer surface 26, or any combination thereof.
- the at least one hard non-oxide or oxide ceramic component 12 comprises a substantially dense ceramic material.
- the at least one hard non-oxide or oxide ceramic component 12 comprises a monolithic ceramic, where "monolithic ceramic” is intended to describe a ceramic that is uniformly formed of a single ceramic or a combination of ceramics that are combined in such a way that the individual components are indistinguishable.
- the at least one hard non-oxide or oxide ceramic component 12 comprises tungsten carbide, aluminum oxide, or silicon nitride.
- the at least one hard non-oxide or oxide ceramic component 12 comprises silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, or reaction bonded silicon carbide.
- the density of the at least one hard non-oxide or oxide ceramic material may have any appropriate density, up to and including 100% of the theoretical density. In some embodiments, the density of the at least one hard non-oxide or oxide ceramic material is at least 95% of theoretical density.
- the silicon carbide material has a solid appearance with few visible pores.
- the silicon carbide material can be of the alpha form, the beta form, or a combination of these or other forms.
- the at least one hard non-oxide or oxide ceramic composite component 14 comprises tungsten carbide, aluminum oxide, or silicon nitride. In other embodiments, the at least one hard non-oxide or oxide ceramic composite component 14 comprises silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, or reaction bonded silicon carbide.
- the hard non-oxide or oxide ceramic composite material has a microstructure of non-interconnected inclusions.
- the composite material comprises a densified self-sintered matrix of approximately 50 to 95% by weight silicon carbide, approximately 5.0 to 50% by weight of inclusions dispersed throughout the matrix, and small amounts, approximately 0.3 or less to 5.0% by weight, of any residual sintering aids, such as (but not limited to) aluminum, beryllium oxide, boron, boron carbide, and/or free carbon.
- any residual sintering aids such as (but not limited to) aluminum, beryllium oxide, boron, boron carbide, and/or free carbon.
- the hard non-oxide or oxide ceramic composite material typically has a density that is representative of the composite's composition as determined by the rule of mixtures.
- the composite silicon carbide can be of the alpha form, the beta form, or a combination of these or other forms.
- the inclusions are distributed throughout the silicon carbide of the composite material.
- the average grain size of the carbon graphite inclusions is greater than the average grain size of the silicon carbide.
- the silicon carbide has an average grain size between approximately 10 and 25 ⁇ m, and the carbon graphite inclusions have an average grain size between approximately 75 and 125 ⁇ m.
- the hard non-oxide or oxide ceramic component materials include but are not limited to silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride.
- the tungsten carbide, aluminum oxide, and silicon nitride embodiments of the at least one hard non- oxide or oxide ceramic component 12 are manufactured in a known manner.
- the silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, and reaction bonded silicon carbide embodiments of the at least one hard non-oxide or oxide ceramic component 12 are also manufactured in a known manner.
- the at least one hard non-oxide or oxide ceramic component 12 may be produced from a raw batch including the hard non-oxide or oxide ceramic material.
- the silicon carbide embodiments of the at least one hard non-oxide or oxide ceramic component 12 may be produced from a raw batch of silicon carbide, which includes fine (sub-micron) and pure silicon carbide powder.
- ⁇ -silicon carbide is used.
- any combination of the forms of silicon carbide may be used.
- sintering aids such as non-oxide sintering aids, aluminum; mineral oxides including but not limited to beryllium oxide, aluminum oxide, magnesium oxide, yttrium oxide; a boron source; and/or a carbon source are added to the raw batch and mixed thoroughly to ensure complete dispersion.
- Boron sources include elemental boron and boron carbide (B 4 C), and carbon sources include elemental carbon or a carbonizable organic material, such as phenolic resin, petroleum pitch, coal tar pitch, furfuryl alcohol or sugar.
- the hard non-oxide or oxide ceramic composite component materials include but are not limited to silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride.
- the tungsten carbide, aluminum oxide, and silicon nitride embodiments of the at least one hard non-oxide or oxide ceramic composite component 14 are manufactured in a known manner.
- the silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, and reaction bonded silicon carbide embodiments of the at least one hard non-oxide or oxide ceramic composite component 14 are also present.
- the at least one hard non-oxide or oxide ceramic composite component 14 may be produced from a raw batch including the hard non-oxide or oxide ceramic material and inclusion particles.
- the composite material may be produced from a raw batch of silicon carbide.
- the raw batch is produced from finegrained, high purity silicon carbide powder.
- any combination of the forms of silicon carbide may be used.
- silicon carbide is dispersed in an inert solvent, such as water, to form a slurry which aids complete mixing of the raw batch ingredients during preparation.
- an inert solvent such as water
- Other mixing aids such as a dispersant (for example ammonium polymethacrylate) or a suspension agent, such as xanthan gum, may also be added.
- a temporary filler may also be added to the raw batch slurry and thoroughly mixed for good dispersion to provide green strength.
- the temporary filler can be any particulate material which will decompose and volatilize out of the mixture at or below the carbonization temperature of the mixture to create a microstructure of non-interconnected inclusions.
- the temporary filler comprises particles of an organic material, such as ground nutshells, wax particles, or polypropylene beads.
- an inorganic material such as ceramic beads might also be used.
- the temporary filler has an average grain size between approximately 10 and 45 ⁇ m.
- Inclusions are also added to the slurry and thoroughly mixed for good dispersion.
- Inclusions suitable for use in the present invention may include any additive capable of improving the tribological capability of the at least one hard non-oxide or oxide ceramic composite component 14.
- inclusions may be, but are not limited to, porosity, graphite, carbon graphite, boron carbide, and other tribology enhancing additives.
- coated graphite particles are added to the slurry.
- the coated graphite particles are coarse graphite particles coated with a carbon precursor, such as phenolic resin, or another resin or material which will decompose upon heating to leave a carbon residue.
- a carbon precursor such as phenolic resin, or another resin or material which will decompose upon heating to leave a carbon residue.
- Such other materials include furfuryl alcohol, polyester, petroleum pitch, coal tar pitch, or mixtures of these and other materials.
- the coating is dissolved in a suitable solvent and mixed thoroughly with the graphite to bond the graphite particles.
- the mixture is then dried to evaporate the solvent and crushed to obtain the coated graphite particles of a desired size.
- the coated graphite particles are passed through a 65 mesh sieve to obtain particles of less than 212 ⁇ m.
- coated graphite particles are then added to the slurry. Typically, approximately at least 5.0 to 50%, and preferably approximately 10 to 20%, by weight (of the total raw batch) of the coated graphite particles are added to the slurry. But any amount of such particles is helpful in improving the self-lubricating properties of the final composite material.
- Process aids including temporary binders and lubricants, for example oleic acid or any other fatty acid, can be added to the slurry to facilitate the molding or shaping of the raw batch into a green body or to facilitate other processing steps.
- a suspension or viscosity agent is particularly helpful if the inclusion particles are large.
- xanthan gum is added to the slurry and mixed, it causes the slurry to coagulate, which holds the inclusion particles in suspension, allowing uniform dispersion.
- Some materials added to the raw batch can perform multiple functions. For example, phenolic resin can function in the raw batch as both a carbon source sintering aid and a temporary binder. Polyethylene glycol can function as both a temporary binder and a die lubricant.
- the inert solvent, temporary filler, temporary binder, dispersant, lubricant, and suspension agent are all temporary additives, which do not form a part of the final hard non-oxide or oxide ceramic composite material.
- sintering aids such as aluminum; mineral oxides including but not limited to beryllium oxide, aluminum oxide, magnesium oxide, yttrium oxide; a boron source; and/or a carbon source are added to the slurry and mixed thoroughly to ensure complete dispersion.
- Boron sources include elemental boron and boron carbide (B 4 C)
- carbon sources include elemental carbon or a carbonizable organic material, such as phenolic resin, petroleum pitch, coal tar pitch, furfuryl alcohol or sugar.
- approximately 2.0 to 20% by weight (of the total raw batch) of the sintering aids are added to the slurry.
- the resulting slurry is mixed thoroughly to ensure sufficient dispersion and dried.
- the slurry is spray dried to form spherical agglomerates.
- Other suitable methods for obtaining such granules such as pan drying followed by crushing and sieving, may be employed.
- the at least one hard non-oxide or oxide ceramic component 12 and the at least one hard non-oxide or oxide ceramic composite component 14 are assembled during the same forming process to create the hybrid article 10 having the interface 16 between the components.
- the at least one hard non-oxide or oxide ceramic component 12 and the at least one hard non-oxide or oxide ceramic composite component 14 include the same hard non-oxide or oxide ceramic material.
- the at least one hard non-oxide or oxide ceramic component 12 and the at least one hard non- oxide or oxide ceramic composite component 14 may include different hard non-oxide or oxide ceramic materials.
- the at least one hard non-oxide or oxide ceramic component 12 is assembled with the at least one hard non-oxide or oxide ceramic composite component 14. In other embodiments, the at least one hard non-oxide or oxide ceramic component 12 is assembled with a plurality of hard non-oxide or oxide ceramic composite components 14. In yet other embodiments, a plurality of hard non-oxide or oxide ceramic components 12 are assembled with a plurality of hard non-oxide or oxide ceramic composite components 14.
- the assembly of the components 12 and 14 in the hybrid article 10 is configured so that the at least one hard non-oxide or oxide ceramic composite component 14 is positioned adjacent surfaces of the hybrid article 10 requiring enhanced tribological capability.
- Conventional methods of molding and shaping can be employed, such as isostatic or die pressing, of the hybrid article to form a green body.
- the hybrid article is pressed at pressures ranging between approximately 3 and 9 tons/in2.
- the hybrid article 10 is then exposed to the appropriate environment, such as heat, to cure any temporary binders included in the composite component.
- the molding and shaping of the hybrid article 10 can also include machining to a desired pre- finished shape and designed in such a manner so that the at least one hard non-oxide or oxide ceramic composite component 14 is positioned adjacent surfaces of the hybrid article 10 requiring enhanced tribological capability.
- the shaped green body is then carbonized in a non-oxidizing atmosphere at a temperature typically above approximately 800 0 F.
- the carbonization step carbonizes any carbonizable carbon source used as a sintering aid and decomposes and volatilizes the temporary filler, which leaves a microstructure of non-interconnected inclusions.
- the carbonization step also carbonizes the resin of the resin-coated graphite particles and volatilizes any residue of any dispersant, lubricant, or suspension agent included in the composite component.
- the green body is heated in an oven from room temperature to 350 0 F during a half hour and allowed to soak at that temperature for another half hour. The temperature is then raised to 850 0 F over a period of 10 hours and held at 850 0 F for five hours to carbonize the body. The hybrid article 10 is then cooled to room temperature. Other carbonization cycles may be used.
- the hybrid article 10 is then sintered via hot isostatic pressing, pressureless sintering, or liquid phase sintering, creating a seamless connection between the two components.
- the temperature is raised to the sintering temperature over an eight hour period, the furnace is held at the peak temperature for one hour, and then allowed to cool to room temperature. The actual times depend upon the particular furnace used. Other suitable sintering cycles may also be employed.
- transient liquid phase sintering occurs when the liquid phase is absorbed by the solid phase during sintering. Because the amount of liquid that forms and the time for which it exists are dependent on the sintering conditions, transient liquid phase sintering is process sensitive.
- the liquid phase can form directly by melting of eutectic phase mixtures that form by diffusion or by incipient melting.
- the liquid flows between the powder particles, filling pores and causing densification by capillary action and through the provision of a fast diffusion pathway. Shrinkage occurs by particle rearrangement if the liquid volume is high enough and the green density is low enough, by the particles changing shape to allow better packing, by pore filling and by solid state sintering if a solid skeleton forms.
- the hybrid article 10 is infiltrated with liquid silicon.
- the silicon reacts with the carbon to form silicon carbide.
- the reaction product bonds the silicon carbide particles, and any excess silicon fills any remaining pores.
- the hybrid article 10 can be finished by grinding, diamond polishing, or any other finishing method.
- the article is designed in such a manner as to ensure the composite material is located on those surfaces requiring enhanced tribological capability.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Inorganic Chemistry (AREA)
- Ceramic Products (AREA)
- Compositions Of Oxide Ceramics (AREA)
- Gasket Seals (AREA)
Abstract
Embodiments of the invention include a hybrid article comprising at least one hard non-oxide or oxide ceramic component of at least 95% of theoretical density directly bonded to, and different from, a hard non-oxide or oxide ceramic composite component comprising a tribology enhancing component. The at least one hard non-oxide or oxide ceramic component comprises a member of the group consisting of silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride. The at least one hard non-oxide or oxide ceramic composite component comprises a member of the group consisting of silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride. In some embodiments, the hybrid article is formed by preparing at least one hard non-oxide or oxide ceramic body of at least 95% of theoretical density, preparing at least one hard non-oxide or oxide ceramic composite body comprising a tribology enhancing component, placing the bodies into contact with one another to form a hybrid article, and treating the hybrid article to directly bond the bodies. In some embodiments, treating the hybrid article may include hot isostatic pressing, pressureless sintering, liquid phase sintering, or reaction bonding.
Description
HARD NON-OXIDE OR OXIDE CERAMIC / HARD NON-OXIDE OR OXIDE CERAMIC COMPOSITE HYBRID ARTICLE
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] This application is related to and claims priority benefits from U.S.
Provisional Application Serial No. 61/223,629, filed on July 7, 2009, entitled
MONOLITHIC/ COMPOSITE SILICON CARBIDE LAYERED ARTICLE, and U.S. Provisional Application Serial No. 61/328,262, filed on April 27, 2010, entitled HARD NON-OXIDE OR OXIDE CERAMIC/HARD NON-OXIDE OR OXIDE CERAMIC COMPOSITE HYBRID ARTICLE. The '629 and '262 applications are hereby incorporated in their entirety by this reference.
FIELD OF THE INVENTION
[0002] This invention relates to the field of articles formed from components of hard non-oxide or oxide ceramic materials and composites of these same materials.
BACKGROUND
[0003] Hard non-oxide or oxide ceramic materials are commonly used in applications requiring materials with a high hardness, superior strength, good corrosion resistance, and high thermal conductivity, such as the materials used in acidic, caustic, corrosive, abrasive, high speed, or high temperature environments. These types of applications include rotating equipment, pump seals and bearings, gas turbine
components, mixing nozzles, and flame holders. Examples of these hard non-oxide or oxide ceramic materials include but are not limited to silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride.
[0004] A drawback to these hard non-oxide or oxide ceramic materials is the lack of self-lubricity when used alone. A self-lubricating solid is one having low friction in the absence of an adequate lubricant. For example, in applications having a high PV (pressure-sliding velocity) or marginal lubrication conditions, parts, such as seals or bearings, having a hard non-oxide or oxide ceramic material surface adjoining with relative motion against another surface made of the same or other hard non-oxide or oxide
ceramic material, other silicon carbide materials, other ceramics, or steel will wear excessively due to the forces generated by the high friction. In marginal lubrication conditions with mating surfaces, special wear surfaces must be provided on at least one of the bodies.
[0005] Graphite is a known lubricant and has been incorporated into carbon and silicon carbide materials to impart a self-lubricating property to the material. For example, U.S. Patent Nos. 5,580,834, 5,656,563, and 5,968,653, the contents of which are incorporated herein by reference, teach the use of a carbon graphite/silicon carbide composite material. Other inclusions, such as tribology enhancing additives, porosity, boron carbide, etc., can also improve the tribology of the material. The composite materials have wear resistance superior to hard non-oxide or oxide ceramic materials, in that the material of the present invention can run against itself or other hard non-oxide or oxide ceramic, non-self-lubricating materials in sliding face applications, such as for mechanical seals and pump bearings, in marginal lubrication conditions. Composite materials also have thermal shock resistance superior to hard non-oxide or oxide ceramic materials. In catastrophic failure or dry run conditions, such as when fluid is lost in pump applications, seals and bearings made of the composite material have enhanced survivability and can maintain their integrity, while seals and bearings made of hard non- oxide or oxide ceramic materials can fail almost immediately. However, a drawback to the use of composite materials alone is that the composite material does not exhibit the same level of superior hardness, corrosion resistance, thermal conductivity, and strength that are enhanced physical properties of hard non-oxide or oxide ceramic materials.
[0006] Accordingly, there is a need to combine the superior physical properties of hard non-oxide or oxide ceramic materials with the enhanced tribological capability of composite versions of these hard non-oxide or oxide ceramic materials.
SUMMARY
[0007] Embodiments of the invention include a hybrid article comprising at least one hard non-oxide or oxide ceramic component of at least 95% of theoretical density directly bonded to, and different from, a hard non-oxide or oxide ceramic composite component comprising a tribology enhancing component.
[0008] In some embodiments, the at least one hard non-oxide or oxide ceramic component comprises a member of the group consisting of silicon carbide, pressureless
sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride.
[0009] In some embodiments, the at least one hard non-oxide or oxide ceramic composite component comprises a member of the group consisting of silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride. The tribology enhancing additive may be selected from the group consisting of but not limited to porosity, carbon graphite, graphite, and boron carbide.
[0010] In some embodiments, the hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article comprises a hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid seal component comprising a wall having a thickness at least in part greater than 2.5 mm.
[0011] In some embodiments, the hybrid article is formed by preparing at least one hard non-oxide or oxide ceramic body of at least 95% of theoretical density, preparing at least one hard non-oxide or oxide ceramic composite body comprising a tribology enhancing component, placing the bodies into contact with one another to form a hybrid article, and treating the hybrid article to directly bond the bodies.
[0012] In some embodiments, treating the hybrid article comprises hot isostatic pressing. In other embodiments, treating the hybrid article comprises pressureless sintering. In yet other embodiments, treating the hybrid article comprises liquid phase sintering. In still other embodiments, treating the hybrid article comprises reaction bonding.
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] The present invention will be more fully understood from the following detailed description considered in conjunction with the accompanying drawings, in which:
[0014] Figure 1 is a front view of a hybrid article according to one embodiment of the present invention.
[0015] Figure 2 is a cross-sectional view of the hybrid article of Figure 1 taken along line 2-2.
[0016] Figure 3 is a side view of a portion of the surface of the hybrid article of
Figure 1.
[0017] Figure 4 is another side view of a portion of the surface of the hybrid article of Figure 1.
[0018] Figure 5 is a front view of a hybrid article according to another
embodiment of the present invention.
[0019] Figure 6 is a cross-sectional view of the hybrid article of Figure 5 taken along line 6-6.
[0020] Figure 7 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1.
[0021] Figure 8 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1.
[0022] Figure 9 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1.
[0023] Figure 10 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1.
[0024] Figure 11 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1 taken from an alternate orientation.
[0025] Figure 12 is a photomicrograph of the cross-sectional view of the hybrid article of Figure 1 taken from an alternate orientation.
DETAILED DESCRIPTION
[0026] Embodiments of the invention provide a hybrid article comprising at least one hard non-oxide or oxide ceramic component coupled to at least hard non-oxide or oxide ceramic composite component to create a hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article.
[0027] Figures 1-12 illustrate embodiments of a hybrid article 10. The hybrid article 10 comprises at least one hard non-oxide or oxide ceramic component 12 and at least one hard non-oxide or oxide ceramic composite component 14. As shown in Figures 7-12, an interface 16 is formed between the components 12 and 14. The interface 16 demonstrates a clear transition from the at least one hard non-oxide or oxide ceramic component 12 to the at least one hard non-oxide or oxide ceramic composite component 14. In other embodiments, the hybrid article 10 comprises at least one hard non-oxide or oxide ceramic component 12 coupled to a plurality of hard non-oxide or
oxide ceramic composite components 14. In yet other embodiments, the hybrid material comprises a plurality of hard non-oxide or oxide ceramic components 12 coupled to a plurality of hard non-oxide or oxide ceramic composite components 14.
[0028] In some embodiments, the combination of the components 12 and 14 in the hybrid article 10 is configured so that at least one hard non-oxide or oxide ceramic composite component 14 is positioned adjacent surfaces of the hybrid article 10 requiring enhanced tribological capability. The interface 16 comprises a robust bond between the at least hard non-oxide or oxide ceramic component 12 and the at least one hard non- oxide or oxide ceramic composite component 14. The resultant hybrid article 10 is a stiff and strong article with enhanced tribological capability, particularly suitable for seal components, axial bearing components, and radial bearing components, although the hybrid article 10 may be used in any suitable application.
[0029] For example, in some embodiments as shown in Figures 1 and 5, the hybrid article 10 may comprise a cylindrical shape 18, although one of ordinary skill in the relevant art will understand that the hybrid article may have any suitable shape including but not limited to rectilinear, spherical, frusto-conical, or other similar shapes. For example, the embodiment of the hybrid article 10 shown in Figures 1-4 comprises a plurality of inner diameters along its length so that an inner surface 24 includes a plurality of cross-sectional shapes. The embodiment of the hybrid article 10 shown in Figures 1-4 also comprises a plurality of outer diameters along its length so that an outer surface 26 includes a plurality of cross-sectional shapes. In contrast, an alternative embodiment of the hybrid article 10 shown in Figures 5 and 6 comprises a uniform inner diameter and a uniform outer diameter along its length so that the inner surface 24 and the outer surface 26 each have a uniform cross-sectional shape. However, one of ordinary skill in the relevant art will understand that any suitable shape for the hybrid article 10 may be used.
[0030] In the embodiments shown in Figures 1-6, the at least one hard non-oxide or oxide ceramic composite component 14 is located on a seal face 20 of the hybrid article 10. In this embodiment, the at least one hard non-oxide or oxide ceramic composite component 14 has a thickness at least in part greater than 2.5 mm. However, one of skill in the relevant art will understand that any appropriate thickness may be used. In other embodiments, the at least one hard non-oxide or oxide ceramic composite component 14 may be located on an opposing end 22 of the hybrid article 10, on both the
seal face 20 and the opposing end 22, the inner surface 24, the outer surface 26, or any combination thereof.
[0031] In some embodiments, the at least one hard non-oxide or oxide ceramic component 12 comprises a substantially dense ceramic material. In some embodiments, the at least one hard non-oxide or oxide ceramic component 12 comprises a monolithic ceramic, where "monolithic ceramic" is intended to describe a ceramic that is uniformly formed of a single ceramic or a combination of ceramics that are combined in such a way that the individual components are indistinguishable. In some embodiments, the at least one hard non-oxide or oxide ceramic component 12 comprises tungsten carbide, aluminum oxide, or silicon nitride. In other embodiments, the at least one hard non-oxide or oxide ceramic component 12 comprises silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, or reaction bonded silicon carbide. The density of the at least one hard non-oxide or oxide ceramic material may have any appropriate density, up to and including 100% of the theoretical density. In some embodiments, the density of the at least one hard non-oxide or oxide ceramic material is at least 95% of theoretical density.
[0032] With respect to the silicon carbide embodiments of the at least one hard non-oxide or oxide ceramic component 12, the silicon carbide material has a solid appearance with few visible pores. The silicon carbide material can be of the alpha form, the beta form, or a combination of these or other forms.
[0033] In some embodiments, the at least one hard non-oxide or oxide ceramic composite component 14 comprises tungsten carbide, aluminum oxide, or silicon nitride. In other embodiments, the at least one hard non-oxide or oxide ceramic composite component 14 comprises silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, or reaction bonded silicon carbide. The hard non-oxide or oxide ceramic composite material has a microstructure of non-interconnected inclusions.
[0034] With respect to the silicon carbide embodiments of the at least one hard non-oxide or oxide ceramic composite component 14, the composite material comprises a densified self-sintered matrix of approximately 50 to 95% by weight silicon carbide, approximately 5.0 to 50% by weight of inclusions dispersed throughout the matrix, and small amounts, approximately 0.3 or less to 5.0% by weight, of any residual sintering
aids, such as (but not limited to) aluminum, beryllium oxide, boron, boron carbide, and/or free carbon.
[0035] The hard non-oxide or oxide ceramic composite material typically has a density that is representative of the composite's composition as determined by the rule of mixtures. With respect to the silicon carbide embodiments of the at least one hard non- oxide or oxide ceramic composite component 14, the composite silicon carbide can be of the alpha form, the beta form, or a combination of these or other forms.
[0036] With respect to the silicon carbide embodiments of the at least one hard non-oxide or oxide ceramic composite component 14, the inclusions are distributed throughout the silicon carbide of the composite material. In one embodiment, the average grain size of the carbon graphite inclusions is greater than the average grain size of the silicon carbide. For example, in this embodiment, the silicon carbide has an average grain size between approximately 10 and 25 μm, and the carbon graphite inclusions have an average grain size between approximately 75 and 125 μm.
A. Preparation of the Hard Non-Oxide or Oxide Ceramic Component
[0037] The hard non-oxide or oxide ceramic component materials include but are not limited to silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride. As will be understood by one of skill in the relevant art, the tungsten carbide, aluminum oxide, and silicon nitride embodiments of the at least one hard non- oxide or oxide ceramic component 12 are manufactured in a known manner.
[0038] Likewise, the silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, and reaction bonded silicon carbide embodiments of the at least one hard non-oxide or oxide ceramic component 12 are also manufactured in a known manner. The at least one hard non-oxide or oxide ceramic component 12 may be produced from a raw batch including the hard non-oxide or oxide ceramic material. For example, the silicon carbide embodiments of the at least one hard non-oxide or oxide ceramic component 12 may be produced from a raw batch of silicon carbide, which includes fine (sub-micron) and pure silicon carbide powder. Preferably, α-silicon carbide is used. However, any combination of the forms of silicon carbide may be used.
[0039] In the silicon carbide, pressureless sintered silicon carbide, and liquid phase sintered silicon carbide embodiments, sintering aids, such as non-oxide sintering aids,
aluminum; mineral oxides including but not limited to beryllium oxide, aluminum oxide, magnesium oxide, yttrium oxide; a boron source; and/or a carbon source are added to the raw batch and mixed thoroughly to ensure complete dispersion. Boron sources include elemental boron and boron carbide (B4C), and carbon sources include elemental carbon or a carbonizable organic material, such as phenolic resin, petroleum pitch, coal tar pitch, furfuryl alcohol or sugar.
B. Preparation of the Hard Non-oxide or Oxide Ceramic Composite Component
[0040] The hard non-oxide or oxide ceramic composite component materials include but are not limited to silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, reaction bonded silicon carbide, tungsten carbide, aluminum oxide, and silicon nitride. As will be understood by one of skill in the relevant art, the tungsten carbide, aluminum oxide, and silicon nitride embodiments of the at least one hard non-oxide or oxide ceramic composite component 14 are manufactured in a known manner.
[0041] Likewise, the silicon carbide, pressureless sintered silicon carbide, liquid phase sintered silicon carbide, and reaction bonded silicon carbide embodiments of the at least one hard non-oxide or oxide ceramic composite component 14 are also
manufactured in a known manner.
[0042] The at least one hard non-oxide or oxide ceramic composite component 14 may be produced from a raw batch including the hard non-oxide or oxide ceramic material and inclusion particles. In the silicon carbide embodiments of the at least one hard non-oxide or oxide ceramic composite components 14, the composite material may be produced from a raw batch of silicon carbide. The raw batch is produced from finegrained, high purity silicon carbide powder. Preferably, at least 0.5% α-silicon carbide relative to β-silicon carbide is used. However, any combination of the forms of silicon carbide may be used. Typically, approximately 50 to 90% by weight (of the total raw batch) of silicon carbide is dispersed in an inert solvent, such as water, to form a slurry which aids complete mixing of the raw batch ingredients during preparation. Other mixing aids, such as a dispersant (for example ammonium polymethacrylate) or a suspension agent, such as xanthan gum, may also be added.
[0043] A temporary filler may also be added to the raw batch slurry and thoroughly mixed for good dispersion to provide green strength. Typically,
approximately 0.75 to 15.0% (of the total raw batch) of the temporary filler is added to the slurry. The temporary filler can be any particulate material which will decompose and volatilize out of the mixture at or below the carbonization temperature of the mixture to create a microstructure of non-interconnected inclusions. Typically, the temporary filler comprises particles of an organic material, such as ground nutshells, wax particles, or polypropylene beads. In certain circumstances, for example when the temporary filler is volatilized in a vacuum at very high temperatures (at or above the melting point of the filler), an inorganic material such as ceramic beads might also be used. Preferably, the temporary filler has an average grain size between approximately 10 and 45 μm.
[0044] Inclusions are also added to the slurry and thoroughly mixed for good dispersion. Inclusions suitable for use in the present invention may include any additive capable of improving the tribological capability of the at least one hard non-oxide or oxide ceramic composite component 14. For example, inclusions may be, but are not limited to, porosity, graphite, carbon graphite, boron carbide, and other tribology enhancing additives.
[0045] In one embodiment, coated graphite particles are added to the slurry. The coated graphite particles are coarse graphite particles coated with a carbon precursor, such as phenolic resin, or another resin or material which will decompose upon heating to leave a carbon residue. Such other materials include furfuryl alcohol, polyester, petroleum pitch, coal tar pitch, or mixtures of these and other materials. Typically, the coating is dissolved in a suitable solvent and mixed thoroughly with the graphite to bond the graphite particles. The mixture is then dried to evaporate the solvent and crushed to obtain the coated graphite particles of a desired size. Typically, the coated graphite particles are passed through a 65 mesh sieve to obtain particles of less than 212 μm. The coated graphite particles are then added to the slurry. Typically, approximately at least 5.0 to 50%, and preferably approximately 10 to 20%, by weight (of the total raw batch) of the coated graphite particles are added to the slurry. But any amount of such particles is helpful in improving the self-lubricating properties of the final composite material.
[0046] Process aids, including temporary binders and lubricants, for example oleic acid or any other fatty acid, can be added to the slurry to facilitate the molding or shaping
of the raw batch into a green body or to facilitate other processing steps. The addition of a suspension or viscosity agent is particularly helpful if the inclusion particles are large. For example, if xanthan gum is added to the slurry and mixed, it causes the slurry to coagulate, which holds the inclusion particles in suspension, allowing uniform dispersion. Some materials added to the raw batch can perform multiple functions. For example, phenolic resin can function in the raw batch as both a carbon source sintering aid and a temporary binder. Polyethylene glycol can function as both a temporary binder and a die lubricant.
[0047] The inert solvent, temporary filler, temporary binder, dispersant, lubricant, and suspension agent are all temporary additives, which do not form a part of the final hard non-oxide or oxide ceramic composite material.
[0048] In the silicon carbide, pressureless sintered silicon carbide, and liquid phase sintered silicon carbide embodiments, sintering aids, such as aluminum; mineral oxides including but not limited to beryllium oxide, aluminum oxide, magnesium oxide, yttrium oxide; a boron source; and/or a carbon source are added to the slurry and mixed thoroughly to ensure complete dispersion. Boron sources include elemental boron and boron carbide (B4C), and carbon sources include elemental carbon or a carbonizable organic material, such as phenolic resin, petroleum pitch, coal tar pitch, furfuryl alcohol or sugar. Typically, approximately 2.0 to 20% by weight (of the total raw batch) of the sintering aids are added to the slurry.
[0049] The resulting slurry is mixed thoroughly to ensure sufficient dispersion and dried. Typically, the slurry is spray dried to form spherical agglomerates. Other suitable methods for obtaining such granules, such as pan drying followed by crushing and sieving, may be employed.
C. Preparation of the Hybrid Article
[0050] The at least one hard non-oxide or oxide ceramic component 12 and the at least one hard non-oxide or oxide ceramic composite component 14 are assembled during the same forming process to create the hybrid article 10 having the interface 16 between the components. In some embodiments, the at least one hard non-oxide or oxide ceramic component 12 and the at least one hard non-oxide or oxide ceramic composite component 14 include the same hard non-oxide or oxide ceramic material. In other embodiments, the
at least one hard non-oxide or oxide ceramic component 12 and the at least one hard non- oxide or oxide ceramic composite component 14 may include different hard non-oxide or oxide ceramic materials.
[0051] In one embodiment, the at least one hard non-oxide or oxide ceramic component 12 is assembled with the at least one hard non-oxide or oxide ceramic composite component 14. In other embodiments, the at least one hard non-oxide or oxide ceramic component 12 is assembled with a plurality of hard non-oxide or oxide ceramic composite components 14. In yet other embodiments, a plurality of hard non-oxide or oxide ceramic components 12 are assembled with a plurality of hard non-oxide or oxide ceramic composite components 14.
[0052] The assembly of the components 12 and 14 in the hybrid article 10 is configured so that the at least one hard non-oxide or oxide ceramic composite component 14 is positioned adjacent surfaces of the hybrid article 10 requiring enhanced tribological capability. Conventional methods of molding and shaping can be employed, such as isostatic or die pressing, of the hybrid article to form a green body. Preferably, the hybrid article is pressed at pressures ranging between approximately 3 and 9 tons/in2.
[0053] The hybrid article 10 is then exposed to the appropriate environment, such as heat, to cure any temporary binders included in the composite component. The molding and shaping of the hybrid article 10 can also include machining to a desired pre- finished shape and designed in such a manner so that the at least one hard non-oxide or oxide ceramic composite component 14 is positioned adjacent surfaces of the hybrid article 10 requiring enhanced tribological capability.
[0054] The shaped green body is then carbonized in a non-oxidizing atmosphere at a temperature typically above approximately 800 0F. The carbonization step carbonizes any carbonizable carbon source used as a sintering aid and decomposes and volatilizes the temporary filler, which leaves a microstructure of non-interconnected inclusions. The carbonization step also carbonizes the resin of the resin-coated graphite particles and volatilizes any residue of any dispersant, lubricant, or suspension agent included in the composite component.
[0055] In a typical carbonization cycle, the green body is heated in an oven from room temperature to 350 0F during a half hour and allowed to soak at that temperature for another half hour. The temperature is then raised to 8500F over a period of 10 hours and
held at 850 0F for five hours to carbonize the body. The hybrid article 10 is then cooled to room temperature. Other carbonization cycles may be used.
[0056] With respect to the silicon carbide, pressureless sintered silicon carbide, and liquid phase sintered silicon carbide embodiments, as well as some embodiments of tungsten carbide, aluminum oxide, and silicon nitride, the hybrid article 10 is then sintered via hot isostatic pressing, pressureless sintering, or liquid phase sintering, creating a seamless connection between the two components. In a typical pressureless sintering cycle, the temperature is raised to the sintering temperature over an eight hour period, the furnace is held at the peak temperature for one hour, and then allowed to cool to room temperature. The actual times depend upon the particular furnace used. Other suitable sintering cycles may also be employed.
[0057] In the specific example of liquid phase sintering, transient liquid phase sintering occurs when the liquid phase is absorbed by the solid phase during sintering. Because the amount of liquid that forms and the time for which it exists are dependent on the sintering conditions, transient liquid phase sintering is process sensitive. The liquid phase can form directly by melting of eutectic phase mixtures that form by diffusion or by incipient melting. The liquid flows between the powder particles, filling pores and causing densification by capillary action and through the provision of a fast diffusion pathway. Shrinkage occurs by particle rearrangement if the liquid volume is high enough and the green density is low enough, by the particles changing shape to allow better packing, by pore filling and by solid state sintering if a solid skeleton forms.
[0058] In the reaction bonded silicon carbide embodiments, the hybrid article 10 is infiltrated with liquid silicon. The silicon reacts with the carbon to form silicon carbide. The reaction product bonds the silicon carbide particles, and any excess silicon fills any remaining pores.
[0059] Finally, if necessary, the hybrid article 10 can be finished by grinding, diamond polishing, or any other finishing method. The article is designed in such a manner as to ensure the composite material is located on those surfaces requiring enhanced tribological capability.
[0060] The foregoing is provided for purposes of illustrating, explaining, and describing embodiments of the present invention. Modifications and adaptations to these
embodiments will be apparent to those skilled in the art and may be made without departing from the scope or spirit of the invention.
Claims
1. A hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article comprising:
(a) at least one hard non-oxide or oxide ceramic component of at least 95% of theoretical density;
directly bonded to, and different from
(b) at least one hard non-oxide or oxide ceramic composite component comprising a tribology enhancing component.
2. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article comprises a hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid seal component comprising a wall having a thickness at least in part greater than 2.5 mm.
3. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the at least one hard non-oxide or oxide ceramic composite component comprises silicon carbide.
4. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the at least one hard non-oxide or oxide ceramic composite component comprises pressureless sintered silicon carbide.
5. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the at least one hard non-oxide or oxide ceramic composite component comprises liquid phase sintered silicon carbide.
6. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1 , wherein the at least one hard non-oxide or oxide ceramic composite component comprises reaction bonded silicon carbide.
7. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1 , wherein the at least one hard non-oxide or oxide ceramic composite component comprises tungsten carbide.
8. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the at least one hard non-oxide or oxide ceramic composite component comprises aluminum oxide.
9. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the at least one hard non-oxide or oxide ceramic composite component comprises silicon nitride.
10. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the tribology enhancing component is selected from the group consisting of porosity, carbon graphite, graphite, and boron carbide.
11. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the at least one hard non-oxide or oxide ceramic component comprises silicon carbide.
12. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the at least one hard non-oxide or oxide ceramic component comprises pressureless sintered silicon carbide.
13. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1 , wherein the at least one hard non-oxide or oxide ceramic component comprises liquid phase sintered silicon carbide.
14. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the at least one hard non-oxide or oxide ceramic component comprises reaction bonded silicon carbide.
15. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the at least one hard non-oxide or oxide ceramic component comprises tungsten carbide.
16. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the at least one hard non-oxide or oxide ceramic component comprises aluminum oxide.
17. The hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article according to claim 1, wherein the at least one hard non-oxide or oxide ceramic component comprises silicon nitride.
18. A process of forming a hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid article comprising:
(a) preparing at least one hard non-oxide or oxide ceramic body of at least 95% of theoretical density;
(b) preparing at least one hard non-oxide or oxide ceramic composite body comprising a tribology enhancing component; (c) placing the at least one hard non-oxide or oxide ceramic body into contact with the at least one hard non-oxide or oxide ceramic composite body to form a hybrid article; and
(d) treating the hybrid article to directly bond the at least one hard non-oxide or oxide ceramic body and the at least one hard non-oxide or oxide ceramic composite body.
19. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic composite body comprises silicon carbide.
20. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic composite body comprises pressureless sintered silicon carbide.
21. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic composite body comprises liquid phase sintered silicon carbide.
22. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic composite body comprises reaction bonded silicon carbide.
23. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic composite body comprises tungsten carbide.
24. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic composite body comprises aluminum oxide.
25. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic composite body comprises silicon nitride.
26. The process according to claim 18, wherein the tribology enhancing component is selected from the group consisting of porosity, carbon graphite, graphite, and boron carbide.
27. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic body comprises silicon carbide.
28. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic body comprises pressureless sintered silicon carbide.
29. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic body comprises liquid phase sintered silicon carbide.
30. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic body comprises reaction bonded silicon carbide.
31. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic body comprises tungsten carbide.
32. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic body comprises aluminum oxide.
33. The process according to claim 18, wherein the at least one hard non-oxide or oxide ceramic body comprises silicon nitride.
34. The process according to claim 18, wherein treating the hybrid article comprises hot isostatic pressing.
35. The process according to claim 18, wherein treating the hybrid article comprises pressureless sintering.
36. The process according to claim 18, wherein treating the hybrid article comprises liquid phase sintering.
37. The process according to claim 18, wherein treating the hybrid article comprises reaction bonding.
38. A hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid seal component comprising:
(a) at least one part formed of a hard non-oxide or oxide ceramic of at least 95% of theoretical density;
directly bonded to, and different from
(b) at least two parts formed of a hard non-oxide or oxide ceramic composite comprising a tribology enhancing component;
wherein the hard non-oxide or oxide ceramic/hard non-oxide or oxide ceramic composite hybrid seal component comprises a wall having a thickness at least in part greater than 2.5 mm.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2012519686A JP5735501B2 (en) | 2009-07-07 | 2010-07-07 | Hard non-oxide or oxide ceramic / hard non-oxide or oxide ceramic composite hybrid seal parts |
EP10732583A EP2365949A2 (en) | 2009-07-07 | 2010-07-07 | Hard non-oxide or oxide ceramic / hard non-oxide or oxide ceramic composite hybrid article |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US22362909P | 2009-07-07 | 2009-07-07 | |
US61/223,629 | 2009-07-07 | ||
US32826210P | 2010-04-27 | 2010-04-27 | |
US61/328,262 | 2010-04-27 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2011005808A2 true WO2011005808A2 (en) | 2011-01-13 |
WO2011005808A3 WO2011005808A3 (en) | 2011-04-07 |
Family
ID=43413678
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2010/041131 WO2011005808A2 (en) | 2009-07-07 | 2010-07-07 | Hard non-oxide or oxide ceramic / hard non-oxide or oxide ceramic composite hybrid article |
Country Status (4)
Country | Link |
---|---|
US (1) | US8906522B2 (en) |
EP (1) | EP2365949A2 (en) |
JP (1) | JP5735501B2 (en) |
WO (1) | WO2011005808A2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103764349A (en) * | 2011-06-30 | 2014-04-30 | 圣戈本陶瓷及塑料股份有限公司 | Liquid phase sintered silicon carbide abrasive particles |
US8906522B2 (en) | 2009-07-07 | 2014-12-09 | Morgan Advanced Materials And Technology Inc. | Hard non-oxide or oxide ceramic / hard non-oxide or oxide ceramic composite hybrid article |
Families Citing this family (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2013135445A (en) | 2010-12-31 | 2015-02-10 | Сэнт-Гобэн Керамикс Энд Пластикс, Инк. | ABRASIVE PRODUCT (OPTIONS) AND METHOD FOR ITS FORMING |
CN108262695A (en) | 2011-06-30 | 2018-07-10 | 圣戈本陶瓷及塑料股份有限公司 | Include the abrasive product of silicon nitride abrasive grain |
JP5802336B2 (en) | 2011-09-26 | 2015-10-28 | サン−ゴバン セラミックス アンド プラスティクス,インコーポレイティド | Abrasive product comprising abrasive particle material, abrasive cloth paper using the abrasive particle material, and forming method |
EP2760807B1 (en) | 2011-09-30 | 2019-08-21 | Saint-Gobain Ceramics & Plastics Inc. | Composite silicon nitride body |
EP2797716B1 (en) | 2011-12-30 | 2021-02-17 | Saint-Gobain Ceramics & Plastics, Inc. | Composite shaped abrasive particles and method of forming same |
BR112014016159A8 (en) | 2011-12-30 | 2017-07-04 | Saint Gobain Ceramics | formation of molded abrasive particles |
EP3517245B1 (en) | 2011-12-30 | 2023-12-13 | Saint-Gobain Ceramics & Plastics Inc. | Shaped abrasive particle and method of forming same |
CA2860755C (en) | 2012-01-10 | 2018-01-30 | Saint-Gobain Ceramics & Plastics, Inc. | Abrasive particles having complex shapes and methods of forming same |
US8840696B2 (en) | 2012-01-10 | 2014-09-23 | Saint-Gobain Ceramics & Plastics, Inc. | Abrasive particles having particular shapes and methods of forming such particles |
EP2830829B1 (en) | 2012-03-30 | 2018-01-10 | Saint-Gobain Abrasives, Inc. | Abrasive products having fibrillated fibers |
KR20150020199A (en) | 2012-05-23 | 2015-02-25 | 생-고뱅 세라믹스 앤드 플라스틱스, 인코포레이티드 | Shaped abrasive particles and methods of forming same |
EP2866977B8 (en) | 2012-06-29 | 2023-01-18 | Saint-Gobain Ceramics & Plastics, Inc. | Abrasive particles having particular shapes and methods of forming such particles |
CN104822494B (en) | 2012-10-15 | 2017-11-28 | 圣戈班磨料磨具有限公司 | The method of abrasive particle and this particle of formation with given shape |
JP2016503731A (en) | 2012-12-31 | 2016-02-08 | サン−ゴバン セラミックス アンド プラスティクス,インコーポレイティド | Particulate material and method for forming the same |
CN103113111B (en) * | 2013-02-02 | 2014-08-06 | 宜兴市灵谷塑料设备有限公司 | Manufacturing method of silicon carbide product for centrifugal pump |
US9725367B2 (en) * | 2013-03-29 | 2017-08-08 | Mitsubishi Materials Corporation | Apparatus and method for producing (metal plate)-(ceramic board) laminated assembly, and apparatus and method for producing power-module substrate |
CA2907372C (en) | 2013-03-29 | 2017-12-12 | Saint-Gobain Abrasives, Inc. | Abrasive particles having particular shapes and methods of forming such particles |
TW201502263A (en) | 2013-06-28 | 2015-01-16 | Saint Gobain Ceramics | Abrasive article including shaped abrasive particles |
WO2015048768A1 (en) | 2013-09-30 | 2015-04-02 | Saint-Gobain Ceramics & Plastics, Inc. | Shaped abrasive particles and methods of forming same |
JP6290428B2 (en) | 2013-12-31 | 2018-03-07 | サンーゴバン アブレイシブズ,インコーポレイティド | Abrasive articles containing shaped abrasive particles |
US9771507B2 (en) | 2014-01-31 | 2017-09-26 | Saint-Gobain Ceramics & Plastics, Inc. | Shaped abrasive particle including dopant material and method of forming same |
WO2015160854A1 (en) | 2014-04-14 | 2015-10-22 | Saint-Gobain Ceramics & Plastics, Inc. | Abrasive article including shaped abrasive particles |
JP6484647B2 (en) | 2014-04-14 | 2019-03-13 | サン−ゴバン セラミックス アンド プラスティクス,インコーポレイティド | Abrasive articles containing shaped abrasive particles |
US9902045B2 (en) | 2014-05-30 | 2018-02-27 | Saint-Gobain Abrasives, Inc. | Method of using an abrasive article including shaped abrasive particles |
US9914864B2 (en) | 2014-12-23 | 2018-03-13 | Saint-Gobain Ceramics & Plastics, Inc. | Shaped abrasive particles and method of forming same |
US9707529B2 (en) | 2014-12-23 | 2017-07-18 | Saint-Gobain Ceramics & Plastics, Inc. | Composite shaped abrasive particles and method of forming same |
US9676981B2 (en) | 2014-12-24 | 2017-06-13 | Saint-Gobain Ceramics & Plastics, Inc. | Shaped abrasive particle fractions and method of forming same |
TWI634200B (en) | 2015-03-31 | 2018-09-01 | 聖高拜磨料有限公司 | Fixed abrasive articles and methods of forming same |
WO2016161157A1 (en) | 2015-03-31 | 2016-10-06 | Saint-Gobain Abrasives, Inc. | Fixed abrasive articles and methods of forming same |
CA3118239A1 (en) | 2015-06-11 | 2016-12-15 | Saint-Gobain Ceramics & Plastics, Inc. | Abrasive article including shaped abrasive particles |
CN109415615A (en) | 2016-05-10 | 2019-03-01 | 圣戈本陶瓷及塑料股份有限公司 | Abrasive grain and forming method thereof |
US20170335155A1 (en) | 2016-05-10 | 2017-11-23 | Saint-Gobain Ceramics & Plastics, Inc. | Abrasive particles and methods of forming same |
EP4349896A3 (en) | 2016-09-29 | 2024-06-12 | Saint-Gobain Abrasives, Inc. | Fixed abrasive articles and methods of forming same |
US10563105B2 (en) | 2017-01-31 | 2020-02-18 | Saint-Gobain Ceramics & Plastics, Inc. | Abrasive article including shaped abrasive particles |
US10759024B2 (en) | 2017-01-31 | 2020-09-01 | Saint-Gobain Ceramics & Plastics, Inc. | Abrasive article including shaped abrasive particles |
CN110719946B (en) | 2017-06-21 | 2022-07-15 | 圣戈本陶瓷及塑料股份有限公司 | Particulate material and method of forming the same |
EP4081609A4 (en) | 2019-12-27 | 2024-06-05 | Saint-Gobain Ceramics & Plastics Inc. | Abrasive articles and methods of forming same |
KR20220116556A (en) | 2019-12-27 | 2022-08-23 | 세인트-고바인 세라믹스 앤드 플라스틱스, 인크. | Abrasive articles and methods of forming same |
WO2023129908A1 (en) * | 2021-12-29 | 2023-07-06 | Saint-Gobain Ceramics & Plastics, Inc. | Bearing block and method of forming |
CN115536396B (en) * | 2022-10-14 | 2023-07-18 | 广州市拓道新材料科技有限公司 | High-wear-resistance silicon dioxide/silicon carbide composite ceramic and preparation method and application thereof |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5580834A (en) | 1993-02-10 | 1996-12-03 | The Morgan Crucible Company Plc | Self-sintered silicon carbide/carbon graphite composite material having interconnected pores which may be impregnated and raw batch and process for producing same |
US5656563A (en) | 1993-02-10 | 1997-08-12 | The Morgan Crucible Company Plc | Dense, self-sintered silicon carbide/carbon graphite composite |
US5968653A (en) | 1996-01-11 | 1999-10-19 | The Morgan Crucible Company, Plc | Carbon-graphite/silicon carbide composite article |
Family Cites Families (47)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1231151B (en) | 1965-01-25 | 1966-12-22 | Siemens Planiawerke Ag | Method for joining graphite parts |
US3925577A (en) * | 1972-11-24 | 1975-12-09 | Westinghouse Electric Corp | Silicon carbide coated graphite members and process for producing the same |
US3960577A (en) * | 1974-01-08 | 1976-06-01 | General Electric Company | Dense polycrystalline silicon carbide |
US4108929A (en) * | 1974-09-03 | 1978-08-22 | General Electric Company | Hot pressed silicon carbide |
US4023975A (en) * | 1975-11-17 | 1977-05-17 | General Electric Company | Hot pressed silicon carbide containing beryllium carbide |
GB2082165B (en) * | 1980-07-17 | 1984-03-28 | Asahi Glass Co Ltd | Silicon carbide ceramic |
IE49733B1 (en) | 1978-12-29 | 1985-12-11 | Gen Electric | Integral composite of polycrystalline diamond and/or cubic boron nitride body phase and substrate phase and process for making it |
US4382113A (en) * | 1981-03-23 | 1983-05-03 | Energy Development Associates, Inc. | Method for joining graphite to graphite |
JPS59102872A (en) * | 1982-12-06 | 1984-06-14 | 日本特殊陶業株式会社 | Silicon carbide graphite composite sintered body and manufacture |
US4858817A (en) | 1983-05-05 | 1989-08-22 | The United States Of America As Represented By The Department Of Energy | Graphit-ceramic RF Faraday-thermal shield and plasma limiter |
US4692418A (en) * | 1984-08-29 | 1987-09-08 | Stemcor Corporation | Sintered silicon carbide/carbon composite ceramic body having fine microstructure |
JPS61122164A (en) | 1984-11-15 | 1986-06-10 | 株式会社リケン | Silicon carbide-alumina composite sintered body and manufacture |
JPS62197361A (en) | 1986-02-25 | 1987-09-01 | バブコツク日立株式会社 | Method of joining silicon carbide ceramics |
US4829027A (en) * | 1987-01-12 | 1989-05-09 | Ceramatec, Inc. | Liquid phase sintering of silicon carbide |
US4876226A (en) * | 1987-01-12 | 1989-10-24 | Fuentes Ricardo I | Silicon carbide sintering |
JPS6487562A (en) | 1987-09-30 | 1989-03-31 | Nippon Steel Corp | Non-oxide based composite ceramic sintered body |
US4946808A (en) * | 1988-11-10 | 1990-08-07 | Ceramics Process Systems Corporation | Method for preparing dense, pressureless sintered SiC whisker reinforced composite ceramics |
JPH0832587B2 (en) | 1989-04-10 | 1996-03-29 | 日本タングステン株式会社 | Ceramics sintered body and its manufacturing method |
FR2675713B1 (en) | 1991-04-29 | 1993-07-02 | Pechiney Electrometallurgie | CATALYTIC SYSTEM, PARTICULARLY FOR THE POSTCOMBUSTION OF EXHAUST GASES AND METHOD FOR MANUFACTURING THE SAME. |
US5164344A (en) | 1991-06-26 | 1992-11-17 | Dow Corning Corporation | Borosilazanes as binders for the preparation of sintered silicon carbide monoliths |
US5459112A (en) | 1994-09-14 | 1995-10-17 | The Carborundum Company | Reaction-bonded silicon carbide refractory product |
US5850329A (en) | 1994-10-31 | 1998-12-15 | Sullivan; Thomas Milton | Magnetic recording device components |
US5623386A (en) | 1994-10-31 | 1997-04-22 | Sullivan; Thomas M. | Magnetic recording component |
US5656218A (en) * | 1995-05-19 | 1997-08-12 | Industrial Technology Research Institute | Method for making high performance self-reinforced silicon carbide using a pressureless sintering process |
JP2765543B2 (en) | 1995-12-26 | 1998-06-18 | 株式会社日立製作所 | Reaction sintered ceramics and method for producing the same |
US6245287B1 (en) | 1998-03-24 | 2001-06-12 | Nippon Crucible, Co., Ltd. | Molten metal vessel and molten metal holding furnace |
US6503572B1 (en) * | 1999-07-23 | 2003-01-07 | M Cubed Technologies, Inc. | Silicon carbide composites and methods for making same |
US6887569B1 (en) | 1999-10-20 | 2005-05-03 | The Board Of Trustees Of The University | High temperature tolerant ceramic composites having porous interphases |
WO2001098207A1 (en) | 2000-06-19 | 2001-12-27 | Corning Incorporated | Plasticizable mixture and method of using |
US6555031B2 (en) | 2000-06-19 | 2003-04-29 | Corning Incorporated | Process for producing silicon carbide bodies |
JP5172738B2 (en) | 2000-10-27 | 2013-03-27 | 株式会社東芝 | Semiconductor module and electronic device using the same |
US6613443B2 (en) | 2000-10-27 | 2003-09-02 | Kabushiki Kaisha Toshiba | Silicon nitride ceramic substrate, silicon nitride ceramic circuit board using the substrate, and method of manufacturing the substrate |
US6740286B2 (en) | 2000-12-04 | 2004-05-25 | Advanced Ceramics Research, Inc. | Consolidation and densification methods for fibrous monolith processing |
JP2002293634A (en) | 2001-03-30 | 2002-10-09 | Kyocera Corp | Silicon carbide sintered compact and substrate for magnetic head slider using the same |
DE10133635A1 (en) | 2001-07-11 | 2003-02-06 | Sgl Carbon Ag | Multi-layer ceramic composite |
US6762140B2 (en) * | 2001-08-20 | 2004-07-13 | Saint-Gobain Ceramics & Plastics, Inc. | Silicon carbide ceramic composition and method of making |
US6586886B1 (en) | 2001-12-19 | 2003-07-01 | Applied Materials, Inc. | Gas distribution plate electrode for a plasma reactor |
US6716800B2 (en) * | 2002-04-12 | 2004-04-06 | John Crane Inc. | Composite body of silicon carbide and binderless carbon, process for producing such composite body, and article of manufacturing utilizing such composite body for tribological applications |
DE10231278A1 (en) | 2002-07-10 | 2004-02-05 | Sgl Carbon Ag | Ceramic composite body |
CN101279859B (en) * | 2003-03-26 | 2012-01-04 | 圣戈本陶瓷及塑料股份有限公司 | Silicon carbide ceramic components having oxide layer |
US7452606B2 (en) * | 2003-05-01 | 2008-11-18 | Saint-Gobain Ceramics & Plastics, Inc. | Silicon carbide ceramic components having oxide layer |
US6953760B2 (en) * | 2003-06-04 | 2005-10-11 | Saint-Gobain Ceramics & Plastics, Inc. | Ceramic component containing inclusions |
US7166550B2 (en) | 2005-01-07 | 2007-01-23 | Xin Chen | Ceramic composite body of silicon carbide/boron nitride/carbon |
US8003042B2 (en) * | 2006-03-29 | 2011-08-23 | Ceramatec, Inc. | Toughened silicon carbide and method for making the same |
US7793940B2 (en) * | 2006-05-16 | 2010-09-14 | Skf Usa Inc. | Mechanical end face seal with ultrahard face material |
US8906522B2 (en) | 2009-07-07 | 2014-12-09 | Morgan Advanced Materials And Technology Inc. | Hard non-oxide or oxide ceramic / hard non-oxide or oxide ceramic composite hybrid article |
DE202010011173U1 (en) * | 2010-08-09 | 2011-12-22 | Eagleburgmann Germany Gmbh & Co. Kg | Sliding ring with improved inlet properties |
-
2010
- 2010-07-07 US US12/831,616 patent/US8906522B2/en not_active Expired - Fee Related
- 2010-07-07 JP JP2012519686A patent/JP5735501B2/en not_active Expired - Fee Related
- 2010-07-07 WO PCT/US2010/041131 patent/WO2011005808A2/en active Application Filing
- 2010-07-07 EP EP10732583A patent/EP2365949A2/en not_active Withdrawn
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5580834A (en) | 1993-02-10 | 1996-12-03 | The Morgan Crucible Company Plc | Self-sintered silicon carbide/carbon graphite composite material having interconnected pores which may be impregnated and raw batch and process for producing same |
US5656563A (en) | 1993-02-10 | 1997-08-12 | The Morgan Crucible Company Plc | Dense, self-sintered silicon carbide/carbon graphite composite |
US5968653A (en) | 1996-01-11 | 1999-10-19 | The Morgan Crucible Company, Plc | Carbon-graphite/silicon carbide composite article |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8906522B2 (en) | 2009-07-07 | 2014-12-09 | Morgan Advanced Materials And Technology Inc. | Hard non-oxide or oxide ceramic / hard non-oxide or oxide ceramic composite hybrid article |
CN103764349A (en) * | 2011-06-30 | 2014-04-30 | 圣戈本陶瓷及塑料股份有限公司 | Liquid phase sintered silicon carbide abrasive particles |
US9303196B2 (en) | 2011-06-30 | 2016-04-05 | Saint-Gobain Ceramics & Plastics, Inc. | Liquid phase sintered silicon carbide abrasive particles |
Also Published As
Publication number | Publication date |
---|---|
EP2365949A2 (en) | 2011-09-21 |
US20110008604A1 (en) | 2011-01-13 |
WO2011005808A3 (en) | 2011-04-07 |
US8906522B2 (en) | 2014-12-09 |
JP2012532823A (en) | 2012-12-20 |
JP5735501B2 (en) | 2015-06-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8906522B2 (en) | Hard non-oxide or oxide ceramic / hard non-oxide or oxide ceramic composite hybrid article | |
US5707567A (en) | Process for producing a self-sintered silicon carbide/carbon graphite composite material having interconnected pores which maybe impregnated | |
US5976429A (en) | Process for producing dense, self-sintered silicon carbide/carbon-graphite composites | |
US8697259B2 (en) | Boron carbide composite materials | |
JP2722182B2 (en) | Porous SiC bearing material having three types of pore structure and method of manufacturing the same | |
US7166550B2 (en) | Ceramic composite body of silicon carbide/boron nitride/carbon | |
KR20050003355A (en) | A composite body of silicon carbide and binderless carbon and process for producing | |
US6398991B1 (en) | Processes for making a silicon carbide composition | |
US20020160902A1 (en) | Composite material based on silicon carbide and carbon, process for its production and its use | |
CN105198435B (en) | Silicon carbide-carbon composite material and preparation method thereof | |
CN1169708A (en) | Selfsintered silicon carbide/carbon composite material | |
JP5551778B2 (en) | Dry and wet low friction silicon carbide seal | |
JPS59131577A (en) | Silicon carbide material and manufacture | |
JP2543093B2 (en) | Sliding parts for seals | |
JPH0510303B2 (en) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WWE | Wipo information: entry into national phase |
Ref document number: 2010732583 Country of ref document: EP |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2012519686 Country of ref document: JP |
|
NENP | Non-entry into the national phase |
Ref country code: DE |