US20150197860A1 - Process of Producing a Ceramic Matrix Composite - Google Patents
Process of Producing a Ceramic Matrix Composite Download PDFInfo
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- US20150197860A1 US20150197860A1 US14/151,914 US201414151914A US2015197860A1 US 20150197860 A1 US20150197860 A1 US 20150197860A1 US 201414151914 A US201414151914 A US 201414151914A US 2015197860 A1 US2015197860 A1 US 2015197860A1
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- 239000011153 ceramic matrix composite Substances 0.000 title claims abstract description 65
- 238000000034 method Methods 0.000 title claims abstract description 12
- 230000008569 process Effects 0.000 title claims abstract description 11
- 239000000758 substrate Substances 0.000 claims abstract description 35
- 229910010293 ceramic material Inorganic materials 0.000 claims abstract description 30
- 239000007769 metal material Substances 0.000 claims abstract description 24
- 239000000919 ceramic Substances 0.000 claims abstract description 16
- 229910052751 metal Inorganic materials 0.000 claims abstract description 15
- 239000002184 metal Substances 0.000 claims abstract description 15
- 239000011148 porous material Substances 0.000 claims abstract description 12
- 238000010438 heat treatment Methods 0.000 claims abstract description 8
- 238000006243 chemical reaction Methods 0.000 claims abstract description 5
- 230000000694 effects Effects 0.000 claims abstract description 5
- 238000002844 melting Methods 0.000 claims abstract description 5
- 230000008018 melting Effects 0.000 claims abstract description 5
- 238000001816 cooling Methods 0.000 claims abstract description 3
- 239000002131 composite material Substances 0.000 claims description 8
- MCMNRKCIXSYSNV-UHFFFAOYSA-N ZrO2 Inorganic materials O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 claims description 5
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 claims description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 3
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 3
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 2
- QPLDLSVMHZLSFG-UHFFFAOYSA-N Copper oxide Chemical compound [Cu]=O QPLDLSVMHZLSFG-UHFFFAOYSA-N 0.000 claims description 2
- 239000005751 Copper oxide Substances 0.000 claims description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 2
- 229910052581 Si3N4 Inorganic materials 0.000 claims description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 2
- 239000002253 acid Substances 0.000 claims description 2
- 150000007513 acids Chemical class 0.000 claims description 2
- 229910045601 alloy Inorganic materials 0.000 claims description 2
- 239000000956 alloy Substances 0.000 claims description 2
- 229910052790 beryllium Inorganic materials 0.000 claims description 2
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims description 2
- 229910052804 chromium Inorganic materials 0.000 claims description 2
- 239000011651 chromium Substances 0.000 claims description 2
- 229910052802 copper Inorganic materials 0.000 claims description 2
- 239000010949 copper Substances 0.000 claims description 2
- 229910000431 copper oxide Inorganic materials 0.000 claims description 2
- 238000005530 etching Methods 0.000 claims description 2
- 229910052742 iron Inorganic materials 0.000 claims description 2
- 239000000314 lubricant Substances 0.000 claims description 2
- 229910052749 magnesium Inorganic materials 0.000 claims description 2
- 239000011777 magnesium Substances 0.000 claims description 2
- 229910052759 nickel Inorganic materials 0.000 claims description 2
- 239000000377 silicon dioxide Substances 0.000 claims description 2
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims description 2
- 239000000126 substance Substances 0.000 claims description 2
- 229910052718 tin Inorganic materials 0.000 claims description 2
- 239000011135 tin Substances 0.000 claims description 2
- 239000010936 titanium Substances 0.000 claims description 2
- 229910052719 titanium Inorganic materials 0.000 claims description 2
- 229910052725 zinc Inorganic materials 0.000 claims description 2
- 239000011701 zinc Substances 0.000 claims description 2
- 229910052726 zirconium Inorganic materials 0.000 claims description 2
- 239000000463 material Substances 0.000 description 7
- 150000002739 metals Chemical class 0.000 description 3
- 150000001450 anions Chemical class 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 150000001768 cations Chemical class 0.000 description 2
- 239000004020 conductor Substances 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 230000005012 migration Effects 0.000 description 2
- 238000013508 migration Methods 0.000 description 2
- 229910000873 Beta-alumina solid electrolyte Inorganic materials 0.000 description 1
- 229910020968 MoSi2 Inorganic materials 0.000 description 1
- BNOODXBBXFZASF-UHFFFAOYSA-N [Na].[S] Chemical compound [Na].[S] BNOODXBBXFZASF-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 125000000129 anionic group Chemical group 0.000 description 1
- 125000002091 cationic group Chemical group 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000003670 easy-to-clean Effects 0.000 description 1
- 230000005684 electric field Effects 0.000 description 1
- 239000003792 electrolyte Substances 0.000 description 1
- 239000008151 electrolyte solution Substances 0.000 description 1
- 239000003574 free electron Substances 0.000 description 1
- 235000011389 fruit/vegetable juice Nutrition 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 244000005700 microbiome Species 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- -1 oxygen anions Chemical class 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 229910001415 sodium ion Inorganic materials 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- ZCUFMDLYAMJYST-UHFFFAOYSA-N thorium dioxide Chemical compound O=[Th]=O ZCUFMDLYAMJYST-UHFFFAOYSA-N 0.000 description 1
- 229910003452 thorium oxide Inorganic materials 0.000 description 1
Images
Classifications
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- 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
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/4505—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements characterised by the method of application
- C04B41/4523—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements characterised by the method of application applied from the molten state ; Thermal spraying, e.g. plasma spraying
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F1/00—Etching metallic material by chemical means
-
- 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
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
-
- 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
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/85—Coating or impregnation with inorganic materials
- C04B41/88—Metals
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F4/00—Processes for removing metallic material from surfaces, not provided for in group C23F1/00 or C23F3/00
- C23F4/04—Processes for removing metallic material from surfaces, not provided for in group C23F1/00 or C23F3/00 by physical dissolution
-
- 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
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00241—Physical properties of the materials not provided for elsewhere in C04B2111/00
- C04B2111/00344—Materials with friction-reduced moving parts, e.g. ceramics lubricated by impregnation with carbon
- C04B2111/00353—Sliding parts
-
- 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
- F16C33/10—Construction relative to lubrication
- F16C33/1025—Construction relative to lubrication with liquid, e.g. oil, as lubricant
- F16C33/103—Construction relative to lubrication with liquid, e.g. oil, as lubricant retained in or near the bearing
- F16C33/104—Construction relative to lubrication with liquid, e.g. oil, as lubricant retained in or near the bearing in a porous body, e.g. oil impregnated sintered sleeve
Definitions
- the invention relates to ceramic materials and more particularly to a process of producing a ceramic matrix composite (CMC) having increased fracture toughness, increased heat-resistance, increased electrical conduction, and increased thermal conduction.
- CMC ceramic matrix composite
- Ceramic materials have the following characteristics superior to metals: High elasticity coefficient/weight ratio, high hardness, high compression strength/weight ratio, high/low thermal conductivity, low thermal expansion coefficient, high melting point, and good corrosion/oxidation resistance. These characteristics of the ceramic materials make these materials gradually favored by the industry. Ceramic materials are widely employed in special optical, electrical, thermal and mechanical fields, and many different kinds of ceramic products are developed for producing consumer products.
- ceramic knives are made of zirconium dioxide and have properties similar to natural diamonds.
- the blade can be extremely sharp, hard, and abrasion resistant. Further, the blade surface is dense and is not subject to contamination by food juice. Furthermore, it is easy to clean, which can reduce the growth of microorganisms, and is extremely light. Thus, ceramic knives have become a good house helper.
- Ceramic materials Electrical conduction of ceramic materials is activated by heating or other methods to generate free electrons In addition, an electric field is applied to the ceramic material. As an end, the electrical conduction is generated.
- a typical ceramic material having electrical conduction is SiC which has a maximum operating temperature of 1,450 degrees Celsius.
- MoSi2 has a maximum operating temperature of 1,650 degrees Celsius.
- Novel ceramic materials having electrical conduction include zirconium dioxide having a maximum operating temperature of 2,000 degrees Celsius, and thorium oxide having a maximum operating temperature up to 2,500 degrees Celsius.
- An ion-conducting ceramic material is a molten electrolytic solution or electrolyte having high ion conductivity similar to the solid ceramic material.
- ⁇ alumina ceramic material is a typical cationic conductor. It mainly relies on the migration of sodium ions for being conductive.
- Zirconium dioxide based ceramic material is an anionic conductive material and relies mainly on migration of oxygen anions for being conductive.
- Ion-conducting ceramic materials can also be used to produce a number of novel solid-state batteries such as sodium-sulfur batteries. It may be applied to electric power supply (e.g., battery) for automobile in the future. As described above, ceramic products not only change the traditional manufacturing processes but also deeply affect our daily lives.
- Bonding of ceramic materials is either covalent or ionic. Covalent bonding between atoms is formed by shared and overlapping valence electrons. Ionic bonding is formed by transferring electron(s) from a cation to an anion. Thus, the covalent electron cloud in a covalent bonded ceramic material does not form a bond due to atoms displacement from each other in response to an applied force. Similarly, breaking the ionic bonding between an ionic ceramic material will result in all adjacent atoms becoming either all cations or anions and generate a repulsive force to cause rupture. Consequently, ceramic materials are brittle in nature.
- It is therefore one object of the invention to provide a process of producing a ceramic matrix composite (CMC) comprising the steps of preparing a ceramic material having a plurality of pores as a CMC substrate; heating a metal material to be molten wherein the metal material has a melting point lower than the CMC substrate and has a high activity to react with the component of the CMC substrate; adding the CMC substrate to the molten metal material so that the molten metal material enters the pores of the CMC substrate to occur chemical reactions; removing the CMC substrate filled with the molten metal material; and cooling the removed CMC substrate filled with the molten metal material to form a CMC having a plurality of metal grains.
- CMC ceramic matrix composite
- FIG. 1 is a table showing fracture toughness of typical kinds of ceramic materials
- FIG. 2 is a flow chart illustrating a process of producing a ceramic matrix composite according to the invention
- FIG. 3 is a perspective view of a CMC article formed by the process
- FIG. 4A is an enlarged view of the circle in FIG. 3 ;
- FIG. 4B is another enlarged view of the circle in FIG. 3 ;
- FIG. 5 is a table showing maximum fracture load and fracture toughness of CMC of the invention and S26 ceramic material of the prior art.
- FIG. 2 a process of producing a ceramic matrix composite in accordance with the invention is illustrated below.
- step 10 a porous ceramic material is prepared as a CMC substrate.
- step 20 a metal material is heated to be molten.
- step 30 the CMC substrate is added to the molten metal material so that the molten metal material may enter pores of the CMC substrate to occur chemical reactions.
- step 40 the CMC substrate filled with molten metal material is removed and cooled to form a CMC having a plurality of metal grains.
- the CMC article comprises a CMC substrate 1 and a plurality of metal grains 2 filled in the pores of the CMC substrate 1 .
- the CMC substrate 1 is formed of alumina, silica, zirconium dioxide, silicon carbide, copper oxide, or silicon nitride.
- the metal grains 2 have a melting point lower than the CMC substrate 1 and have the characteristic of high activity.
- the metal grains 2 may be aluminum, nickel, tin, magnesium, beryllium, chromium, iron, zinc, zirconium, copper, or titanium and their alloys.
- the CMC substrate 1 of the invention is a composite and is conductive.
- the CMC having the CMC substrate 1 of the invention can be subject to heat treatment to form as a thermal conductive but electrically non-conductive ceramic composite.
- the CMC having the CMC substrate 1 of the invention can be subject to heat treatment so that the metal such as aluminum can be oxidized to form as a corrosion proof ceramic composite.
- the CMC having the CMC substrate 1 of the invention can be subject to a step of removing portions of the metal grains 2 in the pores by heating to a molten state or by etching with chemicals such as acids so as to form as a ceramic composite having metal residues 3 which are left in the pores near the surface of the CMC.
- the ceramic composite has the effect of absorbing lubricant and thus can be made into ball bearings or self-lubricating bearings.
- the CMC of the invention of the composite ceramic substrate is produced by filling the molten metal material into the pores of the CMC substrate 1 , and causing chemical reactions to occur by replacing the lattice arrangement of ceramic material.
- the CMC of the invention has the benefits of significantly increased fracture toughness, heat-resistance, electrical conduction, and thermal conduction.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Inorganic Chemistry (AREA)
- Metallurgy (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- General Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Compositions Of Oxide Ceramics (AREA)
Abstract
A process of producing a ceramic matrix composite (CMC) is provided the steps of preparing a ceramic material having a plurality of pores as a CMC substrate; heating a metal material to be molten wherein the metal material has a melting point lower than the CMC substrate and has a high activity; adding the CMC substrate to the molten metal material so that the molten metal material enters the pores of the CMC substrate to occur chemical reactions; removing the CMC substrate filled with the molten metal material; and cooling the removed CMC substrate filled with the molten metal material to form a CMC having a plurality of metal grains. Plain strain fracture toughness (KIC) of typical ceramic S26 is 4.53 MPa m1/2. As a comparison, CMC has KIC of 21.11 MPa m1/2 about 466% of ceramic S26.
Description
- 1. Field of the Invention
- The invention relates to ceramic materials and more particularly to a process of producing a ceramic matrix composite (CMC) having increased fracture toughness, increased heat-resistance, increased electrical conduction, and increased thermal conduction.
- 2. Description of Related Art
- Materials technology is advancing rapidly in recent years. The traditional structure provided by the application of metals to replace ceramics has been an increasing tendency. Ceramic materials have the following characteristics superior to metals: High elasticity coefficient/weight ratio, high hardness, high compression strength/weight ratio, high/low thermal conductivity, low thermal expansion coefficient, high melting point, and good corrosion/oxidation resistance. These characteristics of the ceramic materials make these materials gradually favored by the industry. Ceramic materials are widely employed in special optical, electrical, thermal and mechanical fields, and many different kinds of ceramic products are developed for producing consumer products.
- For example, ceramic knives are made of zirconium dioxide and have properties similar to natural diamonds. The blade can be extremely sharp, hard, and abrasion resistant. Further, the blade surface is dense and is not subject to contamination by food juice. Furthermore, it is easy to clean, which can reduce the growth of microorganisms, and is extremely light. Thus, ceramic knives have become a good house helper.
- Electrical conduction of ceramic materials is activated by heating or other methods to generate free electrons In addition, an electric field is applied to the ceramic material. As an end, the electrical conduction is generated. A typical ceramic material having electrical conduction is SiC which has a maximum operating temperature of 1,450 degrees Celsius. Similarly, MoSi2 has a maximum operating temperature of 1,650 degrees Celsius. Novel ceramic materials having electrical conduction include zirconium dioxide having a maximum operating temperature of 2,000 degrees Celsius, and thorium oxide having a maximum operating temperature up to 2,500 degrees Celsius.
- An ion-conducting ceramic material is a molten electrolytic solution or electrolyte having high ion conductivity similar to the solid ceramic material. β alumina ceramic material is a typical cationic conductor. It mainly relies on the migration of sodium ions for being conductive. Zirconium dioxide based ceramic material is an anionic conductive material and relies mainly on migration of oxygen anions for being conductive. Ion-conducting ceramic materials can also be used to produce a number of novel solid-state batteries such as sodium-sulfur batteries. It may be applied to electric power supply (e.g., battery) for automobile in the future. As described above, ceramic products not only change the traditional manufacturing processes but also deeply affect our daily lives.
- While ceramic materials have become the darling of materials, it has inherent shortcomings such as excessive brittleness. Particularly, they tend to fracture when tensile stress is concentrated on a portion thereof. As a result, it leads to failure. Fracture toughness of typical ceramic materials is shown in
FIG. 1 . - Bonding of ceramic materials is either covalent or ionic. Covalent bonding between atoms is formed by shared and overlapping valence electrons. Ionic bonding is formed by transferring electron(s) from a cation to an anion. Thus, the covalent electron cloud in a covalent bonded ceramic material does not form a bond due to atoms displacement from each other in response to an applied force. Similarly, breaking the ionic bonding between an ionic ceramic material will result in all adjacent atoms becoming either all cations or anions and generate a repulsive force to cause rupture. Consequently, ceramic materials are brittle in nature.
- Regarding metals and polymeric materials, use of these materials does not cause fracture or breakage as long as the applied force is lower than the ultimate tensile strengths of the materials. Further, even these materials are overloaded beyond their yield strengths, significant plastic deformation usually occur prior to the final failure and serve as a warning. Because ceramic materials are brittle and have poor toughness, they are subject to sudden failure. Therefore, industrial applications of ceramic materials are significantly limited. Consequently, it is desired to develop a tough ceramic matrix composite maintaining the attractive characteristics but without the disadvantages of conventional ceramic materials.
- It is therefore one object of the invention to provide a process of producing a ceramic matrix composite (CMC) comprising the steps of preparing a ceramic material having a plurality of pores as a CMC substrate; heating a metal material to be molten wherein the metal material has a melting point lower than the CMC substrate and has a high activity to react with the component of the CMC substrate; adding the CMC substrate to the molten metal material so that the molten metal material enters the pores of the CMC substrate to occur chemical reactions; removing the CMC substrate filled with the molten metal material; and cooling the removed CMC substrate filled with the molten metal material to form a CMC having a plurality of metal grains.
- The above and other objects, features and advantages of the invention will become apparent from the following detailed description taken with the accompanying drawings.
-
FIG. 1 is a table showing fracture toughness of typical kinds of ceramic materials; -
FIG. 2 is a flow chart illustrating a process of producing a ceramic matrix composite according to the invention; -
FIG. 3 is a perspective view of a CMC article formed by the process; -
FIG. 4A is an enlarged view of the circle inFIG. 3 ; -
FIG. 4B is another enlarged view of the circle inFIG. 3 ; and -
FIG. 5 is a table showing maximum fracture load and fracture toughness of CMC of the invention and S26 ceramic material of the prior art. - Referring to
FIG. 2 , a process of producing a ceramic matrix composite in accordance with the invention is illustrated below. - In step 10, a porous ceramic material is prepared as a CMC substrate.
- In step 20, a metal material is heated to be molten.
- In step 30, the CMC substrate is added to the molten metal material so that the molten metal material may enter pores of the CMC substrate to occur chemical reactions.
- In step 40, the CMC substrate filled with molten metal material is removed and cooled to form a CMC having a plurality of metal grains.
- Referring to
FIGS. 3 , 4A, 4B, and 5, a CMC article is schematically shown. The CMC article comprises aCMC substrate 1 and a plurality ofmetal grains 2 filled in the pores of theCMC substrate 1. TheCMC substrate 1 is formed of alumina, silica, zirconium dioxide, silicon carbide, copper oxide, or silicon nitride. Themetal grains 2 have a melting point lower than theCMC substrate 1 and have the characteristic of high activity. Themetal grains 2 may be aluminum, nickel, tin, magnesium, beryllium, chromium, iron, zinc, zirconium, copper, or titanium and their alloys. TheCMC substrate 1 of the invention is a composite and is conductive. - The CMC having the
CMC substrate 1 of the invention can be subject to heat treatment to form as a thermal conductive but electrically non-conductive ceramic composite. - The CMC having the
CMC substrate 1 of the invention can be subject to heat treatment so that the metal such as aluminum can be oxidized to form as a corrosion proof ceramic composite. - The CMC having the
CMC substrate 1 of the invention can be subject to a step of removing portions of themetal grains 2 in the pores by heating to a molten state or by etching with chemicals such as acids so as to form as a ceramic composite havingmetal residues 3 which are left in the pores near the surface of the CMC. The ceramic composite has the effect of absorbing lubricant and thus can be made into ball bearings or self-lubricating bearings. - In brief, the CMC of the invention of the composite ceramic substrate is produced by filling the molten metal material into the pores of the
CMC substrate 1, and causing chemical reactions to occur by replacing the lattice arrangement of ceramic material. As a result, the CMC of the invention has the benefits of significantly increased fracture toughness, heat-resistance, electrical conduction, and thermal conduction. - In
FIG. 5 , maximum fracture load and fracture toughness of CMC of the invention and S26 ceramic material of the prior art are shown for comparison. Plain strain fracture toughness (KIC) of typical ceramic S26 is 4.53 MPa m1/2. As a comparison, CMC has KIC of 21.11 MPa m1/2 about 466% of ceramic S26. - While the invention has been described in terms of preferred embodiments, those skilled in the art will recognize that the invention can be practiced with modifications within the spirit and scope of the appended claims.
Claims (4)
1. A process of producing a ceramic matrix composite (CMC) comprising the steps of:
preparing a ceramic material having a plurality of pores as a CMC substrate;
heating a metal material to be molten wherein the metal material has a melting point lower than the CMC substrate and has a high activity to react with the component of the CMC substrate;
adding the CMC substrate to the molten metal material so that the molten metal material enters the pores of the CMC substrate to occur chemical reactions;
removing the CMC substrate filled with the molten metal material; and
cooling the removed CMC substrate filled with the molten metal material to form a CMC having a plurality of metal grains.
2. The process of claim 1 , wherein the CMC substrate is formed of alumina, silica, zirconium dioxide, silicon carbide, copper oxide or silicon nitride.
3. The process of claim 1 , wherein the metal material is aluminum, nickel, tin, magnesium, beryllium, chromium, iron, zinc, zirconium, copper, or titanium and their alloys.
4. The process of claim 1 , wherein the CMC is subject to a step of removing portions of the metal grains by heating to a molten state or by etching with chemicals such as acids to form as a ceramic composite having a plurality of metal residues left in the pores near the surface of the CMC, the ceramic composite being capable of absorbing lubricant and being made into a ball bearing or a self-lubricating bearing.
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| Application Number | Priority Date | Filing Date | Title |
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| US14/151,914 US20150197860A1 (en) | 2014-01-10 | 2014-01-10 | Process of Producing a Ceramic Matrix Composite |
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| Application Number | Priority Date | Filing Date | Title |
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| US14/151,914 US20150197860A1 (en) | 2014-01-10 | 2014-01-10 | Process of Producing a Ceramic Matrix Composite |
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| US20150197860A1 true US20150197860A1 (en) | 2015-07-16 |
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Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4868143A (en) * | 1986-08-13 | 1989-09-19 | Lanxide Technology Company, Lp | Methods of making ceramic articles with a modified metal-containing component |
| US5735332A (en) * | 1992-09-17 | 1998-04-07 | Coors Ceramics Company | Method for making a ceramic metal composite |
| US6338906B1 (en) * | 1992-09-17 | 2002-01-15 | Coorstek, Inc. | Metal-infiltrated ceramic seal |
-
2014
- 2014-01-10 US US14/151,914 patent/US20150197860A1/en not_active Abandoned
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4868143A (en) * | 1986-08-13 | 1989-09-19 | Lanxide Technology Company, Lp | Methods of making ceramic articles with a modified metal-containing component |
| US5735332A (en) * | 1992-09-17 | 1998-04-07 | Coors Ceramics Company | Method for making a ceramic metal composite |
| US6338906B1 (en) * | 1992-09-17 | 2002-01-15 | Coorstek, Inc. | Metal-infiltrated ceramic seal |
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