CN105859295A - Boron carbide-based ceramic-metal composite material and preparation method thereof - Google Patents
Boron carbide-based ceramic-metal composite material and preparation method thereof Download PDFInfo
- Publication number
- CN105859295A CN105859295A CN201610174920.4A CN201610174920A CN105859295A CN 105859295 A CN105859295 A CN 105859295A CN 201610174920 A CN201610174920 A CN 201610174920A CN 105859295 A CN105859295 A CN 105859295A
- Authority
- CN
- China
- Prior art keywords
- parts
- boron carbide
- metallic composite
- boron
- pottery
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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
- C04B35/563—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 boron 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
-
- 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
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/14—Making alloys containing metallic or non-metallic fibres or filaments by powder metallurgy, i.e. by processing mixtures of metal powder and fibres or filaments
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
-
- 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
- C04B2235/3206—Magnesium oxides or oxide-forming salts thereof
-
- 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
- C04B2235/3217—Aluminum oxide or oxide forming salts thereof, e.g. bauxite, alpha-alumina
-
- 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
- C04B2235/3826—Silicon 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
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3891—Silicides, e.g. molybdenum disilicide, iron silicide
-
- 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
- C04B2235/404—Refractory metals
-
- 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
- C04B2235/405—Iron group metals
-
- 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
- C04B2235/407—Copper
-
- 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
- C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
- C04B2235/52—Constituents or additives characterised by their shapes
- C04B2235/5208—Fibers
- C04B2235/5216—Inorganic
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Inorganic Chemistry (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Ceramic Products (AREA)
Abstract
The invention relates to a boron carbide-based ceramic-metal composite material and a preparation method thereof. The boron carbide-based ceramic-metal composite material comprises, by mass, 5 to 15 parts of copper, 3 to 12 parts of cobalt, 10 to 25 parts of titanium alloy, 30 to 50 parts of boron carbide, 20 to 40 parts of ceramic, 10 to 20 parts of boron fiber, 5 to 18 parts of molybdenum disilicide, 3 to 10 parts of silicon carbide, 5 to 15 parts of magnesium oxide, 5 to 13 parts of aluminum oxide, 5 to 12 parts of silicone rubber and 10 to 20 parts of water glass. The boron carbide-based ceramic-metal composite material has good hardness, bending strength, wear resistance, heat conductivity and corrosion resistance and a high melting point.
Description
Technical field
The present invention relates to metallic composite technical field, particularly relate to a kind of boron carbide base ceramic-metallic composite
And preparation method thereof.
Background technology
Boron carbide because of its have that density is low, intensity big, high-temperature stability and the good feature of chemical stability, at wear-resisting material
Material, ceramic enhancement phase, especially at lightweight armor, the aspect such as pile neutron absorbent uses.Additionally, and diamond and cube nitrogen
Changing boron to compare, boron carbide is easy to manufacture, with low cost, thus uses more extensive, can replace expensive in some place
Diamond, be commonly in grinding, grind, the application of the aspect such as boring.
The material that ceramic-metal composite material is made up of pottery and raw metal, has metal and the advantage of pottery concurrently, it
Density is little, hardness is high, wear-resisting, heat conductivity good, will not be because of quenching or shock heating and embrittlement.It addition, at one layer of gas of metal watch topcoating
The ceramic coating that close property is good, fusing point is high, heat transfer property is very poor, also can prevent metal or alloy from high temperature aoxidizing or corroding.Pottery
Porcelain-metallic composite had both had the toughness of metal, high-termal conductivity and good heat stability, have again pottery high temperature resistant,
The characteristic such as corrosion-resistant and wear-resistant.Ceramic metal is widely used in rocket, guided missile, the shell of supersonic plane, combustor
The places such as flame jet.
Boron carbide is combined with ceramic-metal composite material, prepares boron carbide base ceramic-metallic composite
Technology the most rare, and for grinding-material, space flight and aviation science and technology and high-temperature service on application performance also
The most well embody.
Summary of the invention
Solve the technical problem that: use less for existing boron carbide base ceramic-metallic composite and fail to send out
The shortcoming waving superperformance, the present invention provides a kind of boron carbide base ceramic-metallic composite and preparation method thereof.
Technical scheme: a kind of boron carbide base ceramic-metallic composite, containing following component in terms of mass parts: copper 5~15
Part, cobalt 3~12 parts, titanium alloy 10~25 parts, boron carbide 30~50 parts, 20~40 parts of pottery, boron fibre 10~20 parts, two silication
Molybdenum 5~18 parts, carborundum 3~10 parts, magnesium oxide 5~15 parts, aluminium sesquioxide 5~13 parts, silicone rubber 5~12 parts, waterglass
10~20 parts.
A kind of boron carbide base ceramic-metallic composite described above, containing following component in terms of mass parts: copper 7~
13 parts, cobalt 5~11 parts, titanium alloy 13~22 parts, boron carbide 35~45 parts, 25~35 parts of pottery, boron fibre 12~18 parts, two silicon
Change molybdenum 8~15 parts, carborundum 4~9 parts, magnesium oxide 7~12 parts, aluminium sesquioxide 8~12 parts, silicone rubber 7~11 parts, waterglass
12~17 parts.
A kind of boron carbide base ceramic-metallic composite described above, containing following component in terms of mass parts: copper 9 parts,
Cobalt 7 parts, titanium alloy 15 parts, boron carbide 38 parts, 28 parts of pottery, boron fibre 13 parts, molybdenum disilicide 10 parts, carborundum 5 parts, magnesium oxide
9 parts, aluminium sesquioxide 9 parts, 8 parts of silicone rubber, waterglass 14 parts.
A kind of boron carbide base ceramic-metallic composite described above, containing following component in terms of mass parts: copper 10
Part, cobalt 8 parts, titanium alloy 18 parts, boron carbide 40 parts, 30 parts of pottery, boron fibre 15 parts, molybdenum disilicide 12 parts, carborundum 6.5 parts,
Magnesium oxide 9.5 parts, aluminium sesquioxide 10 parts, 9 parts of silicone rubber, waterglass 15 parts.
The preparation method of a kind of boron carbide base ceramic-metallic composite described above, the step of this preparation method is such as
Under:
The first step: mix after copper, cobalt, titanium alloy fusing, then with boron carbide under 1300~1500 DEG C, vacuum or noble gas
Reaction generates boride;
Second step: boride that the first step is obtained, pottery, boron fibre, molybdenum disilicide, carborundum, magnesium oxide, three oxidations two
Aluminum, silicone rubber, waterglass mix homogeneously, with 40~60 mesh sieve pelletizes, then pressure be 100~120MPa, temperature be 100~
It is molded into blank at 120 DEG C;
3rd step: the blank obtained by second step is put into and colded pressing in preforming grinding tool, carries out freezing off mold pressing, obtains boron carbide-based pottery
Porcelain-metallic composite, the temperature wherein freezing off mold pressing is 10~20 DEG C, and pressure is 5~10MPa, and freezing off clamp time is 15
~25min.
In the first step described above, reaction temperature is 1400 DEG C.
With 50 mesh sieve pelletizes in second step described above, then pressure be 110MPa, temperature be to be molded at 110 DEG C
Base.
The temperature freezing off mold pressing in the 3rd step described above is 15 DEG C, and pressure is 7.5MPa, freezes off clamp time and is
20min。
Beneficial effect: a kind of boron carbide base ceramic-metallic composite that the present invention provides and preparation method thereof, this carbonization
Boryl ceramic-metal composite material has possessed boron carbide, pottery, the performance of metal these three material, has good the most simultaneously
Hardness, bending strength, fusing point, wear-resisting, heat conduction, decay resistance, can as tunnel boring material, aerial incendiary dart shell with
And high-temperature service sheathing material.
Detailed description of the invention
Embodiment 1
A kind of boron carbide base ceramic-metallic composite, containing following component in terms of mass parts: copper 5 parts, cobalt 3 parts, titanium alloy 10
Part, boron carbide 30 parts, 20 parts of pottery, boron fibre 10 parts, molybdenum disilicide 5 parts, carborundum 3 parts, magnesium oxide 5 parts, aluminium sesquioxide 5
Part, 5 parts of silicone rubber, waterglass 10 parts.
A kind of preparation method of boron carbide base ceramic-metallic composite, the step of this preparation method is as follows:
The first step: mix after copper, cobalt, titanium alloy fusing, then react raw under 1300 DEG C, vacuum or noble gas with boron carbide
Become boride;
Second step: boride that the first step is obtained, pottery, boron fibre, molybdenum disilicide, carborundum, magnesium oxide, three oxidations two
Aluminum, silicone rubber, waterglass mix homogeneously, with 40 mesh sieve pelletizes, then pressure be 100MPa, temperature be to be molded at 100 DEG C
Blank;
3rd step: the blank obtained by second step is put into and colded pressing in preforming grinding tool, carries out freezing off mold pressing, obtains boron carbide-based pottery
Porcelain-metallic composite, the temperature wherein freezing off mold pressing is 10 DEG C, and pressure is 5MPa, and freezing off clamp time is 15min.
Embodiment 2
A kind of boron carbide base ceramic-metallic composite, containing following component in terms of mass parts: copper 15 parts, cobalt 12 parts, titanium alloy
25 parts, boron carbide 50 parts, 40 parts of pottery, boron fibre 20 parts, molybdenum disilicide 18 parts, carborundum 10 parts, magnesium oxide 15 parts, three oxidations
Two 13 parts of aluminum, 12 parts of silicone rubber, waterglass 20 parts.
A kind of preparation method of boron carbide base ceramic-metallic composite, the step of this preparation method is as follows:
The first step: mix after copper, cobalt, titanium alloy fusing, then react raw under 1500 DEG C, vacuum or noble gas with boron carbide
Become boride;
Second step: boride that the first step is obtained, pottery, boron fibre, molybdenum disilicide, carborundum, magnesium oxide, three oxidations two
Aluminum, silicone rubber, waterglass mix homogeneously, with 60 mesh sieve pelletizes, then pressure be 120MPa, temperature be to be molded at 120 DEG C
Blank;
3rd step: the blank obtained by second step is put into and colded pressing in preforming grinding tool, carries out freezing off mold pressing, obtains boron carbide-based pottery
Porcelain-metallic composite, the temperature wherein freezing off mold pressing is 20 DEG C, and pressure is 10MPa, and freezing off clamp time is 25min.
Embodiment 3
A kind of boron carbide base ceramic-metallic composite, containing following component in terms of mass parts: copper 13 parts, cobalt 11 parts, titanium alloy
22 parts, boron carbide 45 parts, 35 parts of pottery, boron fibre 18 parts, molybdenum disilicide 15 parts, carborundum 9 parts, magnesium oxide 12 parts, three oxidations
Two 12 parts of aluminum, 11 parts of silicone rubber, waterglass 17 parts.
A kind of preparation method of boron carbide base ceramic-metallic composite, the step of this preparation method is as follows:
The first step: mix after copper, cobalt, titanium alloy fusing, then react raw under 1400 DEG C, vacuum or noble gas with boron carbide
Become boride;
Second step: boride that the first step is obtained, pottery, boron fibre, molybdenum disilicide, carborundum, magnesium oxide, three oxidations two
Aluminum, silicone rubber, waterglass mix homogeneously, with 50 mesh sieve pelletizes, then pressure be 110MPa, temperature be to be molded at 110 DEG C
Blank;
3rd step: the blank obtained by second step is put into and colded pressing in preforming grinding tool, carries out freezing off mold pressing, obtains boron carbide-based pottery
Porcelain-metallic composite, the temperature wherein freezing off mold pressing is 15 DEG C, and pressure is 7.5MPa, and freezing off clamp time is 20min.
Embodiment 4
A kind of boron carbide base ceramic-metallic composite, containing following component in terms of mass parts: copper 9 parts, cobalt 7 parts, titanium alloy 15
Part, boron carbide 38 parts, 28 parts of pottery, boron fibre 13 parts, molybdenum disilicide 10 parts, carborundum 5 parts, magnesium oxide 9 parts, aluminium sesquioxide
9 parts, 8 parts of silicone rubber, waterglass 14 parts.
A kind of preparation method of boron carbide base ceramic-metallic composite, the step of this preparation method is as follows:
The first step: mix after copper, cobalt, titanium alloy fusing, then react raw under 1400 DEG C, vacuum or noble gas with boron carbide
Become boride;
Second step: boride that the first step is obtained, pottery, boron fibre, molybdenum disilicide, carborundum, magnesium oxide, three oxidations two
Aluminum, silicone rubber, waterglass mix homogeneously, with 50 mesh sieve pelletizes, then pressure be 110MPa, temperature be to be molded at 110 DEG C
Blank;
3rd step: the blank obtained by second step is put into and colded pressing in preforming grinding tool, carries out freezing off mold pressing, obtains boron carbide-based pottery
Porcelain-metallic composite, the temperature wherein freezing off mold pressing is 15 DEG C, and pressure is 7.5MPa, and freezing off clamp time is 20min.
Embodiment 5
A kind of boron carbide base ceramic-metallic composite, containing following component in terms of mass parts: copper 10 parts, cobalt 8 parts, titanium alloy
18 parts, boron carbide 40 parts, 30 parts of pottery, boron fibre 15 parts, molybdenum disilicide 12 parts, carborundum 6.5 parts, magnesium oxide 9.5 parts, three oxygen
Change 10 parts of two aluminum, 9 parts of silicone rubber, waterglass 15 parts.
A kind of preparation method of boron carbide base ceramic-metallic composite, the step of this preparation method is as follows:
The first step: mix after copper, cobalt, titanium alloy fusing, then react raw under 1400 DEG C, vacuum or noble gas with boron carbide
Become boride;
Second step: boride that the first step is obtained, pottery, boron fibre, molybdenum disilicide, carborundum, magnesium oxide, three oxidations two
Aluminum, silicone rubber, waterglass mix homogeneously, with 50 mesh sieve pelletizes, then pressure be 110MPa, temperature be to be molded at 110 DEG C
Blank;
3rd step: the blank obtained by second step is put into and colded pressing in preforming grinding tool, carries out freezing off mold pressing, obtains boron carbide-based pottery
Porcelain-metallic composite, the temperature wherein freezing off mold pressing is 15 DEG C, and pressure is 7.5MPa, and freezing off clamp time is 20min.
The technical performance index of the above-mentioned boron carbide base ceramic-metallic composite stating embodiment 1~embodiment 5, its inspection
Survey result is as follows:
Above the embodiment of the present invention is described in detail, for one of ordinary skill in the art, implements according to the present invention
The thought of example, the most all will change, and in sum, this specification content should not be managed
Solve as limitation of the present invention.
Claims (8)
1. boron carbide base ceramic-metallic composite, it is characterised in that containing following component in terms of mass parts: copper 5~15
Part, cobalt 3~12 parts, titanium alloy 10~25 parts, boron carbide 30~50 parts, 20~40 parts of pottery, boron fibre 10~20 parts, two silication
Molybdenum 5~18 parts, carborundum 3~10 parts, magnesium oxide 5~15 parts, aluminium sesquioxide 5~13 parts, silicone rubber 5~12 parts, waterglass
10~20 parts.
A kind of boron carbide base ceramic-metallic composite the most according to claim 1, it is characterised in that contain in terms of mass parts
There is a following component: copper 7~13 parts, cobalt 5~11 parts, titanium alloy 13~22 parts, boron carbide 35~45 parts, 25~35 parts of pottery, boron
Fiber 12~18 parts, molybdenum disilicide 8~15 parts, carborundum 4~9 parts, magnesium oxide 7~12 parts, aluminium sesquioxide 8~12 parts, silicon
Rubber 7~11 parts, waterglass 12~17 parts.
A kind of boron carbide base ceramic-metallic composite the most according to claim 1, it is characterised in that contain in terms of mass parts
There is a following component: copper 9 parts, cobalt 7 parts, titanium alloy 15 parts, boron carbide 38 parts, 28 parts of pottery, boron fibre 13 parts, molybdenum disilicide 10
Part, carborundum 5 parts, magnesium oxide 9 parts, aluminium sesquioxide 9 parts, 8 parts of silicone rubber, waterglass 14 parts.
A kind of boron carbide base ceramic-metallic composite the most according to claim 1, it is characterised in that contain in terms of mass parts
There is a following component: copper 10 parts, cobalt 8 parts, titanium alloy 18 parts, boron carbide 40 parts, 30 parts of pottery, boron fibre 15 parts, molybdenum disilicide 12
Part, carborundum 6.5 parts, magnesium oxide 9.5 parts, aluminium sesquioxide 10 parts, 9 parts of silicone rubber, waterglass 15 parts.
5. the preparation method of a kind of boron carbide base ceramic-metallic composite described in claim 1, it is characterised in that this is prepared
The step of method is as follows:
The first step: mix after copper, cobalt, titanium alloy fusing, then with boron carbide under 1300~1500 DEG C, vacuum or noble gas
Reaction generates boride;
Second step: boride that the first step is obtained, pottery, boron fibre, molybdenum disilicide, carborundum, magnesium oxide, three oxidations two
Aluminum, silicone rubber, waterglass mix homogeneously, with 40~60 mesh sieve pelletizes, then pressure be 100~120MPa, temperature be 100~
It is molded into blank at 120 DEG C;
3rd step: the blank obtained by second step is put into and colded pressing in preforming grinding tool, carries out freezing off mold pressing, obtains boron carbide-based pottery
Porcelain-metallic composite, the temperature wherein freezing off mold pressing is 10~20 DEG C, and pressure is 5~10MPa, and freezing off clamp time is 15
~25min.
The preparation method of a kind of boron carbide base ceramic-metallic composite the most according to claim 5, it is characterised in that:
In the described first step, reaction temperature is 1400 DEG C.
The preparation method of a kind of boron carbide base ceramic-metallic composite the most according to claim 5, it is characterised in that:
With 50 mesh sieve pelletizes in described second step, then pressure be 110MPa, temperature be to be molded into base at 110 DEG C.
The preparation method of a kind of boron carbide base ceramic-metallic composite the most according to claim 5, it is characterised in that:
The temperature freezing off mold pressing in described 3rd step is 15 DEG C, and pressure is 7.5MPa, and freezing off clamp time is 20min.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610174920.4A CN105859295A (en) | 2016-03-25 | 2016-03-25 | Boron carbide-based ceramic-metal composite material and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610174920.4A CN105859295A (en) | 2016-03-25 | 2016-03-25 | Boron carbide-based ceramic-metal composite material and preparation method thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
CN105859295A true CN105859295A (en) | 2016-08-17 |
Family
ID=56625810
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610174920.4A Pending CN105859295A (en) | 2016-03-25 | 2016-03-25 | Boron carbide-based ceramic-metal composite material and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN105859295A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106747463A (en) * | 2016-12-14 | 2017-05-31 | 宜兴市华井科技有限公司 | A kind of anticorrosive special cermacis and preparation method thereof |
CN108585871A (en) * | 2018-02-05 | 2018-09-28 | 北京理工大学 | A kind of B4The fast preparation method of C ceramic blocks |
CN116802168A (en) * | 2021-01-26 | 2023-09-22 | 三菱电机株式会社 | Composite ceramic material and method for producing composite ceramic material |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103613389A (en) * | 2013-11-29 | 2014-03-05 | 宁波伏尔肯机械密封件制造有限公司 | Sintering preparation method of boron carbide ceramic |
JP2014125382A (en) * | 2012-12-26 | 2014-07-07 | Nihon Ceratec Co Ltd | Composite material and method for manufacturing the same |
CN105176083A (en) * | 2015-09-25 | 2015-12-23 | 苏州莱特复合材料有限公司 | Composite material for car shell and preparation method thereof |
CN105176058A (en) * | 2015-09-25 | 2015-12-23 | 苏州莱特复合材料有限公司 | Composite for manufacturing helmet and preparation method of composite |
-
2016
- 2016-03-25 CN CN201610174920.4A patent/CN105859295A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2014125382A (en) * | 2012-12-26 | 2014-07-07 | Nihon Ceratec Co Ltd | Composite material and method for manufacturing the same |
CN103613389A (en) * | 2013-11-29 | 2014-03-05 | 宁波伏尔肯机械密封件制造有限公司 | Sintering preparation method of boron carbide ceramic |
CN105176083A (en) * | 2015-09-25 | 2015-12-23 | 苏州莱特复合材料有限公司 | Composite material for car shell and preparation method thereof |
CN105176058A (en) * | 2015-09-25 | 2015-12-23 | 苏州莱特复合材料有限公司 | Composite for manufacturing helmet and preparation method of composite |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106747463A (en) * | 2016-12-14 | 2017-05-31 | 宜兴市华井科技有限公司 | A kind of anticorrosive special cermacis and preparation method thereof |
CN108585871A (en) * | 2018-02-05 | 2018-09-28 | 北京理工大学 | A kind of B4The fast preparation method of C ceramic blocks |
CN108585871B (en) * | 2018-02-05 | 2020-09-25 | 北京理工大学 | B4Quick preparation method of C ceramic block |
CN116802168A (en) * | 2021-01-26 | 2023-09-22 | 三菱电机株式会社 | Composite ceramic material and method for producing composite ceramic material |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2017035916A1 (en) | Enhanced cermet wear-resistant composite material and method for fabrication thereof | |
CN103992115B (en) | A kind of preparation method of C/SiC-HfC fibre reinforced ultra-temperature ceramic-based composite material | |
Yin et al. | The effects of SiC precursors on the microstructures and mechanical properties of SiCf/SiC composites prepared via polymer impregnation and pyrolysis process | |
US9938198B2 (en) | Method for integral joining infiltrated ceramic matrix composites | |
CN105859295A (en) | Boron carbide-based ceramic-metal composite material and preparation method thereof | |
CN109608217B (en) | SiC containing MAX phase interface layerfPreparation method of/SiC composite material | |
CN112592184B (en) | Ultra-light boron carbide bulletproof ceramic and preparation method and application thereof | |
CN102184873B (en) | Method for quickly preparing diamond-silicon carbide electronic packaging material | |
CN103724032B (en) | A kind of two-dimensional fiber cloth strengthens silicon nitride-silicon carbide ceramic composite and preparation method thereof | |
CN112194492B (en) | Silicon nitride ceramic material, preparation method and application thereof, and bulletproof flashboard | |
CN104030688A (en) | Preparation method of low-temperature reactive sintered silicon carbide | |
CN112010663B (en) | C/SiC ceramic matrix composite with refractory metal carbide interface and preparation method thereof | |
CN107746282A (en) | A kind of in-situ carburization silica fibre enhancing liquid phase sintering silicon carbide ceramic and manufacture method | |
CN103981384B (en) | A kind of preparation method of tungsten-aluminium nitride-hafnium boride matrix material | |
CN106631028B (en) | A kind of preparation process of metal composite magnesium silicon carbide bullet-proof ceramics | |
CN105543609B (en) | A kind of boron carbide-based composite material containing zirconium and preparation method thereof | |
KR101616202B1 (en) | Joint structure body for super high-temperature components | |
CN110468358A (en) | A kind of metal ceramic-based composite material barrel support of fibre reinforced and preparation method thereof | |
CN109437955A (en) | A kind of brake material fast preparation method modified based on Polycarbosilane | |
CN106800414A (en) | The method that reaction in-situ prepares the ultra-temperature ceramic-based composite material of nitrogen boron | |
CN104384516B (en) | The preparation method of the metallurgical powder brake material that a kind of bullet train uses | |
CN106756413A (en) | A kind of ceramic-metal composite | |
CN109402480A (en) | A kind of WCoB cermet material and preparation method thereof | |
CN105585324A (en) | Whisker toughened and reinforced carbon-ceramic composite material | |
CN106187263A (en) | The manufacture method of C/C SiC ceramic matrix composite material parts and C/C SiC ceramic matrix composite material parts |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160817 |