CN106747546A - A kind of high-strength and high ductility ceramic composite and its application - Google Patents

A kind of high-strength and high ductility ceramic composite and its application Download PDF

Info

Publication number
CN106747546A
CN106747546A CN201611099135.3A CN201611099135A CN106747546A CN 106747546 A CN106747546 A CN 106747546A CN 201611099135 A CN201611099135 A CN 201611099135A CN 106747546 A CN106747546 A CN 106747546A
Authority
CN
China
Prior art keywords
parts
fiber
weight
composite
auxiliary agent
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
Application number
CN201611099135.3A
Other languages
Chinese (zh)
Inventor
杨淑梅
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zibo Jingcheng Patent Information Consulting Co Ltd
Original Assignee
Zibo Jingcheng Patent Information Consulting Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zibo Jingcheng Patent Information Consulting Co Ltd filed Critical Zibo Jingcheng Patent Information Consulting Co Ltd
Priority to CN201611099135.3A priority Critical patent/CN106747546A/en
Publication of CN106747546A publication Critical patent/CN106747546A/en
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/71Ceramic products containing macroscopic reinforcing agents
    • C04B35/78Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
    • C04B35/80Fibres, filaments, whiskers, platelets, or the like
    • C04B35/82Asbestos; Glass; Fused silica
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B20/00Use of materials as fillers for mortars, concrete or artificial stone according to more than one of groups C04B14/00 - C04B18/00 and characterised by shape or grain distribution; Treatment of materials according to more than one of the groups C04B14/00 - C04B18/00 specially adapted to enhance their filling properties in mortars, concrete or artificial stone; Expanding or defibrillating materials
    • C04B20/02Treatment
    • C04B20/023Chemical treatment
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515Shaped 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
    • C04B35/58Shaped 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 borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides
    • C04B35/584Shaped 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 borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides based on silicon nitride
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/622Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/626Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
    • C04B35/62605Treating the starting powders individually or as mixtures
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/622Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/64Burning or sintering processes
    • C04B35/645Pressure sintering
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/32Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
    • C04B2235/3217Aluminum oxide or oxide forming salts thereof, e.g. bauxite, alpha-alumina
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/32Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
    • C04B2235/3231Refractory metal oxides, their mixed metal oxides, or oxide-forming salts thereof
    • C04B2235/3244Zirconium oxides, zirconates, hafnium oxides, hafnates, or oxide-forming salts thereof
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/34Non-metal oxides, non-metal mixed oxides, or salts thereof that form the non-metal oxides upon heating, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
    • C04B2235/349Clays, e.g. bentonites, smectites such as montmorillonite, vermiculites or kaolines, e.g. illite, talc or sepiolite
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/38Non-oxide ceramic constituents or additives
    • C04B2235/3817Carbides
    • C04B2235/3826Silicon carbides
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/44Metal salt constituents or additives chosen for the nature of the anions, e.g. hydrides or acetylacetonate
    • C04B2235/444Halide containing anions, e.g. bromide, iodate, chlorite
    • C04B2235/445Fluoride containing anions, e.g. fluosilicate

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Compositions Of Oxide Ceramics (AREA)

Abstract

The invention discloses a kind of high-strength and high ductility ceramic composite and its application, it is composited by ceramic matrix, fiber, auxiliary agent, ceramic matrix, fiber, the weight ratio of auxiliary agent are 100:(35‑45):(5‑15);The ceramic matrix is made up of according to weight portion 30 50 parts of silicon nitrides and 25 35 parts of carborundum;The fiber is modified composite fiber, by basalt fibre and brucite fiber by weight (2 4):1 mixing post-modification is obtained, and method of modifying is:First the triethylamine solution ultrasound that composite fibre mass fraction is 10 20% is soaked 24 hours, clear water is rinsed to neutrality, drying, calcined 12 hours then at 450 550 DEG C, di-iso-octyldiphenylamine, 4 6% kojic acid and the 2 4% ethylenediamine tetra-acetic acid disalt of composite fibre weight 7 9% are added after cooling, ground and mixed is uniform after 50 70 DEG C of drying, crosses 200 300 mesh sieves;The auxiliary agent includes 35 parts of 20 30 parts of nano zircite, 5 15 parts of nano aluminium oxide, 48 parts of nano montmorillonite powder and nanometer Fluorspar Powder by weight.Not only intensity and hardness are high for the ceramic composite that the present invention is provided, and tenacity excellent.

Description

A kind of high-strength and high ductility ceramic composite and its application
Technical field
The present invention relates to composite, and in particular to a kind of high-strength and high ductility ceramic composite and its application.
Background technology
Composite generally has the good combination property that different materials are mutually learnt from other's strong points to offset one's weaknesses.Composite have concurrently two kinds or The characteristics of two or more materials, the performance of homogenous material can be improved, such as improve intensity, increase toughness and improve dielectric properties. As the ceramic composite of high-temperature structural material, it is mainly used in the departments such as aerospace, military project.Additionally, in machinery, chemical industry, electricity The fields such as sub- technology also widely used various ceramic composites.
It with ceramics is a class composite of matrix and various fiber composites that ceramic composite is.Ceramic matrix can be nitrogen The high-temperature structural ceramics such as SiClx, carborundum.These advanced ceramics have high temperature resistant, high intensity and rigidity, relative weight lighter, anti- The excellent properties such as corrosion, and its fatal weakness is to enbrittle, and during in stress state, can be cracked, or even fracture is led Cause material failure.And use high intensity, elastomeric fiber and matrix compound, then it is improve ceramics toughness and reliability one Effective method.Fiber can prevent the extension of crackle, so as to obtain the FRCMC of excellent in toughness.
The content of the invention
It is an object of the invention to provide a kind of high-strength and high ductility ceramic composite and its application.
Above-mentioned purpose of the invention is achieved by following technical scheme:
A kind of high-strength and high ductility ceramic composite, is composited by ceramic matrix, fiber, auxiliary agent, ceramic matrix, fiber, The weight ratio of auxiliary agent is 100:(35-45):(5-15);The ceramic matrix is according to weight portion by 30-50 parts of silicon nitride and 25-35 Part carborundum composition;The fiber is modified composite fiber, by basalt fibre and brucite fiber by weight (2-4):1 mixes Close post-modification to be obtained, method of modifying is:The triethylamine solution ultrasound that composite fibre mass fraction is 10-20% is first soaked into 2- 4 hours, clear water was rinsed to neutrality, and drying is calcined 1-2 hours then at 450-550 DEG C, and composite fibre weight 7- is added after cooling The ethylenediamine tetra-acetic acid disalt of 9% di-iso-octyldiphenylamine, the kojic acid of 4-6% and 2-4%, ground and mixed is uniformly after 50- 70 DEG C of drying, cross 200-300 mesh sieves;The auxiliary agent includes nano zircite 20-30 parts, nano aluminium oxide 5-15 by weight Part, nano montmorillonite powder 4-8 parts and 3-5 parts of nanometer Fluorspar Powder.
Further, the ethylenediamine tetra-acetic acid disalt is disodium ethylene diamine tetraacetate or EDTAP dipotassium ethylene diamine tetraacetate.
Further, the ceramic matrix, fiber, the weight ratio of auxiliary agent are 10:4:1.
Further, the ceramic matrix is made up of according to weight portion 40 parts of silicon nitrides and 30 parts of carborundum.
Further, the fiber is modified composite fiber, by basalt fibre and brucite fiber by weight 3:1 mixes Close post-modification to be obtained, method of modifying is:The triethylamine solution ultrasound that composite fibre mass fraction is 15% is first soaked 3 small When, clear water is rinsed to neutrality, and drying is calcined 1.5 hours then at 500 DEG C, and the two of addition composite fibre weight 8% is different pungent after cooling Base diphenylamines, 5% kojic acid and 3% ethylenediamine tetra-acetic acid disalt, ground and mixed uniformly after 60 DEG C of drying, cross 200-300 Mesh sieve.
Further, the auxiliary agent includes 25 parts of nano zircite, 10 parts of nano aluminium oxide, nano montmorillonite by weight 4 parts of 6 parts of powder and nanometer Fluorspar Powder.
The preparation method of above-mentioned high-strength and high ductility ceramic composite, including step:Step A, ceramic matrix is mixed with auxiliary agent Close, be milled to and be uniformly dispersed, cross 200-300 mesh sieves;Step B, to step A gained powder in add equivalent to its weight 25- 35% deionized water and 4-8% ethylene glycol, is mixed into pureed;Step C, it is modified compound to being added in step B gained purees Fiber, be milled to be uniformly dispersed after 300-400 DEG C calcine 2-4 hours, 200-300 mesh sieves were crushed after cooling;Step D, to Add the deionized water and 20-30% glycerine of 1.5-2.5 times of its weight in step C gained powders, be milled to be uniformly dispersed after 100-120 DEG C of drying, crosses 40-60 mesh sieves, obtains final product within hot pressing 40-60 minutes at 1600-1700 DEG C, wherein, hot pressing pressure is 26- 30MPa。
Advantages of the present invention:
Not only intensity and hardness are high for the ceramic composite that the present invention is provided, and tenacity excellent, under stress state not Crackle is also easy to produce, compared with prior art with prominent substantive distinguishing features and significant progress.
Specific embodiment
Essentiality content of the invention is further illustrated with reference to embodiment.
Embodiment 1:The preparation of ceramic composite
It is composited by ceramic matrix, fiber, auxiliary agent, ceramic matrix, fiber, the weight ratio of auxiliary agent are 100:40:10;Institute Ceramic matrix is stated to be made up of 40 parts of silicon nitrides and 30 parts of carborundum according to weight portion;The fiber is modified composite fiber, by profound Military rock fiber and brucite fiber are by weight 3:1 mixing post-modification is obtained, and method of modifying is:First by composite fibre quality point Number is soaked 3 hours for 15% triethylamine solution ultrasound, and clear water is rinsed to neutrality, and drying is calcined 1.5 hours then at 500 DEG C, cold But di-iso-octyldiphenylamine, 5% kojic acid and the 3% ethylenediamine tetra-acetic acid disalt of composite fibre weight 8%, grinding are added afterwards It is well mixed to be dried after 60 DEG C, cross 200-300 mesh sieves;The auxiliary agent includes 25 parts of nano zircite, nano oxygen by weight Change 4 parts of 10 parts of aluminium, 6 parts of nano montmorillonite powder and nanometer Fluorspar Powder.
Wherein, ethylenediamine tetra-acetic acid disalt is disodium ethylene diamine tetraacetate, it is also possible to EDTAP dipotassium ethylene diamine tetraacetate.
Preparation method:
Step A, ceramic matrix is mixed with auxiliary agent, is milled to and is uniformly dispersed, and crosses 200-300 mesh sieves;Step B, to step A The deionized water and 6% ethylene glycol equivalent to its weight 30% are added in gained powder, pureed is mixed into;Step C, to step B Add modified composite fiber in gained purees, be milled to be uniformly dispersed after 350 DEG C calcine 3 hours, crushed after cooling 200-300 mesh sieves;Step D, to the deionized water and 25% glycerine of 2 times of its weight is added in step C gained powders, is milled to point Dissipate uniformly after 110 DEG C of drying, cross 40-60 mesh sieves, hot pressing is obtained final product for 50 minutes at 1650 DEG C, and hot pressing pressure is 28MPa.
Embodiment 2:The preparation of ceramic composite
It is composited by ceramic matrix, fiber, auxiliary agent, ceramic matrix, fiber, the weight ratio of auxiliary agent are 100:35:15;Institute Ceramic matrix is stated to be made up of 30 parts of silicon nitrides and 25 parts of carborundum according to weight portion;The fiber is modified composite fiber, by profound Military rock fiber and brucite fiber are by weight 2:1 mixing post-modification is obtained, and method of modifying is:First by composite fibre quality point Number is soaked 4 hours for 10% triethylamine solution ultrasound, and clear water is rinsed to neutrality, and drying is calcined 2 hours then at 450 DEG C, cooling Di-iso-octyldiphenylamine, 4% kojic acid and the 2% ethylenediamine tetra-acetic acid disalt of composite fibre weight 7% are added afterwards, and grinding is mixed Close uniform after 50 DEG C of drying, cross 200-300 mesh sieves;The auxiliary agent includes 20 parts of nano zircite, nano oxidized by weight 3 parts of 5 parts of aluminium, 4 parts of nano montmorillonite powder and nanometer Fluorspar Powder.Wherein, ethylenediamine tetra-acetic acid disalt is disodium ethylene diamine tetraacetate, Also EDTAP dipotassium ethylene diamine tetraacetate can be used.
Preparation method:
Step A, ceramic matrix is mixed with auxiliary agent, is milled to and is uniformly dispersed, and crosses 200-300 mesh sieves;Step B, to step A The deionized water and 6% ethylene glycol equivalent to its weight 30% are added in gained powder, pureed is mixed into;Step C, to step B Add modified composite fiber in gained purees, be milled to be uniformly dispersed after 350 DEG C calcine 3 hours, crushed after cooling 200-300 mesh sieves;Step D, to the deionized water and 25% glycerine of 2 times of its weight is added in step C gained powders, is milled to point Dissipate uniformly after 110 DEG C of drying, cross 40-60 mesh sieves, hot pressing is obtained final product for 50 minutes at 1650 DEG C, and hot pressing pressure is 28MPa.
Embodiment 3:The preparation of ceramic composite
It is composited by ceramic matrix, fiber, auxiliary agent, ceramic matrix, fiber, the weight ratio of auxiliary agent are 100:45:5;Institute Ceramic matrix is stated to be made up of 50 parts of silicon nitrides and 35 parts of carborundum according to weight portion;The fiber is modified composite fiber, by profound Military rock fiber and brucite fiber are by weight 4:1 mixing post-modification is obtained, and method of modifying is:First by composite fibre quality point Number is soaked 2 hours for 20% triethylamine solution ultrasound, and clear water is rinsed to neutrality, and drying is calcined 1 hour then at 550 DEG C, cooling Di-iso-octyldiphenylamine, 6% kojic acid and the 4% ethylenediamine tetra-acetic acid disalt of composite fibre weight 9% are added afterwards, and grinding is mixed Close uniform after 70 DEG C of drying, cross 200-300 mesh sieves;The auxiliary agent includes 30 parts of nano zircite, nano oxidized by weight 5 parts of 15 parts of aluminium, 8 parts of nano montmorillonite powder and nanometer Fluorspar Powder.Wherein, ethylenediamine tetra-acetic acid disalt is ethylenediamine tetra-acetic acid two Sodium, it is also possible to EDTAP dipotassium ethylene diamine tetraacetate.
Preparation method:
Step A, ceramic matrix is mixed with auxiliary agent, is milled to and is uniformly dispersed, and crosses 200-300 mesh sieves;Step B, to step A The deionized water and 6% ethylene glycol equivalent to its weight 30% are added in gained powder, pureed is mixed into;Step C, to step B Add modified composite fiber in gained purees, be milled to be uniformly dispersed after 350 DEG C calcine 3 hours, crushed after cooling 200-300 mesh sieves;Step D, to the deionized water and 25% glycerine of 2 times of its weight is added in step C gained powders, is milled to point Dissipate uniformly after 110 DEG C of drying, cross 40-60 mesh sieves, hot pressing is obtained final product for 50 minutes at 1650 DEG C, and hot pressing pressure is 28MPa.
Embodiment 4:The preparation of ceramic composite
It is composited by ceramic matrix, fiber, auxiliary agent, ceramic matrix, fiber, the weight ratio of auxiliary agent are 100:35:10;Institute Ceramic matrix is stated to be made up of 40 parts of silicon nitrides and 30 parts of carborundum according to weight portion;The fiber is modified composite fiber, by profound Military rock fiber and brucite fiber are by weight 3:1 mixing post-modification is obtained, and method of modifying is:First by composite fibre quality point Number is soaked 3 hours for 15% triethylamine solution ultrasound, and clear water is rinsed to neutrality, and drying is calcined 1.5 hours then at 500 DEG C, cold But di-iso-octyldiphenylamine, 5% kojic acid and the 3% ethylenediamine tetra-acetic acid disalt of composite fibre weight 8%, grinding are added afterwards It is well mixed to be dried after 60 DEG C, cross 200-300 mesh sieves;The auxiliary agent includes 25 parts of nano zircite, nano oxygen by weight Change 4 parts of 10 parts of aluminium, 6 parts of nano montmorillonite powder and nanometer Fluorspar Powder.
Wherein, ethylenediamine tetra-acetic acid disalt is disodium ethylene diamine tetraacetate, it is also possible to EDTAP dipotassium ethylene diamine tetraacetate.
Preparation method:
Step A, ceramic matrix is mixed with auxiliary agent, is milled to and is uniformly dispersed, and crosses 200-300 mesh sieves;Step B, to step A The deionized water and 6% ethylene glycol equivalent to its weight 30% are added in gained powder, pureed is mixed into;Step C, to step B Add modified composite fiber in gained purees, be milled to be uniformly dispersed after 350 DEG C calcine 3 hours, crushed after cooling 200-300 mesh sieves;Step D, to the deionized water and 25% glycerine of 2 times of its weight is added in step C gained powders, is milled to point Dissipate uniformly after 110 DEG C of drying, cross 40-60 mesh sieves, hot pressing is obtained final product for 50 minutes at 1650 DEG C, and hot pressing pressure is 28MPa.
Embodiment 5:The preparation of ceramic composite
It is composited by ceramic matrix, fiber, auxiliary agent, ceramic matrix, fiber, the weight ratio of auxiliary agent are 100:45:10;Institute Ceramic matrix is stated to be made up of 40 parts of silicon nitrides and 30 parts of carborundum according to weight portion;The fiber is modified composite fiber, by profound Military rock fiber and brucite fiber are by weight 3:1 mixing post-modification is obtained, and method of modifying is:First by composite fibre quality point Number is soaked 3 hours for 15% triethylamine solution ultrasound, and clear water is rinsed to neutrality, and drying is calcined 1.5 hours then at 500 DEG C, cold But di-iso-octyldiphenylamine, 5% kojic acid and the 3% ethylenediamine tetra-acetic acid disalt of composite fibre weight 8%, grinding are added afterwards It is well mixed to be dried after 60 DEG C, cross 200-300 mesh sieves;The auxiliary agent includes 25 parts of nano zircite, nano oxygen by weight Change 4 parts of 10 parts of aluminium, 6 parts of nano montmorillonite powder and nanometer Fluorspar Powder.
Wherein, ethylenediamine tetra-acetic acid disalt is disodium ethylene diamine tetraacetate, it is also possible to EDTAP dipotassium ethylene diamine tetraacetate.
Preparation method:
Step A, ceramic matrix is mixed with auxiliary agent, is milled to and is uniformly dispersed, and crosses 200-300 mesh sieves;Step B, to step A The deionized water and 6% ethylene glycol equivalent to its weight 30% are added in gained powder, pureed is mixed into;Step C, to step B Add modified composite fiber in gained purees, be milled to be uniformly dispersed after 350 DEG C calcine 3 hours, crushed after cooling 200-300 mesh sieves;Step D, to the deionized water and 25% glycerine of 2 times of its weight is added in step C gained powders, is milled to point Dissipate uniformly after 110 DEG C of drying, cross 40-60 mesh sieves, hot pressing is obtained final product for 50 minutes at 1650 DEG C, and hot pressing pressure is 28MPa.
Embodiment 6:The contrast of embodiment 1, fiber is unmodified composite fibre
It is composited by ceramic matrix, fiber, auxiliary agent, ceramic matrix, fiber, the weight ratio of auxiliary agent are 100:40:10;Institute Ceramic matrix is stated to be made up of 40 parts of silicon nitrides and 30 parts of carborundum according to weight portion;The fiber is composite fibre, by basalt Fiber and brucite fiber are by weight 3:1 is mixed to prepare;The auxiliary agent includes 25 parts of nano zircite, nano oxygen by weight Change 4 parts of 10 parts of aluminium, 6 parts of nano montmorillonite powder and nanometer Fluorspar Powder.
Wherein, ethylenediamine tetra-acetic acid disalt is disodium ethylene diamine tetraacetate, it is also possible to EDTAP dipotassium ethylene diamine tetraacetate.
Preparation method:
Step A, ceramic matrix is mixed with auxiliary agent, is milled to and is uniformly dispersed, and crosses 200-300 mesh sieves;Step B, to step A The deionized water and 6% ethylene glycol equivalent to its weight 30% are added in gained powder, pureed is mixed into;Step C, to step B Add composite fibre in gained purees, be milled to be uniformly dispersed after 350 DEG C calcine 3 hours, 200-300 was crushed after cooling Mesh sieve;Step D, to deionized water and 25% glycerine that 2 times of its weight is added in step C gained powders, is milled to and is uniformly dispersed After 110 DEG C of drying, 40-60 mesh sieves are crossed, hot pressing is obtained final product for 50 minutes at 1650 DEG C, and hot pressing pressure is 28MPa.
Embodiment 7:Effect example
The Vickers hardness of ceramic composite, bending strength and fracture toughness obtained by difference testing example 1-6, as a result such as Following table:
Vickers hardness (GPa) Bending strength (MPa) Fracture toughness (MPam1/2)
Embodiment 1 98 1210 21
Embodiment 2 95 1180 19
Embodiment 3 96 1190 20
Embodiment 4 95 1185 19
Embodiment 5 94 1175 20
Embodiment 6 90 1090 8
Certain commercially available ceramics 85 1020 6
Result shows that not only intensity and hardness are high for the ceramic composite that the present invention is provided, and tenacity excellent, in stress Crackle is not likely to produce under state, compared with prior art with prominent substantive distinguishing features and significant progress.

Claims (7)

1. a kind of high-strength and high ductility ceramic composite, is composited by ceramic matrix, fiber, auxiliary agent, it is characterised in that:Ceramic base Body, fiber, the weight ratio of auxiliary agent are 100:(35-45):(5-15);The ceramic matrix is according to weight portion by 30-50 parts of nitridation Silicon and 25-35 parts of carborundum composition;The fiber is modified composite fiber, by basalt fibre and brucite fiber by weight (2-4):1 mixing post-modification is obtained, and method of modifying is:First by triethylamine solution that composite fibre mass fraction is 10-20% Ultrasound immersion 2-4 hours, clear water is rinsed to neutrality, and drying is calcined 1-2 hours then at 450-550 DEG C, and compound fibre is added after cooling The ethylenediamine tetra-acetic acid disalt of the di-iso-octyldiphenylamine, the kojic acid of 4-6% and 2-4% of dimension weight 7-9%, ground and mixed is uniform After 50-70 DEG C of drying, 200-300 mesh sieves are crossed;The auxiliary agent by weight include nano zircite 20-30 parts, it is nano oxidized Aluminium 5-15 parts, nano montmorillonite powder 4-8 parts and 3-5 parts of nanometer Fluorspar Powder.
2. high-strength and high ductility ceramic composite according to claim 1, it is characterised in that:The ethylenediamine tetra-acetic acid disalt It is disodium ethylene diamine tetraacetate or EDTAP dipotassium ethylene diamine tetraacetate.
3. high-strength and high ductility ceramic composite according to claim 1, it is characterised in that:The ceramic matrix, fiber, help The weight ratio of agent is 10:4:1.
4. high-strength and high ductility ceramic composite according to claim 1, it is characterised in that:The ceramic matrix is according to weight Part is made up of 40 parts of silicon nitrides and 30 parts of carborundum.
5. high-strength and high ductility ceramic composite according to claim 1, it is characterised in that the fiber is modified compound fibre Dimension, by basalt fibre and brucite fiber by weight 3:1 mixing post-modification is obtained, and method of modifying is:First by composite fibre With the triethylamine solution ultrasound immersion that mass fraction is 15% 3 hours, clear water was rinsed to neutrality, is dried, then at 500 DEG C of calcinings 1.5 hours, di-iso-octyldiphenylamine, 5% kojic acid and the 3% ethylenediamine tetrem of composite fibre weight 8% are added after cooling Sour disalt, ground and mixed is crossed 200-300 mesh sieves and is obtained final product uniformly after 60 DEG C of drying.
6. high-strength and high ductility ceramic composite according to claim 1, it is characterised in that:The auxiliary agent includes by weight 4 parts of 25 parts of nano zircite, 10 parts of nano aluminium oxide, 6 parts of nano montmorillonite powder and nanometer Fluorspar Powder.
7. the preparation method of any high-strength and high ductility ceramic composites of claim 1-6, it is characterised in that including step: Step A, ceramic matrix is mixed with auxiliary agent, is milled to and is uniformly dispersed, and crosses 200-300 mesh sieves;Step B, to step A gained powders Middle deionized water and 4-8% ethylene glycol of the addition equivalent to its weight 25-35%, is mixed into pureed;Step C, to step B gained Modified composite fiber is added in purees, be milled to be uniformly dispersed after 300-400 DEG C calcine 2-4 hours, crushed after cooling 200-300 mesh sieves;Step D, to step C gained powder in add the deionized water and 20-30% of 1.5-2.5 times of its weight sweet Oil, is milled to and is uniformly dispersed after 100-120 DEG C of drying, crosses 40-60 mesh sieves, is within hot pressing 40-60 minutes at 1600-1700 DEG C , wherein, hot pressing pressure is 26-30MPa.
CN201611099135.3A 2016-12-04 2016-12-04 A kind of high-strength and high ductility ceramic composite and its application Pending CN106747546A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611099135.3A CN106747546A (en) 2016-12-04 2016-12-04 A kind of high-strength and high ductility ceramic composite and its application

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611099135.3A CN106747546A (en) 2016-12-04 2016-12-04 A kind of high-strength and high ductility ceramic composite and its application

Publications (1)

Publication Number Publication Date
CN106747546A true CN106747546A (en) 2017-05-31

Family

ID=58884672

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611099135.3A Pending CN106747546A (en) 2016-12-04 2016-12-04 A kind of high-strength and high ductility ceramic composite and its application

Country Status (1)

Country Link
CN (1) CN106747546A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110950674A (en) * 2019-12-26 2020-04-03 九牧厨卫股份有限公司 Preparation method of fiber-reinforced sanitary ceramic body

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4888311A (en) * 1986-10-14 1989-12-19 Nicolas Davidovits Ceramic-ceramic composite material and production method
CN102701770A (en) * 2012-03-27 2012-10-03 郭丰亮 Continuous basalt fiber reinforced ceramic composite and preparation method for same
CN103724032A (en) * 2013-07-23 2014-04-16 太仓派欧技术咨询服务有限公司 Two-dimension fiber cloth-reinforced silicon nitride-silicon carbide ceramic composite material and preparation method thereof
CN104803696A (en) * 2015-04-13 2015-07-29 安徽省含山瓷业股份有限公司 High-strength carbon fiber enhanced silicon nitride ceramic matrix composite and preparation method thereof
CN104844241A (en) * 2015-04-13 2015-08-19 安徽省含山瓷业股份有限公司 High strength carbon fiber reinforced silicon carbide ceramic matrix composite material and preparation method thereof
CN105345679A (en) * 2015-09-24 2016-02-24 安徽威铭耐磨材料有限公司 Basalt fiber enhanced nano-vitrified bond diamond grinding wheel and preparation method thereof
CN106007758A (en) * 2016-04-22 2016-10-12 葫芦岛市华能工业陶瓷有限公司 Toughened silicon nitride combined silicon carbide ceramic composite material and preparation method thereof

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4888311A (en) * 1986-10-14 1989-12-19 Nicolas Davidovits Ceramic-ceramic composite material and production method
CN102701770A (en) * 2012-03-27 2012-10-03 郭丰亮 Continuous basalt fiber reinforced ceramic composite and preparation method for same
CN103724032A (en) * 2013-07-23 2014-04-16 太仓派欧技术咨询服务有限公司 Two-dimension fiber cloth-reinforced silicon nitride-silicon carbide ceramic composite material and preparation method thereof
CN104803696A (en) * 2015-04-13 2015-07-29 安徽省含山瓷业股份有限公司 High-strength carbon fiber enhanced silicon nitride ceramic matrix composite and preparation method thereof
CN104844241A (en) * 2015-04-13 2015-08-19 安徽省含山瓷业股份有限公司 High strength carbon fiber reinforced silicon carbide ceramic matrix composite material and preparation method thereof
CN105345679A (en) * 2015-09-24 2016-02-24 安徽威铭耐磨材料有限公司 Basalt fiber enhanced nano-vitrified bond diamond grinding wheel and preparation method thereof
CN106007758A (en) * 2016-04-22 2016-10-12 葫芦岛市华能工业陶瓷有限公司 Toughened silicon nitride combined silicon carbide ceramic composite material and preparation method thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
刘宝林等: "SiCf /SiC复合材料高温抗氧化研究进展", 《硅酸盐通报》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110950674A (en) * 2019-12-26 2020-04-03 九牧厨卫股份有限公司 Preparation method of fiber-reinforced sanitary ceramic body

Similar Documents

Publication Publication Date Title
CN108165793B (en) Preparation method of endogenous nano-sized particle reinforced aluminum alloy material
CN103665851B (en) A kind of manufacture method of gear
CN108192547A (en) Height filling high tenacity epoxy stone adhesive and preparation method thereof
CN104387005A (en) Carbon nanotube/cement composite material and preparation method thereof
CN105198279A (en) Preparation method of carbon-fiber-reinforced composite material
CN103788910A (en) Packaging adhesive containing modified sepiolite powder
CN106747546A (en) A kind of high-strength and high ductility ceramic composite and its application
CN102390999A (en) Liquid-phase-sintered SiC-TiC composite ceramic and preparation method thereof
CN105384450A (en) Production method of aluminum silicon sol reinforced silicon carbide kiln furniture
CN103467987A (en) Toughening modification method for bismaleimide resin
CN108165855A (en) A kind of bonding agent, polycrystalline cubic boron nitride compound sheets and preparation method thereof
CN104231603A (en) Railway freight transport open wagon vertical column and preparation method thereof
CN114014667A (en) Preparation method of composite silicon carbide ceramic powder and ceramic separation valve
CN104370548A (en) Ceramic material for high-speed steel cutters and preparation method thereof
CN106278254B (en) A kind of high-strength and high ductility ceramic composite and its application in manufacture cutter
KR102008761B1 (en) Epoxy composites containing pitch coated glass fiber
CN104262694A (en) Anti-wear heat-resistant rubber
Starokadomsky On strengthening of epoxy-composites by filling with microdispersions of sic, tin, and cement
CN107930781B (en) A kind of wear-resistant liner for grinding operation production aluminium oxide
CN105060895A (en) High-strength silicon carbide ceramic material and preparation method therefor
Wu et al. Silicone rubber composites modified by chopped basalt fibers treated with coupling agent
CN106396684B (en) A kind of high-strength, high-ductility ceramic composite and preparation method thereof
KR20190074655A (en) Epoxy nanocomposite reinforced with graphene oxide decorated with nanodiamond nanocluster and method for manufacturing thereof
CN105601284B (en) A kind of Sialon-Ti (CN) ceramic material and preparation method thereof
CN114790121A (en) Heat-resistant high-strength carbon/ceramic fastener and preparation method thereof

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20170531

WD01 Invention patent application deemed withdrawn after publication