CN110317047A - A kind of temperature gradient selfreparing multi-layered ceramic cutter - Google Patents
A kind of temperature gradient selfreparing multi-layered ceramic cutter Download PDFInfo
- Publication number
- CN110317047A CN110317047A CN201910620318.2A CN201910620318A CN110317047A CN 110317047 A CN110317047 A CN 110317047A CN 201910620318 A CN201910620318 A CN 201910620318A CN 110317047 A CN110317047 A CN 110317047A
- Authority
- CN
- China
- Prior art keywords
- mos
- sic
- tin
- layered ceramic
- cutter
- 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
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/10—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on aluminium oxide
-
- 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
- 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
- C04B2235/3224—Rare earth oxide or oxide forming salts thereof, e.g. scandium oxide
- C04B2235/3225—Yttrium oxide 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
- C04B2235/38—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
- C04B2235/3852—Nitrides, e.g. oxynitrides, carbonitrides, oxycarbonitrides, lithium nitride, magnesium nitride
- C04B2235/3886—Refractory metal nitrides, e.g. vanadium nitride, tungsten nitride
-
- 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
- C04B2235/44—Metal salt constituents or additives chosen for the nature of the anions, e.g. hydrides or acetylacetonate
- C04B2235/446—Sulfides, tellurides or selenides
-
- 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
- C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
- C04B2235/656—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
-
- 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
- C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
- C04B2235/656—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
- C04B2235/6567—Treatment time
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Ceramic Products (AREA)
- Compositions Of Oxide Ceramics (AREA)
Abstract
The present invention provides a kind of temperature gradient selfreparing multi-layered ceramic cutter, it is characterized in that being inhibited using cutting temperature gradient, pulling and pressed effect is contained and repairs the crackle in multi-layered ceramic cutter;When cutting temperature is lower, Al is derived from2O3Additive (TiN, MoS when lamination cutter is sintered institute2, SiC) and Al2O3Matrix, Al2O3‑TiN‑MoS2‑Y2O3Layer and Al2O3‑SiC‑MoS2‑Y2O3Low-temp. extrusion effect caused by the residual stress formed between layer inhibits the generation of crackle;Al is increased in cutting temperature2O3Multi-layered ceramic tool-chip-oxygen-enriched environment, machined surface occur chemical reaction and (mainly rely on TiN, MoS2, SiC oxidation reaction generate TiO2、MoO3、SiO2), generate bridging particle (mainly TiO2、MoO3、SiO2);And product is because of high temperature extrusion effect caused by the coefficient of thermal expansion mismatch with matrix;TiO2、MoO3、SiO2Bridging particle generates and grows up in inside crack, forms the comprehensive effect for drawing effect to combine with pressure effect.
Description
Technical field
The invention belongs to technical field of mechanical cutting tool manufacture, in particular to a kind of temperature gradient selfreparing multi-layered ceramic
Cutter preparation method.
Background technique
As High-speed Machining Technology gradually promotes and applies, sintex becomes a kind of quite promising cutter.To the greatest extent
Existing numerous studies are managed to be dedicated to improving brittleness of ceramics, however compared with other materials, brittleness is still far below hard alloy
Brittleness.Laminated construction is a kind of cross structure, can effectively improve ceramic composite to the ability to bear of defect, avoids it prominent
So fracture, improves the reliability and system stability of ceramic component.Stack technology is applied in sintex, ceramics can be taken into account
The hardness and toughness reguirements of cutter, thus multi-layered ceramic cutter comes into being.
When multi-layered ceramic cutter is applied to high-speed dry cutting, at its rake face-chip and flank-machined surface two
The secondary temperature of key friction is higher, acts on it by coupling stress (mechanical stress and thermal stress), and thermal stress is followed with heat
Ring number increases and increases.It is cracked when coupling stress is more than laminated material strength degree;It is microcosmic with the increase of stress
It is extended in laminated material with macroscopic cracking;Eventually lead to the failure of multi-layered ceramic cutter.
For the extension for resisting microfissure, the ability that multi-layered ceramic cutter supports coupling stress, a kind of feasible solution are improved
Approach is as follows: when cutting temperature is lower, being formed by the effect of low-temp. extrusion caused by remaining compressive pre-stress from cutter sintering
It should inhibit the generation of crackle;Chemistry occurs for multi-layered ceramic tool-chip-environment, machined surface instead after cutting temperature raising
It answers, generates the particle (bridging particle) of filling crackle;And product is because of high temperature caused by the coefficient of thermal expansion mismatch with matrix
Extrusion effect (pressure effect).Bridging particle generates and grows up in inside crack, holds crackle two sides (drawing effect), and pressure effect
It answers, forms a kind of utilization cutting temperature gradient selfreparing multi-layered ceramic cutter.The cutter has the ability of selfreparing, not only makes it
It endures defect ability to further increase, improves its reliability, extended period service life.
Summary of the invention
It is an object of the invention to overcome the problems, such as that above-mentioned existing sintex is insufficient to coupling stress resilience, provide
A kind of temperature gradient selfreparing multi-layered ceramic cutter preparation method.
The present invention is accomplished by the following way:
A kind of temperature gradient selfreparing multi-layered ceramic cutter, it is characterized in that being inhibited using cutting temperature gradient, pulling and pressed effect is contained
With the crackle in reparation multi-layered ceramic cutter;When cutting temperature is lower, Al is derived from2O3Additive when lamination cutter is sintered institute
(TiN、MoS2, SiC) and Al2O3Matrix, Al2O3-TiN-MoS2-Y2O3Layer and Al2O3-SiC-MoS2-Y2O3It is formed between layer
The generation of the inhibition crackle of low-temp. extrusion effect caused by residual stress;Al is increased in cutting temperature2O3Multi-layered ceramic tool-chip-
Oxygen-enriched environment, machined surface occur chemical reaction and (mainly rely on TiN, MoS2, SiC oxidation reaction generate TiO2、MoO3、
SiO2), generate bridging particle (mainly TiO2、MoO3、SiO2);And high temperature extrusion effect;TiO2、MoO3、SiO2Bridging
Grain generates and grows up in inside crack, forms the comprehensive effect for drawing effect to combine with pressure effect.
A kind of temperature gradient selfreparing multi-layered ceramic cutter, the cutter is with Al2O3-TiN-MoS2-Y2O3With Al2O3-SiC-
MoS2-Y2O3It is staggered to form multilayered structure;Al2O3-TiN-MoS2-Y2O3Layer and Al2O3-SiC-MoS2-Y2O3The Thickness ratio of layer is 2
To 5, the number of plies is respectively 3 to 5 layers, Al2O3-SiC-MoS2-Y2O3Thickness is 0.2-1mm, and step of preparation process is as follows:
(1) according to Al2O3Content is 69-89wt.%, and TiN content is 5-15wt.%, MoS2Content is 5-15wt.%, Y2O3Content
For the ratio of 1-3wt.%, composite powder is configured, using ethyl alcohol as medium, Ball-milling Time is 120 hours, and ball milling speed is
50rpm;
(2) according to Al2O3Content is 69-89wt.%, SiC content 5-15wt.%, MoS2Content is 5-15wt.%, Y2O3Content
For the ratio of 1-3wt.%, composite powder is configured, using ethyl alcohol as medium, Ball-milling Time is 120 hours, and ball milling speed is
50rpm;
(3) Al that ball milling is good2O3-TiN-MoS2-Y2O3With Al2O3-SiC-MoS2-Y2O3Two kinds of ceramic composite powders are put into very
It is dry in empty drying box, after waiting it to cool completely, utilize the sieve of 120 mesh;
(4) by Al2O3-TiN-MoS2-Y2O3With Al2O3-SiC-MoS2-Y2O3Two kinds of ceramic composite powders are staggeredly put into three Gao Shi
In black mold, tablet press machine precompressed ceramic idiosome, preload pressure 3MPa are then utilized;
(5) heat pressing process preparation temperature gradient selfreparing multi-layered ceramic cutter, technological parameter are utilized are as follows: sintering temperature is
1600 DEG C, pressure 30MPa, soaking time 45-90min;
(6) it when using this tool sharpening, is passed through oxygen and forms oxygen-enriched environment, promote the selfreparing of cutter.
The temperature gradient selfreparing multi-layered ceramic cutter that the present invention is prepared by above-mentioned technique, can be used for cutting austenitic not
The difficult-to-machine materials such as rust steel (lCrl8Ni9Ti), nickel-base alloy Inconel-718, Ti6A14V alloy.
Detailed description of the invention
Fig. 1 is that the temperature gradient selfreparing multi-layered ceramic cutter of the invention depression effect in low temperature forms schematic diagram, Fig. 2
Inhibit to form schematic diagram with self-repair effect at high temperature for temperature gradient selfreparing multi-layered ceramic cutter, Fig. 3 is temperature gradient
Selfreparing multi-layered ceramic cutter SEM picture;Wherein: 1 has an effect original extruding particle for low temperature, 2 compression when being low temperature,
The 3 original extruding particles having an effect for high temperature, the 4 low-temp. extrusion particles later for volume expansion, 5 be cutter-oxygen and knife
Tool-chip reactant, 6 be the crackle formed, and 7 be bridging particle, and 8 compression formed when higher for cutting temperature, 9 be to narrow
Crackle, 10 be the later high temperature extrusion particles of volume expansion, and 11 be ateliosis bridging particle, and 12 be full grown bridge
Join particle, 13 be the crackle being filled.
Specific embodiment
According to Al2O3: TiN:MoS2: Y2O3The mass ratio of=79:12.5:7.5:1, configure composite powder, using ethyl alcohol as
Medium, Ball-milling Time are 120 hours, ball milling speed 50rpm;According to Al2O3: SiC:MoS2: Y2O3=79:12.5:7.5:1's
Mass ratio configures composite powder, and using ethyl alcohol as medium, Ball-milling Time is 120 hours, ball milling speed 50rpm;Ball milling is good
Al2O3-TiN-MoS2-Y2O3With Al2O3-SiC-MoS2-Y2O3Two kinds of ceramic composite powders are put into drying in vacuum oven,
After cooling completely Deng it, the sieve of 120 mesh is utilized;Al2O3-TiN-MoS2-Y2O3Layer and Al2O3-SiC-MoS2-Y2O3The layer of layer
Thickness rate is 2, Al2O3-TiN-MoS2-Y2O3The number of plies of layer is 4 layers, and its outer layer, Al2O3-SiC-MoS2-Y2O3Layer is 3 layers,
Al2O3-SiC-MoS2-Y2O3Thickness is 0.2mm, by Al2O3-TiN-MoS2-Y2O3With Al2O3-SiC-MoS2-Y2O3Two kinds of ceramics
Composite powder is staggeredly put into three high graphite jigs, then utilizes tablet press machine precompressed ceramic idiosome, preload pressure 3MPa;It utilizes
Heat pressing process preparation temperature gradient selfreparing multi-layered ceramic cutter, technological parameter are as follows: sintering temperature is 1600 DEG C, pressure
30MPa, soaking time 60min;When using this tool sharpening, it is passed through oxygen and forms oxygen-enriched environment, promote the selfreparing of cutter.
Claims (3)
1. a kind of temperature gradient selfreparing multi-layered ceramic cutter, it is characterized in that being inhibited using cutting temperature gradient, pulling and pressed effect is held back
Crackle in system and reparation multi-layered ceramic cutter;When cutting temperature is lower, Al is derived from2O3Lamination cutter is sintered institute Shi Tianjia
Object (TiN, MoS2, SiC) and Al2O3Matrix, Al2O3-TiN-MoS2-Y2O3Layer and Al2O3-SiC-MoS2-Y2O3It is formed between layer
Residual stress caused by low-temp. extrusion effect inhibit crackle generation;Al is increased in cutting temperature2O3Multi-layered ceramic cutter-cut
Bits-oxygen-enriched environment, machined surface occur chemical reaction and (mainly rely on TiN, MoS2, SiC oxidation reaction generate TiO2、
MoO3、SiO2), generate bridging particle (mainly TiO2、MoO3、SiO2);And product with the thermal expansion coefficient of matrix because losing
With caused high temperature extrusion effect;TiO2、MoO3、SiO2Bridging particle generates and grows up in inside crack, is formed and draws effect and pressure
The comprehensive effect that effect combines.
2. requiring a kind of temperature gradient selfreparing multi-layered ceramic cutter according to claim 1, it is characterised in that with Al2O3-TiN-
MoS2-Y2O3With Al2O3-SiC-MoS2-Y2O3It is staggered to form multilayered structure;Al2O3-TiN-MoS2-Y2O3Layer and Al2O3-SiC-
MoS2-Y2O3The Thickness ratio of layer is 2 to 5, and the number of plies is respectively 3 to 5 layers, Al2O3-SiC-MoS2-Y2O3Thickness is 0.2-1mm, base
Steps are as follows for preparation process:
(1) according to Al2O3Content is 69-89wt.%, and TiN content is 5-15wt.%, MoS2Content is 5-15wt.%, Y2O3Content
For the ratio of 1-3wt.%, composite powder is configured, using ethyl alcohol as medium, Ball-milling Time is 120 hours, and ball milling speed is
50rpm;
(2) according to Al2O3Content is 69-89wt.%, SiC content 5-15wt.%, MoS2Content is 5-15wt.%, Y2O3Content
For the ratio of 1-3wt.%, composite powder is configured, using ethyl alcohol as medium, Ball-milling Time is 120 hours, and ball milling speed is
50rpm;
(3) Al that ball milling is good2O3-TiN-MoS2-Y2O3With Al2O3-SiC-MoS2-Y2O3Two kinds of ceramic composite powders are put into very
It is dry in empty drying box, after waiting it to cool completely, utilize the sieve of 120 mesh.
3. requiring a kind of temperature gradient selfreparing multi-layered ceramic cutter according to claim 1, which is characterized in that its sintering step is such as
Under:
(1) by Al2O3-TiN-MoS2-Y2O3With Al2O3-SiC-MoS2-Y2O3Two kinds of ceramic composite powders are staggeredly put into three Gao Shi
In black mold, tablet press machine precompressed ceramic idiosome, preload pressure 3MPa are then utilized;
(2) heat pressing process preparation temperature gradient selfreparing multi-layered ceramic cutter, technological parameter are utilized are as follows: sintering temperature is
1600 DEG C, pressure 30MPa, soaking time 45-90min;
(3) it when using this tool sharpening, is passed through oxygen and forms oxygen-enriched environment, promote the selfreparing of cutter.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910620318.2A CN110317047A (en) | 2019-07-10 | 2019-07-10 | A kind of temperature gradient selfreparing multi-layered ceramic cutter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910620318.2A CN110317047A (en) | 2019-07-10 | 2019-07-10 | A kind of temperature gradient selfreparing multi-layered ceramic cutter |
Publications (1)
Publication Number | Publication Date |
---|---|
CN110317047A true CN110317047A (en) | 2019-10-11 |
Family
ID=68121743
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201910620318.2A Pending CN110317047A (en) | 2019-07-10 | 2019-07-10 | A kind of temperature gradient selfreparing multi-layered ceramic cutter |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN110317047A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116789440A (en) * | 2023-06-29 | 2023-09-22 | 齐鲁工业大学(山东省科学院) | Self-repairing ceramic material capable of reducing porosity and preparation method thereof |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02248360A (en) * | 1989-03-17 | 1990-10-04 | Kao Corp | Metal oxide ceramic-molybdenum disulfide type combined material and sliding parts using the same |
CN1073503A (en) * | 1992-12-29 | 1993-06-23 | 王魁久 | Rare-earth ceramic bearing part and manufacture method thereof |
JP2002001668A (en) * | 2000-06-19 | 2002-01-08 | Mitsubishi Materials Corp | Metal bonded grinding wheel |
CN1986483A (en) * | 2006-12-25 | 2007-06-27 | 西南科技大学 | Nano-nano type Al2O3-base heterogeneous ceramic and its preparing method |
CN105879922A (en) * | 2016-05-19 | 2016-08-24 | 四川福思达生物技术开发有限责任公司 | Molybdenum disulfide modified catalytic wet oxidation catalyst and preparation method thereof |
CN106904947A (en) * | 2017-02-27 | 2017-06-30 | 齐鲁工业大学 | Add self-lubrication ceramic cutter material of h BN@Ni core shell structure composite granules and preparation method thereof |
CN107586134A (en) * | 2017-03-07 | 2018-01-16 | 鲁东大学 | One kind is based on theory of stress wave multi-layered ceramic nozzle preparation method |
-
2019
- 2019-07-10 CN CN201910620318.2A patent/CN110317047A/en active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02248360A (en) * | 1989-03-17 | 1990-10-04 | Kao Corp | Metal oxide ceramic-molybdenum disulfide type combined material and sliding parts using the same |
CN1073503A (en) * | 1992-12-29 | 1993-06-23 | 王魁久 | Rare-earth ceramic bearing part and manufacture method thereof |
JP2002001668A (en) * | 2000-06-19 | 2002-01-08 | Mitsubishi Materials Corp | Metal bonded grinding wheel |
CN1986483A (en) * | 2006-12-25 | 2007-06-27 | 西南科技大学 | Nano-nano type Al2O3-base heterogeneous ceramic and its preparing method |
CN105879922A (en) * | 2016-05-19 | 2016-08-24 | 四川福思达生物技术开发有限责任公司 | Molybdenum disulfide modified catalytic wet oxidation catalyst and preparation method thereof |
CN106904947A (en) * | 2017-02-27 | 2017-06-30 | 齐鲁工业大学 | Add self-lubrication ceramic cutter material of h BN@Ni core shell structure composite granules and preparation method thereof |
CN107586134A (en) * | 2017-03-07 | 2018-01-16 | 鲁东大学 | One kind is based on theory of stress wave multi-layered ceramic nozzle preparation method |
Non-Patent Citations (2)
Title |
---|
JUNJIE SONG等: "Fabrication and tribological behavior of Al2O3/MoS2–BaSO4 laminated composites doped with in situ formed BaMoO4", 《TRIBOLOGY INTERNATIONAL》 * |
JUNLONG SUN等: "Comprehensive effect of the mechanical properties, laminated structure and healing conditions on the self-healing behaviors of laminated Al2O3-MgO ceramic composites", 《CERAMICS INTERNATIONAL》 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116789440A (en) * | 2023-06-29 | 2023-09-22 | 齐鲁工业大学(山东省科学院) | Self-repairing ceramic material capable of reducing porosity and preparation method thereof |
CN116789440B (en) * | 2023-06-29 | 2024-04-05 | 齐鲁工业大学(山东省科学院) | Self-repairing ceramic material capable of reducing porosity and preparation method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106048360B (en) | A kind of surface has hard alloy of double-deck gradient-structure and preparation method thereof | |
CN102703742B (en) | Metal-based composite material with substrate of nano laminated structure and preparation method thereof | |
CN111235453B (en) | Hard alloy with high-entropy alloy layer on surface and preparation method thereof | |
CN104690274B (en) | A kind of polycrystal diamond hard alloy complex sheet and preparation method thereof | |
CN107900352A (en) | A kind of stratiform high niobium containing titanium aluminium alloy composite panel and preparation method thereof | |
CN112743080B (en) | Method for preparing Ti (C, N) -based metal ceramic cutter material with high heat resistance through in-situ integration | |
CN111646801B (en) | Boron carbide-tungsten carbide composite ceramic gradient material for cutter and preparation method and application thereof | |
WO2013185511A1 (en) | Method for manufacturing polycrystalline diamond compact enhanced by cvd diamond | |
CN111304479A (en) | Preparation method of VCrNbMoW refractory high-entropy alloy | |
US20230303453A1 (en) | Crack self-healing functionally gradient material for ceramic cutting tools and preparation method thereof | |
CN112939581A (en) | Zirconia toughened alumina cutter and preparation method thereof | |
CN112745127A (en) | Silicon nitride ceramic cutter and preparation method and application thereof | |
CN111663062B (en) | Method for preparing Cu-Cr-Mg-Zr-Ce high-performance end ring by using hot isostatic pressing near-net shape | |
CN110317047A (en) | A kind of temperature gradient selfreparing multi-layered ceramic cutter | |
CN111825454A (en) | Preparation method of layered structure ceramic ring for mechanical seal | |
CN113976892A (en) | Manufacturing method of low-residual-stress polycrystalline diamond compact | |
JP2016068156A (en) | Composite sintered body cutting tool | |
CN112725676A (en) | Preparation method of high-strength hard alloy with good red hardness | |
CN108585907B (en) | Cr (chromium)2Preparation method of AlC modified self-healing silicon carbide ceramic matrix composite | |
CN110565049B (en) | Polycrystalline cubic boron nitride composite sheet with sandwich layer structure and preparation method thereof | |
CN112813393B (en) | Molybdenum-nickel alloy target and preparation method thereof | |
CN207547632U (en) | Composite polycrystal-diamond | |
CN115703683B (en) | High-strength high-heat-conductivity large-size silicon nitride ceramic and preparation method thereof | |
CN109396448B (en) | Polycrystalline diamond compact and preparation method thereof | |
CN112059191B (en) | Cutting tool and method for manufacturing the same |
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 | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20191011 |