CN101913880B - Method for manufacturing silicon carbide ceramics based on silane-titanate two-component coupling agent - Google Patents
Method for manufacturing silicon carbide ceramics based on silane-titanate two-component coupling agent Download PDFInfo
- Publication number
- CN101913880B CN101913880B CN 200910161250 CN200910161250A CN101913880B CN 101913880 B CN101913880 B CN 101913880B CN 200910161250 CN200910161250 CN 200910161250 CN 200910161250 A CN200910161250 A CN 200910161250A CN 101913880 B CN101913880 B CN 101913880B
- Authority
- CN
- China
- Prior art keywords
- sintering
- silicon carbide
- coupling agent
- temperature
- silane
- 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.)
- Expired - Fee Related
Links
Images
Landscapes
- Ceramic Products (AREA)
Abstract
The invention relates to a method for manufacturing silicon carbide ceramics based on a silane-titanate two-component coupling agent, which is characterized by adopting a silane-titanate two-component coupling agent bonded SiC-Al2O3-Y2O3 system, wherein Al2O3 and Y2O3 are sintering auxiliary agents of the system; the two-component coupling agent forms firm chemical bonding on the surface of main SiC and the surfaces of the auxiliary agents which are Al2O3 and Y2O3 by the hydrolysis of alkoxy; meanwhile, a firm and dense sintering auxiliary agent coating is formed on the surface layer of the main SiC by group reaction between the two coupling agents; and main raw materials of SiC powder (0.5-5microns), a silane coupling agent A, a titanate coupling agent B and sintering auxiliary agents of Al2O3 and Y2O3 (smaller than 200nano) are subjected to the main process steps of screening, moulding, solidification, high-temperature sintering, and the like after high-energy ball-milling by steps to form a silicon carbide ceramics product. In the method, dense silicon carbide ceramics with the relative density beyond 98 percent can be prepared by sintering at the low temperature of 1,800 DEG C through simple process, thereby greatly reducing the energy consumption in the production process of silicon carbide.
Description
Technical field
The present invention relates to high-compactness method for manufacturing silicon carbide ceramics technical field under a kind of low temperature.
Background technology
Good characteristics such as thyrite has that hot strength is big, high-temperature oxidation resistance is strong, abrasion resistance properties is good, thermostability is good, thermal expansivity is little, thermal conductivity is big, hardness is high, anti-thermal shock and resistance to chemical attack; in fields such as automobile, mechanical chemical industry, environment protection, space technology, information electronics, the energy increasingly extensive application is arranged, become a kind of irreplaceable structural ceramics of other materials at a lot of industrial circle excellent performances.
Dynamic seal in the mechanical means is to be undertaken by the rotational slide of two seal face materials, as the seal face material, requires the hardness height, has wearability.Suitable height of the hardness of silicon carbide ceramics and frictional coefficient are little, so silicon carbide ceramics can obtain sliding properties that other material is beyond one's reach as the mechanical seal end surface material.On the other hand, two mechanical seal materials can produce certain heat owing to rub in rotary movement, thereby the local temperature of seal face is raise, so the end face material also must can tolerate certain temperature.In the rotational slide process, produce thermal strain and hot tearing for fear of the mechanical seal material, require thermal conductivity height, the good thermal shock of end face material.At present, silicon carbide ceramics has obtained a large amount of application in all kinds of mechanical seals, and for the laborsaving of mechanical means with energy-conservationly made very big contribution, demonstrate other materials incomparable superiority.Silicon carbide ceramics also successfully is used as various bearings, cutting tool in mechanical industry.
In automotive industry,, make full use of the energy in order to improve the thermo-efficiency of engine, reduce fuel consumption, reduce topsoil, the working temperature of wishing engine is higher than 1200 ℃ and (it is calculated that, when the working temperature of engine was brought up to 1370 ℃ by 1100 ℃, thermo-efficiency can increase by 30%).The hot strength of silicon carbide ceramics because of being had, lower thermal expansivity, higher thermal conductivity and thermal-shock resistance and be considered to use temperature and surpass 1200 ℃ of candidate materials the most promising preferably.The country such as the U.S., Germany and the Japan that have the advanced ceramics technology have developed engine component such as motor stator, rotor, burner and the volute pipe that adopts silicon carbide ceramics and have obtained good result of use, just are being devoted to the development research of full ceramic engine at present.
What need in the occasion of needs such as aerospace, nuclear industry tolerances ultra high temp such as nuclear fission and the fusion reactor bears 2000 degree left and right sides pyritous heat-stable materials; Rocket and aerospacecraft surface are used for tolerating the thermal insulation tile up to thousands of K temperature that produces with the violent friction of atmosphere; Rocket combustion chamber's larynx lining and inner lining material, gas-turbine blade; The top board of High Temperature Furnaces Heating Apparatus, support, and the high temperature members such as jig of high temperature experiment usefulness also generally adopt the silicon carbide ceramics member.Silicon carbide ceramics also is widely used as various corrosion-resistant with container and pipeline in petrochemical industry.
Because the high-performance of silicon carbide ceramics and the widespread use in industrial circle, the sintering of SiC are the focuses of material circle research always.But because silicon carbide is the extremely strong covalent linkage compound of a kind of covalency, even under 2100 ℃ high temperature, the self-diffusion coefficient of C and Si also only is 1.5 * 10
-10With 2.5 * 10
-13Cm
2/ s.So SiC is difficult to sintering, must just densification (Krishi Negita may realized below 2000 ℃ by sintering aid or external pressure, Effective sintering aids for silicon carbideceramics:reactivities of silicon carbide with various additives, J.Am.Ceram.Soc., 1986,69 (12): C308-310.).We know under such high temperature, if can reduce certain working temperature, energy consumption will reduce sharp, so how obtain the silicon carbide ceramics product of high relative density (＞98%) at alap sintering temperature, satisfy the demand of different industrial circles, become the general character key issue that the silicon carbide ceramics industry needs to be resolved hurrily high-end silicon carbide ceramics goods.
Hot pressed sintering is by means of external pressure, add or do not add sintering aid in the sintering precursor powder, hot pressed sintering reaches 98% density needs about 2000 ℃ temperature usually, as the bright grade in the east of a river at silicate journal 1981, No.9,133-146 have reported SiC+1%B under 2050 ℃ of conditions
4Under 45 minutes processing condition of C+3%C architecture heat preservation, density reaches 98.75% of theoretical density.It is that the system sintering temperature of sintering aid can be lower than 2000 ℃ with Al, B, C that part is also arranged, as Huang Hanquan etc. 1991,9 (2): be reported in 1650 ℃-1950 ℃ on the 70-77, under the hot pressing condition of 50MPa, can obtain relative density and be higher than 98% sintered compact.Yet hot pressed sintering can only prepare the silicon carbide components of simple shape, and seldom can't realize commercially producing through the quantity of the prepared product of once sintered process.Comparatively speaking, pressureless sintering is the most promising sintering method of high-performance silicon carbide ceramic industryization.Can be divided into solid state sintering and liquid phase sintering according to the state pressureless sintering of selecting for use auxiliary agent in sintering process.Adopt B, C and Al or its compound fused second method mutually in sintering process, not occur and be known as solid state sintering.The solid state sintering temperature is higher, usually more than 2000 ℃, and require also very high to purity of raw materials, S.Prochazka (S.Prochazka as U.S. GE company, Ceramics for High-Performance Applications, 1974,239-252.) by in highly purified B-SiC fine powder, adding a spot of B and C simultaneously, adopt non-pressure sintering technology, obtained density in 2020 ℃ and be higher than 98% SiC sintered compact.And in the sintering system, add Al
2O
3-Y
2O
3, AIN-R
2O
3In sintering process, be called as liquid phase sintering Deng sintering aid by the method that forms binary liquid phase eutectic mixture.Liquid phase sintering can obtain having preferably fracture toughness property and flexural strength and have complicated shape and large-sized silicon carbide components at lower sintering temperature.Liquid phase sintering system, particularly SiC-Al
2O
3-Y
2O
3, become the focus of the research of silicon carbide sintering in recent years.Yet present document and patent show, the high-quality silicon carbide pottery that will prepare relative density 98% usually, sintering temperature generally all need be more than 1900 ℃, adopt the silicon carbide/YAG composite granule sintering temperature of collosol and gel preparation to be issued to the 96%-97% density at 1850 ℃, as Wang Jianwu etc. at refractory materials 2005,39 (3): the last report of P192-195 is a main raw material with silicon carbide, six water Yttrium trinitrates, nine water aluminum nitrates and hexamethylenetetramine, introduces Al by sol-gel method
2O
3And Y
2O
3Complex sintering aids, liquid phase sintering prepares SiC-Y
3Al
5O
12Complex phase ceramic; The raw material composite granule is behind dry-pressing, hydrostatic pressing, and at 1860 ℃ of following sintering 45min, the relative density of obtained complex phase ceramic is 96.5%.But collosol and gel cost height, time-consuming, produce a large amount of trade effluents, be difficult to adapt to industrialized production requirement.
In fact YAG promptly begins to produce liquid phase at 1760 ℃, yet we be difficult in the silicon carbide ceramics key that makes high-compactness (＞98%) under the temperature about 1800 ℃ be the YAG sintering aid whether can intactly be wrapped in carborundum particle around, thereby those parts that do not coated by YAG produce the reduction that the space causes density being difficult under the temperature lower about 1800 ℃ fuse by self thermodiffusion in matrix under the situation of liquid phase disappearance.
Summary of the invention
The present invention is directed to existing background technology and proposed a kind of SiC-Al that adopts the double-component coupling agent bonding
2O
3-Y
2O
3System.This system can prepare relative density by simple technological process sintering and surpass 98% compact silicon carbide ceramic under 1800 ℃ low temperature.Al
2O
3And Y
2O
3As the sintering aid of system, under sintering temperature (1750 ℃-1800 ℃), Al
2O
3-Y
2O
3Form liquid phase YAG, make carbon and Siliciumatom can under this lesser temps, quicken diffusion and sintering.And the hydrolysis of the coupling agent in the system by alkoxyl group is on main body SiC surface and auxiliary agent A l
2O
3, Y
2O
3The surface forms firm chemical bonding, forms strong and dense sintering aid coating layer by the radical reaction between two kinds of coupling agents on main body silicon carbide top layer simultaneously.This method can obtain relative density at 1800 ℃ of lower sintering temperatures and surpass 98% compact silicon carbide ceramic, has greatly reduced the energy consumption of silicon carbide production process.As Fig. 1 is the high-compactness silicon carbide ceramics Electronic Speculum picture for preparing, and from figure, grain contours is clear, fine and close, do not have tangible hole, and the thin layer coating that surrounds crystal grain is arranged around the crystal boundary.
This based on double-component coupling agent low-temperature sintering high-density silicon carbide ceramics preparation method, it is characterized in that and will in high energy ball mill, obtain material I under main raw material 95-98wt% carborundum powder, the 2-5wt% silane coupling A normal temperature in mixing and ball milling 3-5 hour; With sintering aid 30-70wt%Al
2O
3, 28-65wt%Y
2O
3, 2-5wt% titanate coupling agent B obtained material II in mixing and ball milling 4-8 hour in high energy ball mill; With 85-95wt% material I, 2-10wt% material II, 3-5wt% wedding agent in high energy ball mill after mixing and ball milling 5-10 hour through sieving, main technique steps such as moulding, curing, high temperature sintering, form the silicon carbide ceramics product.
Above-mentioned silane coupling A should contain more alkoxy grp and contain 1-2 reactive group, alkoxy grp becomes silicon hydroxyl and silicon carbide by hydrolysis silicon hydroxyl is bonded to by polycondensation around the dominant carbon silicon carbide particle, and this reactive group then can carry out bonding with titanate coupling agent B by reaction.Silane coupling A is a kind of in γ-An Bingjisanyiyangjiguiwan, cyclohexylamino propyl group methyl dimethoxysilane, the hexanediamine ylmethyl triethoxyl silane.Coupling agent B has selected the more stable titanate coupling agent of structure, should contain more alkoxy grp equally and contain 1-2 reactive group, and alkoxy grp becomes titanium hydroxyl and Al by hydrolysis
2O
3, Y
2O
3The hydroxyl on surface is bonded to around the sintering aid by polycondensation, this reactive group then can carry out bonding by reaction and silane coupling A, thereby around silicon-carbide particle, form complete firm sintering aid coating layer, thereby ℃ following sintering in lower temperature＜1800, reduce the voidage of burning till product, obtain the silicon carbide ceramics of high-compactness＞98%.Titanate coupling agent B is a kind of in sec.-propyl dodecyl benzene sulfonyl titanic acid ester, sec.-propyl three decoyl titanic acid ester, sec.-propyl three (lauryl-myristyl) titanic acid ester.Silane coupling A and titanate coupling agent B all can buy in market.
The above-mentioned main body silicon carbide powder and the granularity of sintering aid differ bigger; The grain diameter of main body silicon carbide should be between the 0.5-5 micron, Al
2O
3, Y
2O
3The particle scale of sintering aid below 200 nanometers, thereby help forming in main body carborundum powder surface densification, evenly, thin sintering aid coating layer, also help finishing sintering process under the lesser temps with less amount of auxiliary.The starting material of this granularity all can have been bought on market, can buy to the triumphant magnificent silicon carbide micro-powder in Weifang, Shandong company limited as silicon carbide powder.
Above-mentioned wedding agent is a kind of among resol, the PVA (polyvinyl alcohol).
Above-mentioned moulding is that precursor powder is placed in the cylindrical die, under the pressure at 200-250MPa in high tonnage hydropress static 5 minutes again the demoulding obtain.
Above-mentioned high temperature sintering is under the condition of vacuum, temperature programming under minute-pressure Ar gas (0.10-0.13MPa) atmosphere protection, and below 1300 ℃ 5-8 ℃/minute, the temperature rise rate of temperature range is 10-15 ℃/minute more than 1300 ℃.Holding temperature is 1750 ℃-1800 ℃, and soaking time is 0.5-3 hour.Very useful is that silane coupling A is cracked into high reactivity Si-C bond structure under this temperature and atmosphere, and this structure helps the atomic diffusion of silicon carbide.
Compared with prior art, the invention has the advantages that: adopt double-component coupling agent, silane coupling A and titanate coupling agent B the silicon hydroxyl or the titanium hydroxyl bond that form of the hydrolysis by alkoxyl group respectively are combined in main body silicon carbide and sintering aid surface, the functional response group of these two kinds of coupling agents then mutually bonding the sintering aid bonding is coated on the dominant carbon silicon carbide particle forms fine and close evenly sintering aid and coat thin layer, this thin layer helps to obtain at 1800 ℃ of following sintering of lower temperature the silicon carbide ceramics of high-compactness＞98%.
Description of drawings
Fig. 1 is high-compactness silicon carbide ceramics (＞98%) the section electromicroscopic photograph for preparing
Embodiment
Below in conjunction with embodiment the present invention is described in further detail.
Embodiment 1: get 97wt% carborundum powder (mean particle size is the 0.5-5 micron), 3wt% silane coupling agent γ-An Bingjisanyiyangjiguiwan mixture, (rotating speed is 300r/ minute, and ratio of grinding media to material is 5) ground and obtained material I in 3 hours in high energy ball mill; With 68wt%Al
2O
3, 27wt%Y
2O
3, 5wt% titanate coupling agent sec.-propyl dodecyl benzene sulfonyl titanic acid ester (rotating speed is 300r/ minute, and ratio of grinding media to material is 5) in high energy ball mill grinds and to obtain material II in 4 hours; 90wt% material I, 6wt% material II, 4wt%PVA mixing and ball milling in high energy ball mill was obtained the sintering precursor powder in 6 hours.With precursor powder under 80 degree dry 2 hours, after pulverizing, sieving, under 230Mpa, leave standstill in the cylindrical die of packing into and obtained biscuit in 5 minutes.Biscuit 250 ℃ of thermal treatments 20 minutes, is removed the PVA wedding agent.Biscuit is placed on is evacuated down to vacuum tightness 4-5Pa in the vacuum carbon tube furnace, the conversion argon gas is to pressure-fired 0.12MPa.The design temperature controller makes the temperature in the furnace chamber rise to 1300 ℃ with 5 ℃/minute, rise to 1800 ℃ with 10 ℃/minute speed then, closing temperature controller after being incubated 1 hour under 1800 ℃ naturally cools to normal temperature with stove and is high-compactness silicon carbide ceramics sintered body.
Embodiment 2: get 98wt% carborundum powder (mean particle size is the 0.5-5 micron), 2wt% silane coupling agent cyclohexylamino propyl group methyl dimethoxysilane mixture, (rotating speed is 300r/ minute, and ratio of grinding media to material is 5) ground and obtained material I in 5 hours in high energy ball mill; With 50wt%Al
2O
3, 48wt%Y
2O
3, 2wt% titanate coupling agent sec.-propyl three decoyl titanic acid ester (rotating speed is 300r/ minute, and ratio of grinding media to material is 5) in high energy ball mill grind and to obtain material II in 6 hours; 85wt% material I, 10wt% material II, 5wt%PVA mixing and ball milling in high energy ball mill was obtained the sintering precursor powder in 9 hours.With precursor powder under 80 degree dry 2 hours, after pulverizing, sieving, under 230Mpa, leave standstill in the cylindrical die of packing into and obtained biscuit in 5 minutes.Biscuit 250 ℃ of thermal treatments 20 minutes, is removed the PVA wedding agent.Biscuit is placed on is evacuated down to vacuum tightness 4-5Pa in the vacuum carbon tube furnace, the conversion argon gas is to pressure-fired 0.11MPa.The design temperature controller makes the temperature in the furnace chamber rise to 1300 ℃ with 6 ℃/minute, rise to 1780 ℃ with 12 ℃/minute speed then, closing temperature controller after being incubated 3 hours under 1780 ℃ naturally cools to normal temperature with stove and is high-compactness silicon carbide ceramics sintered body.
Embodiment 3: get 95wt% carborundum powder (mean particle size is the 0.5-5 micron), 5wt% silane coupling agent hexanediamine ylmethyl triethoxysilicane alkylating mixture, (rotating speed is 300r/ minute, and ratio of grinding media to material is 5) ground and obtained material I in 4 hours in high energy ball mill; With 35wt%Al
2O
3, 62wt%Y
2O
3, 3wt% titanate coupling agent sec.-propyl three (lauryl-myristyl) titanic acid ester (rotating speed is 300r/ minute, and ratio of grinding media to material is 5) in high energy ball mill grinds and to obtain material II in 8 hours; 93wt% material I, 5wt% material II, 2wt%PVA mixing and ball milling in high energy ball mill was obtained the sintering precursor powder in 10 hours.With precursor powder under 80 degree dry 2 hours, after pulverizing, sieving, under 230Mpa, leave standstill in the cylindrical die of packing into and obtained biscuit in 5 minutes.Biscuit 250 ℃ of thermal treatments 20 minutes, is removed the PVA wedding agent.Biscuit is placed on is evacuated down to vacuum tightness 4-5Pa in the vacuum carbon tube furnace, the conversion argon gas is to pressure-fired 0.11MPa.The design temperature controller makes the temperature in the furnace chamber rise to 1300 ℃ with 6 ℃/minute, rise to 1800 ℃ with 12 ℃/minute speed then, closing temperature controller after being incubated 2.5 hours under 1800 ℃ naturally cools to normal temperature with stove and is high-compactness silicon carbide ceramics sintered body.
Embodiment 4: get 95wt% carborundum powder (mean particle size is the 0.5-5 micron), 5wt% silane coupling agent γ-An Bingjisanyiyangjiguiwan mixture, (rotating speed is 300r/ minute, and ratio of grinding media to material is 5) ground and obtained material I in 4 hours in high energy ball mill; With 37wt%Al
2O
3, 60wt%Y
2O
3, 3wt% titanate coupling agent sec.-propyl three (lauryl-myristyl) titanic acid ester (rotating speed is 300r/ minute, and ratio of grinding media to material is 5) in high energy ball mill grinds and to obtain material II in 8 hours; 93wt% material I, 5wt% material II, 2wt%PVA mixing and ball milling in high energy ball mill was obtained the sintering precursor powder in 10 hours.With precursor powder under 80 degree dry 2 hours, after pulverizing, sieving, under 230Mpa, leave standstill in the cylindrical die of packing into and obtained biscuit in 5 minutes.Biscuit 250 ℃ of thermal treatments 20 minutes, is removed the PVA wedding agent.Biscuit is placed on is evacuated down to vacuum tightness 4-5Pa in the vacuum carbon tube furnace, the conversion argon gas is to pressure-fired 0.11MPa.The design temperature controller makes the temperature in the furnace chamber rise to 1300 ℃ with 6 ℃/minute, rise to 1790 ℃ with 12 ℃/minute speed then, closing temperature controller after being incubated 2.5 hours under 1790 ℃ naturally cools to normal temperature with stove and is high-compactness silicon carbide ceramics sintered body.
Embodiment 5: get 96wt% carborundum powder (mean particle size is the 0.5-5 micron), 4wt% silane coupling agent cyclohexylamino propyl group methyl dimethoxysilane mixture, (rotating speed is 300r/ minute, and ratio of grinding media to material is 5) ground and obtained material I in 4 hours in high energy ball mill; With 38wt%Al
2O
3, 59wt%Y
2O
3, 3wt% titanate coupling agent sec.-propyl dodecyl benzene sulfonyl titanic acid ester (rotating speed is 300r/ minute, and ratio of grinding media to material is 5) in high energy ball mill grinds and to obtain material II in 8 hours; 93wt% material I, 5wt% material II, 2wt% resol mixing and ball milling in high energy ball mill was obtained the sintering precursor powder in 10 hours.With precursor powder under 80 degree dry 2 hours, after pulverizing, sieving, under 230Mpa, leave standstill in the cylindrical die of packing into and obtained biscuit in 5 minutes.Biscuit 300 ℃ of thermal treatments 20 minutes, is removed phenolic resin binder.Biscuit is placed on is evacuated down to vacuum tightness 4-5Pa in the vacuum carbon tube furnace, the conversion argon gas is to pressure-fired 0.11MPa.The design temperature controller makes the temperature in the furnace chamber rise to 1300 ℃ with 6 ℃/minute, rise to 1800 ℃ with 12 ℃/minute speed then, closing temperature controller after being incubated 3 hours under 1800 ℃ naturally cools to normal temperature with stove and is high-compactness silicon carbide ceramics sintered body.
Claims (1)
1. manufacture method based on the silane-titanate two-component coupling agent silicon carbide ceramics is characterized in that adopting the SiC-Al of silane-titanate two-component coupling agent bonding
2O
3-Y
2O
3System, this system can prepare relative density by simple technological process sintering and surpass 98% compact silicon carbide ceramic under 1800 ℃ low temperature, greatly reduced the energy consumption of silicon carbide production process; Al
2O
3And Y
2O
3As the sintering aid of system, under 1750 ℃-1800 ℃ sintering temperature, Al
2O
3-Y
2O
3Form liquid phase YAG, make carbon and Siliciumatom can quicken diffusion at a lower temperature and sintering; And the hydrolysis of the double-component coupling agent in the system by alkoxyl group is on main body SiC surface and auxiliary agent A l
2O
3, Y
2O
3The surface forms firm chemical bonding, forms strong and dense sintering aid coating layer by the radical reaction between two kinds of coupling agents on main body silicon carbide top layer simultaneously; Material I will be obtained in high energy ball mill under main raw material 95-98wt% carborundum powder, the 2-5wt% silane coupling A normal temperature in mixing and ball milling 3-5 hour; With sintering aid 30-70wt%Al
2O
3, 28-65wt%Y
2O
3, 2-5wt% titanate coupling agent B obtained material II in mixing and ball milling 4-8 hour in high energy ball mill; Wherein silane coupling A is a kind of in γ-An Bingjisanyiyangjiguiwan, cyclohexylamino propyl group methyl dimethoxysilane, the hexanediamine ylmethyl triethoxyl silane; Titanate coupling agent B is a kind of in sec.-propyl three (dodecyl benzene sulfonyl) titanic acid ester, sec.-propyl three decoyl titanic acid ester, sec.-propyl three (lauryl-myristyl) titanic acid ester; The grain diameter of main body silicon carbide between the 0.5-5 micron, Al
2O
3, Y
2O
3The particle scale of sintering aid below 200 nanometers, thereby help forming in main body carborundum powder surface densification, evenly, thin sintering aid coating layer, also help finishing sintering process under the lesser temps with less amount of auxiliary; With 85-95wt% material I, 2-10wt% material II, 3-5wt% wedding agent in high energy ball mill after mixing and ball milling 5-10 hour through sieving, moulding, curing, high temperature sintering main technique step, form the silicon carbide ceramics product;
Wherein wedding agent is a kind of in resol, the polyvinyl alcohol;
Wherein high temperature sintering is under the condition of vacuum; temperature programming under the minute-pressure Ar of 0.10-0.13MPa gas atmosphere protection; below 1300 ℃ 5-8 ℃/minute; the temperature rise rate of temperature range is 10-15 ℃/minute more than 1300 ℃; holding temperature is 1750 ℃-1800 ℃, and soaking time is 0.5-3 hour.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200910161250 CN101913880B (en) | 2009-07-20 | 2009-07-20 | Method for manufacturing silicon carbide ceramics based on silane-titanate two-component coupling agent |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200910161250 CN101913880B (en) | 2009-07-20 | 2009-07-20 | Method for manufacturing silicon carbide ceramics based on silane-titanate two-component coupling agent |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101913880A CN101913880A (en) | 2010-12-15 |
| CN101913880B true CN101913880B (en) | 2013-07-31 |
Family
ID=43321562
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200910161250 Expired - Fee Related CN101913880B (en) | 2009-07-20 | 2009-07-20 | Method for manufacturing silicon carbide ceramics based on silane-titanate two-component coupling agent |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101913880B (en) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104628389A (en) * | 2015-01-28 | 2015-05-20 | 安徽省和翰光电科技有限公司 | Low-temperature pressureless-sintered silicon carbide ceramic and preparation method thereof |
| CN104671792A (en) * | 2015-01-28 | 2015-06-03 | 安徽省和翰光电科技有限公司 | High-tenacity silicon carbide ceramic and preparation method thereof |
| CN104671789A (en) * | 2015-01-28 | 2015-06-03 | 安徽省和翰光电科技有限公司 | Silicon carbide ceramic-based composite material for protective components and preparation method of silicon carbide ceramic-based composite material |
| CN104628388A (en) * | 2015-01-28 | 2015-05-20 | 安徽省和翰光电科技有限公司 | High thermal conductivity silicon carbide ceramic material and preparation method thereof |
| CN104671790A (en) * | 2015-01-28 | 2015-06-03 | 安徽省和翰光电科技有限公司 | Silicon carbide ceramic for armor, and preparation method |
| CN105565786A (en) * | 2015-12-16 | 2016-05-11 | 广东昭信照明科技有限公司 | Low-temperature composite high-heat-conductivity ceramic material and preparation method thereof |
| CN108276002A (en) * | 2018-03-06 | 2018-07-13 | 济南大学 | A kind of preparation method for 3DP moulding process ceramic powder of titanium carbide |
| CN112458443B (en) * | 2019-09-06 | 2023-03-21 | 佛山市顺德区美的电热电器制造有限公司 | Stainless steel and preparation method and application thereof |
| CN113912399B (en) * | 2021-12-15 | 2022-02-25 | 山东金鸿新材料股份有限公司 | Preparation method of high-density pressureless sintered silicon carbide ceramic |
| CN115448743A (en) * | 2022-09-02 | 2022-12-09 | 中国兵器工业第五二研究所烟台分所有限责任公司 | Preparation method of diamond particle reinforced silicon carbide-based ceramic |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1172782A (en) * | 1997-07-16 | 1998-02-11 | 国家建筑材料工业局山东工业陶瓷研究设计院 | Nanometre silicon-carbide-silicon nitride complex phase ceramics and its preparation method |
| CN101081738A (en) * | 2006-05-29 | 2007-12-05 | 宁波大学 | Silicon carbide ceramic production technology by using prefabricated YAG nano powder as sintering aid |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS57123869A (en) * | 1981-01-27 | 1982-08-02 | Sumitomo Electric Industries | Manufacture of non-oxide ceramics |
| JPS57166374A (en) * | 1981-04-02 | 1982-10-13 | Sumitomo Electric Industries | Manufacture of non-oxide ceramics |
-
2009
- 2009-07-20 CN CN 200910161250 patent/CN101913880B/en not_active Expired - Fee Related
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1172782A (en) * | 1997-07-16 | 1998-02-11 | 国家建筑材料工业局山东工业陶瓷研究设计院 | Nanometre silicon-carbide-silicon nitride complex phase ceramics and its preparation method |
| CN101081738A (en) * | 2006-05-29 | 2007-12-05 | 宁波大学 | Silicon carbide ceramic production technology by using prefabricated YAG nano powder as sintering aid |
Non-Patent Citations (4)
| Title |
|---|
| "碳化硅纤维及其复合材料";赵稼祥;《高科技纤维与应用》;20020831;第27卷(第4期);第2-6、34页 * |
| JP昭57-123869A 1982.08.02 |
| JP昭57-166374A 1982.10.13 |
| 赵稼祥."碳化硅纤维及其复合材料".《高科技纤维与应用》.2002,第27卷(第4期),第2-6、34页. |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101913880A (en) | 2010-12-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101913880B (en) | Method for manufacturing silicon carbide ceramics based on silane-titanate two-component coupling agent | |
| CN101928148B (en) | Method for manufacturing low-temperature high-density silicon carbide ceramics based on silane coupling agent | |
| CN102060546B (en) | Method for manufacturing silicon carbide ceramic based on silane borate two-component coupling agent | |
| CN111423233A (en) | Silicon carbide reinforced boron carbide-based ceramic material and preparation method thereof | |
| CN107746282A (en) | A kind of in-situ carburization silica fibre enhancing liquid phase sintering silicon carbide ceramic and manufacture method | |
| CN101759435B (en) | Carborundum ceramics based on novel nanometer four-component sintering additives | |
| CN101928147B (en) | Method for manufacturing silicon carbide ceramics based on silane and ester aluminate double-component coupling agent | |
| CN113213960B (en) | High-toughness and high-hardness wear-resistant ceramic and preparation method thereof | |
| CN101164999B (en) | Method for preparing silicon carbide ceramic plasticized by three components combined plasticizing material combination | |
| CN101551012A (en) | A carbonaceous silicon carbide sealed ring and preparation method thereof | |
| CN101172877B (en) | Process for manufacturing multicomponent combination toughness reinforcing silicon carbide ceramic including crystal whisker and fibre | |
| CN101913881B (en) | Method for manufacturing silicon carbide ceramics based on silane-zirconium aluminate two-component coupling agent | |
| CN101759436B (en) | Carborundum ceramics manufacturing method based on novel nanometer four-component sintering additives | |
| CN100515994C (en) | Technique for preparing liquid phase sintering silicon carbide ceramic | |
| CN100558678C (en) | Process for manufacturing polymorphism aluminum oxide grain combination toughness reinforcing silicon carbide ceramic | |
| CN116217233A (en) | Complex-phase ceramic of SiC whisker and high-entropy boride hardened and toughened high-entropy carbide, and preparation method and application thereof | |
| CN101165000B (en) | Technique for preparing silicon carbide ceramic by using sheet aluminum oxide particles to plasticize | |
| CN101164997B (en) | Method for preparing silicon carbide ceramic plasticized by rod-like aluminum oxide particle and silicon carbide whisker combination | |
| CN106800414A (en) | The method that reaction in-situ prepares the ultra-temperature ceramic-based composite material of nitrogen boron | |
| Tressler | An assessment of low cost manufacturing technology for advanced structural ceramics and its impact on ceramic armor | |
| CN101164992B (en) | Method for preparing silicon carbide ceramic plasticized by sheet aluminum oxide particle and silicon carbide whisker combination | |
| CN114573351B (en) | Boron carbide-based composite material and preparation method thereof | |
| CN100590100C (en) | Process for manufacturing multicomponent combined toughness reinforcing silicon carbide ceramic containing carbon fibre | |
| JP2772488B2 (en) | Method for producing polycrystalline composite ceramic coating and method for producing molded polycrystalline composite ceramic | |
| CN100545129C (en) | A kind of process for manufacturing multicomponent combination toughness reinforcing silicon carbide ceramic that comprises silicon carbide wafer |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130731 Termination date: 20160720 |