CN102199373A - Graphite alkene-La2NiO4/zinc-aluminum-titanium series corrosion-resistance coating for polycrystalline silicon ingot casting furnace - Google Patents
Graphite alkene-La2NiO4/zinc-aluminum-titanium series corrosion-resistance coating for polycrystalline silicon ingot casting furnace Download PDFInfo
- Publication number
- CN102199373A CN102199373A CN 201110091484 CN201110091484A CN102199373A CN 102199373 A CN102199373 A CN 102199373A CN 201110091484 CN201110091484 CN 201110091484 CN 201110091484 A CN201110091484 A CN 201110091484A CN 102199373 A CN102199373 A CN 102199373A
- Authority
- CN
- China
- Prior art keywords
- corrosion
- powder
- carbon fiber
- heat insulation
- layer
- 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.)
- Granted
Links
Landscapes
- Chemical Or Physical Treatment Of Fibers (AREA)
- Thermal Insulation (AREA)
Abstract
The invention provides a corrosion-resistance coating for a polycrystalline silicon ingot casting furnace. The corrosion-resistance coating is characterized by comprising an alloy corrosion-resistance layer coated on the surface of a carbon fiber heat insulation layer and a heat insulation corrosion-resistance layer coated on the surface of the alloy corrosion-resistance layer, wherein the alloy corrosion-resistance layer comprises the following components by weight percent: 20wt%-38wt% of aluminum powder, 30wt%-45wt% of zinc powder and 30wt%-45wt% of titanium powder; and the heat insulation corrosion-resistance layer comprises the following components by weight percent: 55wt%-72wt% of graphite alkene powder, 25wt%-40wt% of La2NiO4 powder, 1wt%-5wt% of film-forming agent and 1wt%-5wt% of mixture of a curing agent and a dispersing agent. The invention also provides a high-temperature-resistance protective layer for the polycrystalline silicon ingot casting furnace and a preparation method thereof. The coating provided by the invention has high hardness and corrosion resistance, thereby prolonging the service life of the carbon fiber heat insulation layer.
Description
Technical field
The present invention relates to field polysilicon, be specifically related to a kind of corrosion-resistant finishes that is used for polycrystalline silicon ingot or purifying furnace, the high temperature resistance protective layer that constitutes by this corrosion-resistant finishes and the preparation method of high temperature resistance protective layer.
Background technology
Sun power is developed gradually in the world fast as a kind of reproducible green energy resource; solar energy power generating is to utilize the photovoltaic effect of interface and directly change luminous energy a kind of technology of electric energy into, and solar cell carries out packaging protection after through series connection can form large-area photovoltaic module.Increasingly mature along with solar energy generation technology, photovoltaic module is obtained widespread use at numerous areas such as man-made satellite energy supplies.
Polycrystalline silicon ingot or purifying furnace is one of key equipment of photovoltaic industry chain (supply chain) front end, polycrystalline silicon ingot or purifying furnace furnace wall innermost layer is a working lining, temperature is up to 1560 ℃ in the stove, in hot environment, under the heating of the silicon material graphite heater in argon gas in the crucible, by the solid-state liquid state that becomes, by the conductive force of oriented growth piece, generate the fixedly polycrystal silicon ingot in crystal orientation then.Directly have influence on the electricity conversion of polycrystal silicon cell sheet by the quality of the polycrystal silicon ingot of polycrystalline silicon ingot or purifying furnace preparation.
Existing polycrystalline silicon ingot casting furnace main body adopts stainless steel, to reduce the pollution of equipment material to product.Under the hot environment of producing polysilicon, by roasting bad, on the inwall of working lining, lay the high temperature insulation layer in order to prevent stainless steel casing.In numerous high temperature resistant heat insulation materials, the heat resisting temperature of carbon fiber reaches as high as 3000 ℃, carbon fiber also has characteristics such as erosion resistance, resistance to fatigue and intensity height preferably simultaneously, therefore, in the production technique of existing polysilicon, adopt carbon fiber thermal insulating material usually as high temperature resistant heat insulation material.
As lagging material, carbon fiber is under the situation of not mixing impurity, and carbon fiber can keep characteristic such as high temperature resistant, corrosion-resistant, that the coefficient of expansion is little.But when polycrystalline silicon ingot or purifying furnace is produced polysilicon, the raw material of making polysilicon contains impurity usually, the carbon fiber heat insulation layer, the thermofin at especially simple action position, along with use is easy to adsorb the minute impurities particle, carbon fiber can react with impurity and silicon then, thereby changed the original character of carbon fiber heat insulation layer, cause carbon fiber heat insulation layer density to diminish, wearing and tearing increase, and influence the effect of heat insulation of carbon fiber heat insulation layer.
In order to prevent that the yellow soda ash fibrous insulating layer is corroded, application number is that 200910138449.3 Chinese patent literature discloses a kind of corrosion-resistant finishes that is used for polycrystalline silicon ingot or purifying furnace and preparation method thereof, this patent disclosure a kind of corrosion-resistant finishes that is used for polycrystalline silicon ingot or purifying furnace, it comprises following component in percentage by weight: 85%～93% the carbon fiber powder and the mixture of Graphite Powder 99,1%～4% membrane-forming agent, 1%～3% membrane-forming agent, 1%～3% the solidifying agent and the mixture of dispersion agent, with 5%～12% lagging material powder, the lagging material that uses in this patent is Sr
3Ti
2O
7And Sr
4Ti
3O
10In one or both.Though above-mentioned corrosion-resistant finishes plays thermal insulation layer to the carbon fiber heat insulation layer and plays the certain protection effect, but its intensity and erosion resistance still remain to be improved, and have longer work-ing life to guarantee the carbon fiber heat insulation layer.
Summary of the invention
The technical problem that the present invention solves is to provide a kind of corrosion-resistant finishes that is used for polycrystalline silicon ingot or purifying furnace; this coating has higher hardness and erosion resistance; thereby prolong the work-ing life of carbon fiber heat insulation layer, the high temperature resistance protective layer that is made of this corrosion-resistant finishes and the preparation method of high temperature resistance protective layer also are provided.
In order to solve the problems of the technologies described above, the invention provides following technical scheme:
A kind of corrosion resistant corrosion figure layer that is used for polycrystalline silicon ingot or purifying furnace comprises: the alloy preservative coat and the heat insulating and corrosion layer that is overlying on described alloy preservative coat surface that are overlying on the carbon fiber heat insulation laminar surface.
Described alloy preservative coat comprises: the titanium valve of the aluminium powder of 20wt%～38wt%, the zinc powder of 30wt%～45wt% and 30wt%～45wt%;
Described heat insulating and corrosion layer comprises: the Graphene powder of 55wt%～72wt%, the La of 25wt%～40wt%
2NiO
4The mixture of the membrane-forming agent of powder, 1wt%～5wt% and the solidifying agent of 1wt%～5wt% and dispersion agent.
Preferably, be that the content of graphene powder is 62wt%～68wt% in the described heat insulating and corrosion layer.
Preferably, the particle diameter of zinc powder, aluminium powder and titanium valve is 100 orders～300 orders in the described alloy preservative coat.
Preferably, described membrane-forming agent is a water glass.
Preferably, described solidifying agent is a silicofluoride.
Preferably, described dispersion agent is a tannic acid.
The weight ratio of preferred described silicofluoride and tannic acid is 1: 1～2: 1.
The present invention also provides a kind of high temperature resistance protective layer that is used for polycrystalline silicon ingot or purifying furnace, comprising: carbon fiber heat insulation layer and the above-mentioned corrosion resistant corrosion figure layer that is overlying on described carbon fiber heat insulation laminar surface.
Accordingly, the present invention also provides a kind of preparation method of above-mentioned high temperature resistance protective layer, may further comprise the steps:
1) after being mixed in proportion, aluminium powder, zinc powder and titanium valve obtain the diffusion medium powder, the carbon fiber heat insulation layer is embedded in is heated to 300 ℃～500 ℃ in the described diffusion medium powder, take out after being incubated 2 hours～5 hours, obtain the carbon fiber heat insulation layer that the surface is covered with the alloy preservative coat;
2) mixture of solidifying agent and dispersion agent is applied to the surface of described alloy preservative coat;
3) with Graphene powder, La
2NiO
4After being mixed in proportion, powder and membrane-forming agent be applied to the surface of solidifying agent and dispersion agent;
4) will under vacuum state, be heated to 70 ℃～85 ℃ through the carbon fiber heat insulation layer that step 3) is handled, constant temperature 1.5～3 hours.
Preferably, step 2) in,, under the condition of relative humidity＜90% solidifying agent and dispersion agent are applied to the surface of described alloy preservative coat 0 ℃～100 ℃ of envrionment temperatures.
The invention provides a kind of corrosion-resistant finishes that is used for polycrystalline silicon ingot or purifying furnace, this corrosion-resistant finishes comprises alloy preservative coat and heat insulating and corrosion layer successively.Wherein, the alloy preservative coat comprises: the titanium valve of the aluminium powder of 20wt%～38wt%, the zinc powder of 30wt%～45wt% and 30wt%～45wt%, and it directly is overlying on carbon fiber surface, has higher antiseptic property and hardness, avoid impurity to contact, and improve the mechanical property of carbon fiber with carbon fiber.The heat insulating and corrosion layer comprises: the Graphene powder of 55wt%～72wt%, the La of 25wt%～40wt%
2NiO
4The mixture of the membrane-forming agent of powder, 1wt%～5wt% and the solidifying agent of 1wt%～5wt% and dispersion agent, its be with polycrystalline silicon ingot or purifying furnace in the nearest one deck of hot environment, the heat insulating and corrosion layer has heat-blocking action preferably on the one hand, avoid alloy preservative coat generation fusion, guarantee that the alloy preservative coat plays best preservative activity; On the other hand, the heat insulating and corrosion layer has certain preservative effect and higher hardness, further the carbon fiber heat insulation layer is played a protective role, and prolongs the work-ing life of carbon fiber heat insulation layer.
Embodiment
In order further to understand the present invention, below in conjunction with embodiment the preferred embodiment of the invention is described, but should be appreciated that these describe just to further specifying the features and advantages of the present invention, rather than to the restriction of claim of the present invention.
The embodiment of the invention discloses a kind of corrosion-resistant finishes that is used for polycrystalline silicon ingot or purifying furnace, this coating comprises the alloy preservative coat that is overlying on the carbon fiber heat insulation laminar surface and is overlying on the heat insulating and corrosion layer on alloy preservative coat surface.Above-mentioned alloy preservative coat comprises: the titanium valve of the aluminium powder of 20wt%～38wt%, the zinc powder of 30wt%～45wt% and 30wt%～45wt%.Above-mentioned heat insulating and corrosion layer comprises: the Graphene powder of 5wt%～72wt%, the La of 25wt%～40wt%
2NiO
4The mixture of the membrane-forming agent of powder, 1wt%～5wt% and the solidifying agent of 1wt%～5wt% and dispersion agent.
Alloy preservative coat in the above-mentioned corrosion-resistant finishes directly contacts with carbon fiber, is the coating that the carbon fiber heat insulation layer is played main preservative activity.The content of aluminium powder is 20wt%～38wt% in the interalloy preservative coat of the present invention, is preferably 22wt%～35wt%, 28wt%～34wt% more preferably, preferred 100 orders of the particle diameter of aluminium powder～300 orders, more preferably 200 orders～300 orders.The content of zinc powder is 30wt%～45wt% in the alloy preservative coat of the present invention, is preferably 32wt%～45wt%, 35wt%～40wt% more preferably, preferred 100 orders of the particle diameter of aluminium powder～300 orders, more preferably 200 orders～300 orders.The adding of titanium valve helps to improve the intensity of alloy preservative coat, the content of titanium valve is 30wt%～45wt% in the above-mentioned alloy preservative coat, is preferably 32wt%～45wt%, more preferably 35wt%～40wt%, preferred 100 orders of the particle diameter of titanium valve～300 orders, more preferably 200 orders～300 orders.
As preferred version, alloy preservative coat provided by the invention can also comprise the activator powder of 0.1wt～2.0wt% and the weighting agent of 0.1wt～20wt%.The activator powder content is 0.5wt～1.5wt% more preferably, the particle diameter of activator powder is preferably 50 orders～200 orders, 100 orders～200 orders more preferably, activator can be selected from one or more in ammonium chloride well known to those skilled in the art, sodium-chlor, Repone K, aluminum chloride, zinc chloride, Sodium Fluoride, Potassium monofluoride, aluminum fluoride, the zinc fluoride.Weighting agent is preferably quartz sand, and the particle diameter of weighting agent powder is preferably 50 orders～200 orders, more preferably 100 orders～200 orders.
The process that the alloy preservative coat forms is as follows: obtain the diffusion medium powder after aluminium powder, zinc powder and titanium valve are mixed in proportion, the carbon fiber heat insulation layer is embedded in is heated to 300 ℃～500 ℃ in the described diffusion medium powder, take out after being incubated 2 hours～5 hours, above-mentioned diffusion medium metal-powder is oozing in the treating processes altogether, under the infiltration expanding effect of atoms metal, zinc, aluminium and titanium elements infiltrate carbon fiber surface, form the alloy preservative coat.
The alloy preservative coat of Xing Chenging not only can improve the erosion resistance of carbon fiber surface according to the method described above, in addition, owing to the hardness height, has therefore also improved the wear resisting property of carbon fiber heat insulation layer.
Though the alloy preservative coat has excellent antiseptic property and higher hardness, but resistance toheat is not good, hot environment melts the alloy preservative coat in the ingot furnace, and the present invention sets up the Graphene powder of the heat insulating and corrosion layer of following composition: 55wt%～72wt%, the La of 25wt%～40wt% on the alloy preservative coat
2NiO
4The mixture of the membrane-forming agent of powder, 1wt%～5wt% and the solidifying agent of 1wt%～5wt% and dispersion agent.
In the above-mentioned heat insulating and corrosion layer, Graphene powder and La
2NiO
4Powder is a basic substance, and Graphene is the hardest the thinnest material that has been found that in the world, and its good heat resistance, at high temperature still has excellent chemical stability; In addition, Graphene powder frictional coefficient is little, and lubricity is good, can make the corrosion-resistant finishes smooth surface that makes, and does not have burr.Therefore, the adding of graphene powder makes insulating have very excellent hardness, erosion resistance and higher surface flatness preferably.The content of Graphene powder is 55wt%～72wt% in the heat insulating and corrosion layer, is preferably 62wt%～68wt%, more preferably 63wt%～68wt%.Graphene powder preferably is prepared as follows:
A), graphite is added in the mixture of strong oxidizing acid and nitrate, be cooled to 0 ℃～5 ℃, whipped state slowly adds down and contains the potassium strong oxidizer, be warming up to 10 ℃～15 ℃, and continue stir, subsequently mixing solutions is imported temperature and be in 30 ℃～40 ℃ the water-bath, slowly add entry behind reaction 20min～40min, be warming up to 90 ℃～100 ℃, add hydrogen peroxide and water again, after-filtration is alternately cleaned with hydrochloric acid and water in the back that stirs, filter cake is dried, grind, sieve, obtain oxidation graphite solid.
B), oxidation graphite solid that step a is obtained is dissolved in the solvent, earthquake power is to shake under the condition of 300w～1200w then, obtains graphene oxide solution.
C), graphene oxide solution is placed in the supercritical reaction still; under the protection of inert gas; in 20Mpa～100Mpa; under the condition of the supercritical temperature that is higher than step b solvent for use; reaction 1～24h; emit gas in the reactor after cold with reactor naturally cooling or water are crisp, obtain graphene powder.
La in the heat insulating and corrosion layer
2NiO
4Powder is as lagging material, La
2NiO
4Be that the patent of CN100376505C is disclosed by authorizing publication number.La
2NiO
4The fusing point height, thermal conductivity is little, by La
2NiO
4The corrosion-resistant finishes thermal conductivity that powder constitutes is lower, and good thermotolerance is arranged, and is applicable to the parts that use under thermal environment for a long time, and the alloy preservative coat is played a protective role, and prevents that it from melting at high temperature.
In the corrosion-resistant finishes provided by the invention, the adding of membrane-forming agent makes the heat insulating and corrosion layer can form the continuous film that can adhere to, and it is more firm to adhere on the alloy preservative coat, rub resistance.Membrane-forming agent is preferably water glass among the present invention.Water glass is alkalimetal silicate (M
2OnSiO
2) the aqueous solution, be comparatively general inorganic paint membrane-forming agent.Water glass acid-proof is good, good heat resistance, and at high temperature strength degradation is very little for the silicon-dioxide mesh skeleton that sclerosis back forms, and the coating of formation has high temperature resistant, anti-solvent, heat insulation performance.Water glass has many types according to the kind of metal M and modulus n value different, and M can be Na, K, Li; The size of modulus n can influence cohesiveness and water tolerance.The amount of water glass of the present invention is the 1wt%～5wt% of heat insulating and corrosion stratum total.
When utilizing water glass to make heat-insulating anti-corrosive coating, in order to make the better film forming of water glass, quicken the condensation cure speed of water glass and improve intensity, and increase its water tolerance, add solidifying agent usually water glass is carried out modification.
Solidifying agent is preferably silicofluoride among the present invention.If the silicofluoride incorporation very little, then the water glass condensation cure is slow, the intensity of the corrosion-resistant finishes of making also can be influenced, if the silicofluoride incorporation is too many, then the water glass setting and harden is too fast, and inconvenience is smeared the corrosion-resistant finishes material on thermofin, and after the sclerosis, though the early strength of corrosion-resistant finishes is high, the later stage can descend to some extent, so the amount of solidifying agent and dispersion agent is the 1wt%～5wt% of heat insulating and corrosion stratum total.
Each composition keeps good dispersiveness in the heat insulating and corrosion coated material in order to make, and has also added dispersion agent in the heat insulating and corrosion coated material provided by the invention.Dispersion agent can reduce in the corrosion-resistant finishes material each composition and finish the needed time of dispersion process, homogeneous disperses to be difficult to be dissolved in inorganic, the organic solid particle of liquid, stablizes each discrete particles, the surface properties of modification dispersed particle, adjust the mobility of particle, prevent flocculation and precipitation.
Dispersion agent among the present invention is preferably tannic acid.Tannic acid claims Weibull again, is the compound of a class complexity, and is nontoxic and soluble in water, is present in many plants, and the structure of the tannic acid of different sources is variant, but all has the polyphenol hydroxyl structure, has hydrophilic, oleophilic characteristics, and certain surfactivity is arranged.
As preferably, solidifying agent potassium silicofluoride and dispersion agent tannic acid blending ratio are 1: 1～2: 1, and be preferred, and the blending ratio of potassium silicofluoride and tannic acid is 1: 1.
By such scheme as can be known, corrosion-resistant finishes provided by the invention comprises alloy preservative coat and heat insulating and corrosion layer successively.Wherein, the alloy preservative coat directly is overlying on carbon fiber surface, has higher antiseptic property and hardness, avoids impurity to contact with carbon fiber, and carbon fiber is had provide protection.The heat insulating and corrosion layer be with polycrystalline silicon ingot or purifying furnace in the nearest one deck of hot environment, it has heat-blocking action preferably on the one hand, avoids alloy preservative coat generation fusion, guarantees that the alloy preservative coat plays best preservative activity; On the other hand, the heat insulating and corrosion layer has certain preservative effect and higher hardness, further the carbon fiber heat insulation layer is played a protective role, and prolongs the work-ing life of carbon fiber heat insulation layer.
The high temperature resistance protective layer that is used for polycrystalline silicon ingot or purifying furnace of the present invention comprises the carbon fiber heat insulation layer and is overlying on the corrosion-resistant finishes of carbon fiber heat insulation laminar surface that corrosion-resistant finishes is made by above material.This high temperature resistance protective layer is prepared as follows:
1) after being mixed in proportion, aluminium powder, zinc powder and titanium valve obtain the diffusion medium powder, the carbon fiber heat insulation layer is embedded in is heated to 300 ℃～500 ℃ in the described diffusion medium powder, be incubated and take out the carbon fiber heat insulation layer that the surface is covered with the alloy preservative coat after 2 hours～5 hours;
2) mixture of solidifying agent and dispersion agent is applied to the surface of described alloy preservative coat;
3) with Graphene powder, La
2NiO
4After being mixed in proportion, powder and membrane-forming agent be applied to the surface of solidifying agent and dispersion agent;
4) will under vacuum state, be heated to 70 ℃～85 ℃ through the carbon fiber heat insulation layer that step 3) is handled, constant temperature 1.5～3 hours.
Step 1 is the process that forms the alloy preservative coat at the carbon fiber heat insulation laminar surface, step 2～step 4 is the processes at alloy preservative coat surface-coated heat insulating and corrosion layer, preferably 10 ℃～100 ℃ of envrionment temperatures, under the condition of relative humidity＜90% solidifying agent and dispersion agent are applied to the surface of described alloy preservative coat in the step 2.
The high temperature resistance protective layer intensity height of the present invention's preparation, erosion resistance is strong, avoids impurity to be deposited on carbon fiber surface, and work-ing life is longer.
In order further to understand the present invention, below in conjunction with embodiment the high temperature resistance protective layer that is used for polycrystalline silicon ingot or purifying furnace provided by the invention is described, protection scope of the present invention is not limited by the following examples.
Potassium silicofluoride in following examples is provided by Changshu Xinhua Chemical Factory, and tannic acid is provided by the magnificent forever fine chemicals in Jiangsu company limited, and potash water glass is provided by the prosperous Sheng chemical industry of Shijiazhuang City company limited.
Embodiment 1 preparation Graphene powder
1,10g graphite is added in the mixing solutions of the vitriol oil and SODIUMNITRATE, the mass ratio of the vitriol oil and SODIUMNITRATE is 0.5: 1, the mass ratio of the vitriol oil and graphite is 10: 1, mixing solutions is cooled to 0 ℃～5 ℃, stir 30min, continue to stir and the slow potassium permanganate that adds, the mass ratio of potassium permanganate and graphite is 2: 1, is warming up to 10 ℃～15 ℃, continue to stir 12h, then mixing solutions is imported temperature and be in 30 ℃～40 ℃ the water-bath, slowly add 200ml water behind the reaction 30min, be warming up to 90 ℃～100 ℃ and keep 35min, add hydrogen peroxide and 100ml water again, the mass ratio of hydrogen peroxide and graphite is 0.5: 1, alternately cleans 4 times with hydrochloric acid and water behind the stirring 2h, is using the flushing with clean water after-filtration, filter cake is dried, grind, sieve, obtain oxidation graphite solid.
2, the oxidation graphite solid that step 1 is obtained is dissolved in the ethanol, and earthquake power is to shake 10h under the condition of 700w then, obtains graphene oxide solution.
3, step 2 is obtained graphene oxide solution and place in the supercritical reaction still, under nitrogen protection, in 60Mpa, under 260 ℃ the condition, reaction 1～24h with emitting gas in the reactor behind the reactor naturally cooling, obtains graphene powder.The graphene powder that uses in following examples prepares by present embodiment.
Embodiment 2
1, getting the 25wt% granularity is that the granularity of 100 purpose zinc powders, 40wt% is that 100 purpose aluminium powders, 40wt% granularity are 100 purpose titanium valves, and uniform mixing obtains the diffusion medium powder; Getting the diffusion medium for preparing and carbon fiber heat insulation layer puts into vacuum and oozes stove altogether, and the carbon fiber heat insulation layer is embedded in the diffusion medium, the volume ratio of diffusion medium and workpiece is 1: 1, vacuum oven is evacuated to vacuum tightness less than 0.5kPa, vacuum is oozed stove altogether be warming up to 350 ℃, vacuum flue per minute changes 3 circles, be incubated after 8 hours, the carbon fiber heat insulation layer is taken out, clean up, dry.
Sampling is tested, and forms the about 80 microns alloy preservative coat of thickness at the carbon fiber heat insulation laminar surface.The hardness of beta alloy preservative coat and erosion resistance, test result is listed in table 1.
2, potassium silicofluoride and tannic acid are mixed according to 1: 1 weight ratio, putting into dispersion machine after the mixing stirs, the amount of potassium silicofluoride and tannic acid is the 5wt% of heat insulating and corrosion coating, at 25 ℃, under the condition of relative humidity 70%, the mixture that stirs is applied to the surface of carbon fiber heat insulation layer.
3, being that the amount of 60wt% takes by weighing graphene powder according to content in the heat insulating and corrosion layer, is that the amount of 30wt% takes by weighing La according to content in the heat insulating and corrosion layer
2NiO
4Powder; According to content in the corrosion-resistant finishes is that the amount of 5wt% takes by weighing potash water glass.Above material is put into dispersion machine mix, be applied to the surface of the carbon fiber heat insulation layer that was coated with potassium silicofluoride and tannic acid, evenly smear, the thickness unanimity, coat-thickness is 1.5mm.
4, the carbon fiber heat insulation layer of coating alloy preservative coat and heat insulating and corrosion layer more than the general is put into vacuum furnace, is heated to 80 ℃ under vacuum state, and constant temperature 2 hours obtains high temperature resistance protective layer.The surface hardness of test high temperature resistance protective layer, test result is listed in table 2.
Embodiment 3
1, getting the 35wt% granularity is that the granularity of 300 purpose zinc powders, 35wt% is that 300 purpose aluminium powders, 30wt% granularity are 300 purpose titanium valves, and uniform mixing obtains the diffusion medium powder; Getting the diffusion medium for preparing and carbon fiber heat insulation layer puts into vacuum and oozes stove altogether, and the carbon fiber heat insulation layer is embedded in the diffusion medium, the volume ratio of diffusion medium and workpiece is 1: 1, vacuum oven is evacuated to vacuum tightness less than 0.5kPa, vacuum is oozed stove altogether be warming up to 500 ℃, vacuum flue per minute changes 3 circles, be incubated after 8 hours, the carbon fiber heat insulation layer is taken out, clean up, dry.
Sampling is tested, and forms the about 80 microns alloy preservative coat of thickness at the carbon fiber heat insulation laminar surface.The hardness of beta alloy preservative coat and erosion resistance, test result is listed in table 1.
2, potassium silicofluoride and tannic acid are mixed according to 2: 1 weight ratio, putting into dispersion machine after the mixing stirs, the amount of potassium silicofluoride and tannic acid is the 1.5wt% of heat insulating and corrosion coating, at 15 ℃, under the condition of relative humidity 70%, the mixture that stirs is applied to the surface of carbon fiber heat insulation layer.
3, being that the amount of 70wt% takes by weighing graphene powder according to content in the heat insulating and corrosion layer, is that the amount of 28wt% takes by weighing La according to content in the heat insulating and corrosion layer
2NiO
4Powder; According to content in the corrosion-resistant finishes is that the amount of 1.5wt% takes by weighing potash water glass.Above material is put into dispersion machine mix, be applied to the surface of the carbon fiber heat insulation layer that was coated with potassium silicofluoride and tannic acid, evenly smear, the thickness unanimity, coat-thickness is 1.6mm.
4, the carbon fiber heat insulation layer of coating alloy preservative coat and heat insulating and corrosion layer more than the general is put into vacuum furnace, is heated to 80 ℃ under vacuum state, and constant temperature 2 hours obtains high temperature resistance protective layer.The surface hardness of test high temperature resistance protective layer, test result is listed in table 2.
Embodiment 4
1, getting the 32wt% granularity is that the granularity of 200 purpose zinc powders, 36wt% is that 200 purpose aluminium powders, 32wt% granularity are 200 purpose titanium valves, and uniform mixing obtains the diffusion medium powder; Getting the diffusion medium for preparing and carbon fiber heat insulation layer puts into vacuum and oozes stove altogether, and the carbon fiber heat insulation layer is embedded in the diffusion medium, the volume ratio of diffusion medium and workpiece is 1: 1, vacuum oven is evacuated to vacuum tightness less than 0.5kPa, vacuum is oozed stove altogether be warming up to 400 ℃, vacuum flue per minute changes 3 circles, be incubated after 8 hours, the carbon fiber heat insulation layer is taken out, clean up, dry.
Sampling is tested, and forms the about 75 microns alloy preservative coat of thickness at the carbon fiber heat insulation laminar surface.The hardness of beta alloy preservative coat and erosion resistance, test result is listed in table 1.
2, potassium silicofluoride and tannic acid are mixed according to 1.5: 1 weight ratio, putting into dispersion machine after the mixing stirs, the amount of potassium silicofluoride and tannic acid is the 1wt% of heat insulating and corrosion coating, at 15 ℃, under the condition of relative humidity 70%, the mixture that stirs is applied to the surface of carbon fiber heat insulation layer.
3, being that the amount of 63wt% takes by weighing graphene powder according to content in the heat insulating and corrosion layer, is that the amount of 35wt% takes by weighing La according to content in the heat insulating and corrosion layer
2NiO
4Powder; According to content in the corrosion-resistant finishes is that the amount of 1wt% takes by weighing potash water glass.Above material is put into dispersion machine mix, be applied to the surface of the carbon fiber heat insulation layer that was coated with potassium silicofluoride and tannic acid, evenly smear, the thickness unanimity, coat-thickness is 1.5mm.
4, the carbon fiber heat insulation layer of coating alloy preservative coat and heat insulating and corrosion layer more than the general is put into vacuum furnace, is heated to 80 ℃ under vacuum state, and constant temperature 2 hours obtains high temperature resistance protective layer.The surface hardness of test high temperature resistance protective layer, test result is listed in table 2.
The hardness of table 1 alloy preservative coat and erosion resistance test result
1.2g/L Ca (OH)
2Condition 1.2g/L Ca (OH)
2Condition 1.2g/L Ca (OH)
2The condition alkali resistance
Down, under the nondiscoloration of 167h rete, under the nondiscoloration of 172h rete, the nondiscoloration of 193h rete
By above result as can be known, high temperature resistance protective layer provided by the invention has erosion resistance and hardness preferably, and then guarantees that the carbon fiber heat insulation layer is difficult for being corroded, and character is difficult for changing, and has prolonged the work-ing life of carbon fiber heat insulation layer.
The explanation of above embodiment just is used for helping to understand method of the present invention and core concept thereof.Should be pointed out that for those skilled in the art, under the prerequisite that does not break away from the principle of the invention, can also carry out some improvement and modification to the present invention, these improvement and modification also fall in the protection domain of claim of the present invention.
To the above-mentioned explanation of the disclosed embodiments, make this area professional and technical personnel can realize or use the present invention.Multiple modification to these embodiment will be conspicuous concerning those skilled in the art, and defined herein General Principle can realize under the situation that does not break away from the spirit or scope of the present invention in other embodiments.Therefore, the present invention will can not be restricted to these embodiment shown in this article, but will meet and principle disclosed herein and features of novelty the wideest corresponding to scope.
Claims (10)
1. a corrosion-resistant finishes that is used for polycrystalline silicon ingot or purifying furnace is characterized in that, comprising: the alloy preservative coat and the heat insulating and corrosion layer that is overlying on described alloy preservative coat surface that are overlying on the carbon fiber heat insulation laminar surface;
Described alloy preservative coat comprises: the titanium valve of the aluminium powder of 20wt%～38wt%, the zinc powder of 30wt%～45wt% and 30wt%～45wt%;
Described heat insulating and corrosion layer comprises: the Graphene powder of 55wt%～72wt%, the La of 25wt%～40wt%
2NiO
4The mixture of the membrane-forming agent of powder, 1wt%～5wt% and the solidifying agent of 1wt%～5wt% and dispersion agent.
2. corrosion-resistant finishes according to claim 1 is characterized in that, the content of graphene powder is 62wt%～68wt% in the described heat insulating and corrosion layer.
3. corrosion-resistant finishes according to claim 1 is characterized in that, the particle diameter of zinc powder, aluminium powder and titanium valve is 100 orders～300 orders in the described alloy preservative coat.
4. corrosion-resistant finishes according to claim 1 is characterized in that, described membrane-forming agent is a water glass.
5. corrosion-resistant finishes according to claim 1 is characterized in that, described solidifying agent is a silicofluoride.
6. corrosion-resistant finishes according to claim 5 is characterized in that, described dispersion agent is a tannic acid.
7. corrosion-resistant finishes according to claim 6 is characterized in that, the weight ratio of described silicofluoride and tannic acid is 1: 1～2: 1.
8. a high temperature resistance protective layer that is used for polycrystalline silicon ingot or purifying furnace is characterized in that, comprises the carbon fiber heat insulation layer and is overlying on each described corrosion-resistant finishes in the claim 1 to 7 of described carbon fiber heat insulation laminar surface.
9. the preparation method of the described high temperature resistance protective layer of claim 8 is characterized in that, may further comprise the steps:
1) after being mixed in proportion, aluminium powder, zinc powder and titanium valve obtain the diffusion medium powder, the carbon fiber heat insulation layer is embedded in is heated to 300 ℃～500 ℃ in the described diffusion medium powder, take out after being incubated 2 hours～5 hours, obtain the carbon fiber heat insulation layer that the surface is covered with the alloy preservative coat;
2) mixture of solidifying agent and dispersion agent is applied to the surface of described alloy preservative coat;
3) with Graphene powder, La
2NiO
4After being mixed in proportion, powder and membrane-forming agent be applied to the surface of solidifying agent and dispersion agent;
4) will under vacuum state, be heated to 70 ℃～85 ℃ through the carbon fiber heat insulation layer that step 3) is handled, constant temperature 1.5～3 hours.
10. the preparation method of high temperature resistance protective layer according to claim 9 is characterized in that, described step 2) in, 10 ℃～100 ℃ of envrionment temperatures, under the condition of relative humidity＜90% solidifying agent and dispersion agent are applied to the surface of described alloy preservative coat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110091484 CN102199373B (en) | 2011-04-12 | 2011-04-12 | Graphite alkene-La2NiO4/zinc-aluminum-titanium series corrosion-resistance coating for polycrystalline silicon ingot casting furnace |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110091484 CN102199373B (en) | 2011-04-12 | 2011-04-12 | Graphite alkene-La2NiO4/zinc-aluminum-titanium series corrosion-resistance coating for polycrystalline silicon ingot casting furnace |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102199373A true CN102199373A (en) | 2011-09-28 |
| CN102199373B CN102199373B (en) | 2012-12-19 |
Family
ID=44660376
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201110091484 Expired - Fee Related CN102199373B (en) | 2011-04-12 | 2011-04-12 | Graphite alkene-La2NiO4/zinc-aluminum-titanium series corrosion-resistance coating for polycrystalline silicon ingot casting furnace |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102199373B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103740153A (en) * | 2013-11-12 | 2014-04-23 | 宁波墨西科技有限公司 | Graphene-modified Dacromet coating material |
| CN103740152A (en) * | 2013-11-12 | 2014-04-23 | 宁波墨西科技有限公司 | Graphene-modified chromium-free Dacromet coating material |
| CN105666693A (en) * | 2016-02-29 | 2016-06-15 | 中山市翔实机械设备有限公司 | Cement paste stirring device |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080295294A1 (en) * | 2007-06-01 | 2008-12-04 | Gt Solar Incorporated | Processing of fine silicon powder to produce bulk silicon |
| CN101570651A (en) * | 2009-05-13 | 2009-11-04 | 英利能源（中国）有限公司 | Corrosion-resistance coating of polysilicon ingot furnace, high temperature resistance protective layer and preparation method thereof |
| CN101638322A (en) * | 2009-05-15 | 2010-02-03 | 西安超码科技有限公司 | Method for preparing carbon/carbon heat shields used for polysilicon hydriding furnances |
| CN101643933A (en) * | 2009-08-19 | 2010-02-10 | 蒋建纯 | CZ method silicon single crystal growth furnace quartz crucible carbon protection crucible and manufacturing process thereof |
| CN101886291A (en) * | 2010-07-13 | 2010-11-17 | 王敬 | Heat insulating cage and ingot casting furnace with same |
-
2011
- 2011-04-12 CN CN 201110091484 patent/CN102199373B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080295294A1 (en) * | 2007-06-01 | 2008-12-04 | Gt Solar Incorporated | Processing of fine silicon powder to produce bulk silicon |
| CN101570651A (en) * | 2009-05-13 | 2009-11-04 | 英利能源（中国）有限公司 | Corrosion-resistance coating of polysilicon ingot furnace, high temperature resistance protective layer and preparation method thereof |
| CN101638322A (en) * | 2009-05-15 | 2010-02-03 | 西安超码科技有限公司 | Method for preparing carbon/carbon heat shields used for polysilicon hydriding furnances |
| CN101643933A (en) * | 2009-08-19 | 2010-02-10 | 蒋建纯 | CZ method silicon single crystal growth furnace quartz crucible carbon protection crucible and manufacturing process thereof |
| CN101886291A (en) * | 2010-07-13 | 2010-11-17 | 王敬 | Heat insulating cage and ingot casting furnace with same |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103740153A (en) * | 2013-11-12 | 2014-04-23 | 宁波墨西科技有限公司 | Graphene-modified Dacromet coating material |
| CN103740152A (en) * | 2013-11-12 | 2014-04-23 | 宁波墨西科技有限公司 | Graphene-modified chromium-free Dacromet coating material |
| CN103740152B (en) * | 2013-11-12 | 2016-02-03 | 宁波墨西科技有限公司 | A kind of chromium-free Dyclo paint of Graphene modification |
| CN103740153B (en) * | 2013-11-12 | 2016-02-03 | 宁波墨西科技有限公司 | A kind of Dyclo paint of Graphene modification |
| CN105666693A (en) * | 2016-02-29 | 2016-06-15 | 中山市翔实机械设备有限公司 | Cement paste stirring device |
| CN105666693B (en) * | 2016-02-29 | 2017-10-13 | 中山市翔实机械设备有限公司 | A kind of cement mortar agitating device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102199373B (en) | 2012-12-19 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102199372B (en) | Graphene-La2Ti2O7/zinc-aluminum-zirconium corrosion resisting coating for polycrystalline silicon ingot casting furnace | |
| Fu et al. | Hydrothermal synthesis of pollucite from metakaolin-based geopolymer for hazardous wastes storage | |
| CN101570651B (en) | Corrosion-resistance coating of polysilicon ingot furnace, high temperature resistance protective layer and preparation method thereof | |
| CN103469207A (en) | High-temperature oxidation resistant and corrosion resistant glass ceramic composite coating and preparation technology thereof | |
| CN103388142B (en) | A kind of method of diamond surface plating tungsten | |
| CN104445951B (en) | Compound enamel coating of a kind of heat and corrosion resistant and preparation method thereof | |
| CN112853260B (en) | Preparation method of powder embedding infiltration coating | |
| CN102368411B (en) | Preparation method of aluminum-boron alloy powder and aluminum-boron slurry of crystalline silicon cell | |
| CN102199373B (en) | Graphite alkene-La2NiO4/zinc-aluminum-titanium series corrosion-resistance coating for polycrystalline silicon ingot casting furnace | |
| CN102225650B (en) | Graphene-LaTaO4/zinc-aluminum-nickel system corrosion resisting coating used for polysilicon ingot furnaces | |
| CN102522156A (en) | Preparation method of aluminum boron slurry for crystalline silicon solar battery | |
| CN101367520A (en) | Preparation method for nano- zirconium carbide material | |
| CN102225652B (en) | Grapheme-La2Si2O7/zinc-alumnium-magnesium anticorrosion coating for polycrystalline silicon ingot furnace | |
| CN102225651B (en) | Grapheme-Sr3Ti2O7/zinc-aluminum-zirconium corrosion resistant coating for polysilicon ingot furnace | |
| CN114672233A (en) | Photothermal super-hydrophobic coating based on MXene @ Au hybrid and preparation method thereof | |
| CN102250545B (en) | High temperature resistant antistatic coating and preparation method thereof | |
| Hong et al. | Evaluation of 316L stainless mill additives on microstructure and alkali corrosive behavior of enamel coatings | |
| CN102503562B (en) | Preparation method of carbon/carbon composite material anti-oxidation phosphate glass coating | |
| WO1998046539A1 (en) | High-radiation glass base covering material, high-radiation glass film, and process for the production of high-radiation glass film | |
| CN114853494A (en) | Composite ceramic powder with self-repairing capability and preparation method and application thereof | |
| CN109778251B (en) | Preparation method of composite coating structure and composite coating structure obtained by same | |
| CN207193380U (en) | Titanium-aluminium alloy part with compisite seeping layer, the titanium-aluminium alloy part with diamond coatings | |
| CN1268580C (en) | Method for preparing SIC micro nano ceramic powder via refinery coke salt bath synthesis | |
| CN111455253A (en) | Titanium carbide-based metal ceramic thermal spraying powder and preparation method thereof | |
| Guo et al. | Effect of MoO3/WO3 modulation on high-temperature wettability and crystallization behavior of glass and its application in solar cell |
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 | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121219 Termination date: 20140412 |