CN112341171A - Preparation method of silicon sintering crucible for induction furnace lining - Google Patents
Preparation method of silicon sintering crucible for induction furnace lining Download PDFInfo
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- CN112341171A CN112341171A CN202011335851.3A CN202011335851A CN112341171A CN 112341171 A CN112341171 A CN 112341171A CN 202011335851 A CN202011335851 A CN 202011335851A CN 112341171 A CN112341171 A CN 112341171A
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- 230000006698 induction Effects 0.000 title claims abstract description 30
- 238000002360 preparation method Methods 0.000 title claims abstract description 10
- 238000005245 sintering Methods 0.000 title claims abstract description 8
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 title claims description 6
- 229910052710 silicon Inorganic materials 0.000 title claims description 6
- 239000010703 silicon Substances 0.000 title claims description 6
- 239000000463 material Substances 0.000 claims abstract description 79
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 50
- 239000000377 silicon dioxide Substances 0.000 claims abstract description 22
- 238000010304 firing Methods 0.000 claims abstract description 15
- 238000000034 method Methods 0.000 claims abstract description 14
- 239000002245 particle Substances 0.000 claims abstract description 7
- 239000011230 binding agent Substances 0.000 claims abstract description 5
- 238000002156 mixing Methods 0.000 claims description 8
- 235000008733 Citrus aurantifolia Nutrition 0.000 claims description 6
- 235000011941 Tilia x europaea Nutrition 0.000 claims description 6
- 238000001816 cooling Methods 0.000 claims description 6
- 238000001035 drying Methods 0.000 claims description 6
- 239000004571 lime Substances 0.000 claims description 6
- 239000008267 milk Substances 0.000 claims description 6
- 210000004080 milk Anatomy 0.000 claims description 6
- 235000013336 milk Nutrition 0.000 claims description 6
- 238000003825 pressing Methods 0.000 claims description 6
- 239000011449 brick Substances 0.000 claims description 5
- 238000000465 moulding Methods 0.000 claims description 5
- 238000007873 sieving Methods 0.000 claims description 5
- 238000003826 uniaxial pressing Methods 0.000 claims 1
- 230000035939 shock Effects 0.000 abstract description 8
- 238000003723 Smelting Methods 0.000 abstract description 4
- 238000009991 scouring Methods 0.000 abstract description 3
- 239000002893 slag Substances 0.000 abstract description 3
- 239000012535 impurity Substances 0.000 abstract description 2
- 230000007774 longterm Effects 0.000 abstract description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 239000002994 raw material Substances 0.000 abstract 1
- 238000010438 heat treatment Methods 0.000 description 10
- 239000010431 corundum Substances 0.000 description 8
- 229910052593 corundum Inorganic materials 0.000 description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 7
- 239000011248 coating agent Substances 0.000 description 7
- 238000000576 coating method Methods 0.000 description 7
- 229910052802 copper Inorganic materials 0.000 description 7
- 239000010949 copper Substances 0.000 description 7
- 239000011162 core material Substances 0.000 description 5
- 238000010586 diagram Methods 0.000 description 5
- 239000000956 alloy Substances 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 4
- 238000005056 compaction Methods 0.000 description 4
- 238000011049 filling Methods 0.000 description 4
- 238000000462 isostatic pressing Methods 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 239000010453 quartz Substances 0.000 description 3
- 238000004381 surface treatment Methods 0.000 description 3
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 230000003628 erosive effect Effects 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910052905 tridymite Inorganic materials 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000007767 bonding agent Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
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- 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
- C04B35/14—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 silica
-
- 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
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/74—Physical characteristics
- C04B2235/77—Density
-
- 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
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/96—Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
-
- 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
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/96—Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
- C04B2235/9607—Thermal properties, e.g. thermal expansion coefficient
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Compositions Of Oxide Ceramics (AREA)
- Crucibles And Fluidized-Bed Furnaces (AREA)
Abstract
The invention provides a preparation method of a siliceous firing crucible for an induction furnace lining, belonging to the field of high-temperature structural materials. High-quality silica mined from mines is used as a raw material, and is crushed, sieved to obtain materials with the particle size of 8-6mm, 5-4mm, 3-2mm, 1-0.074mm and the particle size of less than 200 meshes, and the materials are mixed with a binding agent, molded, dried and sintered to obtain the siliceous firing crucible. Compared with the prior art, the lining material of the siliceous sintering crucible prepared by the invention has low impurity content, obviously improves the anti-erosion capability of the lining material in the smelting process, effectively prevents high-temperature melt from scouring the lining material and slag, prolongs the service life of the induction furnace, greatly improves the thermal shock resistance of the material, ensures that the product quality is more stable and reliable, realizes long-term stable production operation in the furnace, improves the working efficiency and increases the profit of enterprises.
Description
Technical Field
The invention belongs to the field of high-temperature structural materials, and particularly relates to a preparation method of a silica crucible for an induction furnace lining.
Background
Induction furnaces have been widely used in industrial production as melting equipment for melting high temperature alloys and special alloys because of their advantages of high melting speed, high temperature of the molten metal, uniform chemical composition, etc. The furnace lining is one of the important components of the induction furnace, not only plays a role of supporting a container, but also participates in the metallurgical physical and chemical reaction processes, and has important influence on the safe and stable operation of the intermediate frequency induction furnace and the quality of steel. Because the operating temperature of the alloy is high in the smelting process, the furnace lining is in a complex and severe working environment for a long time, and the high-temperature liquid is subjected to the scouring of the inner wall and the erosion of slag for a long time, so that the service life of the alloy is shortened, and the quality of the melt is reduced. Therefore, the selection of furnace lining materials and the preparation process directly influence the service life and the generation efficiency of the induction furnace. At present, corundum crucibles, magnesium crucibles and the like are generally used as lining materials of induction furnaces, and although the corundum crucibles, the magnesium crucibles and the like have the characteristics of high refractoriness, stable chemical properties and high strength, the anti-corrosion effect is not ideal in the repeated use process under the harsh smelting environment, and the furnace body needs to be further improved in use. Therefore, the method for preparing the high-performance induction furnace lining material is always concerned by domestic and foreign enterprises.
Disclosure of Invention
The invention aims to overcome the defects of the prior art and provides a preparation method of a siliceous crucible fired by silicon for an induction furnace lining, which has good strength and excellent thermal shock resistance and erosion resistance.
In order to achieve the purpose, the technical scheme of the invention is as follows:
a preparation method of a silicon sintering crucible for an induction furnace lining is characterized by comprising the following steps:
(1) crushing high-quality silica mined in a mine to obtain a silica block material;
(2) sieving the silica block to obtain materials with particle sizes of 8-6mm, 5-4mm, 3-2mm, 1-0.074mm and below 200 meshes;
(3) mixing 15-25% of material with the granularity of 8-6mm, 15-25% of material with the granularity of 5-4mm, 15-25% of material with the granularity of 3-2mm, 15-25% of material with the granularity of 1-0.074mm, 20-30% of material with the granularity of less than 200 meshes and 2-5% of binding agent for 5-30min by mass percentage to obtain mixed material;
(4) placing the mixed material into a mold, and performing mechanical pressing molding at the pressure of 100-300MPa to obtain a molded blank body;
(5) drying the formed blank at the temperature of 100-200 ℃ for 24-40h to obtain a dried formed blank;
(6) and (3) firing the dried and molded blank at the temperature of 1400 ℃ and 1450 ℃ for 5-10h, and naturally cooling along with the furnace to obtain the siliceous firing crucible.
SiO in the high-quality silica in the step (1)2The content is more than 98 percent.
The binding agent in the step (3) is lime milk with the concentration of 20-50%.
The mixing equipment in the step (3) is a wet mill or a high-speed mixer.
The forming equipment in the step (4) is a single-shaft pressing brick machine or an isostatic pressing machine.
In the process of preparing the lining material of the siliceous sintering crucible, quartz can generate complex polycrystalline transformation, and the residual expansion can cause the joint cutting to be tightly adhered along with volume expansion, thereby ensuring that the material has good air tightness and bonding strength. The main crystal phase of the quartz in the material is tridymite which has a spearhead-shaped double-crystal interlaced network structure, and the thermal shock resistance and the mechanical strength of the product can be effectively improved. Meanwhile, a certain amount of bonding agent is introduced to promote the formation of tridymite phase, inhibit the quantity of cristobalite and residual quartz phase, and prevent the phenomena of product loosening and cracking in the sintering process.
Compared with the prior art, the invention has the beneficial effects that: the furnace lining material of the siliceous sintering crucible has low impurity content, obviously improves the anti-erosion capability of the furnace lining material in the smelting process, effectively prevents high-temperature melt from scouring the furnace lining material and slag, prolongs the service life of an induction furnace, greatly improves the thermal shock resistance of the material, ensures that the product quality is more stable and reliable, realizes long-term stable production operation in the furnace, improves the working efficiency and increases the enterprise profit.
Drawings
FIG. 1 is a process flow chart of the preparation of a siliceous firing crucible for an induction furnace lining according to an embodiment of the present invention.
FIG. 2 is a structural diagram of an induction furnace according to an embodiment of the present invention.
FIG. 3 is the isostatic compaction process diagram of the siliceous calcined crucible lining material of the present invention.
In the figure: 21-siliceous firing crucible, 22-coating material, 23-heating copper sleeve, 24-rotating structure, 25-siliceous filling material, 31-lock catch, 32-metal core material, 33-isostatic pressing rubber outer sleeve and 34-forming material.
Detailed Description
The preparation process of the present invention is further illustrated by the following examples:
comparative example
Putting 25kg of corundum with the granularity of 8-6mm, 15kg of corundum with the granularity of 5-4mm, 20kg of corundum with the granularity of 3-2mm, 20kg of corundum with the granularity of 1-0.074mm, 20kg of corundum with the granularity of below 200 meshes and 3kg of lime milk with the concentration of 35% into a wet mill, and jointly mixing for 5min to obtain a mixed material; putting the mixed material into a die of a uniaxial pressure brick press, and performing mechanical pressing molding under 200MPa to obtain a molded green body; drying the formed blank at 150 ℃ for 30h to obtain a dried formed blank; and firing the dried and molded blank at 1400 ℃ for 5h, and naturally cooling along with the furnace to obtain the corundum crucible.
The siliceous calcined crucible lining prepared by the comparative example has the high-temperature rupture strength of 5.9MPa, the thermal shock times of 12 times and the bulk density of 2.23g/cm3。
Example 1
Crushing high-quality silica mined in a mine to obtain a silica block material; sieving the silica block to obtain materials with particle sizes of 8-6mm, 5-4mm, 3-2mm, 1-0.074mm and below 200 meshes; putting 25kg of materials with the granularity of 8-6mm, 15kg of materials with the granularity of 5-4mm, 20kg of materials with the granularity of 3-2mm, 20kg of materials with the granularity of 1-0.074mm, 20kg of materials with the granularity of less than 200 meshes and 3kg of lime milk with the concentration of 35% into a wet mill, and jointly mixing for 5min to obtain a mixed material; putting the mixed material into a die of a uniaxial pressure brick press, and performing mechanical pressing molding under 200MPa to obtain a molded green body; drying the formed blank at 150 ℃ for 30h to obtain a dried formed blank; and (3) firing the dried and molded blank at 1400 ℃ for 5h, and naturally cooling along with the furnace to obtain the siliceous firing crucible.
According to the structure diagram of the induction furnace shown in figure 2, induction heating is arranged and fixed on a rotating mechanism, a fired siliceous crucible is arranged in a heating copper sleeve, siliceous filling material is filled in a crack between the copper sleeve and the fired siliceous crucible, after compaction, coating material is coated in a gap between the fired siliceous crucible and a furnace opening, the surface treatment is smooth, and the coating thickness is 50 mm. And an induction heating device is used after the furnace is burnt.
The siliceous calcined crucible lining prepared in the example has the high-temperature rupture strength of 6.5MPa, the thermal shock times of 14 times and the bulk density of 2.25g/cm3。
Example 2
Crushing high-quality silica mined in a mine to obtain a silica block material; sieving the silica block to obtain materials with particle sizes of 8-6mm, 5-4mm, 3-2mm, 1-0.074mm and below 200 meshes; putting 18kg of materials with the granularity of 8-6mm, 20kg of materials with the granularity of 5-4mm, 20kg of materials with the granularity of 3-2mm, 22kg of materials with the granularity of 1-0.074mm, 20kg of materials with the granularity of less than 200 meshes and 4kg of lime milk with the concentration of 25% into a wet mill, and jointly mixing for 15min to obtain a mixed material; putting the mixed material into a mould for isostatic pressing, wherein the structure of the mould comprises a metal core material, an outer sleeve of isostatic pressing rubber, a lock catch and the material; the operation process comprises the steps of placing materials in a rubber sleeve, then placing a metal core in the inner side of the rubber sleeve, vibrating the core material into the materials in a vibration mode, distributing the materials in a crack of a core liner of the outer sleeve, then clamping a lock catch, placing the integral structure in an isostatic pressure container, pressurizing to 200MPa, and then demolding to obtain a molded blank (as shown in figure 3); drying the formed blank at 150 ℃ for 30h to obtain a dried formed blank; and (3) firing the dried and molded blank body for 8 hours at 1450 ℃, and naturally cooling along with the furnace to obtain the siliceous firing crucible.
According to the structure diagram of the induction furnace shown in figure 2, induction heating is arranged and fixed on a rotating mechanism, a fired siliceous crucible is arranged in a heating copper sleeve, siliceous filling material is filled in a crack between the copper sleeve and the fired siliceous crucible, after compaction, coating material is coated in a gap between the fired siliceous crucible and a furnace opening, the surface treatment is smooth, and the coating thickness is 75 mm. And an induction heating device is used after the furnace is burnt.
The siliceous calcined crucible lining prepared in the example has a high-temperature rupture strength of 5.2MPa, a thermal shock frequency of 12 times and a bulk density of 2.32g/cm3。
Example 3
Crushing high-quality silica mined in a mine to obtain a silica block material; sieving the silica block to obtain materials with particle sizes of 8-6mm, 5-4mm, 3-2mm, 1-0.074mm and below 200 meshes; putting 20kg of materials with the granularity of 8-6mm, 20kg of materials with the granularity of 5-4mm, 15kg of materials with the granularity of 3-2mm, 25kg of materials with the granularity of 1-0.074mm, 20kg of materials with the granularity of less than 200 meshes and 5kg of lime milk with the concentration of 20% into a high-speed mixing roll to be mixed for 25min together to obtain mixed materials; putting the mixed material into a die of a uniaxial pressure brick press, and performing mechanical pressing molding under 280MPa to obtain a molded green body; drying the formed blank at 200 ℃ for 35h to obtain a dried formed blank; and (3) firing the dried and molded blank at 1450 ℃ for 7h, and naturally cooling the blank along with the furnace to obtain the siliceous firing crucible.
According to the structure diagram of the induction furnace shown in figure 2, induction heating is arranged and fixed on a rotating mechanism, a fired siliceous crucible is arranged in a heating copper sleeve, siliceous filling material is filled in a crack between the copper sleeve and the fired siliceous crucible, after compaction, coating material is coated in a gap between the fired siliceous crucible and a furnace opening, the surface treatment is smooth, and the coating thickness is 65 mm. And an induction heating device is used after the furnace is burnt.
The siliceous calcined crucible lining prepared in the example has the high-temperature rupture strength of 4.43MPa, the thermal shock times of 10 times and the bulk density of 2.22g/cm3。
Claims (5)
1. A preparation method of a silicon sintering crucible for an induction furnace lining is characterized by comprising the following steps:
(1) crushing high-quality silica mined in a mine to obtain a silica block material;
(2) sieving the silica block to obtain materials with particle sizes of 8-6mm, 5-4mm, 3-2mm, 1-0.074mm and below 200 meshes;
(3) mixing 15-25% of material with the granularity of 8-6mm, 15-25% of material with the granularity of 5-4mm, 15-25% of material with the granularity of 3-2mm, 15-25% of material with the granularity of 1-0.074mm, 20-30% of material with the granularity of less than 200 meshes and 2-5% of binding agent for 5-30min by mass percentage to obtain mixed material;
(4) placing the mixed material into a mold, and performing mechanical pressing molding at the pressure of 100-300MPa to obtain a molded blank body;
(5) drying the formed blank at the temperature of 100-200 ℃ for 24-40h to obtain a dried formed blank;
(6) and (3) firing the dried and molded blank at the temperature of 1400 ℃ and 1450 ℃ for 5-10h, and naturally cooling along with the furnace to obtain the siliceous firing crucible.
2. The method for preparing the silica crucible for an induction furnace lining according to claim 1, wherein SiO in the high-quality silica in the step (1)2The content is more than 98 percent.
3. The method for preparing the silica crucible for the induction furnace lining according to claim 1, wherein the binder in the step (3) is lime milk with a concentration of 20-50%.
4. The method for preparing the silicon crucible for induction furnace lining according to claim 1, wherein the mixing device in the step (3) is a wet mill or a high-speed mixer.
5. The method for preparing the silica crucible for the induction furnace lining according to claim 1, wherein the forming device in the step (4) is a uniaxial pressing brick press or an isostatic press.
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---|---|---|---|---|
US20020094930A1 (en) * | 1998-10-09 | 2002-07-18 | Brown John T. | Alkali resistant silica refractory brick, method for producing the same and glass manufacturing furnace containing the same |
CN102126866A (en) * | 2011-04-06 | 2011-07-20 | 瑞泰科技股份有限公司 | High-purity silica refractory material and production process thereof |
CN102167606A (en) * | 2011-01-21 | 2011-08-31 | 武汉科技大学 | Silica brick and preparation method thereof |
CN105000896A (en) * | 2015-07-23 | 2015-10-28 | 郑州市科源耐火材料有限公司 | Universal siliceous castable |
CN105272290A (en) * | 2015-10-13 | 2016-01-27 | 中钢集团耐火材料有限公司 | Preparation method of anti-erosion silica brick for carbon calcination furnace |
CN111675544A (en) * | 2020-05-26 | 2020-09-18 | 襄阳聚力新材料科技有限公司 | Acid furnace lining material for ultra-high temperature environment and preparation method thereof |
-
2020
- 2020-11-25 CN CN202011335851.3A patent/CN112341171A/en active Pending
Patent Citations (6)
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US20020094930A1 (en) * | 1998-10-09 | 2002-07-18 | Brown John T. | Alkali resistant silica refractory brick, method for producing the same and glass manufacturing furnace containing the same |
CN102167606A (en) * | 2011-01-21 | 2011-08-31 | 武汉科技大学 | Silica brick and preparation method thereof |
CN102126866A (en) * | 2011-04-06 | 2011-07-20 | 瑞泰科技股份有限公司 | High-purity silica refractory material and production process thereof |
CN105000896A (en) * | 2015-07-23 | 2015-10-28 | 郑州市科源耐火材料有限公司 | Universal siliceous castable |
CN105272290A (en) * | 2015-10-13 | 2016-01-27 | 中钢集团耐火材料有限公司 | Preparation method of anti-erosion silica brick for carbon calcination furnace |
CN111675544A (en) * | 2020-05-26 | 2020-09-18 | 襄阳聚力新材料科技有限公司 | Acid furnace lining material for ultra-high temperature environment and preparation method thereof |
Non-Patent Citations (1)
Title |
---|
中国冶金百科全书总编辑委员会《耐火材料》卷编辑委员会等: "《中国冶金百科全书:耐火材料》", 31 October 1997, 冶金工业出版社 * |
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Application publication date: 20210209 |