CN101428997A - High temperature abrasion-proof paint and method for producing the same - Google Patents
High temperature abrasion-proof paint and method for producing the same Download PDFInfo
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- CN101428997A CN101428997A CNA2008102430117A CN200810243011A CN101428997A CN 101428997 A CN101428997 A CN 101428997A CN A2008102430117 A CNA2008102430117 A CN A2008102430117A CN 200810243011 A CN200810243011 A CN 200810243011A CN 101428997 A CN101428997 A CN 101428997A
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- 238000004519 manufacturing process Methods 0.000 title abstract description 9
- 239000003973 paint Substances 0.000 title description 3
- 239000000463 material Substances 0.000 claims abstract description 95
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 claims abstract description 70
- 239000000843 powder Substances 0.000 claims abstract description 39
- 229910052593 corundum Inorganic materials 0.000 claims abstract description 30
- 239000010431 corundum Substances 0.000 claims abstract description 30
- 229910052845 zircon Inorganic materials 0.000 claims abstract description 19
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims abstract description 19
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims abstract description 18
- 239000004568 cement Substances 0.000 claims abstract description 11
- WNROFYMDJYEPJX-UHFFFAOYSA-K aluminium hydroxide Chemical compound [OH-].[OH-].[OH-].[Al+3] WNROFYMDJYEPJX-UHFFFAOYSA-K 0.000 claims abstract description 10
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims abstract description 10
- XFWJKVMFIVXPKK-UHFFFAOYSA-N calcium;oxido(oxo)alumane Chemical compound [Ca+2].[O-][Al]=O.[O-][Al]=O XFWJKVMFIVXPKK-UHFFFAOYSA-N 0.000 claims abstract description 10
- 238000002360 preparation method Methods 0.000 claims abstract description 7
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 claims description 40
- 238000005299 abrasion Methods 0.000 claims description 28
- 238000003723 Smelting Methods 0.000 claims description 19
- RFAFBXGYHBOUMV-UHFFFAOYSA-N calcium chromate Chemical compound [Ca+2].[O-][Cr]([O-])(=O)=O RFAFBXGYHBOUMV-UHFFFAOYSA-N 0.000 claims description 19
- 229910052727 yttrium Inorganic materials 0.000 claims description 19
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims description 19
- 229910000147 aluminium phosphate Inorganic materials 0.000 claims description 18
- 239000011863 silicon-based powder Substances 0.000 claims description 17
- 235000019832 sodium triphosphate Nutrition 0.000 claims description 16
- 238000002156 mixing Methods 0.000 claims description 15
- 239000002245 particle Substances 0.000 claims description 15
- 229910021502 aluminium hydroxide Inorganic materials 0.000 claims description 9
- 101710194948 Protein phosphatase PhpP Proteins 0.000 claims description 8
- 238000010276 construction Methods 0.000 claims description 8
- HWGNBUXHKFFFIH-UHFFFAOYSA-I pentasodium;[oxido(phosphonatooxy)phosphoryl] phosphate Chemical compound [Na+].[Na+].[Na+].[Na+].[Na+].[O-]P([O-])(=O)OP([O-])(=O)OP([O-])([O-])=O HWGNBUXHKFFFIH-UHFFFAOYSA-I 0.000 claims description 8
- 238000007639 printing Methods 0.000 claims description 8
- 239000011734 sodium Substances 0.000 claims description 8
- 229910052708 sodium Inorganic materials 0.000 claims description 8
- UNXRWKVEANCORM-UHFFFAOYSA-I triphosphate(5-) Chemical compound [O-]P([O-])(=O)OP([O-])(=O)OP([O-])([O-])=O UNXRWKVEANCORM-UHFFFAOYSA-I 0.000 claims description 8
- INJRKJPEYSAMPD-UHFFFAOYSA-N aluminum;silicic acid;hydrate Chemical compound O.[Al].[Al].O[Si](O)(O)O INJRKJPEYSAMPD-UHFFFAOYSA-N 0.000 claims description 7
- 238000006243 chemical reaction Methods 0.000 claims description 7
- 239000000428 dust Substances 0.000 claims description 7
- 239000010443 kyanite Substances 0.000 claims description 7
- 229910052850 kyanite Inorganic materials 0.000 claims description 7
- 239000011248 coating agent Substances 0.000 abstract description 6
- 238000000576 coating method Methods 0.000 abstract description 6
- 239000011819 refractory material Substances 0.000 abstract description 5
- 239000011449 brick Substances 0.000 abstract description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 abstract 2
- BCFSVSISUGYRMF-UHFFFAOYSA-N calcium;dioxido(dioxo)chromium;dihydrate Chemical compound O.O.[Ca+2].[O-][Cr]([O-])(=O)=O BCFSVSISUGYRMF-UHFFFAOYSA-N 0.000 abstract 2
- 229910052726 zirconium Inorganic materials 0.000 abstract 2
- 238000005266 casting Methods 0.000 abstract 1
- 239000000446 fuel Substances 0.000 abstract 1
- 229910052710 silicon Inorganic materials 0.000 abstract 1
- 239000010703 silicon Substances 0.000 abstract 1
- 229910000162 sodium phosphate Inorganic materials 0.000 abstract 1
- 239000001488 sodium phosphate Substances 0.000 abstract 1
- ISIJQEHRDSCQIU-UHFFFAOYSA-N tert-butyl 2,7-diazaspiro[4.5]decane-7-carboxylate Chemical compound C1N(C(=O)OC(C)(C)C)CCCC11CNCC1 ISIJQEHRDSCQIU-UHFFFAOYSA-N 0.000 abstract 1
- RYFMWSXOAZQYPI-UHFFFAOYSA-K trisodium phosphate Chemical compound [Na+].[Na+].[Na+].[O-]P([O-])([O-])=O RYFMWSXOAZQYPI-UHFFFAOYSA-K 0.000 abstract 1
- 239000012530 fluid Substances 0.000 description 10
- 239000012467 final product Substances 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 4
- 230000035939 shock Effects 0.000 description 3
- 238000007873 sieving Methods 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 239000003082 abrasive agent Substances 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 238000003303 reheating Methods 0.000 description 2
- 238000003756 stirring Methods 0.000 description 2
- 238000005303 weighing Methods 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 239000002817 coal dust Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 235000013312 flour Nutrition 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Compositions Of Oxide Ceramics (AREA)
Abstract
The invention relates to a 318 high-temperature wear-resistant coating and a preparation method thereof, in particular to a rapid repair material for repairing various abrasive bricks and wear-resistant casting damage positions in circulating fluidized bed boilers of fuel electric plants. At the same time, the invention provides a method for producing the high-temperature wear-resistant coating, and belongs to the technical field of refractory material. The rapid repair material consists of a material A and a material B according to the weight portion proportion of 70-85 to 30-15, wherein the material A is prepared by zircon corundum, fine corundum powder, cyanite, yttrium-stabilized zirconium, silicon micropowder, alumina micropowder, pure calcium aluminate cement, trimeric sodium phosphate, and fused calcium chromate; and the material B is prepared by phosphorous acid, ink grade aluminum hydroxide, zirconia ultrafine powder, yttrium-stabilized zirconium, and fused calcium chromate.
Description
Technical field
The present invention relates to a kind of 318 high temperature abrasion materials and preparation method thereof, be used to repair the rapid repair material of each abrasive brick, wear-resistant pouring damaged location in the circular fluid bed of specifically a kind of fuel-burning power plant, the manufacture method of this high temperature abrasion material is provided simultaneously.Belong to technical field of refractory materials.
Background technology
The circular fluid bed technology is the clean coal combustion technology of generally acknowledging at present, because circulating fluidized bed electricity generation boiler construction system complexity is great in constructing amount, and coal dust flow velocity height in the system pipeline, flow is big, therefore refractory materials is required excellent performance.But the refractory materials that uses in circular fluid bed at present adopts high alumina or fused corundom raw material, the cement content height, its wear resistance, anti-erosion, abrasion resistance and thermal shock resistance all can not satisfy the requirement of circular fluid bed technology, life cycle is short, need often to repair or change, influence the normal operation of circular fluid bed, consume a large amount of manpower and financial resources.
Summary of the invention
The present invention seeks at above-mentioned weak point, a kind of high temperature abrasion material and preparation method thereof is provided, it is the high temperature abrasion material of circular fluid bed, adopt zircon corundum, super-fine powder, 98 above dusts are agree silica flour, pure calcium aluminate cement, glossy black level aluminium hydroxide, yttrium base stabilised zirconia, compatibilities such as electric smelting yellow ultramarine, the wear resistance high-adhesion of refractory materials, resistance to fouling, abrasion resistance and thermal shock resistance excellence, life cycle can reach more than a year and a half, significantly reduce the turn(a)round of circular fluid bed, saved patching material, save baker material and furnace drying time, reduced running cost.
High temperature abrasion material and preparation method thereof is to take following technical scheme to realize:
High temperature abrasion material is characterized in that being made up of 70～85:30～15 by weight ratio first material and second material, wherein:
First material each component weight percent proportioning is
Zircon corundum particle diameter 1～3mm 15%～25%
Zircon corundum particle diameter 0.4～1mm 25%～35%
Corundum fine powder 15%～25%
No. three kyanites 10%～20% in river
Yttrium base stabilised zirconia 3%～9%
Silicon powder 3%～7%
Alumina powder 4%～8%
Pure calcium aluminate cement 3%～8%
Tripoly phosphate sodium STPP 0.1%～0.5%
Electric smelting yellow ultramarine 0.5%～2.5%
Wherein, The corundum fine powder fineness is 220～250 orders (sieving); No. three kyanite fineness in river are 180 orders～220 orders (sieving); Silicon powder adopts SI 〉=98% dust to agree silicon powder.
Second material each component weight percent proportioning is
Phosphoric acid 75%-85%
Printing ink level aluminium hydroxide 6%～15%
Ultrafine zirconia powder 5%～7%
Yttrium base stabilised zirconia 3%～8%
Electric smelting yellow ultramarine 0.3%～2.3%
Wherein: it is 85% phosphoric acid that phosphoric acid adopts concentration; The ultrafine zirconia powder fineness is 0.007～0.04mm (sieving).
The present invention selects zircon corundum as aggregate, powder, be because its apparent porosity less than 3%, volume density is greater than 3.3g/Cm
3, Mohs' hardness is higher than 10, and the volume density of product is improved, and shows porosity and reduces, and intensity significantly improves; Fine aluminium sour water mud can strengthen the avidity of synthetic material, and the effect that adds super-fine powder is to have increased fillibility, has improved application property, thereby makes its mobile increase.Because the first material increases yttrium base stabilised zirconia as raw material, can increase the coating high thermal resistance, stability, the first material adds the electric smelting yellow ultramarine, can increase coating high thermal resistance and paint adhesion intensity.The second material can further increase coating high thermal resistance, stability owing to add yttrium base stabilised zirconia, and the second material adds the electric smelting yellow ultramarine, can further increase coating high thermal resistance and paint adhesion intensity.High temperature abrasion material of the present invention and the high-abrasive material and the application number that use at present: the performance of 2007100235172 high temperature abrasion material patent application products compares: high temperature abrasion material of the present invention makes folding strength increase by 4～5 times, compressive strength increases nearly 2 times, and reheating linear change rate on reheating is reduced, volume density increases, and abrasion loss reduces greatly.
The preparation method of high temperature abrasion material of the present invention is with first material each component per distribution ratio weighing by weight: zircon corundum aggregate size 1～3mm, zircon corundum powder particle size 0.4～1mm, corundum fine powder, No. three kyanites in river, yttrium base stabilised zirconia, silicon powder, alumina powder, pure calcium aluminate cement, tripoly phosphate sodium STPP, electric smelting yellow ultramarine, above-mentioned first material each component is put into mixing agitator mixes, discharging, be encapsulated into the bag standby; With second material each component per distribution ratio weighing by weight: phosphoric acid, printing ink level aluminium hydroxide, ultrafine zirconia powder, yttrium base stabilised zirconia, electric smelting yellow ultramarine, after above-mentioned second material each component put into mixing agitator uniform mixing reaction, discharging, plastic tank barreled were standby.During construction the first material of high temperature abrasion material and second material joined in the forced mixer according to weight proportion and stir, the back employing streak method that stirs was applied to it reparation position of all abrasive bricks in the circular fluid bed, each damaged location of wear-resistant castable in 30 minutes, behind the normal temperature 48 hours, can finish circular fluid bed abrasive brick, wear-resistant castable broken parts recovery project, need not baker and just can directly open stove.Baker cost and furnace drying time have been saved.
High temperature abrasion material of the present invention has very high compressive strength, hardness is bigger, Mohs' hardness is higher than 10,1590 ℃, 3 hours abrasion losies of sintering are lower than 5/cm3, the density height, has excellent abrasive, resistance to fouling, abrasion resistance, thermal shock resistance and high-adhesion. under the same conditions, the mould material of using with present this area relatively, circular fluid bed was brought up to accumulative total and move more than 15000 hours running period from about 3500 hours, having overcome the boiler liner needs often to repair the problem of changing, save and understand manpower and materials, improved production efficiency greatly.
Embodiment
Embodiment 1, high temperature abrasion material are made up of the first material of 70 parts of weight and the second material of 30 parts of weight, wherein:
The weight percent of first material each component is:
Zircon corundum particle diameter 1～3mm 15%
Zircon corundum particle diameter 0.4～1mm 35%
Corundum fine powder 220～250 orders 20%
No. 3 kyanite 180 orders in river～220 orders 16%
Yttrium base stabilised zirconia 3%
Silicon powder SI 〉=98% dust is agree silicon powder 3%
Alumina powder 4%
Pure calcium aluminate cement 3%
Tripoly phosphate sodium STPP 0.5%
Electric smelting yellow ultramarine 0.5%;
The weight percent of second material each component is:
Phosphoric acid 75%
Printing ink level aluminium hydroxide 15%
Ultrafine zirconia powder 5%
Yttrium base stabilised zirconia 3%
Electric smelting yellow ultramarine 2%
Wherein: it is 85% phosphoric acid that phosphoric acid adopts concentration; The ultrafine zirconia powder fineness is 0.007～0.04mm,
During manufacturing, first material each component by packed behind the proportioning uniform mixing, by proportioning uniform mixing reaction back plastic tank barreled, is expected the A material second material each component mix by weight ratio to get final product with B before the construction.
Embodiment 2, high temperature abrasion material are made up of the first material of 80 parts of weight and the second material of 20 parts of weight, wherein:
The weight percent of first material each component is:
Zircon corundum particle diameter 1～3mm 19%
Zircon corundum particle diameter 0.4～1mm 25%
Corundum fine powder 220～250 orders 15%
No. 3 kyanite 180 orders in river～220 orders 10%
Yttrium base stabilised zirconia 9%
Silicon powder SI 〉=98% dust is agree silicon powder 7%
Alumina powder 8%
Pure calcium aluminate cement 5.5%
Tripoly phosphate sodium STPP 0.3%
Electric smelting yellow ultramarine 1.2%;
The weight percent of second material each component is:
Phosphoric acid 85%
Printing ink level aluminium hydroxide 6%
Ultrafine zirconia powder 5%
Yttrium base stabilised zirconia 3.7%
Electric smelting yellow ultramarine 0.3%
Wherein: it is 85% phosphoric acid that phosphoric acid adopts concentration; The ultrafine zirconia powder fineness is 0.007～0.04mm,
During manufacturing, first material each component by packed behind the proportioning uniform mixing, by proportioning uniform mixing reaction back plastic tank barreled, is expected the A material second material each component mix by weight ratio to get final product with B before the construction.
Embodiment 3, high temperature abrasion material are made up of the first material of 85 parts of weight and the second material of 15 parts of weight, wherein:
The weight percent of first material each component is:
Zircon corundum particle diameter 1～3mm 25%
Zircon corundum particle diameter 0.4～1mm 28%
Corundum fine powder 220～250 orders 15%
No. 3 kyanite 180 orders in river～220 orders 10%
Yttrium base stabilised zirconia 5%
Silicon powder SI 〉=98% dust is agree silicon powder 5%
Alumina powder 5.4%
Pure calcium aluminate cement 4%
Tripoly phosphate sodium STPP 0.1%
Electric smelting yellow ultramarine 2.5%;
The weight percent of second material each component is:
Phosphoric acid 75%
Printing ink level aluminium hydroxide 7.7%
Ultrafine zirconia powder 7%
Yttrium base stabilised zirconia 8%
Electric smelting yellow ultramarine 2.3%
Wherein: it is 85% phosphoric acid that phosphoric acid adopts concentration; The ultrafine zirconia powder fineness is 0.007～0.04mm,
During manufacturing, first material each component by packed behind the proportioning uniform mixing, by proportioning uniform mixing reaction back plastic tank barreled, is expected the A material second material each component mix by weight ratio to get final product with B before the construction.
Embodiment 4, high temperature abrasion material are made up of the first material of 75 parts of weight and the second material of 25 parts of weight, wherein:
The weight percent of first material each component is:
Zircon corundum particle diameter 1～3mm 15%
Zircon corundum particle diameter 0.4～1mm 25%
Corundum fine powder 220～250 orders 25%
No. 3 kyanite 180 orders in river～220 orders 16%
Yttrium base stabilised zirconia 3%
Silicon powder SI 〉=98% dust is agree silicon powder 3%
Alumina powder 4%
Pure calcium aluminate cement 8%
Tripoly phosphate sodium STPP 0.5%
Electric smelting yellow ultramarine 0.5%;
The weight percent of second material each component is:
Phosphoric acid 80%
Printing ink level aluminium hydroxide 15%
Ultrafine zirconia powder 5%
Yttrium base stabilised zirconia 4%
Electric smelting yellow ultramarine 1%
Wherein: it is 85% phosphoric acid that phosphoric acid adopts concentration; The ultrafine zirconia powder fineness is 0.007～0.04mm,
During manufacturing, first material each component by packed behind the proportioning uniform mixing, by proportioning uniform mixing reaction back plastic tank barreled, is expected the A material second material each component mix by weight ratio to get final product with B before the construction.
Embodiment 5, high temperature abrasion material are made up of the first material of 80 parts of weight and the second material of 20 parts of weight, wherein:
The weight percent of first material each component is:
Zircon corundum particle diameter 1～3mm 20%
Zircon corundum particle diameter 0.4～1mm 24%
Corundum fine powder 220～250 orders 15%
No. 3 kyanite 180 orders in river～220 orders 20%
Yttrium base stabilised zirconia 9%
Silicon powder SI 〉=98% dust is agree silicon powder 3%
Alumina powder 4%
Pure calcium aluminate cement 3%
Tripoly phosphate sodium STPP 0.5%
Electric smelting yellow ultramarine 1.5%;
The weight percent of second material each component is:
Phosphoric acid 75%
Printing ink level aluminium hydroxide 10%
Ultrafine zirconia powder 7%
Yttrium base stabilised zirconia 6%
Electric smelting yellow ultramarine 2%
Wherein: it is 85% phosphoric acid that phosphoric acid adopts concentration; The ultrafine zirconia powder fineness is 0.007～0.04mm,
During manufacturing, first material each component by packed behind the proportioning uniform mixing, by proportioning uniform mixing reaction back plastic tank barreled, is expected the A material second material each component mix by weight ratio to get final product with B before the construction.
Table 1 compares for the performance of high temperature abrasion material of the present invention and the present high-abrasive material that uses.
Claims (4)
1, a kind of high temperature abrasion material is characterized in that being made up of 70～85:30～15 by weight ratio first material and second material, wherein:
First material each component weight percent proportioning is
Zircon corundum particle diameter 1～3mm 15%～25%
Zircon corundum particle diameter 0.4～1mm 25%～35%
Corundum fine powder 15%～25%
No. three kyanites 10%～20% in river
Yttrium base stabilised zirconia 3%～9%
Silicon powder 3%～7%
Alumina powder 4%～8%
Pure calcium aluminate cement 3%～8%
Tripoly phosphate sodium STPP 0.1%～0.5%
Electric smelting yellow ultramarine 0.5%～2.5%;
Second material each component weight percent proportioning is
Phosphoric acid 75%-85%
Printing ink level aluminium hydroxide 6%～15%
Ultrafine zirconia powder 5%～7%
Yttrium base stabilised zirconia 3%～8%
Electric smelting yellow ultramarine 0.3%～2.3%.
2, high temperature abrasion material according to claim 1 is characterized in that the corundum fine powder fineness is 220～250 orders in the described first material component; No. three kyanite fineness in river are 180 orders～220 orders; Silicon powder adopts SI 〉=98% dust to agree silicon powder.
3, high temperature abrasion material according to claim 1 is characterized in that phosphoric acid employing concentration is 85% phosphoric acid in the described second material component, and the ultrafine zirconia powder fineness is 0.007～0.04mm.
4, the preparation method of the described high temperature abrasion material of claim 1, it is characterized in that weight percent proportioning by described first material of claim 1 and second material, with first material each component by packed behind the proportioning uniform mixing, second material each component by proportioning uniform mixing reaction back plastic tank barreled, is mixed A material and B material before the construction by weight ratio.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2008102430117A CN101428997B (en) | 2008-12-08 | 2008-12-08 | High temperature abrasion-proof paint and method for producing the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2008102430117A CN101428997B (en) | 2008-12-08 | 2008-12-08 | High temperature abrasion-proof paint and method for producing the same |
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| Publication Number | Publication Date |
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| CN101428997A true CN101428997A (en) | 2009-05-13 |
| CN101428997B CN101428997B (en) | 2011-09-07 |
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| WO2011088742A1 (en) * | 2010-01-21 | 2011-07-28 | 宜兴市国强炉业有限公司 | High temperature abrasion resistant repairing paint and preparing method thereof |
| CN103819165A (en) * | 2013-12-05 | 2014-05-28 | 江南大学 | High-temperature inorganic surface wear-resistant paint for CFB (circulating fluid bed) boiler and preparation method of high-temperature inorganic surface wear-resistant paint |
| CN107385161A (en) * | 2017-07-26 | 2017-11-24 | 江苏苏丰机械科技有限公司 | A kind of new material Major-diameter annealing machine |
| CN107599181A (en) * | 2017-10-16 | 2018-01-19 | 宜兴市国强炉业有限公司 | High temperature abrasion material mixes induction system |
| CN107828947A (en) * | 2017-10-25 | 2018-03-23 | 江苏广盛源科技发展有限公司 | A kind of welding annealing device |
| CN111763092A (en) * | 2020-06-17 | 2020-10-13 | 林国强 | Anti-slagging high-temperature wear-resistant composite material and preparation method thereof |
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| CN112194472A (en) * | 2020-10-14 | 2021-01-08 | 郑州东方炉衬材料有限公司 | Wear-resistant adhesive for repairing gasification furnace and power station boiler and production process |
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| CN100351209C (en) * | 2005-11-03 | 2007-11-28 | 武汉钢铁(集团)公司 | Refractory pouring material used for melten iron desulfur agitator |
| CN100410209C (en) * | 2005-11-25 | 2008-08-13 | 首钢总公司 | Pouring material for torpedo tank liner repairing |
| CN100424041C (en) * | 2005-12-22 | 2008-10-08 | 濮阳濮耐高温材料（集团）股份有限公司 | Waterless taphole mix for blast furnace taphole |
| CN1884201A (en) * | 2006-07-11 | 2006-12-27 | 中钢集团洛阳耐火材料研究院 | Permeable fireproof materials for aluminium refining and process for preparing same |
| CN100467428C (en) * | 2007-06-04 | 2009-03-11 | 宜兴市国强炉业有限公司 | High temperature wear resistant paint and its production process |
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2008
- 2008-12-08 CN CN2008102430117A patent/CN101428997B/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011088742A1 (en) * | 2010-01-21 | 2011-07-28 | 宜兴市国强炉业有限公司 | High temperature abrasion resistant repairing paint and preparing method thereof |
| CN102134164B (en) * | 2010-01-21 | 2013-04-17 | 宜兴市国强炉业有限公司 | High-temperature wear-resistant repairing coating and preparation method thereof |
| CN103819165A (en) * | 2013-12-05 | 2014-05-28 | 江南大学 | High-temperature inorganic surface wear-resistant paint for CFB (circulating fluid bed) boiler and preparation method of high-temperature inorganic surface wear-resistant paint |
| CN103819165B (en) * | 2013-12-05 | 2016-08-24 | 江南大学 | A kind of CFB boiler high temperature inorganic surface abrasion resistance coating and preparation method thereof |
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| CN107599181A (en) * | 2017-10-16 | 2018-01-19 | 宜兴市国强炉业有限公司 | High temperature abrasion material mixes induction system |
| CN107599181B (en) * | 2017-10-16 | 2023-06-06 | 宜兴市国强炉业有限公司 | High-temperature wear-resistant coating mixing, stirring and conveying system |
| CN107828947A (en) * | 2017-10-25 | 2018-03-23 | 江苏广盛源科技发展有限公司 | A kind of welding annealing device |
| CN111763092A (en) * | 2020-06-17 | 2020-10-13 | 林国强 | Anti-slagging high-temperature wear-resistant composite material and preparation method thereof |
| CN111763091A (en) * | 2020-06-17 | 2020-10-13 | 林国强 | High-thermal-shock wear-resistant coating and preparation method thereof |
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Effective date of registration: 20171229 Address after: Ding Shu Zhen Zhang Ze Cun Yixing 214225 Jiangsu province Yixing Guoqiang Furnace Industry Co Ltd Patentee after: YIXING GUOQIANG FURNACE INDUSTRY Co.,Ltd. Address before: Ding Shu Zhen Zhang Ze Cun Yixing 214225 Jiangsu province Yixing Guoqiang Furnace Industry Co Ltd Patentee before: Lin Guoqiang |
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