EP1720812A1 - Melange ceramique et produit associe pour des utilisations ignifuges - Google Patents
Melange ceramique et produit associe pour des utilisations ignifugesInfo
- Publication number
- EP1720812A1 EP1720812A1 EP05715686A EP05715686A EP1720812A1 EP 1720812 A1 EP1720812 A1 EP 1720812A1 EP 05715686 A EP05715686 A EP 05715686A EP 05715686 A EP05715686 A EP 05715686A EP 1720812 A1 EP1720812 A1 EP 1720812A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- sio
- base material
- carrier
- batch according
- weight
- 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.)
- Withdrawn
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- 239000000919 ceramic Substances 0.000 title claims abstract description 10
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 34
- 229910052906 cristobalite Inorganic materials 0.000 claims abstract description 13
- 229910052905 tridymite Inorganic materials 0.000 claims abstract description 7
- 229910052681 coesite Inorganic materials 0.000 claims abstract description 4
- 239000000470 constituent Substances 0.000 claims abstract description 4
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 70
- 229910004298 SiO 2 Inorganic materials 0.000 claims description 46
- 239000000463 material Substances 0.000 claims description 39
- 239000000395 magnesium oxide Substances 0.000 claims description 35
- 238000012360 testing method Methods 0.000 claims description 33
- 239000000203 mixture Substances 0.000 claims description 15
- 229910052596 spinel Inorganic materials 0.000 claims description 12
- 239000011029 spinel Substances 0.000 claims description 12
- 239000002994 raw material Substances 0.000 claims description 11
- 229910052593 corundum Inorganic materials 0.000 claims description 8
- 239000010431 corundum Substances 0.000 claims description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 7
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 claims description 6
- 229910052863 mullite Inorganic materials 0.000 claims description 6
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 claims description 6
- 229910052799 carbon Inorganic materials 0.000 claims description 5
- 229910001928 zirconium oxide Inorganic materials 0.000 claims description 5
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 4
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 4
- 239000011822 basic refractory Substances 0.000 claims description 4
- 229910001570 bauxite Inorganic materials 0.000 claims description 4
- 230000004048 modification Effects 0.000 claims description 4
- 238000012986 modification Methods 0.000 claims description 4
- 229910052726 zirconium Inorganic materials 0.000 claims description 4
- 229910003023 Mg-Al Inorganic materials 0.000 claims description 3
- 239000002245 particle Substances 0.000 claims description 3
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 3
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 3
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims description 3
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 claims description 2
- INJRKJPEYSAMPD-UHFFFAOYSA-N aluminum;silicic acid;hydrate Chemical compound O.[Al].[Al].O[Si](O)(O)O INJRKJPEYSAMPD-UHFFFAOYSA-N 0.000 claims description 2
- 229910052849 andalusite Inorganic materials 0.000 claims description 2
- 239000000571 coke Substances 0.000 claims description 2
- 238000009826 distribution Methods 0.000 claims description 2
- 239000010439 graphite Substances 0.000 claims description 2
- 229910002804 graphite Inorganic materials 0.000 claims description 2
- 239000010443 kyanite Substances 0.000 claims description 2
- 229910052850 kyanite Inorganic materials 0.000 claims description 2
- 239000011295 pitch Substances 0.000 claims description 2
- 239000011044 quartzite Substances 0.000 claims description 2
- 229920005989 resin Polymers 0.000 claims description 2
- 239000011347 resin Substances 0.000 claims description 2
- 239000004071 soot Substances 0.000 claims description 2
- 239000011269 tar Substances 0.000 claims description 2
- 239000004927 clay Substances 0.000 claims 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 claims 1
- 239000000377 silicon dioxide Substances 0.000 abstract 1
- 235000012239 silicon dioxide Nutrition 0.000 abstract 1
- 229910052682 stishovite Inorganic materials 0.000 abstract 1
- 235000012245 magnesium oxide Nutrition 0.000 description 33
- 235000013339 cereals Nutrition 0.000 description 29
- 238000004519 manufacturing process Methods 0.000 description 12
- 239000011230 binding agent Substances 0.000 description 11
- 230000015572 biosynthetic process Effects 0.000 description 11
- 238000005266 casting Methods 0.000 description 10
- 150000001875 compounds Chemical class 0.000 description 9
- 238000010304 firing Methods 0.000 description 8
- 238000002844 melting Methods 0.000 description 8
- 230000008018 melting Effects 0.000 description 8
- 230000009467 reduction Effects 0.000 description 8
- 239000000126 substance Substances 0.000 description 8
- 239000000654 additive Substances 0.000 description 7
- 230000008901 benefit Effects 0.000 description 7
- 239000004575 stone Substances 0.000 description 7
- 239000004568 cement Substances 0.000 description 6
- 238000006073 displacement reaction Methods 0.000 description 5
- 238000001035 drying Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 210000003041 ligament Anatomy 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 239000010453 quartz Substances 0.000 description 5
- 238000005245 sintering Methods 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 4
- 229910021488 crystalline silicon dioxide Inorganic materials 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000035939 shock Effects 0.000 description 4
- 229910052566 spinel group Inorganic materials 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 229910021493 α-cristobalite Inorganic materials 0.000 description 4
- 239000004566 building material Substances 0.000 description 3
- 239000000969 carrier Substances 0.000 description 3
- 239000011651 chromium Substances 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 230000000977 initiatory effect Effects 0.000 description 3
- 238000007493 shaping process Methods 0.000 description 3
- 239000002893 slag Substances 0.000 description 3
- 238000005496 tempering Methods 0.000 description 3
- 230000000930 thermomechanical effect Effects 0.000 description 3
- 230000009466 transformation Effects 0.000 description 3
- 229910021494 β-cristobalite Inorganic materials 0.000 description 3
- 229910020068 MgAl Inorganic materials 0.000 description 2
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 2
- 239000004567 concrete Substances 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 235000013312 flour Nutrition 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- ZLNQQNXFFQJAID-UHFFFAOYSA-L magnesium carbonate Chemical group [Mg+2].[O-]C([O-])=O ZLNQQNXFFQJAID-UHFFFAOYSA-L 0.000 description 2
- 239000001095 magnesium carbonate Substances 0.000 description 2
- 235000014380 magnesium carbonate Nutrition 0.000 description 2
- 229910000021 magnesium carbonate Inorganic materials 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000004014 plasticizer Substances 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 239000011214 refractory ceramic Substances 0.000 description 2
- 230000000717 retained effect Effects 0.000 description 2
- 229920003002 synthetic resin Polymers 0.000 description 2
- 239000000057 synthetic resin Substances 0.000 description 2
- 229910021489 α-quartz Inorganic materials 0.000 description 2
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 description 1
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 1
- 229920001732 Lignosulfonate Polymers 0.000 description 1
- MXRIRQGCELJRSN-UHFFFAOYSA-N O.O.O.[Al] Chemical compound O.O.O.[Al] MXRIRQGCELJRSN-UHFFFAOYSA-N 0.000 description 1
- 229910000805 Pig iron Inorganic materials 0.000 description 1
- LSNNMFCWUKXFEE-UHFFFAOYSA-N Sulfurous acid Chemical compound OS(O)=O LSNNMFCWUKXFEE-UHFFFAOYSA-N 0.000 description 1
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 1
- MCMNRKCIXSYSNV-UHFFFAOYSA-N ZrO2 Inorganic materials O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- ILRRQNADMUWWFW-UHFFFAOYSA-K aluminium phosphate Chemical compound O1[Al]2OP1(=O)O2 ILRRQNADMUWWFW-UHFFFAOYSA-K 0.000 description 1
- 229910000147 aluminium phosphate Inorganic materials 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000001311 chemical methods and process Methods 0.000 description 1
- 229910000423 chromium oxide Inorganic materials 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000002270 dispersing agent Substances 0.000 description 1
- 239000010459 dolomite Substances 0.000 description 1
- 229910000514 dolomite Inorganic materials 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000009970 fire resistant effect Effects 0.000 description 1
- 229910052839 forsterite Inorganic materials 0.000 description 1
- 238000001033 granulometry Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 239000004413 injection moulding compound Substances 0.000 description 1
- HCWCAKKEBCNQJP-UHFFFAOYSA-N magnesium orthosilicate Chemical compound [Mg+2].[Mg+2].[O-][Si]([O-])([O-])[O-] HCWCAKKEBCNQJP-UHFFFAOYSA-N 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 229920001568 phenolic resin Polymers 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000002250 progressing effect Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 229910052851 sillimanite Inorganic materials 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 230000031068 symbiosis, encompassing mutualism through parasitism Effects 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 231100000331 toxic Toxicity 0.000 description 1
- 230000002588 toxic effect Effects 0.000 description 1
- 238000000844 transformation Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000003826 uniaxial pressing Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
- 229910052845 zircon Inorganic materials 0.000 description 1
- 229910000500 β-quartz Inorganic materials 0.000 description 1
Classifications
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- 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
- C04B35/013—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 containing carbon
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- 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
- C04B35/03—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 magnesium oxide, calcium oxide or oxide mixtures derived from dolomite
- C04B35/04—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 magnesium oxide, calcium oxide or oxide mixtures derived from dolomite based on magnesium oxide
- C04B35/043—Refractories from grain sized mixtures
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- C04B35/03—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 magnesium oxide, calcium oxide or oxide mixtures derived from dolomite
- C04B35/06—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 magnesium oxide, calcium oxide or oxide mixtures derived from dolomite based on oxide mixtures derived from dolomite
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- C04B35/10—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on aluminium oxide
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- C04B35/16—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 silicates other than clay
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- C04B35/16—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 silicates other than clay
- C04B35/18—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 silicates other than clay rich in aluminium oxide
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- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
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- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
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- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3217—Aluminum oxide or oxide forming salts thereof, e.g. bauxite, alpha-alumina
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- C04B2235/34—Non-metal oxides, non-metal mixed oxides, or salts thereof that form the non-metal oxides upon heating, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3418—Silicon oxide, silicic acids or oxide forming salts thereof, e.g. silica sol, fused silica, silica fume, cristobalite, quartz or flint
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- C04B2235/34—Non-metal oxides, non-metal mixed oxides, or salts thereof that form the non-metal oxides upon heating, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3427—Silicates other than clay, e.g. water glass
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Definitions
- the invention relates to a ceramic substitute and an associated product for refractory applications.
- Ceramic additives with refractory raw materials are used to manufacture refractory ceramic products and are used in many areas of technology, especially for lining
- the refractory raw materials are both basic and non-basic varieties.
- MgO in particular MgO sinter, is an essential component of all MgO and MgO spinel products.
- the main component of MgO sinter is periclase.
- the main raw material base for the production of MgO sinter is magnesite, i.e. magnesium carbonate, or a synthetic magnesia source.
- Unformed products for example casting compounds, are formed from batches which are brought to a desired processing consistency with a certain viscosity by water or other liquids and, if appropriate, additives (such as binders, plasticizers, dispersants). These masses are then processed directly as monolithic masses, for example for the monolithic lining of a metallurgical melting vessel, or they are used for the production of so-called prefabricated components. In this case, the offsets can also be processed as such or in combination with certain additives, for example cast in molds.
- additives such as binders, plasticizers, dispersants
- cracks may form during subsequent drying and / or shrinkage during the subsequent sintering, which reduce the durability of the infeed or the prefabricated component.
- the mentioned products based on MgO in combination with various spinels have proven themselves in principle.
- the introduction of the spinels introduces additional oxides into the batch, which can lead to a reduction in the hot strength of the fired products.
- the invariant point which is the temperature of the first melting phase formation
- calcium-rich infiltrates such as basic slags or cement clinker melts, can then reduce the heat resistance and durability.
- the invention has for its object to offer a ceramic offset and associated products that have a symbiosis of the required property characteristics mentioned.
- the products formed from the offset should have reduced brittleness (ie improved ductility), good thermal shock properties, advantageous heat resistance and the best possible resistance to corrosion while at the same time being inexpensive to produce.
- the term “product” includes in particular unshaped and shaped products, those with and without heat treatment before use, sintered products and products that are / have been heat treated (heated) during use.
- the invention is based on the knowledge that the brittleness of refractory products or products intended for refractory applications can be significantly reduced if the formation of macroscopically recognizable (large) cracks is avoided and the system is set so that it only serves to form microcracks in the Structure is coming. This is achieved by adding a separate SiO 2 carrier to the offset.
- the crack density is increased (expressed, for example, as the number of cracks per square meter of the surface).
- the cracks have a much smaller crack width (in particular ⁇ 20 ⁇ m), and are therefore significantly smaller than the macroscopically recognizable cracks in products in the prior art.
- These micro cracks do not have the same negative impact on the durability of the products. These products are also better able to withstand thermo-mechanical loads during use, for example due to thermal shocks.
- the fact that the SiO 2 carrier as a largely independent component is retained and no melting phases form, the effects of microcracking are retained even after temperature treatment.
- the physical changes in the structure can be achieved in certain mass fractions by adding a separate, grained SiO 2 carrier.
- SiO 2 carrier encompasses all crystalline SiO 2 modifications which have sufficient stability at room temperature. These include primarily cristobalite (ß-form) and tridymite ( ⁇ -tridymite). Another possible SiO 2 modification is coesite. Quartz (ß-shape) or quartz can also be used as SiO 2 carrier. This also applies to substances that have been prepared from the above-mentioned SiO 2 raw materials by physical and / or chemical processes (pretreatment). For example, quartz can be ground, compacted, sintered and then processed in a suitable grain.
- the pretreatment or preparation of the SiO 2 carrier can be used to reduce its bulk density to values of ⁇ 2.65 g / cm 3 , for example to values between 2.2 and 2.5 g / cm 3 .
- the chemical composition of the SiO 2 carrier can also be varied by admixtures such as CaO.
- microcracks is caused by a non-linear thermal expansion during phase transformations of the crystalline SiO 2 carrier.
- phase transformation is, for example, that of ⁇ -quartz to ⁇ -quartz at 573 ° C and the transformation of ⁇ -quartz to ⁇ -cristobalite at over 1050 ° C, often at around 1250 ° C.
- Ss-Cristobalite is already changing at 270 ° C in ⁇ -cristobalite, which is also associated with a volume expansion. Therefore, the desired effect can be seen in the product of Example 5 below after drying at 380 ° C.
- the invention then relates to a ceramic offset for refractory applications
- the offset can only consist of components A and B.
- the refractory base material can be a basic substance such as doloma (i.e. burnt dolomite) or magnesia (ie MgO), or a non-basic substance, for example based on Al 2 O 3 or ZrO 2 .
- doloma i.e. burnt dolomite
- magnesia ie MgO
- non-basic substance for example based on Al 2 O 3 or ZrO 2 .
- the proportion of the refractory base material is 90-99% by weight.
- the proportion of the granular SiO 2 carrier is, for example,> 1 and / or ⁇ 7% by weight, in each case based on the total offset, the upper limit also being able to be set at ⁇ 5% by weight or ⁇ 4% by weight.
- the mixture of refractory base material for example an MgO base material and crystalline SiO 2 support , leads to expansion in the corresponding modification conversions of the SiO support during a temperature treatment (in particular in the case of fire) after shaping the offset, according to current knowledge, which leads to generation of micro-cracks in the structure. These micro cracks are responsible for reducing the brittleness.
- microcracks are formed when the crystalline SiO 2 support is added during the heating phase of the firing process, while in the prior art microcracking can be observed in the cooling phase. If a glassy SiO 2 carrier (quartz material) is used, the crack formation is due to the greater shrinkage of the refractory (refractory) basic component when cooling after the fire.
- the principle of microcrack initiation by a separate, grained SiO 2 carrier is basically independent of the raw material (the refractory basic component) and is therefore, for example, based on ceramic-bonded, chemically bonded, carbon-bonded, hydraulically bonded, shaped and unshaped, annealed, fired and unburned refractory displacements and products applicable.
- the temperature can be a criterion for the selection of the SiO 2 carrier.
- the prefabricated components casting compounds or carbon-bonded refractory products mentioned, it can make sense to use cristobalite as an SiO 2 carrier.
- the desired microcracks can be formed even at a very low temperature level, for example when the casting compounds are heated up. The unwanted shrinkage cracks can be avoided.
- An important group for the application of the invention are unshaped products such as concrete masses or casting masses for the production of refractory linings or prefabricated components. These masses can be hydraulic or harden semi-hydraulically, e.g. be masses based on cement, especially alumina cement.
- the invention can also be applied to low-cement or cement-free casting compounds, for example those based on bauxite as a non-basic refractory base material.
- the dry mix (e.g. bauxite and cristobalite) is mixed with the required amount of water to achieve a desired processing consistency. If necessary, additives such as plasticizers are added.
- the described conversion of ß-cristobalite to ⁇ -cristobalite takes place already during drying from 270 ° Celsius.
- the mode of operation described is largely independent of the grain fraction of the refractory basic component.
- small maximum grain sizes (for example 2 mm) or small proportions (for example 5% by weight) of the coarse fraction (for example 2 to 4 mm) can have an unfavorable effect on the reduction in brittleness.
- the SiO 2 carrier has a grain size d 50 or d 05 which is larger than a maximum grain (or larger than at least 95% by weight) of the fine grain fraction of the refractory base material. Accordingly, 50 or 95% by weight of the SiO 2 carrier is coarser than 95 or 100% by weight of the fine grain of the refractory base material.
- the refractory base material is typically used in a relatively wide range of particles.
- the component can have a proportion of a medium grain, for example 0.25- ⁇ 1mm and a fine grain fraction (flour fraction) ⁇ 0.25mm.
- the limit grain size between coarse grain and medium grain can also be set at 1, 5 or 2mm.
- the proportion of flour grain can be determined, for example, to a grain fraction ⁇ 0.125 mm (125 ⁇ m).
- the abovementioned fine grain fraction of the refractory base material is 10-30% by weight, 15-25% by weight or 25-30% by weight, in each case based on the total batch.
- the average grain fraction as stated above, can be, for example, orders of magnitude of 5-30% by weight, 10-25% by weight or 10-20% by weight, again based on the total offset.
- the coarse grain fraction is calculated accordingly from the above proportions of fine grain or medium grain.
- the refractory, in particular oxidic, raw material is proposed in the following particle size distribution:
- the granular SiO 2 carrier has a grain size of up to 6 mm, the upper grain limit also being selected at 3.0 or 1.5 mm and the lower grain limit at 0.25, 0.50, 1 or 2 mm can.
- the SiO 2 carrier is typically present in a grain fraction between 0.5 and 3 mm. In comparison with grain sizes in the range below 1 mm, the increase in the grain size (> 1 mm) with the same amount leads to a higher effectiveness in the sense of the invention. A grain size of 1 to 2mm is therefore more effective than a grain size of 0.5 to 1mm.
- At least one of the following components can be selected as the non-basic refractory base material: chamotte, sillimanite, andalusite, kyanite, mullite, bauxite, corundum raw materials such as high-grade corundum or brown corundum, Tabular alumina, calcined alumina, basic materials containing zirconium oxide such as zirconium mullite, zirconium corundum, zirconium silicate or zirconium oxide, titanium oxide (TiO 2 ), Mg-Al spinel, silicon carbide.
- Quartzite can also be used as a refractory base material, with cristobalite, tridymite, coesite and / or the aforementioned pretreated SiO 2 carrier being used as an additive.
- MgO base material with an MgO content of 83 to 99.5% by weight is proposed in particular as the basic refractory base material.
- the lower limit for the MgO content is 85, 88, 93, 94, 95, 96 or 97% by weight, the upper limit for example 97, 98 or 99% by weight.
- the MgO content is 94 to 99 or 96 to 99% by weight.
- the MgO base material can consist of sintered magnesia, melted magnesia or mixtures thereof.
- the MgO content of the batch can be provided in a proportionate amount of 3 to 20% by weight (or 3 to 10% by weight) based on the total mixture, a spinel of the Herzynit type, the Galaxit type or mixtures thereof become.
- the microcracks initiated by the granular SiO 2 carrier in the heating phase are supplemented by further microcracks by the spinel component during the cooling phase in the pyroprocess.
- the batch can contain other constituents in relatively small proportions, for example at least one of the following components: (elementary) carbon, graphite, resin, pitch, soot, coke, tar.
- the offset can therefore be used to produce C-linked products. This applies in particular to applications of the offsets in carbon-bound products or products that are soaked in tar.
- ASC products include so-called ASC products, the names of which derive from the main components A (for Al O 3 carriers), S (for SiC and / or Si metal) and C (for the carbon carrier).
- ASC products the names of which derive from the main components A (for Al O 3 carriers), S (for SiC and / or Si metal) and C (for the carbon carrier).
- Magnesia carriers (for spinel formation) and Mg-Al spinels can also be part of the recipe.
- Such offsets are bound with a synthetic resin, for example a phenolic resin, as a binder. They are used for example for pig iron pans, but also for shadow pipes, dip pipes, etc.
- the curing process can be carried out in such a way that, for example, the transition temperature from ß-cristobalite to ⁇ -cristobalite is reached or exceeded, so that microcracks are already present in the product when the pre-assembled molded parts are delivered.
- the offset described also serves in particular for the production of fired refractory products, in particular fired refractory molded parts.
- a binder in particular a temporary binder, for example a lignin sulfonate solution, is mixed into the batch and the mixture is then pressed, for example into stones, dried and fired.
- a typical firing temperature is 1300-1700 ° Celsius.
- a typical firing temperature for a batch with 96% by weight of MgO and 4% of a granular SiO 2 carrier is 1,400 ° C (+/- 50 ° C).
- Too high a firing temperature or application temperature can lead to a reduced effect of the SiO 2 carrier and increase the brittleness again due to too intensive sintering (usually involving melting phases).
- the reaction behavior in particular the formation of melting phases, between the SiO 2 carrier and the refractory base material must be taken into account without preventing sufficient sintering.
- the exact firing temperature is dependent on the specifically selected components of the offset and has to be determined empirically.
- the offsets of Examples 1-3 are used to produce fired, shaped products based on non-basic raw materials.
- a temporary binder must be added to the offset components.
- This can be, for example, sulfite waste liquor, phosphoric acid or monoaluminum phosphate.
- a binding tone can also be used in the recipe be included.
- stones or other molded parts can be produced from the offsets, which are then fired.
- the firing temperature should be selected so that the sintering is sufficient, but not so high that excessive sintering counteracts the effect of reducing the brittleness.
- the granulometry of the fine-grain fraction of the non-basic raw material and the binder are decisive.
- a firing temperature of 1450 ° Celsius was chosen.
- the (pressed) stones produced from offsets 2 and 3 were fired at 1550 ° Celsius.
- Offset No. 4 is used to manufacture a so-called ASC product, i.e. a C-linked product, as was presented above, with an addition of cristobalite. Via the cristobalite conversion, microcracks in the structure are initiated during the tempering (400 ° Celsius) of the products made from the offset.
- Example 5 shows an offset for a casting compound with a proportion of alumina cement.
- the batch was mixed with water and molded parts were made from it, which were dried or tempered at temperatures up to 380 ° Celsius.
- a comparison mass No. 6
- analog samples were produced and also dried or tempered at 380 ° Celsius.
- all other basic components of batch No. 5 were increased by 4% each.
- G F denotes this specific breaking energy (N / m), E the modulus of elasticity (Pa), and f t (Pa) the tensile strength.
- Gp / ft of the specific breaking energy G F to the tensile strength f t The ratio G F / O Z is used to characterize products according to the invention.
- a basic wedge gap test to determine the specific breaking energy G F and the nominal notch tensile strength ⁇ _z is described in K. Rieder et.al.
- the wedge gap test is carried out after a temperature treatment of the product (for example after drying, tempering or fire of the product) at room temperature.
- the table at the end of the description lists the conditions for the wedge gap test depending on the starting product.
- “Unformed product” denotes an offset, if appropriate after adding a binder and / or a mixing liquid.
- molded product includes all shapes and shaping processes, the product having to be at least the size of the test specimen described below. A distinction is made between molded products without and after temperature treatment and according to their different types of bonds.
- An "originally unshaped product" for example a casting or injection molding compound, can become Solidification of the creation of a monolithic body (for example a furnace lining) solidifies during use and thus virtually becomes a “molded” part. This also applies analogously to prefabricated components which are exposed to higher temperatures at least during use.
- the shape of the test specimen is shown in FIG. 1.
- the cuboid test specimen has the following dimensions: width W: 1 10 mm, length L: 75 mm, height H: 100 mm.
- a recess A with the following dimensions can be seen on the upper side: width b: 24 mm; Length 1: 75 mm, height h: 22 mm.
- the recess A is used to hold strips, rollers and a wedge for power transmission. From the bottom of the recess A, a notch Kl extends with a width b 'of 3 mm and a height h' of 12 mm downwards in the direction of the base area G. In each case, another notch adjoins the notch Kl
- K2, K3 each have a width b "of 3 mm and a height h" of 6 mm.
- a wedge K1 according to FIG. 3 (above) is placed in the middle between the strips LS and is supported against the strips LS via two rollers R (FIG. 3 below), as shown in FIG.
- the shaping process of product manufacture is done by uniaxial pressing, the sample is taken so that the direction of the pressing force is parallel to the plane of the ligament surface (that is the surface where the fracture is generated during the test).
- the length of the wedge K and the strips LS corresponds to the sample length of 75 mm.
- the rolls R are a little longer.
- Wedge Kl, strips LS and rollers R are made of steel.
- the test specimen rests on a linear support.
- This is a square steel rod S, which has an edge length of 5 mm and whose length corresponds at least to the specimen width of 75 mm and extends over the entire length of the specimen.
- the bar S covers the width of the Notches K2, K3 even on both sides.
- the course of the test is shown in FIG. 5.
- a load cell KM can be seen in the upper image area.
- the vertical force V exerted by the testing machine on the wedge Kl causes horizontal forces which lead to a steadily progressing crack formation during the test.
- the vertical load F v and the vertical displacement ⁇ v are determined. These sizes are registered until the load drops to 10% or less of the maximum load.
- the fracture energy GF is determined as the area under the load / displacement diagram.
- A is the ligament area of 66 x 63 mm [(100-22-12) x (75-6-6)]
- ⁇ max is the maximum displacement during the measurement.
- the nominal notch tensile strength is calculated using the following equation:
- B is the ligament length (63mm) and W is the ligament height (66mm).
- the size y denotes the vertical distance of the line of action of the horizontal force introduced by the rollers from the center of gravity of the ligament surface. A value of 62 mm is used as a sufficient approximation for this (FIGS. 1 and 4).
- the horizontal maximum load FH max used in this relationship (III) can be determined from the vertical maximum load Fy ma according to the following relationship:
- the following table shows the comparison values for the specific breaking energy G F , the nominal notch tensile strength ⁇ j z and the quotient of the two.
- Products according to the invention are characterized by a ratio G F / Ü Z > 40. Values> 50 are aimed for.
- the product according to the invention shows a more than doubled quotient of specific breaking energy and nominal notch tensile strength, from which a significantly reduced brittleness can be read.
- FIG. 6 shows the load / displacement diagrams of the wedge gap test (carried out at room temperature) and demonstrates the significantly less brittle behavior of the offset (7) according to the invention. In the table above, this can be seen from the higher quotient of the specific breaking energy G F by the nominal notch tensile strength ⁇ : z.
- the addition of the granular SiO 2 support to the magnesia component causes a significant reduction in the modulus of elasticity, namely from 75.8 GPa to 14.9 GPa.
- the table also shows that the ratio of the nominal notch tensile strength to the dynamic modulus of elasticity is significantly higher in the variant according to the invention. This leads to an increase in the thermal stress parameter R according to Kingery [WD Kingery et.al. : Introduction to Ceramics, John Wiley & Sons, 1960; ISBN 0-471 -4786C- 1].
- the invention manages with a simple, inexpensive additive (granular SiO 2 carrier) in addition to the refractory basic component, the said offset proves to be a good basis for the production of refractory products which have a relatively low brittleness, so that they show good thermal shock resistance, are corrosion resistant, but also do not cause a reduction in the heat resistance in comparison to other products from the prior art.
- the selection of the offset components and manufacturing conditions is such that the product gives a ratio Gp / ⁇ z> 40.
- the product according to the invention has the advantage of a higher mechanical or thermomechanical resistance to thermal shock or impressed deformations.
- magnesia chromite products there is the advantage of a chromium-free delivery material, whereby the risk of Cr 6+ formation can be avoided.
- spinel products there is a cost advantage due to the relatively inexpensive SiO 2 carrier available.
- building materials in the CaO-MgO-SiO 2 system with mass ratios of CaO to SiO 2 (C / S ratios) below 0.93 have an invariant point of at least 1502 ° C., which at C / S ratios below approx. 0.25 (presence of a forsterite mixed crystal as the only silicatic secondary phase) can be increased further with a decreasing C / S ratio up to a maximum of approx. 1860 ° C.
- a magnesia stone containing spinel (MgAl 2 O 4 ) with a C / S ratio above 1.87, as it corresponds to the prior art has an invariant point of 1325 ° C.
- the higher invariant point in the product according to the invention can be used to improve the hot properties if, taking into account the product composition and any infiltrates in use, the amount of melting phase is also more favorable. Compared to products with the addition of ZrO 2 there is in any case an economic advantage due to the lower cost of the SiO 2 carrier.
- the product according to the invention allows a material composition that consists exclusively of crystalline phases.
- Another advantage is that when using cristobalite, microcrack initiation and thus a reduction in brittleness already occurs at a temperature of 270 ° C. This allows unburned products to be manufactured or used even at low temperatures with reduced brittleness. These include, for example, casting compounds and prefabricated components. It is also possible, for example, to reduce the brittleness of carbon-bound unbaked products in this way.
- a test specimen is formed from the batch, optionally after adding a binder and / or water (for example: chemical or hydraulic binder), and this is heat-treated at 350 ° C.
- a binder and / or water for example: chemical or hydraulic binder
- test specimen is formed from the batch, optionally after adding a binder and / or water (for example: chemical or hydraulic binder), and this is heat-treated at 650 ° C., alternatively> 1350 ° C.
- a binder and / or water for example: chemical or hydraulic binder
- test specimen is cut from the product and this is heat-treated at 350 ° C., provided that the product has not previously been heat-treated at a temperature> 350 ° C.
- test specimen is cut from the product and this is heat-treated at 650 ° C, alternatively 1350 ° C, provided the product has not previously been heat-treated at a temperature> 650 C, alternatively> 1350 ° C.
- test specimen is cut from the product formed during use and this is heat-treated at 350 ° C., provided the product has not already been temperature-treated during use> 350 ° C.
- test specimen is cut from the product formed during use and this is heat-treated at 650 ° C, alternatively 1350 ° C, provided the product has not already been heat-treated during use> 650 C, alternatively> 1350 ° C.
- the SiO 2 carrier consists of at least 50% by weight of cristobalite and / or tridymite.
- the SiO 2 carrier consists of less than 50% by weight of cristobalite and / or tridymite.
- the temperature treatment is usually carried out at 1350 ° C. If the temperature of 1350 ° C is too high to reduce brittleness, the temperature treatment is carried out alternatively at 650 ° C, which is higher than the temperature for the quartz crack.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Compositions Of Oxide Ceramics (AREA)
Abstract
L'invention concerne un mélange céramique utilisés dans applications ignifuges comprenant entre 83 et 99,5% en poids d'au moins une substance réfractaire dans une fraction de noyau inférieur à 8 mm, et entre 0,5 et 12% en poids d'au moins un support de SiO2 en granulés, séparé et un résidu éventuel : des composants restants. L'invention concerne un produit comprenant ledit mélange.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200410010740 DE102004010740C5 (de) | 2004-03-05 | 2004-03-05 | Feuerfester keramischer Versatz und dessen Verwendung |
DE200410010739 DE102004010739B4 (de) | 2004-03-05 | 2004-03-05 | Verfahren zur Herstellung eines ungeformten oder geformten, gebrannten oder nicht gebrannten feuerfesten Produkts |
PCT/EP2005/002226 WO2005085155A1 (fr) | 2004-03-05 | 2005-03-03 | Melange ceramique et produit associe pour des utilisations ignifuges |
Publications (1)
Publication Number | Publication Date |
---|---|
EP1720812A1 true EP1720812A1 (fr) | 2006-11-15 |
Family
ID=34921208
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05715686A Withdrawn EP1720812A1 (fr) | 2004-03-05 | 2005-03-03 | Melange ceramique et produit associe pour des utilisations ignifuges |
Country Status (7)
Country | Link |
---|---|
US (1) | US20070203013A1 (fr) |
EP (1) | EP1720812A1 (fr) |
BR (1) | BRPI0507341A (fr) |
CA (1) | CA2558526C (fr) |
RU (1) | RU2386604C2 (fr) |
WO (1) | WO2005085155A1 (fr) |
ZA (1) | ZA200607731B (fr) |
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JP4823626B2 (ja) * | 2005-09-26 | 2011-11-24 | 新日本製鐵株式会社 | 高炉炉底極小空隙への骨材圧入方法 |
DE102006007781B4 (de) | 2006-02-20 | 2008-09-25 | Refratechnik Holding Gmbh | Grobkeramischer feuerfester Versatz sowie feuerfestes Erzeugnis daraus |
DE102006038772B4 (de) * | 2006-08-17 | 2009-09-10 | Refractory Intellectual Property Gmbh & Co. Kg | Versatz zur Herstellung eines feuerfesten keramischen Produktes und daraus hergestelltes gebranntes feuerfestes keramisches Produkt |
DE102006040269B4 (de) | 2006-08-28 | 2009-09-24 | Refractory Intellectual Property Gmbh & Co. Kg | Gebranntes feuerfestes keramisches Produkt |
US8030235B2 (en) * | 2008-12-18 | 2011-10-04 | North American Refractories Company | Refractory brick for steel ladles |
FR2954768A1 (fr) * | 2009-12-24 | 2011-07-01 | Saint Gobain Ct Recherches | Poudre pour pise sec vitroceramique |
CN102049464B (zh) * | 2011-01-26 | 2012-07-04 | 东风汽车有限公司 | 实型铸造专用涂料及其制备方法 |
EP3434661B1 (fr) | 2011-03-11 | 2021-04-28 | Saint-Gobain Ceramics&Plastics, Inc. | Objet réfractaire |
KR20140018935A (ko) * | 2011-03-30 | 2014-02-13 | 생-고뱅 세라믹스 앤드 플라스틱스, 인코포레이티드 | 내화성 물체, 유리 오버플로우 형성 블록, 및 내화성 물체를 형성하고 이용하는 방법 |
MY185000A (en) | 2011-04-13 | 2021-04-30 | Saint Gobain Ceramics | Refractory object including beta alumina and processes of making and using the same |
CN102320844B (zh) * | 2011-07-08 | 2013-07-31 | 郑州市裕丰耐火材料有限公司 | Rh浸渍管及环流管用铝镁锆砖及其制备方法 |
RU2477452C1 (ru) * | 2011-08-22 | 2013-03-10 | Учреждение Российской академии наук Институт химии твердого тела и механохимии Сибирского отделения РАН (ИХТТМ СО РАН) | Способ анализа вяжущего материала на основе альфа-оксида алюминия (экспресс-метод) |
ES2412454B1 (es) * | 2011-10-14 | 2014-05-07 | Refractaria, S.A. | Material refractario de protección para hornos de clinker (cemento) que evita el ataque termo-químico sin la formación de encostramiento o anillos. |
HUE046163T2 (hu) * | 2012-01-11 | 2020-02-28 | Saint Gobain Ceramics | Tûzálló tárgy |
DE102012004987B4 (de) * | 2012-03-14 | 2014-03-06 | Heraeus Electro-Nite International N.V. | Vorrichtung zur Temperaturmessung in Metallschmelzen |
RU2530935C2 (ru) * | 2013-01-09 | 2014-10-20 | Федеральное Государственное Бюджетное Учреждение Науки Институт Геологии Дагестанского Научного Центра Российской Академии Наук | Огнеупорная масса для футеровки тепловых агрегатов |
DE102013010854A1 (de) * | 2013-06-28 | 2014-12-31 | Refratechnik Holding Gmbh | Feuerfester Versatz und seine Verwendung |
FR3008967B1 (fr) * | 2013-07-26 | 2016-12-30 | Saint-Gobain Centre De Rech Et D'Etudes Europeen | Produit a haute teneur en alumine |
WO2015148631A1 (fr) * | 2014-03-27 | 2015-10-01 | Corning Incorporated | Corps en oxyde de céramique, procédé de fabrication de celui-ci, et procédé de fabrication d'une feuille de verre |
EP3262011A4 (fr) | 2015-02-24 | 2018-08-01 | Saint-Gobain Ceramics&Plastics, Inc. | Article réfractaire et procédé de fabrication |
RU2612375C1 (ru) * | 2016-02-09 | 2017-03-09 | Юлия Алексеевна Щепочкина | Керамическая масса для изготовления облицовочной плитки, печных изразцов |
CN106007745A (zh) * | 2016-05-17 | 2016-10-12 | 江苏江能新材料科技有限公司 | 一种红土镍矿回转窑专用浇注料及其制造方法 |
JP6758147B2 (ja) * | 2016-10-11 | 2020-09-23 | 黒崎播磨株式会社 | コージェライト含有アルミナ−シリカれんがの製造方法 |
CN108530042A (zh) * | 2018-06-08 | 2018-09-14 | 郑州凯翔耐火材料有限公司 | 一种烧制高抗热震铝矾土砖及其生产工艺 |
CN111763092A (zh) * | 2020-06-17 | 2020-10-13 | 林国强 | 一种抗结渣高温耐磨复合材料及其制备方法 |
CN115403253B (zh) * | 2022-10-09 | 2023-06-16 | 江苏德和绝热科技有限公司 | 一种高强度耐高温泡沫玻璃的生产工艺 |
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US3652307A (en) * | 1969-07-07 | 1972-03-28 | Gen Refractories Co | Alumina refractories |
FR2142149A5 (en) * | 1971-06-14 | 1973-01-26 | Snecma | Magnesia-based refractory concrete - forcasting or ramming |
DE2605949C3 (de) * | 1976-02-14 | 1979-03-15 | Kwm Keramik-Werk Mering Gmbh & Co Kg, 8905 Mering | Brennhilfsmittel mit verbesserter Temperaturwechselbestandigkeit |
US4231800A (en) * | 1979-05-14 | 1980-11-04 | Valley Mineral Products Corporation | Dry heat setting refractory and methods of using same |
CA1156686A (fr) * | 1980-10-27 | 1983-11-08 | Berhl E. Wishon | Brique refractaire en aluminosilicate |
US4391917A (en) * | 1980-10-27 | 1983-07-05 | Dresser Industries, Inc. | Alumino-silicate refractory brick |
GB2138927B (en) * | 1983-02-18 | 1986-09-03 | Glaverbel | Adding to silica refractory structures |
US5298200A (en) * | 1987-11-18 | 1994-03-29 | G-C Dental Industrial Corp. | Dental refractory model materials |
JPH0657619B2 (ja) * | 1987-12-28 | 1994-08-03 | 品川白煉瓦株式会社 | カーボン含有耐火物 |
DE4403869C2 (de) * | 1994-02-08 | 1998-01-15 | Veitsch Radex Ag | Feuerfester keramischer Versatz und dessen Verwendung |
FR2798378B1 (fr) * | 1999-08-17 | 2001-12-21 | Philippe Dubois | Composition pour moulage |
US6753299B2 (en) * | 2001-11-09 | 2004-06-22 | Badger Mining Corporation | Composite silica proppant material |
-
2005
- 2005-03-03 WO PCT/EP2005/002226 patent/WO2005085155A1/fr active Application Filing
- 2005-03-03 BR BRPI0507341-3A patent/BRPI0507341A/pt not_active Application Discontinuation
- 2005-03-03 US US10/598,543 patent/US20070203013A1/en not_active Abandoned
- 2005-03-03 CA CA2558526A patent/CA2558526C/fr not_active Expired - Fee Related
- 2005-03-03 RU RU2006134295/03A patent/RU2386604C2/ru not_active IP Right Cessation
- 2005-03-03 EP EP05715686A patent/EP1720812A1/fr not_active Withdrawn
-
2006
- 2006-09-15 ZA ZA2006/07731A patent/ZA200607731B/en unknown
Non-Patent Citations (1)
Title |
---|
See references of WO2005085155A1 * |
Also Published As
Publication number | Publication date |
---|---|
WO2005085155A1 (fr) | 2005-09-15 |
RU2006134295A (ru) | 2008-04-10 |
CA2558526C (fr) | 2010-06-22 |
ZA200607731B (en) | 2008-04-30 |
BRPI0507341A (pt) | 2007-07-03 |
US20070203013A1 (en) | 2007-08-30 |
CA2558526A1 (fr) | 2005-09-15 |
RU2386604C2 (ru) | 2010-04-20 |
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