WO2015129745A1 - 鋼の鋳造用耐火物,及びスライディングノズル装置用のプレート,並びに鋼の鋳造用耐火物の製造方法 - Google Patents
鋼の鋳造用耐火物,及びスライディングノズル装置用のプレート,並びに鋼の鋳造用耐火物の製造方法 Download PDFInfo
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- WO2015129745A1 WO2015129745A1 PCT/JP2015/055388 JP2015055388W WO2015129745A1 WO 2015129745 A1 WO2015129745 A1 WO 2015129745A1 JP 2015055388 W JP2015055388 W JP 2015055388W WO 2015129745 A1 WO2015129745 A1 WO 2015129745A1
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- WIPO (PCT)
- Prior art keywords
- refractory
- mass
- aluminum
- metal
- casting
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 39
- 239000010959 steel Substances 0.000 title claims abstract description 39
- 238000005266 casting Methods 0.000 title claims abstract description 29
- 238000004519 manufacturing process Methods 0.000 title claims description 20
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 131
- 229910052751 metal Inorganic materials 0.000 claims abstract description 106
- 239000002184 metal Substances 0.000 claims abstract description 106
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 81
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 38
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 34
- 239000011819 refractory material Substances 0.000 claims abstract description 34
- 229910044991 metal oxide Inorganic materials 0.000 claims abstract description 15
- 150000004706 metal oxides Chemical class 0.000 claims abstract description 15
- 239000002994 raw material Substances 0.000 claims description 25
- 238000010438 heat treatment Methods 0.000 claims description 21
- 229910045601 alloy Inorganic materials 0.000 claims description 16
- 239000000956 alloy Substances 0.000 claims description 16
- 239000004927 clay Substances 0.000 claims description 14
- 229910052710 silicon Inorganic materials 0.000 claims description 13
- 239000010703 silicon Substances 0.000 claims description 13
- 229910004298 SiO 2 Inorganic materials 0.000 claims description 12
- 229910018072 Al 2 O 3 Inorganic materials 0.000 claims description 11
- 239000002245 particle Substances 0.000 claims description 11
- 229910000861 Mg alloy Inorganic materials 0.000 claims description 10
- 229910010413 TiO 2 Inorganic materials 0.000 claims description 10
- SNAAJJQQZSMGQD-UHFFFAOYSA-N aluminum magnesium Chemical compound [Mg].[Al] SNAAJJQQZSMGQD-UHFFFAOYSA-N 0.000 claims description 10
- 238000000465 moulding Methods 0.000 claims description 10
- 229910000676 Si alloy Inorganic materials 0.000 claims description 9
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 claims description 9
- 239000011812 mixed powder Substances 0.000 claims description 8
- GEIAQOFPUVMAGM-UHFFFAOYSA-N ZrO Inorganic materials [Zr]=O GEIAQOFPUVMAGM-UHFFFAOYSA-N 0.000 claims description 6
- 239000011347 resin Substances 0.000 claims description 5
- 229920005989 resin Polymers 0.000 claims description 5
- 239000000126 substance Substances 0.000 claims description 5
- 230000005484 gravity Effects 0.000 claims description 3
- 238000004898 kneading Methods 0.000 claims description 3
- 229920001187 thermosetting polymer Polymers 0.000 claims description 3
- 239000004411 aluminium Substances 0.000 abstract 3
- 230000015556 catabolic process Effects 0.000 abstract 1
- 238000006243 chemical reaction Methods 0.000 description 49
- 230000035939 shock Effects 0.000 description 43
- 230000007797 corrosion Effects 0.000 description 41
- 238000005260 corrosion Methods 0.000 description 41
- 230000000052 comparative effect Effects 0.000 description 22
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 18
- 238000007254 oxidation reaction Methods 0.000 description 16
- 230000003647 oxidation Effects 0.000 description 15
- 230000000694 effects Effects 0.000 description 14
- 238000000034 method Methods 0.000 description 14
- 230000006378 damage Effects 0.000 description 13
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 12
- 238000012360 testing method Methods 0.000 description 10
- 238000000280 densification Methods 0.000 description 9
- 239000000395 magnesium oxide Substances 0.000 description 9
- 235000012245 magnesium oxide Nutrition 0.000 description 9
- 239000000203 mixture Substances 0.000 description 9
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 8
- 230000007423 decrease Effects 0.000 description 8
- 230000029087 digestion Effects 0.000 description 8
- 239000000463 material Substances 0.000 description 8
- 238000002844 melting Methods 0.000 description 8
- 230000008018 melting Effects 0.000 description 8
- CAVCGVPGBKGDTG-UHFFFAOYSA-N alumanylidynemethyl(alumanylidynemethylalumanylidenemethylidene)alumane Chemical compound [Al]#C[Al]=C=[Al]C#[Al] CAVCGVPGBKGDTG-UHFFFAOYSA-N 0.000 description 7
- 239000000470 constituent Substances 0.000 description 6
- 230000014509 gene expression Effects 0.000 description 6
- 239000000843 powder Substances 0.000 description 6
- 239000011800 void material Substances 0.000 description 6
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 5
- 239000003575 carbonaceous material Substances 0.000 description 5
- 230000003247 decreasing effect Effects 0.000 description 5
- 239000010439 graphite Substances 0.000 description 5
- 229910002804 graphite Inorganic materials 0.000 description 5
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 4
- 229910002091 carbon monoxide Inorganic materials 0.000 description 4
- 230000008859 change Effects 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 4
- 238000005336 cracking Methods 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 239000011777 magnesium Substances 0.000 description 4
- 230000009257 reactivity Effects 0.000 description 4
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 4
- 229910010271 silicon carbide Inorganic materials 0.000 description 4
- 230000003078 antioxidant effect Effects 0.000 description 3
- 230000006866 deterioration Effects 0.000 description 3
- 238000011156 evaluation Methods 0.000 description 3
- 238000005470 impregnation Methods 0.000 description 3
- 239000012535 impurity Substances 0.000 description 3
- 230000008595 infiltration Effects 0.000 description 3
- 238000001764 infiltration Methods 0.000 description 3
- 150000001247 metal acetylides Chemical class 0.000 description 3
- 150000004767 nitrides Chemical class 0.000 description 3
- 230000001590 oxidative effect Effects 0.000 description 3
- 230000035699 permeability Effects 0.000 description 3
- 230000000704 physical effect Effects 0.000 description 3
- 239000011148 porous material Substances 0.000 description 3
- 230000003746 surface roughness Effects 0.000 description 3
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- 238000002441 X-ray diffraction Methods 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical compound [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 2
- 239000003963 antioxidant agent Substances 0.000 description 2
- 238000009749 continuous casting Methods 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 2
- 229910052593 corundum Inorganic materials 0.000 description 2
- 239000010431 corundum Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 230000001627 detrimental effect Effects 0.000 description 2
- 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 description 2
- 230000003628 erosive effect Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 238000010813 internal standard method Methods 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 229910052863 mullite Inorganic materials 0.000 description 2
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 2
- 239000005011 phenolic resin Substances 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 239000002893 slag Substances 0.000 description 2
- 229910052596 spinel Inorganic materials 0.000 description 2
- 239000011029 spinel Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 229910052783 alkali metal Inorganic materials 0.000 description 1
- 229910000272 alkali metal oxide Inorganic materials 0.000 description 1
- 150000001340 alkali metals Chemical class 0.000 description 1
- WNROFYMDJYEPJX-UHFFFAOYSA-K aluminium hydroxide Chemical compound [OH-].[OH-].[OH-].[Al+3] WNROFYMDJYEPJX-UHFFFAOYSA-K 0.000 description 1
- INJRKJPEYSAMPD-UHFFFAOYSA-N aluminum;silicic acid;hydrate Chemical compound O.[Al].[Al].O[Si](O)(O)O INJRKJPEYSAMPD-UHFFFAOYSA-N 0.000 description 1
- 230000003064 anti-oxidating effect Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 229910001570 bauxite Inorganic materials 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 238000011088 calibration curve Methods 0.000 description 1
- 239000000084 colloidal system Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 239000010443 kyanite Substances 0.000 description 1
- 229910052850 kyanite Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000011344 liquid material Substances 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 235000010755 mineral Nutrition 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- 238000010405 reoxidation reaction Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000002436 steel type Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N titanium dioxide Inorganic materials O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 1
- 239000011882 ultra-fine particle Substances 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
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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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- 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
- C04B2235/42—Non metallic elements added as constituents or additives, e.g. sulfur, phosphor, selenium or tellurium
- C04B2235/428—Silicon
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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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- 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
- C04B2235/48—Organic compounds becoming part of a ceramic after heat treatment, e.g. carbonising phenol resins
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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
- 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
Definitions
- the present invention relates to a refractory for casting steel, a plate for a sliding nozzle device using the refractory, and further relates to a method for manufacturing the refractory.
- the plate for the sliding nozzle device (hereinafter referred to as “sliding nozzle plate”, the refractory for this plate is referred to as “plate refractory”) is the secondary process in the ladle as a member for controlling the flow rate of molten metal.
- sliding nozzle plate the refractory for this plate is referred to as “plate refractory”
- plate refractory is the secondary process in the ladle as a member for controlling the flow rate of molten metal.
- this sliding nozzle plate is a component that controls the flow of molten metal such as molten steel, it requires a very high level of performance and has excellent properties that can cope with various severe conditions in a well-balanced manner. It is necessary to do.
- the sliding nozzle plate has chemical actions such as rapid corrosion and corrosion caused by molten metal and molten slag, in addition to physical actions such as rapid thermal shock and wear caused by molten metal flow. Therefore, products with excellent thermal shock resistance, wear resistance, corrosion resistance, strength characteristics, etc. are required as characteristics to be provided.
- alumina / carbon refractories having the most stable durability are widely used.
- Patent Document 1 proposes a fired plate refractory that is formed by adding a maximum of 10% by mass of expanded graphite and a maximum of 8% by mass of metal to a refractory aggregate and heat-treating it at 1000 ° C. or higher. ing.
- the fired plate refractory has no effect of improving the thermal shock resistance of the metal added as an antioxidant, the thermal shock resistance is improved by the addition of expanded graphite. As the strength is lowered and the roughness of the sliding part is increased, the service life is reduced.
- Patent Document 2 generically refers to unfired or lightly fired products (hereinafter referred to as “nonfired” and “lightly fired”) by adding a low melting point metal and heat treatment at a temperature of 1000 ° C. or less.
- a plate refractory called “non-fired” has been proposed.
- Advantages of non-fired plate refractories include high hot strength due to the addition of a large amount of metal and corrosion resistance against molten steel. When the refractory comes into contact with molten steel, the structure produced near the working surface is densified by the product produced by the reaction of the metal, suppressing the infiltration of slag.
- Non-fired plate refractories have excellent FeO resistance, but on the other hand, they have the disadvantages that the structure becomes excessively dense due to heat reception during casting, the elasticity becomes extremely high, and the thermal shock resistance is low. For this reason, there are problems such as edge cracks and cracks due to thermal shock.
- the carbon mass is in the range of 0.2 to 0.45 times that of an aluminum-containing metal, and the carbon and metal are reacted without excess or deficiency, and the strength, oxidation resistance, corrosion resistance, and thermal shock resistance of the refractory. It has been shown to increase sex. However, it does not take into account the increase in volume due to the reaction that occurs when receiving heat of metallic aluminum, and its thermal shock resistance is insufficient because the elastic modulus increases significantly due to excessive densification.
- JP 2003-245770 A Japanese Patent Publication No. 60-29664 JP 2012-200733 A
- the problem to be solved by the present invention is to suppress the destruction of a refractory containing metal aluminum.
- the present invention relates to the following steel refractories for casting, plates for sliding nozzle devices, and methods for producing refractories for steel casting.
- a refractory for casting steel made of a refractory material containing 1 to 15% by mass of free carbon, 1 to 15% by mass of metallic aluminum, and the balance comprising a metal oxide.
- a refractory for casting steel characterized by satisfying Equation 1 when the content of metallic aluminum in the object is Al mass%, the apparent porosity is P%, and the bulk specific gravity is D. 0.31 ⁇ Al ⁇ (P-4) / D Formula 1 (Claim 1) 2.
- the metal oxide includes one or more components selected from Al 2 O 3 , SiO 2 , ZrO 2 , MgO, TiO 2, and the total amount of the balance is 100% by mass, the total of the components is The steel refractory for casting according to the above 1, which is 95% by mass or more.
- (Claim 2) 3. The refractory as described in 1 or 2 above, containing metal silicon in an amount of 0.5 mass% to 4 mass%. (Claim 3) 4). 4. The refractory according to any one of 1 to 3, wherein the content of metal aluminum is 64% by mass or more and 15% by mass or less. (Claim 4) 5. 4. The refractory according to any one of 1 to 3 above, wherein the content of metal aluminum is 6% by mass or more and 15% by mass or less. (Claim 5) 6). 5. A plate for a sliding nozzle device, part or all of which is made of the steel casting refractory according to any one of 1 to 4 above. (Claim 6) 7).
- Mixed powder comprising a refractory material comprising a metal oxide comprising a metal containing aluminum and the balance comprising one or more components selected from Al 2 O 3 , SiO 2 , ZrO 2 , MgO, TiO 2 Adding a thermosetting resin in an amount of 1% by mass to 7% by mass and kneading to produce a molding clay, a step of pressure-molding the molding clay, and a heat treatment step.
- the metal containing aluminum contained in the mixed powder is a scaly shape having a maximum length of 140 ⁇ m or less, a particle shape having a particle size of 140 ⁇ m or less, or a maximum cross-sectional diameter of 200 ⁇ m or less and a maximum length of 5 mm.
- the manufacturing method of the refractory material for casting of steel of Claim 7 which originates in the raw material which consists of the metal aluminum simple substance of 1 or several form selected from the following fibrous forms. (Claim 8) 9.
- the reaction that occurs when receiving heat of metallic aluminum is mainly a reaction with carbon monoxide or carbon.
- receiving heat of metallic aluminum it means during heat treatment during production or during use in casting operations, that is, during steel passing. These reactions produce carbides or oxides that increase in volume.
- metal aluminum reduces carbon monoxide gas to supply carbon to the refractory structure, and also produces aluminum carbide or aluminum oxide.
- the generation of aluminum oxide may be caused by reaction with oxygen in the air.
- the metal aluminum content is set to 1% by mass or more and 15% by mass or less is to exhibit the antioxidant effect, the strength improvement effect, and the densification effect, but if the content is less than 1% by mass, the above effect is insufficient. This is because if it exceeds 15% by mass, too much carbide or oxide is produced, causing structural destruction or deterioration.
- reaction of metal aluminum with heat receiving carbon monoxide and carbon can be expressed by the following equation. 2Al + 3CO ⁇ Al 2 O 3 + 3C Formula 2 4Al + 4CO ⁇ Al 4 O 4 C + 3C Formula 3 4Al + 3C ⁇ Al 4 C 3 Formula 4
- volume increase rates due to these reactions are 135% (volume is 2.35 times), 115% (volume is 2.15 times), and 0% (volume is 1.0 times or the same).
- Formula 4 is 0 because carbon exists in the refractory composition before metal aluminum reacts, and the total amount of the volume of metal aluminum and carbon before and after the reaction is the same.
- the volume increase due to such a reaction fills the voids existing in the refractory, so that the structure of the refractory is densified.
- the volume increase due to the reaction of metallic aluminum exceeds the amount of voids existing in the refractory before the reaction, the volume increase due to the reaction is absorbed inside the refractory. It can no longer be done and the refractory itself will expand or be destroyed.
- the material is designed so that the volume increase after the reaction of the metallic aluminum before the reaction does not exceed the amount of voids existing in the refractory before the reaction.
- oxidation resistance, infiltration resistance, corrosion resistance, wear resistance, etc. are improved to some extent. Although it can be done, it is not always sufficient, and it becomes unstable.
- the void volume in the refractory before the reaction is hereinafter simply referred to as “optimum amount”.
- the present invention provides the above-mentioned optimal amount of voids in the refractory according to the content of metallic aluminum before the reaction in the refractory.
- the prior art does not have the above-mentioned technical idea, and in order to densify the refractory regardless of the metal aluminum content, it has mainly been impregnated with a liquid material that retains carbon after receiving heat such as tar. .
- the present invention eliminates such disadvantages of the prior art, does not increase voids in the refractory due to carbon reoxidation, and the like, and the minimum amount of refractory inside as described above according to the content of metal aluminum.
- the amount of voids is provided.
- the volume increase due to the reaction of metallic aluminum can be expressed as follows.
- the density of metallic aluminum is 2.7 g ⁇ cm ⁇ 3
- the volume of metallic aluminum contained in 1 g of the refractory product is ⁇ 1 ⁇ (Al / 100) ⁇ where the content of metallic aluminum is Al mass%. /2.7.
- the volume increase rate due to the reaction of metal aluminum is the above-mentioned formula 2, formula 3, formula 4
- the volume increase rate is approximately the same as the volume increase rate calculated on the assumption that each reaction occurs at a ratio of approximately 1: 1: 1.
- ⁇ V 0.31 ⁇ (Al / 100) Equation 6 It becomes.
- the volume increase caused by the reaction due to the heat reception according to the amount of metal aluminum contained in the refractory can be absorbed within the range of the apparent porosity of the refractory. .
- the volume increase of the metal aluminum is a lower limit value that does not excessively expand or destroy the refractory. In other words, if the right side of Equation 1 is greater than or equal to this lower limit, the volume increase due to the reaction of the metallic aluminum will not increase the volume of the refractory and cause excessive expansion or destruction of the refractory structure. .
- the right side of Formula 1 is larger than the left side. Since the apparent porosity of the refractory, that is, the volume of the void, is larger than the volume increase due to the reaction of the metal aluminum, the excess void suppresses the increase in the elastic modulus of the refractory after the reaction of the metal aluminum. , Or contribute to increasing toughness. However, if the difference between the right side and the left side increases, the corrosion resistance, strength, and the like may be reduced. Therefore, it is preferable to optimize according to individual use conditions and equipment conditions.
- Thermal shock is one of the factors that cause destruction of a refractory that has been subjected to operation at least once and has received heat, that is, a refractory that has increased in volume due to the reaction of metal aluminum. Therefore, thermal shock resistance is mainly effective as an index for suppressing destruction during repeated use.
- thermal shock resistance is a characteristic that should be optimized according to individual operating conditions.
- the refractory of the present invention shows a characteristic in a state as a product, that is, a state in which the refractory is used for a predetermined use. That is, the feature of the present invention is not limited to a specific temperature, and further, in a state that can absorb at least expansion due to oxidation of metal aluminum, etc., close to the state when it is used for a predetermined application. It relates to refractories (porosity, etc.).
- the lower limit value of the apparent porosity due to the reaction of this metal aluminum was obtained by experiments.
- an alumina-carbon refractory with a metal aluminum content of 8% by mass and an apparent porosity of 5% was heat treated at 1500 ° C. in a carbonaceous material, that is, in a CO gas or CO 2 gas atmosphere, the apparent porosity decreased to 4%.
- an alumina-carbon refractory having a metal aluminum content of 8% by mass and an apparent porosity of 4% was heat treated at 1500 ° C. in the carbonaceous material, the apparent porosity remained at 4%.
- the decrease in apparent porosity due to the reaction of metallic aluminum indicates that the limit is up to 4%. That is, the increase in volume due to the reaction of metallic aluminum can be absorbed in the refractory until the apparent porosity becomes 4%.
- the apparent porosity is a value measured using water or kerosene by a boiling method or a vacuum method by an apparent porosity measurement method described in JIS R 2205.
- the content of aluminum as a metal can be determined by X-ray diffraction.
- standard samples of various patterns were prepared, their calibration curves were prepared and quantified by the internal standard method.
- an alloy containing metal aluminum may be used within the range of the content (residual amount) of metal aluminum described above. That is, the metallic aluminum as a raw material contained in the powder mixed in the production of the casting refractory of the present invention is a raw material made of a metallic aluminum alone, or a part or all of the metallic aluminum is metallic aluminum. It can also be a raw material made of an alloy containing.
- the alloy containing metal aluminum is preferably an aluminum-magnesium alloy or an aluminum-silicon alloy.
- an aluminum-magnesium alloy or aluminum-silicon alloy the present inventors have experimented that the relationship between the content (residual amount) of metal aluminum and the porosity should be in accordance with the aforementioned conditions. Etc.
- the volume expansion coefficient when Mg is oxidized to MgO is smaller than Al by about 20 to 30%, which is an index with Al as 100. This is because Mg does not have a detrimental effect on the destruction of the refractory.
- the volume expansion coefficient when using an aluminum-silicon alloy is approximately 200%, which is an index with Al as 100 compared to Al, but the Si component in a high temperature range of about 1000 ° C or higher. Part or all of the material becomes SiO and volatilizes, increasing the porosity of the refractory. This prevents Si from having a detrimental effect on the destruction of the refractory.
- the melting temperature of these alloys is about 430 ° C. when the magnesium content is about 50% by mass for an aluminum-magnesium alloy, and about 13% by mass for the aluminum-silicon alloy, for example. In this case, the temperature is about 480 ° C.
- the temperature at which these alloys melt is lower than about 660 ° C. of metallic aluminum alone.
- these alloys can be used in combination, or these alloys and metal aluminum alone can be used in combination.
- the present invention relates to the relationship between the metal aluminum content and the apparent porosity, that is, the expansion of the volume that is caused by the reaction that takes place during the heat reception of the metal aluminum is reduced by the voids in the refractory structure. Can suppress destruction of the refractory structure.
- thermal shock resistance can be improved by suppressing densification and increase in elastic modulus at the voids in the refractory structure.
- the prior art has taken measures such as suppressing the content of metallic aluminum and using a large amount of carbonaceous raw materials such as graphite and refractory aggregates having excellent thermal shock resistance. It was.
- such conventional techniques cause a decrease in corrosion resistance, oxidation resistance, wear resistance, and the like.
- the present invention can contain a large amount of metallic aluminum, and is excellent in thermal shock resistance, but on the other hand, carbonaceous raw materials such as graphite and the like that have reduced corrosion resistance, oxidation resistance, wear resistance, etc. There is no need to use a large amount of refractory aggregate.
- the thermal shock resistance of the refractory can be maintained or enhanced, and the corrosion resistance, oxidation resistance, wear resistance, etc. can be further improved.
- the physical properties such as thermal shock resistance, corrosion resistance, oxidation resistance, and wear resistance according to the content of metal aluminum and according to individual operating conditions are arbitrarily adjusted and optimized.
- the refractory material of the present invention is suitable for an upper nozzle, a lower nozzle, a tuyere, a sliding nozzle plate for flow rate control, etc. used for steel casting.
- satisfying the formula 1 means adjusting the apparent porosity of the refractory before the metal aluminum reacts.
- the refractory of the present invention contains 1% by mass to 15% by mass of metallic aluminum, it is not necessary to specify the heat treatment conditions for obtaining the refractory.
- the particle size and shape of metallic aluminum can be used properly according to the characteristics described below. That is, in terms of reactivity, metallic aluminum on the scale is the best, but it reduces formability. On the other hand, in terms of formability, it is desirable to use particulate aluminum (also referred to as “atomize”). Also, when the maximum length or particle size of metallic aluminum is more than 140 ⁇ m, it is difficult to disperse metallic aluminum into the clay, and the effect of densification due to the reaction of metallic aluminum is difficult to occur uniformly. Things may break. Therefore, the maximum length or particle size of metallic aluminum is preferably 140 ⁇ m or less. It is also effective to use fibrous metallic aluminum that has a high crack suppression effect.
- the maximum diameter is preferably 200 ⁇ m or less and the maximum length is 5 mm or less in order to improve dispersibility.
- the maximum diameter exceeds 200 ⁇ m and when the maximum length exceeds 5 mm, the flexibility becomes poor and the refractory structure tends to be roughened, and the porosity may be excessively increased.
- a scale-like, spherical, or fibrous metallic aluminum may be used in combination as appropriate depending on the balance between formability and reactivity and other required properties. In the case of scaly, the thinner the thickness, the higher the reactivity. There is no limit to this thickness.
- the metal aluminum is contained in the refractory after the heat treatment in an amount of 1% by mass to 15% by mass.
- the metal aluminum content in the clay before forming may be adjusted according to the heat treatment conditions by adding, for example, about 1% by mass to 20% by mass in the clay according to the individual composition, heat treatment conditions, and the like.
- Metal aluminum is for preventing oxidation, improving strength, and exerting a densification effect. If it is less than 1% by mass, the oxidation resistance is not sufficient, and the working surface is densified by the reaction of metal aluminum. Is not clearly obtained. When it exceeds 15 mass%, there is a possibility of causing tissue deterioration during use.
- the free carbon in the refractory of the present invention is 1% by mass or more and 10% by mass or less.
- free carbon means carbon not forming a compound with other elements, regardless of whether it is crystalline or amorphous.
- the basic part of the bonding function of the refractory structure of the present invention is borne by carbon derived from a resin or the like. In order to form and maintain the basic structure of this refractory, 1% by mass or more of free carbon is required. Exceeding 10% by mass is not preferable because the oxidation resistance decreases.
- the remaining carbon of 1% by mass to 10% by mass of free carbon and 1% by mass to 15% by mass of metal aluminum is made of a refractory material containing a metal oxide. Specifically, it is possible to obtain an optimum component configuration according to the operating conditions such as the steel type and the usage time.
- the refractory material containing the remaining metal oxide refers to metal oxides, carbides, nitrides, metals, and the like that are used as raw materials for steel refractories.
- metal oxide for example, one or a plurality of components selected from Al 2 O 3 , SiO 2 , ZrO 2 , MgO, and TiO 2 can be used.
- Alkali metal oxides and CaO when coexisting with Al 2 O 3 or the like, produce a low melt, so it is not preferable to use them as main constituents unless they are dispersed at several mass% or less.
- raw materials mainly containing Al 2 O 3 components such as corundum, and refractory materials containing SiO 2 components and MgO components in addition to Al 2 O 3 components, such as mullite and silimanite family materials. It is possible to use raw materials containing ZrO 2 in various forms (including andrewite and kyanite), spinel, and the like.
- the TiO 2 component can be used as a mineral composed of TiO 2 such as rutile for the purpose of accelerating sintering or the like, and in a natural alumina material (bauxite, clay shale, etc.) Including the case where it is included.
- the SiO 2 component for example, amorphous amorphous silica, quartz, cristobalite, etc., in the case of the MgO component, periclase, etc.
- the raw material which has these single components as a main component can also be used.
- the refractory of the present invention further contains carbide, nitride, metal, etc. such as SiC, SiN, B 4 C, and BN for the purpose of strengthening the antioxidant function at high temperature and adjusting the elastic modulus. be able to.
- carbide, nitride, metal, etc. such as SiC, SiN, B 4 C, and BN for the purpose of strengthening the antioxidant function at high temperature and adjusting the elastic modulus. be able to.
- the total of the metal oxide components is preferably 95% by mass or more when the total amount of the remainder is 100% by mass. That is, it is preferable that the total of carbides, nitrides, metals, impurities contained in the raw materials, impurities mixed in the manufacturing process, and the like other than these metal oxides is less than 5% by mass. If the component other than these metal oxides exceeds 5% by mass in the balance, the corrosion resistance, the thermal shock resistance, and the like are liable to occur.
- the refractory may be used a plurality of times (repeatedly) in addition to the use of the refractory only once. If it is used multiple times and the temperature drops in the meantime, the produced aluminum carbide may be digested (hydrated) to deteriorate or destroy the refractory structure. In order to suppress deterioration or destruction of the refractory structure caused by such digestion of aluminum carbide, it is preferable to use metal silicon in combination with the refractory in an amount of about 0.5 mass% to 4 mass%. In the case of a carbon-containing refractory containing metallic aluminum, in a temperature range of 700 ° C.
- metallic aluminum reacts with carbon and begins to produce aluminum carbide.
- This aluminum carbide is easily dissolved with water at normal temperature and normal pressure.
- aluminum hydroxide is produced, which is accompanied by an increase in volume and weight, so the refractory often collapses (digestion phenomenon).
- Silica produced by the oxidation reaction of metallic silicon is dissolved in aluminum carbide to prevent digestion of aluminum carbide.
- metallic silicon undergoes a reaction such as Si + 2CO ⁇ SiO 2 + 2C, reduces the carbon monoxide gas, and supplies carbon to the refractory structure to improve the oxidation resistance.
- the metal silicon content is preferably 4% by mass or less.
- Metallic silicon contributes to the prevention of digestion and also has an antioxidation effect on the refractory structure in a high temperature range (temperature range exceeding about 1200 ° C.).
- the refractory according to the present invention can basically employ a production method according to a conventional production method for a refractory containing metal aluminum or a metal aluminum alloy.
- the metal Al content in the refractory basically provided as a product is set to 1% by mass or more and 15% by mass or less, and the present invention of the formula 1 or the like is provided.
- the forming clay is made of a refractory material containing a metal oxide containing a metal containing aluminum and the balance being one or more components selected from Al 2 O 3 , SiO 2 , ZrO 2 , MgO, TiO 2.
- a thermosetting resin such as a phenol resin is added to the mixed powder in an amount of 1% by mass to 7% by mass and kneaded.
- the metal raw material containing aluminum contained in the mixed powder is a scaly shape having a maximum length of 140 ⁇ m or less, a particle shape having a particle size of 140 ⁇ m or less, or a maximum cross-sectional diameter of 200 ⁇ m or less.
- one or a plurality of forms can be selected from a fibrous form having a maximum length of 5 mm or less and used in combination.
- the raw material which the one part or all consists of an alloy containing metal aluminum can also be used.
- the alloy containing metallic aluminum is preferably an aluminum-magnesium alloy or an aluminum-silicon alloy.
- metal raw materials have different melting points and reactivities, which cause changes in physical properties of refractories such as strength development, corrosion resistance, thermal shock resistance, and fracture resistance.
- the selection or combination of these metal raw materials can be arbitrarily prepared according to individual operating conditions and characteristics (for example, thermal shock resistance, corrosion resistance, fracture resistance) required according to individual needs.
- the apparent porosity may be adjusted, for example, by adjusting the molding pressure so as to satisfy the above-mentioned formula 1.
- the pressure and compression allowance are varied during molding, or volatile or flammable liquids (including colloids) and ultrafine particles are dispersed in the clay.
- Arbitrary methods such as adjusting the raw material particle size and form can be adopted.
- the heat treatment is performed as long as the metal Al content in the refractory after the heat treatment is 1% by mass or more and 15% by mass or less and satisfies the above formula 1.
- the temperature, etc. May be arbitrarily set so as to suit individual operation conditions and equipment conditions.
- the temperature can be appropriately optimized in a temperature range between about 1100 ° C. and a temperature at which a resin bearing a carbon bond is cured.
- the above formula 1 can be satisfied by adjusting the size of metal aluminum particles, the form of presence in the refractory structure, etc. in addition to the atmosphere, time and other heat treatment conditions.
- Example A shows the result of investigating the relationship with the above-mentioned formula 1 with the amount of metallic aluminum (Al) and the amount of free carbon (FC) of the present invention.
- the sample was prepared by kneading a mixture of refractory raw material mainly composed of corundum made of alumina, graphite, metallic aluminum, and phenol resin with a mixer, forming a sliding nozzle plate using a 500-ton vacuum oil press, It was manufactured by performing a heat treatment at 800 ° C. in an oxidizing atmosphere.
- the content of aluminum as a metal was quantified by an internal standard method by X-ray diffraction.
- the sample obtained by the above method is cooled after heat treatment at 1500 ° C. in a carbonaceous material, that is, in a reducing atmosphere, and cracks and defects at room temperature are obtained. The state of was observed and evaluated. A case where a crack that does not maintain the continuity of a part of the sample was rejected was rejected, and indicated as “x” as “push crack” in the table. Although micro cracks or cracks occurred, changes that did not lose the continuity of the sample were accepted and indicated by “ ⁇ ” in the table.
- the elastic modulus and air permeability after the sample was heat treated in a carbonaceous material at 1500 ° C. and then cooled to room temperature were measured, and the rate of change before and after the heat treatment was investigated.
- the air permeability was measured by the method of JIS R2115.
- the elastic modulus was measured by a sonic method.
- the thermal shock resistance test is a four-stage evaluation by observing and evaluating the amount of cracks generated in the sample by immersing the sample produced in the above 40 ⁇ 40 ⁇ 160 mm in hot metal at 1600 ° C. for 3 minutes and air-cooling.
- the case of exceeding the degree of Comparative Example 1 is accepted as “ ⁇ ”, “ ⁇ ”
- the case where it is superior to “” is indicated as “ ⁇ ”
- the case where it is further excellent is indicated as “ ⁇ ”
- the case where it is comparable or inferior to Comparative Example 1 is indicated as “x”.
- Table 1 shows the composition and results of each sample.
- the rate of change of the air permeability is higher when the metal aluminum content is 6% by mass and 15% by mass than when it is 1% by mass, that is, a denser structure is obtained.
- the cases where the content of metal aluminum is 6% by mass and 15% by mass are generally better than the case of 1% by mass. From these facts, it can be seen that the effect of the present invention is higher and preferable when the content of metal aluminum is a high content of at least 6% by mass or more.
- Example B is the result of investigating the influence of metal aluminum content. Table 2 shows the sample configuration and results.
- the metal aluminum content was varied from 0.5 mass% to 16 mass%, but all examples satisfied the formula 1 and no cracking was observed, but 0.5 mass% % (Comparative Example 4), the corrosion resistance was x, and 16 mass% (Comparative Example 5), the corrosion resistance and the thermal shock resistance were x. From these results, it is understood that an appropriate amount of metallic aluminum is 1% by mass to 15% by mass.
- Example A it is understood that the effect of improving the thermal shock resistance and corrosion resistance is more preferable when the content of metal aluminum is a high content of at least 4% by mass or more.
- the content of metal aluminum is preferably as high as possible and more preferably 6% by mass or more from the viewpoint of increasing strength, densification, and high corrosion resistance.
- Example C is the result of investigating the effect of free carbon content. Table 3 shows the sample configuration and results.
- the free carbon content was varied from 0.5 mass% to 11 mass%, but all examples satisfied Formula 1 and no cracking was observed.
- mass% Comparative Example 6
- thermal shock resistance as well as corrosion resistance was x
- 11 mass% Comparative Example 7
- corrosion resistance was x. From these results, it can be seen that an appropriate free carbon content is 1% by mass to 10% by mass.
- Example D is the result of investigating the influence of the types of constituents other than metallic aluminum and free carbon (remainder). Table 4 shows the sample configuration and results.
- Example 19 is an example in which mullite is arranged on a part of coarse aggregate
- Example 20 is an example in which alumina zirconia clinker is arranged on a part of coarse aggregate
- Example 24 is an example in which spinel clinker is arranged on a part of fine powder area.
- Example 25 is an example in which an alumina clinker having a high TiO 2 content is disposed on a part of the coarse aggregate
- Example 26 is an example in which B 4 C is disposed on a part of the fine powder region
- Example 27 is a fine powder. This is an example in which SiC is arranged in a part of the area.
- Examples 17 and 18 are examples in which amorphous silica fine powder is arranged on a part of the coarse aggregate
- Examples 21, 22 and 23 are examples in which periclase fine powder is arranged on a part of the coarse aggregate. It is.
- the constituent materials comprising these components do not significantly affect the reaction of the aluminum metal, and do not cause significant fluctuations in the properties of the refractory, particularly the apparent porosity. There were no push cracks, and good results were obtained. There are differences in the degree of thermal shock resistance and corrosion resistance depending on the characteristics and characteristics of each component.
- Example E is the result of investigating the effect of the presence and content of metallic silicon.
- the digestion test is based on experience by using a method in which the sample is left in a thermostatic chamber maintained at 40 ° C. and humidity is kept at 90 ° C., and evaluated by the weight change rate of the sample after 30 days and the weight before the treatment.
- Table 5 shows the sample composition and results.
- Example 28 The result of the digestion test was “ ⁇ ” in Example 28 containing no metallic silicon, but “ ⁇ ” in Examples 29 to 32 containing metallic silicon, indicating that the digestion resistance of metallic silicon was improved. Is recognized.
- the content of metal silicon since the fall of corrosion resistance is seen in Example 32 which is 5 mass%, and the further fall of corrosion resistance is estimated in content more than this, it may be 4 mass% or less. preferable.
- Example F is an example when the heat treatment temperatures are greatly different. Table 6 shows the sample configuration and results.
- Example 33 shows a temperature range lower than the melting point of metal aluminum
- Example 34 shows an example of a temperature range where the reaction exceeds the melting point of metal aluminum but the reaction is suppressed.
- Example G In Example G, a part or all of the metal Al (not the amount of remaining Al after heat treatment) contained in the clay is partially converted into an aluminum-magnesium alloy (Examples 35 to 41), or an aluminum-silicon alloy (implementation). Examples 42 to 44) show examples of substitution.
- Examples 38 to 41 are examples in which all of the metal in the clay was replaced with an aluminum-magnesium alloy, but the heat treatment conditions were different, and Examples 38 and 39 were examples in an 800 ° C. non-oxidizing atmosphere. 40 and Example 41 are in a non-oxidizing atmosphere at 500 ° C.
- Table 7 shows the sample composition and results.
- Embodiment 35 Any embodiment of Embodiments 35 to 44 satisfies the formula 1, and is not split. Other properties (thermal shock resistance test results and corrosion resistance test results) are also good.
- Example H shows the result of using the refractory material of the present invention as a plate used in a sliding nozzle device used for continuous casting of steel.
- Example 1 The refractories of the samples were each of Example 1 in which the content of metal aluminum was 6% by mass and Formula 1 was satisfied, and Comparative Example 8 and Example 45 that did not satisfy Formula 1 were tar impregnated. It was set as the comparative example 9 which does not satisfy.
- These plates were attached to a 120 ton molten steel pan and used under conditions of repeated use 6 times (ch) each.
- Center crack is a crack that occurs in the sliding direction of the center of the plate and has a strong adverse effect on the service life.
- Erge chipping is a form of destruction in which a portion near the intersection of the inner wall surface (vertical surface) and the sliding surface (horizontal surface) is lost. Both of these evaluations of cracking and thermal shock resistance were evaluated by visual observation, based on the results of use in the actual operation of Comparative Example 8, with a case where the result was superior to that of Comparative Example 8 as “Good”, and even better. The case was indicated as “ ⁇ ”, and the case similar to or inferior to Comparative Example 8 was indicated as “x”.
- Table 8 shows the sample composition and results.
- the plate of Example 45 satisfied Expression 1, and no crack with a large central crack (in the stroke direction) that significantly affected the life of the plate was generated.
- the plate of Comparative Example 8 that does not satisfy Equation 1 the above-mentioned central crack is generated, the edge of the crack tends to expand, and the sliding surface side end portion of the inner hole is further observed.
- the degree of edge defect was larger than that of the plate of Example 45.
- the surface roughness (except for the vicinity of the central crack), which is also an index of corrosion resistance, maintained a good state in both the example and the comparative example.
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Abstract
Description
0.31×Al≦(P-4)/D ・・・式1 (請求項1)
2.前記金属酸化物が,Al2O3,SiO2,ZrO2,MgO,TiO2から選択する1又は複数の成分を含み,前記残部の総量を100質量%とするときに,前記成分の合計が95質量%以上である,前記1に記載の鋼の鋳造用耐火物。(請求項2)
3.金属シリコンを0.5質量%以上4質量%以下含有する,前記1又は前記2に記載の耐火物。(請求項3)
4.金属アルミニウムの含有量が64質量%以上15質量%以下である,前記1から前記3のいずれかに記載の耐火物。(請求項4)
5.金属アルミニウムの含有量が6質量%以上15質量%以下である,前記1から前記3のいずれかに記載の耐火物。(請求項5)
6.一部又は全部が前記1から前記4のいずれかに記載の鋼の鋳造用耐火物から構成された,スライディングノズル装置用のプレート。(請求項6)
7.アルミニウムを含有する金属を含み,残部がAl2O3,SiO2,ZrO2,MgO,TiO2から選択する1又は複数の成分を含む金属酸化物を含む耐火材料からなる混合された粉体に,熱硬化性樹脂を1質量%以上7質量%以下添加し混練して成形用坏土を作製する工程と,前記成形用坏土を加圧成形する工程と,熱処理する工程をと含む,請求項1から請求項5のいずれかに記載の鋼の鋳造用耐火物の製造方法であって,
前記熱処理後の耐火物中の金属アルミニウム含有量を1質量%以上15質量%以下とし,前記式1を満たすように見掛気孔率を調整することを特徴とする,鋼の鋳造用耐火物の製造方法。(請求項7)
8.前記の混合された粉体中に含まれるアルミニウムを含有する金属は,最大長が140μm以下の鱗片状,粒径140μm以下の粒子状,又は横断面の最大径が200μm以下かつ最大長さが5mm以下の繊維状から選択する1又は複数の形態の金属アルミニウム単体からなる原料に由来する,請求項7に記載の鋼の鋳造用耐火物の製造方法。(請求項8)
9.前記の混合された粉体中に含まれるアルミニウムを含有する金属の一部又は全部が,金属アルミニウムを含む合金からなる原料に由来する,請求項7に記載の鋼の鋳造用耐火物の製造方法。(請求項9)
10.前記の金属アルミニウムを含む合金は,アルミニウム-マグネシウム合金又はアルミニウム-シリコン合金である,前記9に記載の鋼の鋳造用耐火物の製造方法。(請求項10)
2Al+3CO → Al2O3+3C ・・・式2
4Al+4CO → Al4O4C+3C ・・・式3
4Al+3C → Al4C3 ・・・式4
ΔV={1×(Al/100)}/2.7×{(1.35+1.15+0)/3}
・・・式5
となり,これを整理すると
ΔV=0.31×(Al/100) ・・・式6
となる。
Vp=(1/D)×{(P-4)/100} ・・・式7
ΔV≦Vp ・・・式8
0.31×(Al/100)≦(1/D)×{(P-4)/100} ・・・式9
0.31×Al≦(P-4)/D ・・・式1
(1)坏土の成形時に成形圧力を増減させて,構成原料間の接触点を減じて又は接触距離等を変化させてその充填度合いを調整する,
(2)坏土の粒度構成を,最密充填の理論曲線から所要量ずらして,構成原料間の接触点は維持した上で構成原料間の空隙を増減させる。
実施例Aは,本発明の金属アルミニウム(Al)量,フリーの炭素(F.C.)量での,前記の式1との関係を調査した結果を示す。
実施例Bは,金属アルミニウム含有量の影響を調査した結果である。表2に試料構成と結果を示す。
実施例Cは,フリーの炭素含有量の影響を調査した結果である。表3に試料構成と結果を示す。
実施例Dは,金属アルミニウム,フリーの炭素以外(残部)の構成物の種類による影響を調査した結果である。表4に試料構成と結果を示す。
実施例Eは,金属シリコンの有無及びその含有量の影響を調査した結果である。消化試験は,温度を40℃,湿度を90℃に保った恒温槽に試料を放置し,30日経過後の試料の重量と前記処理前の重量の重量変化率で評価する方法により,経験上一般的な操業条件で標準的又は下限程度と考えられる耐消化性を備えた実施例29の重量変化率を基準とし,それと同程度以下の場合を「○」で表示し,それより高いものの,通常の操業条件で少なくとも1回の使用が可能と考えられる程度の場合を「△」として表示した。
実施例Fは,熱処理温度が大きく異なる場合の例示である。表6に試料構成と結果を示す。
実施例Gは,坏土中に含有する金属Al(熱処理後の残存Al量ではない)の一部又は全部をアルミニウム-マグネシウム合金(実施例35~実施例41),又はアルミニウム-シリコン合金(実施例42~実施例44)に置換した例を示す。
実施例Hは,本発明の耐火物を鋼の連続鋳造に用いられるスライディングノズル装置に使用するプレートとして使用した結果を示す。
Claims (10)
- フリーの炭素を1質量%以上10質量%以下,金属アルミニウムを1質量%以上15質量%以下含有し,残部が金属酸化物を含む耐火材料からなる鋼の鋳造用耐火物であって,1
当該耐火物内の金属アルミニウム含有量をAl質量%,見掛気孔率をP%,かさ比重をDとするときに,式1を満たすことを特徴とする,鋼の鋳造用耐火物。
0.31×Al≦(P-4)/D ・・・式1 - 前記金属酸化物が,Al2O3,SiO2,ZrO2,MgO,TiO2から選択する1又は複数の成分を含み,前記残部の総量を100質量%とするときに,前記成分の合計が95質量%以上である,請求項1に記載の鋼の鋳造用耐火物。
- 金属シリコンを0.5質量%以上4質量%以下含有する,請求項1又は請求項2に記載の鋼の鋳造用耐火物。
- 金属アルミニウムの含有量が4質量%以上15質量%以下である,請求項1から請求項3のいずれかに記載の鋼の鋳造用耐火物。
- 金属アルミニウムの含有量が6質量%以上15質量%以下である,請求項1から請求項3のいずれかに記載の鋼の鋳造用耐火物。
- 一部又は全部が請求項1から請求項5のいずれかに記載の鋼の鋳造用耐火物から構成された,スライディングノズル装置用のプレート。
- アルミニウムを含有する金属を含み,残部がAl2O3,SiO2,ZrO2,MgO,TiO2から選択する1又は複数の成分を含む金属酸化物を含む耐火材料からなる混合された粉体に,熱硬化性樹脂を1質量%以上7質量%以下添加し混練して成形用坏土を作製する工程と,前記成形用坏土を加圧成形する工程と,熱処理する工程をと含む,請求項1から請求項5のいずれかに記載の鋼の鋳造用耐火物の製造方法であって,
前記熱処理後の耐火物中の金属アルミニウム含有量を1質量%以上15質量%以下とし,前記式1を満たすように見掛気孔率を調整することを特徴とする,鋼の鋳造用耐火物の製造方法。 - 前記の混合された粉体中に含まれるアルミニウムを含有する金属は,最大長が140μm以下の鱗片状,粒径140μm以下の粒子状,又は横断面の最大径が200μm以下かつ最大長さが5mm以下の繊維状から選択する1又は複数の形態の金属アルミニウム単体からなる原料に由来する,請求項7に記載の鋼の鋳造用耐火物の製造方法。
- 前記の混合された粉体中に含まれるアルミニウムを含有する金属の一部又は全部が,金属アルミニウムを含む合金からなる原料に由来する,請求項7に記載の鋼の鋳造用耐火物の製造方法。
- 前記の金属アルミニウムを含む合金は,アルミニウム-マグネシウム合金又はアルミニウム-シリコン合金である,請求項9に記載の鋼の鋳造用耐火物の製造方法。
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EP15755886.7A EP3112054B1 (en) | 2014-02-28 | 2015-02-25 | Refractory for steel casting, plate for sliding nozzle device, and method for producing refractory for steel casting |
JP2016505261A JP6279068B2 (ja) | 2014-02-28 | 2015-02-25 | 鋼の鋳造用耐火物,及びスライディングノズル装置用のプレート,並びに鋼の鋳造用耐火物の製造方法 |
US15/121,462 US20160361758A1 (en) | 2014-02-28 | 2015-02-25 | Refractory for steel casting, plate for sliding nozzle device, and method for producing refractory for steel casting |
CN201580010741.0A CN106029259B (zh) | 2014-02-28 | 2015-02-25 | 钢的铸造用耐火物、及滑动喷嘴装置用板、以及钢的铸造用耐火物的制造方法 |
KR1020167021653A KR101823665B1 (ko) | 2014-02-28 | 2015-02-25 | 강의 주조용 내화물 및 슬라이딩 노즐 장치용 플레이트와 강의 주조용 내화물의 제조 방법 |
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CA2939720A CA2939720C (en) | 2014-02-28 | 2015-02-25 | Refractory for steel casting, plate for sliding nozzle device, and method for producing refractory for steel casting |
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US20230028785A1 (en) * | 2019-12-10 | 2023-01-26 | Krosakiharima Corporation | Refractory product |
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US11192825B2 (en) | 2017-02-22 | 2021-12-07 | Krosakiharima Corporation | Refractory product for casting of steel, and plate for sliding nozzle device |
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CN106029259A (zh) | 2016-10-12 |
JP6279068B2 (ja) | 2018-02-14 |
KR20160107249A (ko) | 2016-09-13 |
US20160361758A1 (en) | 2016-12-15 |
TWI632126B (zh) | 2018-08-11 |
EP3112054A1 (en) | 2017-01-04 |
CA2939720C (en) | 2020-07-21 |
TW201544487A (zh) | 2015-12-01 |
ES2787208T3 (es) | 2020-10-15 |
PL3112054T3 (pl) | 2020-08-24 |
JPWO2015129745A1 (ja) | 2017-03-30 |
CN106029259B (zh) | 2018-08-03 |
KR101823665B1 (ko) | 2018-01-30 |
EP3112054B1 (en) | 2020-04-01 |
CA2939720A1 (en) | 2015-09-03 |
EP3112054A4 (en) | 2017-11-01 |
BR112016019650B1 (pt) | 2021-06-22 |
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