NZ625322B2 - Nozzle assembly comprising first and second elements being coupled to one|another in a sliding translation relationship and a sealing member made of|thermally intumescent material, refractory element.method for producing a|refractory element, method for coupling two refractory elements - Google Patents
Nozzle assembly comprising first and second elements being coupled to one|another in a sliding translation relationship and a sealing member made of|thermally intumescent material, refractory element.method for producing a|refractory element, method for coupling two refractory elements Download PDFInfo
- Publication number
- NZ625322B2 NZ625322B2 NZ625322A NZ62532212A NZ625322B2 NZ 625322 B2 NZ625322 B2 NZ 625322B2 NZ 625322 A NZ625322 A NZ 625322A NZ 62532212 A NZ62532212 A NZ 62532212A NZ 625322 B2 NZ625322 B2 NZ 625322B2
- Authority
- NZ
- New Zealand
- Prior art keywords
- sealing member
- nozzle assembly
- coupling
- coupling surface
- bore
- Prior art date
Links
- 230000001808 coupling Effects 0.000 title claims abstract description 87
- 238000010168 coupling process Methods 0.000 title claims abstract description 87
- 238000005859 coupling reaction Methods 0.000 title claims abstract description 87
- 238000007789 sealing Methods 0.000 title claims abstract description 80
- 239000000463 material Substances 0.000 title claims abstract description 72
- 238000004519 manufacturing process Methods 0.000 title claims description 5
- 229910052751 metal Inorganic materials 0.000 claims abstract description 37
- 239000002184 metal Substances 0.000 claims abstract description 37
- OKTJSMMVPCPJKN-UHFFFAOYSA-N carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 23
- 239000010439 graphite Substances 0.000 claims abstract description 22
- 229910002804 graphite Inorganic materials 0.000 claims abstract description 22
- 238000005058 metal casting Methods 0.000 claims abstract description 14
- 238000007599 discharging Methods 0.000 claims abstract description 4
- 239000000203 mixture Substances 0.000 claims description 26
- 239000010410 layer Substances 0.000 claims description 25
- 238000005266 casting Methods 0.000 claims description 17
- VTYYLEPIZMXCLO-UHFFFAOYSA-L calcium carbonate Chemical compound [Ca+2].[O-]C([O-])=O VTYYLEPIZMXCLO-UHFFFAOYSA-L 0.000 claims description 16
- 239000011248 coating agent Substances 0.000 claims description 15
- 238000000576 coating method Methods 0.000 claims description 15
- 238000010438 heat treatment Methods 0.000 claims description 14
- CDBYLPFSWZWCQE-UHFFFAOYSA-L sodium carbonate Chemical compound [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 claims description 14
- 150000002500 ions Chemical class 0.000 claims description 13
- UIIMBOGNXHQVGW-UHFFFAOYSA-M NaHCO3 Chemical compound [Na+].OC([O-])=O UIIMBOGNXHQVGW-UHFFFAOYSA-M 0.000 claims description 12
- 239000010455 vermiculite Substances 0.000 claims description 12
- 229910052902 vermiculite Inorganic materials 0.000 claims description 12
- 235000019354 vermiculite Nutrition 0.000 claims description 12
- NTHWMYGWWRZVTN-UHFFFAOYSA-N Sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 claims description 11
- 239000004927 clay Substances 0.000 claims description 11
- 229910052570 clay Inorganic materials 0.000 claims description 11
- 235000019353 potassium silicate Nutrition 0.000 claims description 11
- 239000011230 binding agent Substances 0.000 claims description 8
- 229910000019 calcium carbonate Inorganic materials 0.000 claims description 8
- 235000010216 calcium carbonate Nutrition 0.000 claims description 8
- ZLNQQNXFFQJAID-UHFFFAOYSA-L Magnesium carbonate Chemical compound [Mg+2].[O-]C([O-])=O ZLNQQNXFFQJAID-UHFFFAOYSA-L 0.000 claims description 7
- 230000035852 Tmax Effects 0.000 claims description 7
- 230000003078 antioxidant Effects 0.000 claims description 7
- 239000003963 antioxidant agent Substances 0.000 claims description 7
- 239000000314 lubricant Substances 0.000 claims description 7
- 239000011776 magnesium carbonate Substances 0.000 claims description 7
- 235000014380 magnesium carbonate Nutrition 0.000 claims description 7
- 229910000021 magnesium carbonate Inorganic materials 0.000 claims description 7
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 7
- 235000017550 sodium carbonate Nutrition 0.000 claims description 7
- 229910000029 sodium carbonate Inorganic materials 0.000 claims description 7
- NKWPZUCBCARRDP-UHFFFAOYSA-L Calcium bicarbonate Chemical compound [Ca+2].OC([O-])=O.OC([O-])=O NKWPZUCBCARRDP-UHFFFAOYSA-L 0.000 claims description 6
- HYBBIBNJHNGZAN-UHFFFAOYSA-N Furfural Chemical compound O=CC1=CC=CO1 HYBBIBNJHNGZAN-UHFFFAOYSA-N 0.000 claims description 6
- 229910000147 aluminium phosphate Inorganic materials 0.000 claims description 6
- 229910000020 calcium bicarbonate Inorganic materials 0.000 claims description 6
- 229910000022 magnesium bicarbonate Inorganic materials 0.000 claims description 6
- 235000014824 magnesium bicarbonate Nutrition 0.000 claims description 6
- 239000005011 phenolic resin Substances 0.000 claims description 6
- 229920001568 phenolic resin Polymers 0.000 claims description 6
- 235000017557 sodium bicarbonate Nutrition 0.000 claims description 6
- 229910000030 sodium bicarbonate Inorganic materials 0.000 claims description 6
- 239000007787 solid Substances 0.000 claims description 6
- ILRRQNADMUWWFW-UHFFFAOYSA-K Aluminium phosphate Chemical compound O1[Al]2OP1(=O)O2 ILRRQNADMUWWFW-UHFFFAOYSA-K 0.000 claims description 4
- 239000004411 aluminium Substances 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- 229940001007 aluminium phosphate Drugs 0.000 claims description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminum Chemical group [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- 239000011247 coating layer Substances 0.000 claims description 4
- 238000009830 intercalation Methods 0.000 claims description 4
- NBIIXXVUZAFLBC-UHFFFAOYSA-N phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 claims description 4
- 230000001681 protective Effects 0.000 claims description 4
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 claims description 3
- 230000035969 Vmax Effects 0.000 claims description 3
- QTBSBXVTEAMEQO-UHFFFAOYSA-N acetic acid Chemical compound CC(O)=O QTBSBXVTEAMEQO-UHFFFAOYSA-N 0.000 claims description 3
- 235000011054 acetic acid Nutrition 0.000 claims description 3
- GDTBXPJZTBHREO-UHFFFAOYSA-N bromine Substances BrBr GDTBXPJZTBHREO-UHFFFAOYSA-N 0.000 claims description 3
- WKBOTKDWSSQWDR-UHFFFAOYSA-N bromine atom Chemical compound [Br] WKBOTKDWSSQWDR-UHFFFAOYSA-N 0.000 claims description 3
- 239000000460 chlorine Substances 0.000 claims description 3
- 229910052801 chlorine Inorganic materials 0.000 claims description 3
- ZAMOUSCENKQFHK-UHFFFAOYSA-N chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 claims description 3
- 239000010445 mica Substances 0.000 claims description 3
- 229910052618 mica group Inorganic materials 0.000 claims description 3
- GRYLNZFGIOXLOG-UHFFFAOYSA-N nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 claims description 3
- 150000007524 organic acids Chemical class 0.000 claims description 3
- 235000005985 organic acids Nutrition 0.000 claims description 3
- 229910001562 pearlite Inorganic materials 0.000 claims description 3
- 150000007965 phenolic acids Chemical class 0.000 claims description 3
- 235000009048 phenolic acids Nutrition 0.000 claims description 3
- 239000001117 sulphuric acid Substances 0.000 claims description 3
- 235000011149 sulphuric acid Nutrition 0.000 claims description 3
- 229910052626 biotite Inorganic materials 0.000 claims description 2
- 230000001680 brushing Effects 0.000 claims description 2
- 230000000875 corresponding Effects 0.000 claims description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 2
- 239000011733 molybdenum Substances 0.000 claims description 2
- 229910052750 molybdenum Inorganic materials 0.000 claims description 2
- 238000007639 printing Methods 0.000 claims description 2
- 238000007650 screen-printing Methods 0.000 claims description 2
- 238000010008 shearing Methods 0.000 claims description 2
- 239000010703 silicon Substances 0.000 claims description 2
- 229910052710 silicon Inorganic materials 0.000 claims description 2
- 239000000377 silicon dioxide Substances 0.000 claims description 2
- 238000005507 spraying Methods 0.000 claims description 2
- 239000002202 Polyethylene glycol Substances 0.000 claims 2
- 229920001223 polyethylene glycol Polymers 0.000 claims 2
- 241000220450 Cajanus cajan Species 0.000 claims 1
- 235000017168 chlorine Nutrition 0.000 claims 1
- 238000007646 gravure printing Methods 0.000 claims 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims 1
- 239000003566 sealing material Substances 0.000 abstract description 5
- 230000002522 swelling Effects 0.000 description 7
- 239000007789 gas Substances 0.000 description 6
- 239000000243 solution Substances 0.000 description 6
- 239000002245 particle Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 230000000712 assembly Effects 0.000 description 3
- 239000008119 colloidal silica Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000003628 erosive Effects 0.000 description 3
- 230000001965 increased Effects 0.000 description 3
- 230000035882 stress Effects 0.000 description 3
- VSCWAEJMTAWNJL-UHFFFAOYSA-K Aluminium chloride Chemical compound Cl[Al](Cl)Cl VSCWAEJMTAWNJL-UHFFFAOYSA-K 0.000 description 2
- 239000002253 acid Substances 0.000 description 2
- XKRFYHLGVUSROY-UHFFFAOYSA-N argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 239000011324 bead Substances 0.000 description 2
- ODINCKMPIJJUCX-UHFFFAOYSA-N calcium monoxide Chemical compound [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000009749 continuous casting Methods 0.000 description 2
- 239000008367 deionised water Substances 0.000 description 2
- 230000002708 enhancing Effects 0.000 description 2
- -1 ium Substances 0.000 description 2
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N oxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 2
- 239000012071 phase Substances 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 239000011780 sodium chloride Substances 0.000 description 2
- 235000002639 sodium chloride Nutrition 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- UKUVVAMSXXBMRX-UHFFFAOYSA-N 2,4,5-trithia-1,3-diarsabicyclo[1.1.1]pentane Chemical compound S1[As]2S[As]1S2 UKUVVAMSXXBMRX-UHFFFAOYSA-N 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N AI2O3 Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- RBTARNINKXHZNM-UHFFFAOYSA-K Iron(III) chloride Chemical compound Cl[Fe](Cl)Cl RBTARNINKXHZNM-UHFFFAOYSA-K 0.000 description 1
- 229920002584 Polyethylene Glycol 6000 Polymers 0.000 description 1
- 206010040844 Skin exfoliation Diseases 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000005864 Sulphur Substances 0.000 description 1
- HWKQNAWCHQMZHK-UHFFFAOYSA-N Trolnitrate Chemical compound [O-][N+](=O)OCCN(CCO[N+]([O-])=O)CCO[N+]([O-])=O HWKQNAWCHQMZHK-UHFFFAOYSA-N 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 229910052783 alkali metal Inorganic materials 0.000 description 1
- 150000001340 alkali metals Chemical class 0.000 description 1
- 239000008346 aqueous phase Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 239000000440 bentonite Substances 0.000 description 1
- 229910000278 bentonite Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052681 coesite Inorganic materials 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 230000003247 decreasing Effects 0.000 description 1
- 230000001419 dependent Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000005538 encapsulation Methods 0.000 description 1
- 238000004299 exfoliation Methods 0.000 description 1
- 238000004079 fireproofing Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 229910021389 graphene Inorganic materials 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 229910052736 halogen Inorganic materials 0.000 description 1
- 150000002367 halogens Chemical class 0.000 description 1
- 150000004677 hydrates Chemical class 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 230000001050 lubricating Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- VASIZKWUTCETSD-UHFFFAOYSA-N manganese(II) oxide Inorganic materials [Mn]=O VASIZKWUTCETSD-UHFFFAOYSA-N 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229910001507 metal halide Inorganic materials 0.000 description 1
- 150000005309 metal halides Chemical class 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 230000000051 modifying Effects 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 229910052904 quartz Inorganic materials 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 230000031070 response to heat Effects 0.000 description 1
- 230000000452 restraining Effects 0.000 description 1
- 238000000550 scanning electron microscopy energy dispersive X-ray spectroscopy Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 235000012239 silicon dioxide Nutrition 0.000 description 1
- KISFEBPWFCGRGN-UHFFFAOYSA-M sodium;2-(2,4-dichlorophenoxy)ethyl sulfate Chemical compound [Na+].[O-]S(=O)(=O)OCCOC1=CC=C(Cl)C=C1Cl KISFEBPWFCGRGN-UHFFFAOYSA-M 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229910052682 stishovite Inorganic materials 0.000 description 1
- QAOWNCQODCNURD-UHFFFAOYSA-L sulfate Chemical compound [O-]S([O-])(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-L 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 230000001131 transforming Effects 0.000 description 1
- 229910052905 tridymite Inorganic materials 0.000 description 1
- 230000001960 triggered Effects 0.000 description 1
- 229910001845 yogo sapphire Inorganic materials 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/08—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like for bottom pouring
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/14—Closures
- B22D41/22—Closures sliding-gate type, i.e. having a fixed plate and a movable plate in sliding contact with each other for selective registry of their openings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/14—Closures
- B22D41/22—Closures sliding-gate type, i.e. having a fixed plate and a movable plate in sliding contact with each other for selective registry of their openings
- B22D41/28—Plates therefor
- B22D41/30—Manufacturing or repairing thereof
- B22D41/32—Manufacturing or repairing thereof characterised by the materials used therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/14—Closures
- B22D41/22—Closures sliding-gate type, i.e. having a fixed plate and a movable plate in sliding contact with each other for selective registry of their openings
- B22D41/28—Plates therefor
- B22D41/36—Treating the plates, e.g. lubricating, heating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/50—Pouring-nozzles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/50—Pouring-nozzles
- B22D41/502—Connection arrangements; Sealing means therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/50—Pouring-nozzles
- B22D41/52—Manufacturing or repairing thereof
- B22D41/54—Manufacturing or repairing thereof characterised by the materials used therefor
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C2209/00—Compositions specially applicable for the manufacture of vitreous glazes
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C8/00—Enamels; Glazes; Fusion seal compositions being frit compositions having non-frit additions
- C03C8/24—Fusion seal compositions being frit compositions having non-frit additions, i.e. for use as seals between dissimilar materials, e.g. glass and metal; Glass solders
-
- 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
- C04B14/00—Use of inorganic materials as fillers, e.g. pigments, for mortars, concrete or artificial stone; Treatment of inorganic materials specially adapted to enhance their filling properties in mortars, concrete or artificial stone
- C04B14/02—Granular materials, e.g. microballoons
- C04B14/022—Carbon
- C04B14/024—Graphite
-
- 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
- C04B14/00—Use of inorganic materials as fillers, e.g. pigments, for mortars, concrete or artificial stone; Treatment of inorganic materials specially adapted to enhance their filling properties in mortars, concrete or artificial stone
- C04B14/02—Granular materials, e.g. microballoons
- C04B14/04—Silica-rich materials; Silicates
- C04B14/10—Clay
-
- 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
- C04B14/00—Use of inorganic materials as fillers, e.g. pigments, for mortars, concrete or artificial stone; Treatment of inorganic materials specially adapted to enhance their filling properties in mortars, concrete or artificial stone
- C04B14/02—Granular materials, e.g. microballoons
- C04B14/04—Silica-rich materials; Silicates
- C04B14/20—Mica; Vermiculite
- C04B14/202—Vermiculite
-
- 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
- C04B2103/00—Function or property of ingredients for mortars, concrete or artificial stone
- C04B2103/60—Agents for protection against chemical, physical or biological attack
- C04B2103/608—Anti-oxidants
-
- 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
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/20—Resistance against chemical, physical or biological attack
- C04B2111/28—Fire resistance, i.e. materials resistant to accidental fires or high temperatures
-
- 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
- C04B22/00—Use of inorganic materials as active ingredients for mortars, concrete or artificial stone, e.g. accelerators, shrinkage compensating agents
- C04B22/08—Acids or salts thereof
- C04B22/10—Acids or salts thereof containing carbon in the anion
-
- 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
- C04B22/00—Use of inorganic materials as active ingredients for mortars, concrete or artificial stone, e.g. accelerators, shrinkage compensating agents
- C04B22/08—Acids or salts thereof
- C04B22/10—Acids or salts thereof containing carbon in the anion
- C04B22/106—Bicarbonates
-
- 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
- C04B24/00—Use of organic materials as active ingredients for mortars, concrete or artificial stone, e.g. plasticisers
- C04B24/24—Macromolecular compounds
- C04B24/28—Macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
- C04B24/32—Polyethers, e.g. alkylphenol polyglycolether
-
- 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
- C04B28/00—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements
- C04B28/24—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements containing alkyl, ammonium or metal silicates; containing silica sols
- C04B28/26—Silicates of the alkali metals
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K3/00—Materials not provided for elsewhere
- C09K3/10—Materials in mouldable or extrudable form for sealing or packing joints or covers
- C09K2003/1034—Materials or components characterised by specific properties
- C09K2003/1037—Intumescent materials
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K2200/00—Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
- C09K2200/02—Inorganic compounds
- C09K2200/0204—Elements
- C09K2200/0208—Carbon
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K2200/00—Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
- C09K2200/02—Inorganic compounds
- C09K2200/0243—Silica-rich compounds, e.g. silicates, cement, glass
- C09K2200/0252—Clays
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K2200/00—Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
- C09K2200/02—Inorganic compounds
- C09K2200/0243—Silica-rich compounds, e.g. silicates, cement, glass
- C09K2200/0265—Mica
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K3/00—Materials not provided for elsewhere
- C09K3/10—Materials in mouldable or extrudable form for sealing or packing joints or covers
- C09K3/1003—Pure inorganic mixtures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/02—Sealings between relatively-stationary surfaces
- F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
- F16J15/064—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces the packing combining the sealing function with other functions
- F16J15/065—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces the packing combining the sealing function with other functions fire resistant
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49908—Joining by deforming
- Y10T29/49938—Radially expanding part in cavity, aperture, or hollow body
Abstract
Disclosed is a nozzle assembly and a intumescent sealing material (e.g. graphite) which is suitable for sealing the interface between elements of the nozzle assembly in a metal casting line which are coupled in a translation sliding relationship, such as a gate plate in a sliding gate device or a nozzle unit suitable for being used with a tube exchange device. The nozzle assembly (20, 30) for a metal casting apparatus selected from a sliding gate and a tube exchange device comprises: a first refractory element (1 ) comprising a first coupling surface (1 a) which includes a first bore aperture, and a second refractory element (11 ) comprising a second coupling surface (11a), which includes a second bore aperture, the first and second elements being coupled to one another in a sliding translation relationship through their respective first and second coupling surfaces such that the first and second bore apertures can be brought into and out of registry to define, when in registry, a continuous bore (3, 13) for discharging molten metal from a molten metal inlet (13a) to a molten metal outlet (3b) of said nozzle assembly, a sealing member (2) provided between the first and second coupling surfaces of the first and second elements, characterized in that, the sealing member (2) comprises a thermally intumescent material. zzle unit suitable for being used with a tube exchange device. The nozzle assembly (20, 30) for a metal casting apparatus selected from a sliding gate and a tube exchange device comprises: a first refractory element (1 ) comprising a first coupling surface (1 a) which includes a first bore aperture, and a second refractory element (11 ) comprising a second coupling surface (11a), which includes a second bore aperture, the first and second elements being coupled to one another in a sliding translation relationship through their respective first and second coupling surfaces such that the first and second bore apertures can be brought into and out of registry to define, when in registry, a continuous bore (3, 13) for discharging molten metal from a molten metal inlet (13a) to a molten metal outlet (3b) of said nozzle assembly, a sealing member (2) provided between the first and second coupling surfaces of the first and second elements, characterized in that, the sealing member (2) comprises a thermally intumescent material.
Description
NOZZLE ASSEMBLY COMPRISING FIRST AND SECOND ELEMENTS BEING COUPLED TO
ONE ANOTHER IN A SLIDING ATION RELATIONSHIP AND A SEALING MEMBER
MADE OF THERMALLY INTUMESCENT MATERIAL, REFRACTORY ELEMENT. METHOD
FOR PRODUCING A REFRACTORY ELEMENT, METHOD FOR COUPLING TWO
REFRACTORY ELEMENTS
FIELD OF THE INVENTION
The present ion generally relates to continuous metal casting lines. In particular, it
s to a sealing which is particularly le for sealing the interface between elements of a
nozzle assembly in a metal casting line which are coupled in a translation sliding relationship, such as
a gate plate in a sliding gate device or a nozzle unit suitable for being used with a tube exchange
device.
BACKGROUND OF THE INVENTION
In metal forming processes, molten metal is transferred from one metallurgical vessel to
another, to a mould or to a tool. For example, as shown in Figure 1 a ladle (100) is filled with a metal
melt out of a furnace and transferred to a tundish (200). The molten metal can then be cast from the
tundish to a continuous casting mould for forming slabs, blooms, billets or other type of continuously
cast products or to ingots or other discrete defined shapes in foundry . Flow of metal melt out
of a metallurgic vessel is driven by gravity through various nozzle assemblies (20, 30) located at the
bottom of such vessels.
[0003] Some of such nozzle assemblies comprise elements which are movable with respect to each
other. For example, the ladle (100) is provided at its bottom floor (100a) with a slide gate device (20)
as illustrated in Figure 2 coupling an inner nozzle (21) ed in a refractory coating of the ladle
floor to a collector nozzle (22) extending outside of the ladle. A gate plate (25) comprising a through
bore is ched between the inner nozzle and the collector nozzle and is able to linearly slide
between the two to bring the through bore thereof into or out of registry with the through bores of the
inner and outer nozzles.
Another example is a tube exchange device (30), mounted at the bottom floor of a tundish
(200) for discharging the molten metal contained in the tundish into a mould or a tool. It comprises an
inner nozzle (31) embedded in the refractory coating of the h floor and a pouring nozzle (32)
extending outside of the tundish. Because the service time of such pouring nozzles is generally
shorter than a full casting operation, a tube ge device is often used allowing the changing of
the pouring nozzle (32) t interrupting the casting operation, by sliding a new pouring nozzle
along riate guiding means to push out and replace the worn pouring nozzle as illustrated in
Figures 3 and 4.
[0005] t tightness to air of the interfaces n coupled elements is of prime importance in
a metal casting equipment because, on the one hand, most molten metals promptly oxidize in contact
with air at such high temperatures and, on the other hand, because of the flow through the nozzle
bore, air suction is d at any untight interface by Venturi effect. This problem is particularly
sensitive in elements which can be moved during ion and yet, must retain their full tightness.
40 [0006] To prevent air from being sucked into gaps at interfaces n elements of a nozzle
assembly, two elements are coupled to one another by clamping means, such as s,
applying strong forces to press the contact surfaces of the two elements against one another.
This solution has limitations, because too high clamping forces would jeopardize the sliding of
the two elements with respect to each other and it is inefficient in case of small defects at the
interface, such as some local roughness. A gas t is often used by injecting a gas such as
argon or nitrogen, through channels provided at or adjacent to the interfaces. This solution,
however, consumes large volumes of gas and does not prevent tely air intake. The
surfaces in sliding contact are often coated with a layer of lubricant, such as graphite, embedded
in a binder such as water glass and ves such as clays, like bentonite or the like. Such
lubricating layers act to some extent as a g of the interface between two refractory
surfaces, but the environmental conditions around nozzle assemblies are so extreme, with
y very high temperatures and high heat gradients, that the sealing effect is lly
insufficient to ensure complete air tightness of the assembly.
The present invention proposes a solution for ensuring an air tight interface between two
refractory surfaces of a nozzle assembly, even when they are coupled to one another in a sliding
translation relationship. The present solution does not require any fine machining of the coupling
surfaces.
SUMMARY OF THE INVENTION
The present invention is defined by the ed independent claims. The dependent
claims define preferred embodiments. In ular, the present invention concerns nozzle
assembly for a metal casting apparatus selected from a sliding gate and a tube exchange
device, said nozzle assembly comprising:
- a first refractory element comprising a first coupling surface which includes a first bore
aperture, and
- a second refractory element sing a second coupling surface, which includes a
second bore re, the first and second elements being coupled to one another in a sliding
translation relationship through their respective first and second coupling surfaces such that the
first and second bore apertures can be brought into and out of registry to define, when in
registry, a continuous bore for rging molten metal from a molten metal inlet to a molten
metal outlet of said nozzle assembly,
- a sealing member provided between the first and second coupling surfaces of the first
and second elements,
characterized in that, the sealing member comprises a thermally intumescent material.
In the t context, a “nozzle assembly” is defined as any assembly sing at
least one nozzle comprising a bore allowing the g of molten metal out of a vessel.
The intumescent sealing member of a nozzle ly according to the t
invention preferably has:
- an initial expansion temperature, Ti, of at least 130°C, preferably at least 400°C, more
preferably at least 600°C, and/or
40 - a maximum relative expansion, Vmax / V20, at a temperature, Tmax, of maximum
[Link]
http://en.wikipedia.org/wiki/Heat
[Link]
http://en.wikipedia.org/wiki/Volume
[Link]
http://en.wikipedia.org/wiki/Density
expansion comprised between, Ti, and 1400°C, with respect to its volume measured at 20°C, of
at least 10, preferably at least 25, more preferably at least 50, most preferably at least 80.
A “thermally intumescent material” is a substance which swells as a result of heat
exposure, thus increasing in volume, and decreasing in density. The swelling of an intumescent
material is generally caused by a phase transformation of at least one component of said
material and is clearly distinguished from normal thermal expansion which generally increases
linearly with temperature, DV = a DT, wherein a is the coefficient of heat expansion. An
scent material suitable for the present invention may be composed of a layered material
which is modified by intercalating other materials between the layers to cause intumescence
upon exposure to heat, such as:
- expandable graphite, clay, mica, or pearlite, which ses one or more of sulphuric
acid, nitric acid, oric acid, organic acids such as acetic or phenolic acids, and salts
thereof, chlorine and bromine gas alated between nt crystalline layers; expandable
graphite intercalated with a sulphur or phosphorus containing compound is preferred;
- vermiculite, preferably in the shape of interstratified layers of vermiculite and e,
In one embodiment of the present invention, the scent sealing member is a
coating layer of unexpanded thickness ably comprised between 0.1 and 3.0 mm, more
preferably between 0.2 and 1.0 mm, most preferably between 0.3 and 0.6 mm. Said coating
layer may be optionally d by a final sealing layer as for instance a standard graphite
mixture. The sealing member may thus be coated over a substantial portion, preferably the
whole of the first and/or second coupling es. atively the sealing member may be
applied into a groove on the first and/or the second coupling surfaces, circumscribing at least
partly the first and/or second bore apertures, respectively. The groove is preferably at least
0.5 mm deep, more preferably at least 1.0 mm deep, most preferably, at least 3.0 mm deep.
[0013] In an alternative embodiment, the sealing member may be in the form of a gasket,
preferably nested in a groove on the first and/or the second coupling surfaces, circumscribing at
least partly the first and/or second bore apertures, tively.
The sealing member may se:
- 5-95 wt.% of an intumescent material, comprising expandable graphite and/or
vermiculite;
- 5-95 wt.% of a binder, such as water glass, preferably admixed with one or more of
clay, Na2CO3, CaCO3, MgCO3, NaHCO3, Ca(HCO3)2, 3)2;
- 0-80 wt.% of a lubricant, such as (non expandable) graphite;
- 0-20 wt.% of an antioxidant such as ium, silicon or molybdenum,
wherein the wt.% are measured as solids dry weight with respect to the total dry weight of the
sealing member composition.
In a preferred embodiment, the intumescent material is encapsulated in a microshell
which can flow, volatilize or degrade upon exposure to a given ature, or to a mechanical
stress, such as shearing upon g one coupling surface over the other. Such microshells are
40 advantageously composed of water glass, colloidal silica or aluminium phosphate, preferably in
combination with one or more of clay, Na2CO3, CaCO3, MgCO3, , Ca(HCO3)2, or
Mg(HCO3)2, preferably present in an amount in the range of 0.5-80 wt.% , more preferably 5-
%. Such protective shell layer can be:
- applied onto a primer, preferably composed of a mixture of phenolic resin and furfural
in a weight ratio comprised between 3:8 and 3:1, preferably between 1:1 and 3:2, said primer
being applied ly onto the intumescent flakes; and/or
- covered by a finishing top layer, preferably comprising a mixture of phenolic resin and
furfural.
This ment is particularly suitable for exchangeable pouring nozzles because they
are often preheated prior to mounting onto a tube exchange device. Indeed, encapsulation
ensures that the intumescent material starts swelling only when the first coupling surface is
mounted in a nozzle assembly and exposed to shear stresses upon sliding and/or to high
temperatures when in casting position.
The present ion also concerns a refractory element of a nozzle assembly for a
metal casting apparatus, said tory element comprising a first through bore opening at a
first, substantially planar coupling surface suitable for being coupled in a sliding translation
relationship with a second coupling surface of a second refractory t, characterized in
that, the first coupling surface of said refractory element is provided with a sealing member
comprising a thermally intumescent material. The sealing member and intumescent material is
preferably as discussed above. The refractory t of the present ion is preferably one
of: - a pouring nozzle suitable for being loaded in and unloaded out of a tube exchange
device;
- an inner nozzle to be mounted in the bottom floor of a vessel and fixed to a tube
exchange ;
- a sliding plate in a slide gate device mounted under a ladle or a tundish;
- a fixed plate in sliding contact with a sliding plate (25) in a slide gate device d
under a ladle or a tundish.
The present invention also concerns a method for ing a refractory element as
discussed supra comprising the following steps:
(a) providing a refractory element comprising a first through bore (3) opening at a first
coupling e, said first coupling surface being suitable for being coupled in a g
translation relationship with a second coupling surface of a second refractory element;
(b) applying a sealing member onto the first coupling surface, such as to preferably
circumscribe the bore aperture,
characterized in that, the sealing member comprises a thermally intumescent material.
The sealing member can be applied to the first coupling surface as:
- a g covering the whole or a portion only of the first coupling surface, by brushing,
spraying, use of a squeegee or of a roller, printing, such as screen printing or e ng;
- a coating g a groove provided on the first coupling surface and circumscribing the
40 aperture of the through bore by injection, squeegee, casting; or
- a preformed gasket g into a groove provided on the first ng surface and
preferably circumscribing the aperture of the through bore.
Once a refractory element comprising an scent sealing member circumscribing a
bore re on a first ng surface thereof has been produced by the foregoing method, it
can be: - coupled by slide translating said first coupling surface over a second coupling surface
comprising a second bore aperture of a second refractory element of the nozzle assembly, such
that the sealing member contacts both first and second coupling surfaces and bringing the first
and second bore apertures into and out of ry, to , when in registry, a continuous
through bore from a molten metal inlet to a molten metal outlet; the thus coupled first and second
refractory elements can then be,
- heated to a temperature at least sufficient to swell the intumescent material of the
g member.
At which point, the casting of molten metal through the nozzle assembly can take place with little
risk of air intake through the joint between first and second refractory elements.
The heating step to a temperature sufficient to swell the intumescent material may rely on the
heat of the molten metal being transferred to the intumescent material or imply another source of
heat like a separate burner or others.
In case the first refractory element and sealing member are pre-heated at a pre-heating
temperature prior to coupling to the second refractory t, the intumescent material should
be ted from reaching its maximum expansion before being mounted into a corresponding
nozzle ly. This can be achieved:
- by ining the pre-heating temperature below the temperature, Tmax, of maximum
expansion of the intumescent material, and preferably below the initial swelling temperature, Ti,
- by encapsulating the intumescent material into shells which are chemically and/or
mechanically and/or thermally damaged upon sliding the first refractory element into casting
position into the nozzle assembly and/or (ii) upon casting molten metal.
BRIEF DESCRIPTION OF THE FIGURES
Various embodiments of the present invention are illustrated in the attached Figures:
Figure 1: shows tically a typical continuous casting line.
Figure 2: shows a side cut view of a first (a)&(b) and second (c)&(d) embodiments of a slide
gate device ing to the present invention.
Figure 3: shows a cut-off perspective view of a tube exchange device according to the
present invention
Figure 4: shows a cut-off perspective view of an alternative tube exchange device according
to the present invention
Figure 5: shows side views of various embodiments of a coupling surface comprising a
sealing member in accordance with the present invention
DETAILED DESCRIPTION OF THE INVENTION
The present invention solves in a simple and reliable way the problem of preventing air
from being sucked into the molten metal flowing through a nozzle assembly by Venturi effect
through the interface between two refractory elements. The present ion is particularly
ageous for sealing the interface n two refractory es which are coupled in a
sliding translation relationship, such as in a sliding gate or a tube exchange device as illustrated
in Figures 2 to 4. When two refractrory elements are coupled statically, it is somewhat easier —
albeit still a challenge— to seal the joint between the two parts. When two elements are coupled
dynamically, the challenge of sealing the joint between the two is increased substantially. The
t invention meets this challenge.
[0024] When two refractory elements are to be coupled in a ation sliding relationship,
such as an exchangeable pouring nozzle (32) in a tube exchange device (30) mounted at the
bottom of a tundish as illustrated in Figures 3 and 4, or a g gate (25) in a slide gate device
(20) as illustrated in Figure 2, it is extremely difficult to ensure a complete tightness between the
coupling surfaces (1a, 11a) of the two refractory elements. Indeed, the clamping forces applied
to cally coupled elements cannot be as high as between statically coupled elements, lest
sliding between the two coupling es be hindered, which ses the risk of a gap
between the two elements. The g of one coupling surface over the other may create
scratches at the joint, which may easily turn into leaking passageways for the air. Finally, it is not
possible to seal the joint between two ts with a bead running at the periphery of said joint,
because the bead would be broken when moving one element with respect to the other. The
present ion solves this long known —albeit never actorily solved— problem in a very
, cheap and efficient way, by providing between the first and second coupling surfaces of
two refractory elements a sealing element (2) comprising a thermally intumescent material.
Strictly speaking, the term “thermally” is redundant, since intumescent als are defined as
materials which swell upon exposure to heat, but it was deemed necessary to specify the term
“thermally’ to avoid any (unjustified) extension of the term ‘intumescent’ to swelling caused by
other sources, such as exposure to water, which would be unacceptable in a molten metal
casting nozzle assembly.
There is a large variety of scent materials with differing properties. They are
widely used in fireproofing applications. In such applications, the endothermic release of water
by hydrates upon exposure to heat generated by a fire is taken advantage of to maintain the
temperature of a structure low and the char produced by such material is lly a poor heat
conductor. They are usually applied in fireproof doors, windows, and pipes. For the sake of the
present invention, the important features of intumescent materials are their expansion
characteristics. An intumescent sealing member (2) particularly suitable for the present invention
should preferably have an initial expansion temperature, Ti, of at least 130°C, preferably at least
400°C, more ably at least 600°C. The maximum relative ion, Vmax / V20, at a
temperature, Tmax, of maximum expansion comprised between, Ti, and 1400°C, with respect to
its volume measured at 20°C, should preferably be at least 10, preferably at least 25, more
40 preferably at least 50, most preferably at least 80.
scent materials are generally composed of a layered host material which is
modified by intercalating other materials between adjacent layers. Upon heating, the material
intercalated between layers changes phase, generally turning into gas and thus strongly
increasing in volume, and produces a strong pressure pushing apart adjacent layers of the host
material. This sudden and sometimes substantial expansion is called intumescence, or
exfoliation. The expansion magnitude for a given host material depends on a number of
parameters. First, the nature of the intercalated material affects expansion ude and the
temperature at which expansion . For a given intumescent material, the size of the host
material particles may also influence the expansion ratio of the material. The heating rate of an
intumescent material may also affect its response to heat, a slow heating rate reducing
expansion, compared with a high heating rate. Finally, encapsulating an intumescent material
may also delay swelling of the material.
es of scent materials suitable for use in the sealing element (2) of a nozzle
assembly according to the present invention se one or a mixture of:
- expandable graphite, clay, mica, or pearlite, which comprises one or more acids and
salts thereof, such as sulphuric acid, nitric acid, phosphoric acid, organic acids such as acetic or
phenolic acids, as well as halogens, alkali metals, aluminium chloride, ferric chloride, other metal
halides, arsenic sulphide, um de, chlorine and bromine gas intercalated between
nt crystalline ne layers;
- vermiculite, ably in the shape of interstratified layers of vermiculite and biotite as
disclosed for example in US5340643, which disclosure is herein incorporated by reference;
Amongst those materials, able graphite is preferred.
The sealing material comprises at least one intumescent material, preferably in an
amount comprised between 5 and 95 wt.%. Other materials are preferably used:
- a binder can be used to bind together intumescent particles or for encapsulating such
particles. An example of suitable binder is water glass, ably admixed with one or more of
clay, Na2CO3, CaCO3, MgCO3, NaHCO3, Ca(HCO3)2, Mg(HCO3)2. The binder is preferably
present in an amount of 5-95 wt.%.
- a lubricant is particularly useful to facilitate sliding of a coupling surface over the other.
An e of lubricant suitable for the present invention is (non-expandable) te. It is
ably present in an amount comprised between 0 and 80 wt.%, preferably between 10 and
50 wt.%, more preferably between15 and 40 wt.%, most preferably between 20 and 35 wt.%.
- an antioxidant is used to protect the sealing material exposed to extreme thermal
conditions. An example of antioxidant is aluminium, which can be present in an amount of 0-
20 wt.%, preferably between 2 and 10 wt.%.
The wt.% are measured as solids dry weight with respect to the total dry weight of the
sealing member composition.
The sealing member (2) can be in the form of a g on a coupling surface (1a, 11a).
The sealing member (2) may be coated over a substantial portion, preferably the whole of the
40 first and/or second ng surfaces (1a, 1b) (cf. Figure 2, bottom of sliding plate (25) and
Figures 3 and 5(a)). The thickness of the unexpanded coating can be of the order of 0.1 to
3.0 mm, ably of 0.2 to 1.0 mm, more ably of 0.3 to 0.6 mm. atively, the
intumescent coating may be applied into a groove scribing (at least partly) the bore (3a)
as illustrated in Figure 5(b). The groove may be at least 0.5 mm deep, preferably at least
1.0 mm deep, most preferably, at least 3.0 mm deep, and is preferably filled with unexpanded
g material to at least 50% of the depth thereof, preferably at least 75%. The groove may
also be fully filled with sealing material flush with the coupling surface in its unexpanded state.
In an alternative embodiment, the sealing member (2) may be formed into a gasket (cf.
Figure 2, top of sliding gate (25), Figures 3 and 5(c)). Such gasket can be positioned into a
groove circumscribing (at least partly) the bore (3a) as illustrated in Figure 5(c).
To avoid a thermal shock, refractories are pre-heated prior to being mounted and
contacted with molten metal at high temperatures. In some cases, the pre-heating is performed
in situ, but sometimes it is performed in a furnace separate from the casting installation. This is
called “offline pre-heating.” This is typically the case in tube exchange devices (30), wherein a
new pouring nozzle is preheated to a preheating temperature in a furnace prior to loading it into
the device and sliding it into casting on in order to prevent crack formation due to too high
thermal shock. In offline pre-heating, there is a risk of early expansion of the sealing member (2)
during the preheating and transfer stages, which should be avoided. This can be achieved very
simply by preheating the pouring nozzle to a temperature below the initial expansion
temperature, Ti, or at least below the temperature, Tmax, of maximum ve expansion. In a
preferred ment, the intumescent material is in the form of flakes which are encapsulated
in microshells. The microshell should be ‘closed’ during the preheating stage impeding the
ion of the scent material and ‘open’ during the casting of metal to release the
expansion of the sealing member to achieve its high sealing function. The ‘opening’ of the
microshells can be triggered in various ways. The microshells can be made of a material which
is solid at the preheating temperature, and melts, volatilizes, or degrades at casting temperature.
The term “degrade” may include a ial failure mechanism due to the fact that the force
applied by the expandable te increases with temperature to a point that it is great enough
to rupture the shells. Alternatively or concomitantly, the microshells may be mechanically broken
by shear stresses generated upon sliding the coupling surface of a pouring nozzle into the tube
exchange device. The microshells are advantageously ed of water glass, colloidal silica
or aluminium phosphate, preferably in combination with one or more of clay, Na2CO3, CaCO3,
MgCO3, NaHCO3, Ca(HCO3)2, or Mg(HCO3)2, preferably present in an amount in the range of
0.5-80 wt.%, more preferably 5-30%.
[0033] The microshells may consist of several layers, the foregoing composition constituting a
tive shell layer, which can be applied onto a primer usly coated onto the intumescent
flakes, and/or can be capped by a finishing top coating. A primer is advantageous for enhancing
the wettability and adhesion of the protective shell layer to the surface of the intumescent flakes,
in particular in case of materials having low e es like able graphite. For
40 example the primer can be composed of a mixture of phenolic resin and furfural in a weight ratio
comprised between 3:8 and 3:1, preferably between 1:1 and 3:2, said primer being applied
ly onto the intumescent flakes. A finishing top coat can help to stabilise the shell protective
layer against chemical attack from the aqueous phase of the final coating that is generally
applied to refractory pieces, which typically contains water glass, colloidal silica, aluminium
phosphate or other materials. .The finishing top layer can se a mixture of phenolic resin
and furfural.
The graphite coating can consist of one or more layers. g als should be
available in a dispersion or solution form, and applied to the intumescent flakes in an amount
comprised n 1 and 50 wt.%, preferably 10-20 wt.% of coating solution with respect to the
weight of the intumescent flakes, depending on the size and surface area of the intumescent
flakes. The coating should be able to dry or set to a hard strong shell preventing oxygen
impingement on the intumescent material, and thus ng its tendency to exfoliate and
expand. The shell should also exert mechanical strength sufficient to resist the expansion
process at lower temperatures. The expansion of the intumescent materail is therefore
prevented until such ature is reached that the shell loses its strength. A second function
of the microshells in on to mechanically restraining the expansion is to reduce the oxygen
access to the interlayers of the graphite. This massively reduces the ion. Once the shells
are ruptured, then air can ingress and the expansion is much larger and more powerful.
A sealing member (2) as discussed supra may be applied to various tory elements
(1, 11) of a nozzle assembly (20, 30). In particular, in a tube exchange device (30) mounted on
the bottom floor of a vessel (100, 200), such sealing member can be applied to the coupling
surface of a pouring nozzle (32) and/or of the inner nozzle (31). As illustrated in Figure 2, in a
slide gate device (20) mounted on the bottom floor of a ladle (100) or of a tundish (200), of the
slide gate device and the sliding plates (25) slides between two fixed plates. a g plate (25)
comprising a bore and sandwiched between an inner nozzle (21) and a collector nozzle (22) can
slide to bring the bore in or out of registry with the bore of the inner and collector nozzles
re Figures c) with Figures 2(b)&(d)). There are several types of slide gate devices,
the two most current ones being schematically illustrated in Figures 2(a)&(b) and 2(c)&(d). The
inner nozzle is embedded in the floor of a vessel and coupled to a top fixed plate of the slide
gate device. In a first ment illustrated in Figures 2(a)&(b) the collector nozzle is fixed to
the sliding plate (25) and moves together with it as it slides over the contact surface of the top
fixed plate. In a second embodiment illustrated in Figure 2(c)&(d) the collector nozzle is coupled
to a bottom fixed plate The g member (2) may be applied to the coupling surfaces of a
fixed plate and/or on one or both surfaces of a sliding plate (25), depending on the type of slide
gate device. A sealing coating (2) d to the top coupling surface of the sliding plate (25) is
illustrated in Figure 2(c)&(d), and a g gasket (2) applied to the top and bottom surfaces of
the sliding plate (25) is illustrated in Figures 2(a)&(b) and d), respectively.
A refractory element (1) provided with an intumescent sealing member (2) according to
the present invention can be processed without altering significantly the normal production of
40 such traditional refractory elements and only es an additional coating step of a coupling
surface of such refractory elements.
A refractory element (1) comprising according to the present invention an intumescent
g member (2) circumscribing a bore aperture on a first coupling surface (1a) can be used
as follows. It may optionally be preheated to a preheating temperature, taking care to not trigger
full expansion of the sealing member during this optional step. Next, the refractory element (1)
may be coupled by slide translating said first coupling surface (1a) over a second coupling
surface (11a) sing a second bore aperture of a second refractory element (11) of the
nozzle assembly. The slide translation of the coupling es (1a, 11a) brings the first and
second bore apertures into and out of registry, to define, when in registry, a continuous through
bore from a molten metal inlet (13a) to a molten metal outlet (3b). When exposed to the casting
temperature, the sealing member (2) swells applying a pressure to the coupling surfaces (1a,
11a) of the two joined refractory elements (1, 11) and thus efficiently sealing the joint. g
can proceed with little to no risk of air intake through the joint. The pressure generated by the
swelling of the sealing member (2) is much smaller than the clamping pressure applied to couple
the two refractory elements (1, 11) together, and therefore does not create any substantial
separation of the two elements. The swelling of the sealing material ensures that any gap at the
joint is properly filled thus g the casting bore (3) from ambient.
As mentioned above, ion of the intumescent material should be contained during
the preheating stage, if any, to prevent it from reaching its full expansion prior to being coupled
to a second refractory t in a nozzle assembly. This can be achieved by:
- maintaining the pre-heating temperature below the temperature, Tmax, of m
expansion of the intumescent material, preferably below the initial expansion temperature, Ti, or
- encapsulating the intumescent material into shells which are chemically and/or
mechanically and/or thermally damaged (i) upon sliding the first refractory t into casting
on into the nozzle assembly and/or (ii) upon casting molten metal.
Table 1 gives five compositions of sealing members suitable for the present invention
(EX1-5) and one comparative example (CEX6). In the es, the expandable graphite is
obtained by intercalating sulphate between graphene , sometimes called ‘graphite
hate.’ The vermiculite is a mesh 100 powder of composition 37-42% SiO2, 9-17% Al2O3,
11-23% MgO, 5-18% CaO.
The thermal ties of the sealing member may be modulated according to the
requirements. For example, whilst the composition of EX5 is fully expanded at 450°C, the one of
EX4 expands only at 650°C. After real scale tests in a tube exchange device of a steel g
production line, SEM-EDX examination of a pouring nozzle which coupling surface was coated
with a sealing member of composition EX1 revealed substantially no erosion, with very few
pores on the surface area, comparable with the ty measured in the bulk of the plate. By
contrast, similar tests carried out on uncoated refractory , and on plates coated with a
ition CEX6 revealed substantial erosion with an increase of the surface porosity
compared with the bulk porosity, as well as the ion of a thick reaction layer formed on the
40 eroded area, by oxidized CEX6 coating material. Traces of MnO and other oxides were detected
at the plate surface, close to the bore, locally reacting and forming with the refractory a lower
g ature material which was progressively flushed away by the flowing metal. In view
of the excellent stability of the nozzle plate coated with the EX1 sealing composition according to
the present invention, it is clear that the presence of an intumescent material ntially
enhances the tightness of the joint of the present invention, thus extending the service life of the
refractory elements and ing the y of the cast metal.
Firing tests carried out at 1000°C in air suggested that in the absence of a strong binder,
both vermiculite (cf. EX2) and expandable graphite tended to strongly oxidize and lose integrity.
The on of a binder, such as water glass to expandable vermiculite and graphite particles
improved their resistance to oxidation and the integrity of the coatings (cf. EX1, 3-5).
Table 1: composition of sealing members according to the present invention (EX1-5) and prior
art (CEX6).
EX1 EX2 EX3 EX4 EX5 CEX6
Water glass (wt.%) 50 13 33 20 48
Clay (wt.%) 13 12
Expand. Graphite
17 33 40
(wt.%)
Vermiculite (wt.%) 58 61
Graphite (wt.%) 17 25 26 33 40 32
Aluminium (wt.%) 4 4
PEG6000 (wt.%) 17
CaCO3 (wt.%) 4
Deionized water (wt.%) 21 83 87 33 60 20
Wt.% measured with respect to solids weight. Deionized water is added on top of 100 wt.%
solids.
The present invention constitutes a breakthrough in metal casting equipment, since the
intumescent sealing member (2) applied to a coupling e (1a) of a refractory element (1)
substantially increases the service time of such element, and ensures a metal of better quality,
with fewer oxide ions formed by reaction with rated air, and with fewer nozzles
residues due to erosion of weakened refractory als than ever achieved to date.
Claims (22)
1. Nozzle assembly for a metal g apparatus selected from a sliding gate and a tube exchange , said nozzle assembly comprising : 5 - a first refractory element comprising a first coupling surface which includes a first bore aperture, and - a second tory element comprising a second coupling surface, which includes a second bore aperture, the first and second elements being coupled to one another in a sliding ation relationship through their respective first and second coupling 10 surfaces such that the first and second bore apertures can be brought into and out of registry to , when in ry, a continuous bore for discharging molten metal from a molten metal inlet to a molten metal outlet of said nozzle assembly, - a sealing member provided between the first and second coupling surfaces of the first and second ts, 15 wherein the sealing member comprises a thermally intumescent material.
2. Nozzle ly according to claim 1, wherein the scent sealing member has: - an initial expansion temperature, Ti, of at least 130°C, preferably at least 400°C, more preferably at least 600°C, and/or - a maximum relative expansion, Vmax / V20, at a temperature, Tmax, of maximum 20 expansion comprised between, Ti, and 1400°C, with respect to its volume measured at 20°C, of at least 10, preferably at least 25, more preferably at least 50, most preferably at least 80.
3. Nozzle assembly according to claim 1 or claim 2, n the intumescent material is composed of a layered material which is modified by intercalating other materials 25 between the layers to cause intumescence upon exposure to heat, and is preferably selected from: - expandable graphite, clay, mica, or pearlite, which comprises one or more of sulphuric acid, nitric acid, phosphoric acid, organic acids such as acetic or phenolic acids, chlorine and bromine gas intercalated between adjacent crystalline layers; 30 - vermiculite, preferably in the shape of interstratified layers of vermiculite and biotite, - or mixtures f.
4. Nozzle assembly according to any one of the preceding claims, wherein the sealing member is a coating layer of unexpanded thickness preferably comprised between 0.1 and 3.0 mm, more preferably between 0.2 and 1.0 mm, most preferably between 0.3 35 and 0.6 mm; said coating layer being optionally d by a final sealing layer.
5. Nozzle assembly according to the preceding claim, wherein the sealing member is coated over a ntial portion, ably the whole of the first and/or second 2797881v1 coupling surfaces or the sealing member is applied into a groove on the first and/or the second coupling surfaces, scribing the first and/or second bore apertures, respectively, wherein the groove is ably at least 0.5 mm deep, more preferably at least 1.0 mm deep, most preferably, at least 3.0 mm deep. 5
6. Nozzle assembly according to any one of claims 1 to 3, wherein the g member is in the form of a gasket, preferably nested in a groove on the first and/or the second coupling surfaces, circumscribing the first and/or second bore apertures, respectively,
7. Nozzle assembly according to any one of the ing claims, wherein, the sealing member comprises: 10 - 5-95 wt.% of an intumescent material, comprising expandable graphite and/or vermiculite; - 5-95 wt.% of a binder, such as water glass, preferably admixed with one or more of polyethyleneglycol (PEG), clay, Na2CO3, CaCO3, MgCO3, NaHCO3, Ca(HCO3)2, Mg(HCO3)2; 15 - 0-80 wt.% of a lubricant; - 0-20 wt.% of an antioxidant, wherein the wt.% are measured as solids dry weight with respect to the total dry weight of the sealing member composition.
8. Nozzle assembly according to the preceding claim, wherein the ant is (non 20 expandable) graphite.
9. Nozzle assembly according to claim 7 or claim 8, n the antioxidant is aluminium, silicon or molybdenum.
10. Nozzle assembly according to any one of claim 7 to 9, wherein the intumescent material is in the shape of flakes encapsulated in microshells which can flow, volatilize or 25 degrade upon exposure to a given temperature, or to a mechanical stress, such as shearing upon sliding one coupling e over the other.
11. Nozzle assembly according to the preceding claim, wherein the hells comprise at least one protective shell layer, preferably composed of water glass, dal silica or aluminium phosphate, preferably in combination with one or more of clay, Na2CO3, 30 CaCO3, MgCO3, NaHCO3, 3)2, or Mg(HCO3)2, preferably present in an amount in the range of 0.5-80 wt.% , more preferably 5-30%, said protective shell being optionally: - applied onto a primer, preferably composed of a mixture of phenolic resin and furfural in a weight ratio comprised between 3:8 and 3:1, preferably between 1:1 and 3:2, said primer being applied directly onto the intumescent flakes; and/or 35 - d by a finishing top layer, preferably comprising a e of phenolic resin and furfural. 2797881v1
12. Refractory element of a nozzle assembly for a metal casting apparatus, said refractory element sing a first through bore opening at a first, substantially planar coupling surface suitable for being coupled in a sliding translation relationship with a second coupling surface of a second refractory element, wherein the first coupling surface of 5 said refractory element is provided with a sealing member comprising a thermally intumescent material, wherein, said first planar coupling surface is one of: - the coupling surface of a pouring nozzle suitable for being loaded in and unloaded out of a tube exchange device in sliding relationship with a corresponding contact surface of an inner nozzle ed within the floor of a h; 10 - the coupling surface of an inner nozzle to be d in the bottom floor of a tundish and fixed to a tube exchange device such that said ng surface enters in g relationship with a g nozzle upon introduction of the latter in said tube exchange device; - the coupling surface of a slide gate device plate such that said coupling surface 15 enters in sliding relationship with the coupling surface of a second plate of said slide gate.
13. Refractory element according to the ing claim, wherein the sealing member and intumescent material are as defined in any one of claims 2 to 11.
14. Method for producing a refractory element according to claim 12 or claim 13 comprising 20 the following steps: - providing a refractory element comprising a first through bore opening at a first coupling surface, said first coupling surface being suitable for being coupled in a sliding translation relationship with a second coupling surface of a second refractory t; - applying a sealing member onto the first coupling surface, such as to preferably 25 circumscribe the bore re, wherein, the sealing member ses a thermally intumescent al.
15. Method according to the preceding claim, wherein the sealing member is applied to the first coupling surface as: - a coating covering the whole or a portion only of the first coupling surface, by brushing, 30 spraying, use of a squeegee or of a , printing, such as screen printing or gravure printing; - a coating filling a groove provided on the first ng surface (1a) and circumscribing the aperture of the through bore by ion, squeegee, casting; or - a preformed gasket fitting into a groove provided on the first coupling surface and 35 ably circumscribing the aperture of the through bore.
16. Method for coupling two refractory elements of a nozzle assembly for a metal casting apparatus selected from a sliding gate and a tube exchange device, said method 2797881v1 comprising the following steps: - ng out the method steps of claim 14 or 15 to provide a refractory element comprising an scent sealing member circumscribing a bore aperture on a first coupling surface ; 5 - ng by slide ating said first coupling surface over a second coupling surface comprising a second bore aperture of a second refractory element of the nozzle assembly, such that the sealing member contacts both first and second coupling surfaces) and bringing the first and second bore apertures into and out of registry, to define, when in ry, a continuous through bore from a molten metal inlet to a molten 10 metal outlet - heating the thus coupled first and second refractory elements to a temperature at least sufficient to swell the scent material of the sealing member.
17. Method according to the preceding claim, wherein the first tory element and sealing member are pre-heated prior to coupling to the second refractory element, at a 15 pre-heating temperature under conditions such as to prevent the scent material from reaching its maximum expansion, either by: (a) by maintaining the pre-heating temperature below the temperature, Tmax, of maximum expansion of the intumescent material, or (b) by encapsulating the intumescent material into shells which are chemically and/or 20 mechanically and/or thermally damaged (i) upon sliding the first refractory element into casting position into the nozzle assembly and/or (ii) upon casting molten metal.
18. Sealing composition for use in the nozzle assembly of any one of claims 1 to 11, or the refractory element of claim 12 or claim 13, or the method of any one of claims 15 to 17, said sealing composition comprising: 25 - 5-95 wt.% of an intumescent material, , - 5-95 wt.% of water glass as , preferably admixed with one or more of: clay, Na2CO3, CaCO3, MgCO3, NaHCO3, Ca(HCO3)2, Mg(HCO3)2; - 5-50 wt.% of a lubricant; - up to 20 wt.% of an antioxidant. 30
19. Sealing composition according to claim 18 wherein the intumescent material is expandable graphite.
20. Sealing composition according to claim 18 or 19, wherein the lubricant is (non expandable) te.
21. Sealing composition according to any one of claims 18 to 20, wherein the antioxidant is 35 aluminium.
22. Use of an scent sealing element for sealing the contact interface between a first 2797881v1 and second coupling es of a first and a second refractory elements of a nozzle assembly in a metal casting apparatus, wherein, said first and second coupling surfaces are in a sliding translation relationship.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP11193966.6 | 2011-12-16 | ||
EP20110193966 EP2604363A1 (en) | 2011-12-16 | 2011-12-16 | intumescent sealing for metal casting apparatus |
PCT/IB2012/002949 WO2013088249A2 (en) | 2011-12-16 | 2012-12-14 | Intumescent sealing for metal casting apparatuses |
Publications (2)
Publication Number | Publication Date |
---|---|
NZ625322A NZ625322A (en) | 2016-08-26 |
NZ625322B2 true NZ625322B2 (en) | 2016-11-29 |
Family
ID=
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