CA2804505A1 - Refractory structural element - Google Patents
Refractory structural element Download PDFInfo
- Publication number
- CA2804505A1 CA2804505A1 CA 2804505 CA2804505A CA2804505A1 CA 2804505 A1 CA2804505 A1 CA 2804505A1 CA 2804505 CA2804505 CA 2804505 CA 2804505 A CA2804505 A CA 2804505A CA 2804505 A1 CA2804505 A1 CA 2804505A1
- Authority
- CA
- Canada
- Prior art keywords
- optionally
- flared end
- end block
- stem portion
- face
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 239000000463 material Substances 0.000 claims description 45
- 230000000295 complement effect Effects 0.000 claims description 20
- 239000000919 ceramic Substances 0.000 claims description 15
- 239000000835 fiber Substances 0.000 claims description 12
- 238000011049 filling Methods 0.000 claims description 7
- 230000001788 irregular Effects 0.000 claims description 7
- 239000004568 cement Substances 0.000 claims description 5
- 239000010451 perlite Substances 0.000 claims description 4
- 235000019362 perlite Nutrition 0.000 claims description 4
- 239000010455 vermiculite Substances 0.000 claims description 4
- 229910052902 vermiculite Inorganic materials 0.000 claims description 4
- 235000019354 vermiculite Nutrition 0.000 claims description 4
- 239000000758 substrate Substances 0.000 claims description 2
- 230000017525 heat dissipation Effects 0.000 abstract description 3
- 239000002245 particle Substances 0.000 description 16
- ILRRQNADMUWWFW-UHFFFAOYSA-K aluminium phosphate Chemical compound O1[Al]2OP1(=O)O2 ILRRQNADMUWWFW-UHFFFAOYSA-K 0.000 description 13
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 12
- 239000000654 additive Substances 0.000 description 11
- 239000011230 binding agent Substances 0.000 description 10
- 239000011449 brick Substances 0.000 description 9
- 239000002002 slurry Substances 0.000 description 9
- DHAHRLDIUIPTCJ-UHFFFAOYSA-K aluminium metaphosphate Chemical compound [Al+3].[O-]P(=O)=O.[O-]P(=O)=O.[O-]P(=O)=O DHAHRLDIUIPTCJ-UHFFFAOYSA-K 0.000 description 8
- 238000010438 heat treatment Methods 0.000 description 8
- 239000000203 mixture Substances 0.000 description 8
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 7
- 239000003513 alkali Substances 0.000 description 7
- 229910019142 PO4 Inorganic materials 0.000 description 6
- 238000006243 chemical reaction Methods 0.000 description 6
- 239000010452 phosphate Chemical group 0.000 description 6
- 229910000831 Steel Inorganic materials 0.000 description 5
- XFWJKVMFIVXPKK-UHFFFAOYSA-N calcium;oxido(oxo)alumane Chemical compound [Ca+2].[O-][Al]=O.[O-][Al]=O XFWJKVMFIVXPKK-UHFFFAOYSA-N 0.000 description 5
- -1 citric Chemical class 0.000 description 5
- 238000011068 loading method Methods 0.000 description 5
- NBIIXXVUZAFLBC-UHFFFAOYSA-K phosphate Chemical compound [O-]P([O-])([O-])=O NBIIXXVUZAFLBC-UHFFFAOYSA-K 0.000 description 5
- 229920000642 polymer Polymers 0.000 description 5
- 239000010959 steel Substances 0.000 description 5
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 4
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 4
- 229910001570 bauxite Inorganic materials 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 4
- 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 4
- 238000010304 firing Methods 0.000 description 4
- 150000002500 ions Chemical class 0.000 description 4
- 229910052863 mullite Inorganic materials 0.000 description 4
- WSFSSNUMVMOOMR-UHFFFAOYSA-N Formaldehyde Chemical compound O=C WSFSSNUMVMOOMR-UHFFFAOYSA-N 0.000 description 3
- KWYUFKZDYYNOTN-UHFFFAOYSA-M Potassium hydroxide Chemical compound [OH-].[K+] KWYUFKZDYYNOTN-UHFFFAOYSA-M 0.000 description 3
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 125000005341 metaphosphate group Chemical group 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 3
- 239000003960 organic solvent Substances 0.000 description 3
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 3
- 229910010271 silicon carbide Inorganic materials 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- BHPQYMZQTOCNFJ-UHFFFAOYSA-N Calcium cation Chemical compound [Ca+2] BHPQYMZQTOCNFJ-UHFFFAOYSA-N 0.000 description 2
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 2
- 239000004698 Polyethylene Substances 0.000 description 2
- 239000004743 Polypropylene Substances 0.000 description 2
- CDBYLPFSWZWCQE-UHFFFAOYSA-L Sodium Carbonate Chemical compound [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 description 2
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 2
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910000147 aluminium phosphate Inorganic materials 0.000 description 2
- INJRKJPEYSAMPD-UHFFFAOYSA-N aluminum;silicic acid;hydrate Chemical compound O.[Al].[Al].O[Si](O)(O)O INJRKJPEYSAMPD-UHFFFAOYSA-N 0.000 description 2
- 238000004873 anchoring Methods 0.000 description 2
- TZCXTZWJZNENPQ-UHFFFAOYSA-L barium sulfate Chemical compound [Ba+2].[O-]S([O-])(=O)=O TZCXTZWJZNENPQ-UHFFFAOYSA-L 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- 229910001424 calcium ion Inorganic materials 0.000 description 2
- 150000001720 carbohydrates Chemical class 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 229910000423 chromium oxide Inorganic materials 0.000 description 2
- 238000000354 decomposition reaction Methods 0.000 description 2
- HOOWDPSAHIOHCC-UHFFFAOYSA-N dialuminum tricalcium oxygen(2-) Chemical compound [O--].[O--].[O--].[O--].[O--].[O--].[Al+3].[Al+3].[Ca++].[Ca++].[Ca++] HOOWDPSAHIOHCC-UHFFFAOYSA-N 0.000 description 2
- 239000010459 dolomite Substances 0.000 description 2
- 229910000514 dolomite Inorganic materials 0.000 description 2
- 150000002170 ethers Chemical class 0.000 description 2
- 229910021485 fumed silica Inorganic materials 0.000 description 2
- AMWRITDGCCNYAT-UHFFFAOYSA-L hydroxy(oxo)manganese;manganese Chemical compound [Mn].O[Mn]=O.O[Mn]=O AMWRITDGCCNYAT-UHFFFAOYSA-L 0.000 description 2
- 239000010443 kyanite Substances 0.000 description 2
- 229910052850 kyanite Inorganic materials 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000000395 magnesium oxide Substances 0.000 description 2
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 2
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 125000002467 phosphate group Chemical group [H]OP(=O)(O[H])O[*] 0.000 description 2
- 229920005646 polycarboxylate Polymers 0.000 description 2
- 229920000573 polyethylene Polymers 0.000 description 2
- 229920000139 polyethylene terephthalate Polymers 0.000 description 2
- 239000005020 polyethylene terephthalate Substances 0.000 description 2
- 229920001155 polypropylene Polymers 0.000 description 2
- BWHMMNNQKKPAPP-UHFFFAOYSA-L potassium carbonate Chemical compound [K+].[K+].[O-]C([O-])=O BWHMMNNQKKPAPP-UHFFFAOYSA-L 0.000 description 2
- 239000002243 precursor Substances 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 239000004094 surface-active agent Substances 0.000 description 2
- LWIHDJKSTIGBAC-UHFFFAOYSA-K tripotassium phosphate Chemical compound [K+].[K+].[K+].[O-]P([O-])([O-])=O LWIHDJKSTIGBAC-UHFFFAOYSA-K 0.000 description 2
- IVORCBKUUYGUOL-UHFFFAOYSA-N 1-ethynyl-2,4-dimethoxybenzene Chemical compound COC1=CC=C(C#C)C(OC)=C1 IVORCBKUUYGUOL-UHFFFAOYSA-N 0.000 description 1
- FOGYNLXERPKEGN-UHFFFAOYSA-N 3-(2-hydroxy-3-methoxyphenyl)-2-[2-methoxy-4-(3-sulfopropyl)phenoxy]propane-1-sulfonic acid Chemical compound COC1=CC=CC(CC(CS(O)(=O)=O)OC=2C(=CC(CCCS(O)(=O)=O)=CC=2)OC)=C1O FOGYNLXERPKEGN-UHFFFAOYSA-N 0.000 description 1
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 229910000680 Aluminized steel Inorganic materials 0.000 description 1
- 239000004254 Ammonium phosphate Substances 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910021503 Cobalt(II) hydroxide Inorganic materials 0.000 description 1
- 229920001353 Dextrin Polymers 0.000 description 1
- 239000004375 Dextrin Substances 0.000 description 1
- FEWJPZIEWOKRBE-JCYAYHJZSA-N Dextrotartaric acid Chemical compound OC(=O)[C@H](O)[C@@H](O)C(O)=O FEWJPZIEWOKRBE-JCYAYHJZSA-N 0.000 description 1
- 229910052691 Erbium Inorganic materials 0.000 description 1
- 229910052688 Gadolinium Inorganic materials 0.000 description 1
- DSLZVSRJTYRBFB-UHFFFAOYSA-N Galactaric acid Natural products OC(=O)C(O)C(O)C(O)C(O)C(O)=O DSLZVSRJTYRBFB-UHFFFAOYSA-N 0.000 description 1
- 229920000877 Melamine resin Polymers 0.000 description 1
- 229920000881 Modified starch Polymers 0.000 description 1
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical class O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 1
- 229920000388 Polyphosphate Polymers 0.000 description 1
- 239000004111 Potassium silicate Substances 0.000 description 1
- 239000004115 Sodium Silicate Substances 0.000 description 1
- 229920002472 Starch Polymers 0.000 description 1
- 235000019892 Stellar Nutrition 0.000 description 1
- FEWJPZIEWOKRBE-UHFFFAOYSA-N Tartaric acid Natural products [H+].[H+].[O-]C(=O)C(O)C(O)C([O-])=O FEWJPZIEWOKRBE-UHFFFAOYSA-N 0.000 description 1
- 240000008042 Zea mays Species 0.000 description 1
- 235000005824 Zea mays ssp. parviglumis Nutrition 0.000 description 1
- 235000002017 Zea mays subsp mays Nutrition 0.000 description 1
- XHCLAFWTIXFWPH-UHFFFAOYSA-N [O-2].[O-2].[O-2].[O-2].[O-2].[V+5].[V+5] Chemical compound [O-2].[O-2].[O-2].[O-2].[O-2].[V+5].[V+5] XHCLAFWTIXFWPH-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000001252 acrylic acid derivatives Chemical class 0.000 description 1
- 150000001253 acrylic acids Chemical class 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- 150000001335 aliphatic alkanes Chemical class 0.000 description 1
- 229910052783 alkali metal 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
- 150000001408 amides Chemical class 0.000 description 1
- 150000001412 amines Chemical class 0.000 description 1
- 229910000148 ammonium phosphate Inorganic materials 0.000 description 1
- 235000019289 ammonium phosphates Nutrition 0.000 description 1
- 229910052849 andalusite Inorganic materials 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- 239000012298 atmosphere Substances 0.000 description 1
- AYJRCSIUFZENHW-DEQYMQKBSA-L barium(2+);oxomethanediolate Chemical compound [Ba+2].[O-][14C]([O-])=O AYJRCSIUFZENHW-DEQYMQKBSA-L 0.000 description 1
- 239000002585 base Substances 0.000 description 1
- YZYDPPZYDIRSJT-UHFFFAOYSA-K boron phosphate Chemical compound [B+3].[O-]P([O-])([O-])=O YZYDPPZYDIRSJT-UHFFFAOYSA-K 0.000 description 1
- 229910000149 boron phosphate Inorganic materials 0.000 description 1
- AXCZMVOFGPJBDE-UHFFFAOYSA-L calcium dihydroxide Chemical compound [OH-].[OH-].[Ca+2] AXCZMVOFGPJBDE-UHFFFAOYSA-L 0.000 description 1
- 239000000920 calcium hydroxide Substances 0.000 description 1
- 229910001861 calcium hydroxide Inorganic materials 0.000 description 1
- BRPQOXSCLDDYGP-UHFFFAOYSA-N calcium oxide Chemical compound [O-2].[Ca+2] BRPQOXSCLDDYGP-UHFFFAOYSA-N 0.000 description 1
- 239000000292 calcium oxide Substances 0.000 description 1
- ODINCKMPIJJUCX-UHFFFAOYSA-N calcium oxide Inorganic materials [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 description 1
- 239000001506 calcium phosphate Substances 0.000 description 1
- 229910000389 calcium phosphate Inorganic materials 0.000 description 1
- 235000011010 calcium phosphates Nutrition 0.000 description 1
- 239000000378 calcium silicate Substances 0.000 description 1
- 229910052918 calcium silicate Inorganic materials 0.000 description 1
- OYACROKNLOSFPA-UHFFFAOYSA-N calcium;dioxido(oxo)silane Chemical compound [Ca+2].[O-][Si]([O-])=O OYACROKNLOSFPA-UHFFFAOYSA-N 0.000 description 1
- 235000014633 carbohydrates Nutrition 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 239000003153 chemical reaction reagent Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- VQWFNAGFNGABOH-UHFFFAOYSA-K chromium(iii) hydroxide Chemical compound [OH-].[OH-].[OH-].[Cr+3] VQWFNAGFNGABOH-UHFFFAOYSA-K 0.000 description 1
- 239000004927 clay Substances 0.000 description 1
- 229910000428 cobalt oxide Inorganic materials 0.000 description 1
- ASKVAEGIVYSGNY-UHFFFAOYSA-L cobalt(ii) hydroxide Chemical compound [OH-].[OH-].[Co+2] ASKVAEGIVYSGNY-UHFFFAOYSA-L 0.000 description 1
- IVMYJDGYRUAWML-UHFFFAOYSA-N cobalt(ii) oxide Chemical compound [Co]=O IVMYJDGYRUAWML-UHFFFAOYSA-N 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 235000005822 corn Nutrition 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 235000019425 dextrin Nutrition 0.000 description 1
- MNNHAPBLZZVQHP-UHFFFAOYSA-N diammonium hydrogen phosphate Chemical compound [NH4+].[NH4+].OP([O-])([O-])=O MNNHAPBLZZVQHP-UHFFFAOYSA-N 0.000 description 1
- QDOXWKRWXJOMAK-UHFFFAOYSA-N dichromium trioxide Chemical compound O=[Cr]O[Cr]=O QDOXWKRWXJOMAK-UHFFFAOYSA-N 0.000 description 1
- 239000002270 dispersing agent Substances 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 150000002148 esters Chemical class 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- NVVZQXQBYZPMLJ-UHFFFAOYSA-N formaldehyde;naphthalene-1-sulfonic acid Chemical compound O=C.C1=CC=C2C(S(=O)(=O)O)=CC=CC2=C1 NVVZQXQBYZPMLJ-UHFFFAOYSA-N 0.000 description 1
- 229910052839 forsterite Inorganic materials 0.000 description 1
- 239000005350 fused silica glass Substances 0.000 description 1
- DSLZVSRJTYRBFB-DUHBMQHGSA-N galactaric acid Chemical compound OC(=O)[C@H](O)[C@@H](O)[C@@H](O)[C@H](O)C(O)=O DSLZVSRJTYRBFB-DUHBMQHGSA-N 0.000 description 1
- 229910001679 gibbsite Inorganic materials 0.000 description 1
- 150000004676 glycans Chemical class 0.000 description 1
- 150000002334 glycols Chemical class 0.000 description 1
- 238000001513 hot isostatic pressing Methods 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 150000002576 ketones Chemical class 0.000 description 1
- XGZVUEUWXADBQD-UHFFFAOYSA-L lithium carbonate Chemical compound [Li+].[Li+].[O-]C([O-])=O XGZVUEUWXADBQD-UHFFFAOYSA-L 0.000 description 1
- 229910052808 lithium carbonate Inorganic materials 0.000 description 1
- PAZHGORSDKKUPI-UHFFFAOYSA-N lithium metasilicate Chemical compound [Li+].[Li+].[O-][Si]([O-])=O PAZHGORSDKKUPI-UHFFFAOYSA-N 0.000 description 1
- 229910052912 lithium silicate Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000001095 magnesium carbonate Substances 0.000 description 1
- ZLNQQNXFFQJAID-UHFFFAOYSA-L magnesium carbonate Chemical compound [Mg+2].[O-]C([O-])=O ZLNQQNXFFQJAID-UHFFFAOYSA-L 0.000 description 1
- 229910000021 magnesium carbonate Inorganic materials 0.000 description 1
- 235000014380 magnesium carbonate Nutrition 0.000 description 1
- VTHJTEIRLNZDEV-UHFFFAOYSA-L magnesium dihydroxide Chemical compound [OH-].[OH-].[Mg+2] VTHJTEIRLNZDEV-UHFFFAOYSA-L 0.000 description 1
- 239000000347 magnesium hydroxide Substances 0.000 description 1
- 229910001862 magnesium hydroxide Inorganic materials 0.000 description 1
- HCWCAKKEBCNQJP-UHFFFAOYSA-N magnesium orthosilicate Chemical compound [Mg+2].[Mg+2].[O-][Si]([O-])([O-])[O-] HCWCAKKEBCNQJP-UHFFFAOYSA-N 0.000 description 1
- GVALZJMUIHGIMD-UHFFFAOYSA-H magnesium phosphate Chemical compound [Mg+2].[Mg+2].[Mg+2].[O-]P([O-])([O-])=O.[O-]P([O-])([O-])=O GVALZJMUIHGIMD-UHFFFAOYSA-H 0.000 description 1
- 239000004137 magnesium phosphate Substances 0.000 description 1
- 229910000157 magnesium phosphate Inorganic materials 0.000 description 1
- 229960002261 magnesium phosphate Drugs 0.000 description 1
- 235000010994 magnesium phosphates Nutrition 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- JDSHMPZPIAZGSV-UHFFFAOYSA-N melamine Chemical compound NC1=NC(N)=NC(N)=N1 JDSHMPZPIAZGSV-UHFFFAOYSA-N 0.000 description 1
- 150000002739 metals Chemical group 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 229910000476 molybdenum oxide Inorganic materials 0.000 description 1
- 239000000178 monomer Substances 0.000 description 1
- 239000004570 mortar (masonry) Substances 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910000480 nickel oxide Inorganic materials 0.000 description 1
- BFDHFSHZJLFAMC-UHFFFAOYSA-L nickel(ii) hydroxide Chemical compound [OH-].[OH-].[Ni+2] BFDHFSHZJLFAMC-UHFFFAOYSA-L 0.000 description 1
- 229910052609 olivine Inorganic materials 0.000 description 1
- 239000010450 olivine Substances 0.000 description 1
- 150000007524 organic acids Chemical class 0.000 description 1
- 235000005985 organic acids Nutrition 0.000 description 1
- 229920000620 organic polymer Polymers 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- PQQKPALAQIIWST-UHFFFAOYSA-N oxomolybdenum Chemical compound [Mo]=O PQQKPALAQIIWST-UHFFFAOYSA-N 0.000 description 1
- GNRSAWUEBMWBQH-UHFFFAOYSA-N oxonickel Chemical compound [Ni]=O GNRSAWUEBMWBQH-UHFFFAOYSA-N 0.000 description 1
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 1
- 239000002367 phosphate rock Substances 0.000 description 1
- 235000011007 phosphoric acid Nutrition 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 229920001515 polyalkylene glycol Polymers 0.000 description 1
- 229920001223 polyethylene glycol Polymers 0.000 description 1
- 239000012704 polymeric precursor Substances 0.000 description 1
- 239000001205 polyphosphate Substances 0.000 description 1
- 235000011176 polyphosphates Nutrition 0.000 description 1
- 229920001282 polysaccharide Polymers 0.000 description 1
- 239000005017 polysaccharide Substances 0.000 description 1
- 229910000027 potassium carbonate Inorganic materials 0.000 description 1
- 229910000160 potassium phosphate Inorganic materials 0.000 description 1
- 235000011009 potassium phosphates Nutrition 0.000 description 1
- NNHHDJVEYQHLHG-UHFFFAOYSA-N potassium silicate Chemical compound [K+].[K+].[O-][Si]([O-])=O NNHHDJVEYQHLHG-UHFFFAOYSA-N 0.000 description 1
- 229910052913 potassium silicate Inorganic materials 0.000 description 1
- 235000019353 potassium silicate Nutrition 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 239000011214 refractory ceramic Substances 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 239000012783 reinforcing fiber Substances 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 229910052814 silicon oxide Inorganic materials 0.000 description 1
- 229910052851 sillimanite Inorganic materials 0.000 description 1
- 229910000029 sodium carbonate Inorganic materials 0.000 description 1
- 239000001488 sodium phosphate Substances 0.000 description 1
- 229910000162 sodium phosphate Inorganic materials 0.000 description 1
- 235000011008 sodium phosphates Nutrition 0.000 description 1
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 1
- 229910052911 sodium silicate Inorganic materials 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 235000019698 starch Nutrition 0.000 description 1
- 239000008107 starch Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- BDHFUVZGWQCTTF-UHFFFAOYSA-M sulfonate Chemical compound [O-]S(=O)=O BDHFUVZGWQCTTF-UHFFFAOYSA-M 0.000 description 1
- 239000012209 synthetic fiber Substances 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- 239000006188 syrup Substances 0.000 description 1
- 235000020357 syrup Nutrition 0.000 description 1
- 235000002906 tartaric acid Nutrition 0.000 description 1
- 239000011975 tartaric acid Substances 0.000 description 1
- XOLBLPGZBRYERU-UHFFFAOYSA-N tin dioxide Chemical compound O=[Sn]=O XOLBLPGZBRYERU-UHFFFAOYSA-N 0.000 description 1
- 229910001887 tin oxide Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
- QORWJWZARLRLPR-UHFFFAOYSA-H tricalcium bis(phosphate) Chemical compound [Ca+2].[Ca+2].[Ca+2].[O-]P([O-])([O-])=O.[O-]P([O-])([O-])=O QORWJWZARLRLPR-UHFFFAOYSA-H 0.000 description 1
- RYFMWSXOAZQYPI-UHFFFAOYSA-K trisodium phosphate Chemical compound [Na+].[Na+].[Na+].[O-]P([O-])([O-])=O RYFMWSXOAZQYPI-UHFFFAOYSA-K 0.000 description 1
- 229910001935 vanadium oxide Inorganic materials 0.000 description 1
- 239000011345 viscous material Substances 0.000 description 1
- 239000011787 zinc oxide Substances 0.000 description 1
- LRXTYHSAJDENHV-UHFFFAOYSA-H zinc phosphate Chemical compound [Zn+2].[Zn+2].[Zn+2].[O-]P([O-])([O-])=O.[O-]P([O-])([O-])=O LRXTYHSAJDENHV-UHFFFAOYSA-H 0.000 description 1
- 229910000165 zinc phosphate Inorganic materials 0.000 description 1
- 229910001928 zirconium oxide Inorganic materials 0.000 description 1
Classifications
-
- 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
- C04B28/34—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 cold phosphate binders
- C04B28/344—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 cold phosphate binders the phosphate binder being present in the starting composition solely as one or more phosphates
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D1/00—Casings; Linings; Walls; Roofs
- F27D1/0003—Linings or walls
- F27D1/0006—Linings or walls formed from bricks or layers with a particular composition or specific characteristics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D1/00—Casings; Linings; Walls; Roofs
- F27D1/04—Casings; Linings; Walls; Roofs characterised by the form, e.g. shape of the bricks or blocks used
-
- 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
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02W—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
- Y02W30/00—Technologies for solid waste management
- Y02W30/50—Reuse, recycling or recovery technologies
- Y02W30/91—Use of waste materials as fillers for mortars or concrete
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Inorganic Chemistry (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Furnace Housings, Linings, Walls, And Ceilings (AREA)
- Building Environments (AREA)
- Curing Cements, Concrete, And Artificial Stone (AREA)
- Muffle Furnaces And Rotary Kilns (AREA)
Abstract
A refractory strucutral element is provided that is useful for lining the inner surface of a construct typically used as a kiln or other high temperature system. An element includes a stem portion associated with a flared end block portion whereby the flared end block portion is compatible with other strucutral elements to form a substantially continuous tiled surface when a plurality of refractory structural elements are laid adjacent to each other. The stem portion optionally has a plurality of protrusions decorated on its outer surface that may serve to adjust heat dissipation from the element.
Description
REFRACTORY STRUCTURAL ELEMENT
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] This application depends from and claims priority to U.S. Provisional Patent Application No. 61/362,489, filed July 8, 2010, the entire contents of which are incorporated herein by reference.
FIELD OF THE INVENTION
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] This application depends from and claims priority to U.S. Provisional Patent Application No. 61/362,489, filed July 8, 2010, the entire contents of which are incorporated herein by reference.
FIELD OF THE INVENTION
[0002] The present invention relates to refractory materials and in particular to a cast structural element from which furnaces, kilns, and other high temperature forms are constructed.
BACKGROUND OF THE INVENTION
BACKGROUND OF THE INVENTION
[0003] A conventional high temperature construct such as a furnace or kiln is based on the interlocking of rectilinear bricks to form a desired construct. The sides of the bricks often are produced with undulations to facilitate interlocking and limit material and heat transfer along the sides of such bricks. Specialized variants of such conventional bricks have a rearward facing end relative to the face defining a surface of the kiln or furnace, the rearward end engages a hanger so as to form a roof portion for such a construct.
[0004] These conventional bricks suffer a number of limitations that add to the cost of creating a high temperature construct and the maintenance thereof. These limitations include an inefficient use of material along the sides of the brick between the face defining a surface of the high temperature construct and the rearward face, as well as a limited ability to tailor the properties of a construct formed from such bricks to the conditions of temperature and corrosivity associated with the intended usage of the construct.
[0005] Thus, there exists a need for a refractory structural element that more efficiently forms a portion of a high temperature construct. There also exists a need for a refractory structural element that is readily tailored so as to match the thermal and compositional conditions that the construct will experience in operation.
SUMMARY OF THE INVENTION
SUMMARY OF THE INVENTION
[0006] The following summary of the invention is provided to facilitate an understanding of some of the innovative features unique to the present invention and is not intended to be a full description. A full appreciation of the various aspects of the invention can be gained by taking the entire specification, claims, drawings, and abstract as a whole.
[0007] A refractory structural element is provided that can be made of a variety of cementitious materials that is useful for lining a construct exposed to high internal temperatures or other extreme conditions. A refractory strucutral element is formed in a shape having a stem portion, the stem portion having a first end and a second end, the second end associated with a flared end block portion, the flared end block portion including a face, the face having a cross sectional dimension that is greater than a cross sectional dimension of said stem portion. This provides an element that creates a space filling end and a space behind the space filling end.
[0007] A refractory structural element is provided that can be made of a variety of cementitious materials that is useful for lining a construct exposed to high internal temperatures or other extreme conditions. A refractory strucutral element is formed in a shape having a stem portion, the stem portion having a first end and a second end, the second end associated with a flared end block portion, the flared end block portion including a face, the face having a cross sectional dimension that is greater than a cross sectional dimension of said stem portion. This provides an element that creates a space filling end and a space behind the space filling end.
[0008] The stem portion is optionally continuous with the flared end block portion or is formed of a separate material (same or different) that is then physically associated with the flared end block portion either fixedly or removably. A stem portion has a cross sectional shape. A
stem cross sectional shape is optionally circular, ellipsoidal, or polygonal.
The side of the stem portion is optionally decorated with protrusions. These protrusions increase the surface area of the stem portion relative to that of a smooth cylinder. Such protrusions may be in a variety of shapes including undulations, spirals, ridges, irregular scores, or a combination thereof. A stem portion also optionally includes a flange operable to engage a fastener for securement of the element to a substrate such as the interior surface of a construct.
stem cross sectional shape is optionally circular, ellipsoidal, or polygonal.
The side of the stem portion is optionally decorated with protrusions. These protrusions increase the surface area of the stem portion relative to that of a smooth cylinder. Such protrusions may be in a variety of shapes including undulations, spirals, ridges, irregular scores, or a combination thereof. A stem portion also optionally includes a flange operable to engage a fastener for securement of the element to a substrate such as the interior surface of a construct.
[0009] The space created by the shape of an element optionally includes fill material surrounding the stem portion. A fill material is optionally ceramic fiber, perlite, vermiculite, or combinations thereof.
[0010] The face of the flared end block portion is intended to be directed to the interior of a construct. The shape of this face is optionally planar or arcuate. An arcuate face is optionally convex, concave, irregular, or other shape. The flared end block portion has a first edge that optionally includes a contour feature where the contour feature is shaped to interlock with a complementary feature of a complementary refractory article to be located adjacent to the refractory structural element. A second edge of a flared end block portion optionally includes a complementary contour feature. A complementary contour feature optionally has a complementary shape to a contour feature. The shape of a contour feature or a complementary contour feature is optionally a tongue, groove, pin, socket, or combinations thereof.
[0011] On a side opposing a face, a flared end block portion optionally is shaped to include one or more walls extending from an edge of the flared end portion to the second end of the stem. The walls are optionally angled relative to a plane of the face where the plane is defined by the outer edges of the face. A flared end block portion has a thickness that is optionally uniform over the plane of the face. Optionally, the thickness of the flared end block portion at a central point is greater than the thickness at an edge of the flared end block portion.
[0012] A heat refractive cementitious material is optionally used to form a refractory structural element. A cementitious material is optionally a phosphate-bonded cement.
BRIEF DESCRIPTION OF THE DRAWINGS
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Fig. 1 is a partial cutaway view of an inventive refractory structural element (A) with a flange associatable with a fastener (B);
[0014] Fig. 2 is a perspective view of an alternate embodiment of an inventive structural element;
[0015] Figs. 3A-3C are exemplary end block portions of an inventive refractory structural element; and [0016] Figs. 4A-4C are exemplary edge profiles of stem portions of an inventive refractory structural element.
DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
[0017] The following description of particular embodiment(s) is merely exemplary in nature and is in no way intended to limit the scope of the invention, its application, or uses, which may, of course, vary. The invention is described with relation to the non-limiting definitions and terminology included herein. These definitions and terminology are not designed to function as a limitation on the scope or practice of the invention but are presented for illustrative and descriptive purposes only.
[0018] The present invention has utility as a structural element for the construction of a refractory construct such as an incinerator, kiln, oven, or furnace; or conduits or other structures in thermal communication with such a construct. An inventive element is operative in forming various surfaces of the construct including a base, a side wall, a roof, or tubular structure.
[0019] Referring now to Fig. 1A, an inventive refractory structural element is shown generally at 10. The element 10 includes a stem portion 12 having a first end 14 and a second end 16. A stem portion has a length and a cross sectional dimension. A length is optionally from 5 to 50 cm, or any value or range therebetween. A cross sectional dimension is optionally from 0.5 to 10 cm. A stem portion has a cross sectional area that is optionally circular, elliptical, or other irregularly curved shape, or polygonal such as triangular, square, pentagonal, hexagonal, or other polygon of any number of sides.
[0020] A flared end block portion 18 is associated with a second end 16 illustratively by being continuous with or joined to the second end 16. While the unitary, joined version of an element 10 is depicted in Fig. 1, a dashed line 20 is provided to depict an optional joinder from a multipart element 10. It is appreciated that a flared end block portion 18 is made from the same material or a different material than the stem portion 12. The flared end block portion has a face 22. The face 22 is intended to be proximal to a heat source or otherwise define a confinement surface of the construct. Optionally, the face 22 is shaped to be space filling. As used herein, "space filling" is defined as able to propagate through and cover a space only with resort to translation of the face shape. With joinder of multiple elements 10, the face 22, and duplicates thereof or complementary faces, readily tile a planar or curved space that is operative in the context of a construct to form a floor, side wall, or roof of a construct.
[0021] A face optionally has a cross-sectional dimension that is from 10 to 50 cm, or any value or range therebetween. A cross sectional dimension is optionally the length of an edge, a diagonal, a diameter, or other dimension across the face from one edge to another edge.
[0022] A flared end block portion has a thickness that is either uniform across the cross sectional dimension of a flared end block portion, is irregular, or sloping. A
thickness is appreciated to be sufficient at the narrowest dimension to provide sufficient heat refraction for operation. Illustratively, a thickness is from 1 to 10 cm, or any value or range therebetween.
thickness is appreciated to be sufficient at the narrowest dimension to provide sufficient heat refraction for operation. Illustratively, a thickness is from 1 to 10 cm, or any value or range therebetween.
[0023] In some embodiments, an element has one or more walls extending from an edge 23 to the second end 16. The walls are optionally sloped such that the flared end block portion has a thickness in the center that is greater than at the edge. The ratio of the thickness of the center to the thickness of the edge of a flared end block portion is optionally from 0.1-1 to 1-0.1. As such, the central point of a flared end block portion is optionally thicker or thinner than the thickness at an edge. The number of walls is optionally identical to the number of edges of a flared end block portion. Illustratively, the number of walls is 3, 4, 5, 6, 7, 8, or more. A wall optionally slopes at an angle relative to the plane of a face of the flared end block portion. Such angles are optionally from -20 degrees to 60 degrees, or any value or range therebetween depending on the relative dimensions of the flared end block portion and the stem portion. The slope of a wall is optionally uniform so as to provide a substantially flat wall, or is curved. A
curved wall optionally increases in angle from the edge to the stem portion, or decreases in angle from the edge to the stem portion. In some embodiments, a single wall is present such as a conical or globed wall that is continuous with the outer edges of the flared end block portion.
While the walls of FIG. 1A are substantially pyramidal in shape, it is appreciated that a flared end block portion need not have pyramidal sloped walls 24 or a face 22 that is planar.
Alternative flared end block portions relative to 18 are provided in Figs. 3A-3C.
5 [0024] The stem portion 12 has a side 32 optionally including protrusions shown generally at 34. The protrusions 34 decorate the side 32 or are integral with the side 32. The protrusions may take a variety of forms illustratively including undulations, spirals, ridges, regular or irregular scores, or combinations thereof. The protrusions, regardless of the form, function to increase the surface area of the side 32. This additional surface area on the side 32 allows for additional radiative heat dissipation as well as provides additional surface area for interlocking of element 10 with other joining pieces and/or mortar. In addition to the protrusions 34, other illustrative side profiles for such protrusions are depicted in Fig. 2 and Figs. 4A-4C. Optionally, any shape to the protrusions are operable so long as the presence of the shape increases the surface area of the side relative to a smooth cylinder.
[0025] As depicted in FIG. 1B, a stem portion 12 optionally has a first end 14 configured to be complementary to a fastener 28, either conventional or specific to the first end 14. A fastener 28 is fixedly or removably associated with an anchoring optionally formed from refractory brick that forms the inner surface of a construct. As depicted in FIG. 1B, a first end 14 optionally includes a flange 26 that is complementary to the fastener 28 to provide fixed or removable association of the element 28 with the fastener. While FIG. 1B illustrates a flange in a circular or ellipsoidal configuration, it is appreciated that other shapes are similarly operable such as a any pentagonal shape, or an irregular shape.
[0026] Optionally, the flared end block portion 18 has an edge 23 that has a contoured feature 25 to interlock with a complementary feature on another refractory article (not shown), the other refractory article optionally being another element 10, or an element with a shape complementary to the end block portion of the element 10, to better join an inventive element to neighboring elements and thereby form a more robust refractory construct. A
flared end block portion optionally has 3, 4, 5, 6, 7, 8, or more edges. A contour portion on a flared end block portion on a first edge is optionally a complementary feature to a contour portion on a different edge.
[0027] While contour feature 25 is shown as a protrusion, a complementary contour feature as a recess (e.g. groove) is depicted at 25. In addition to the tongue-and-groove contour features depicted in Fig. 1A, it is appreciated that other contour features are operative herein illustratively including dovetails, pin and socket, and other such complementary features conventional to the joinder arts. As such, a contour feature is optionally a tongue (optionally rectilinear or curved), groove (optionally rectilinear or curved), angular so as to form a dovetail joint, pin shape such as a tenon or cylindrical protrusion, or socket shape such as that of a mortise (rectangular or curved).
[0028] A edge optionally includes a plurality of contoured features, complementary features, or both. Contoured features and complementary features are optionally interdispersed, optionally to form an undulating surface for interlocking with another refractory structural element or other surface. The number of contoured features or complementary features is optionally 1, 2, 3, 4, 5, 6, or more.
[0029] FIG. 2 is a perspective view of an alternate embodiment of a structural element shown generally at 40. The element 40 is readily formed from the same materials and by the same techniques as element 10. Additionally, element 40 is also amenable to formation of the stem portion 42 and the flared end block portion 48 as unitary or joined portions consistent with the above description relative to element 10. The face 52 of element 40 is noted to be a regular hexagon in shape and also suitable for space filling to tile a plane or other shaped surface. The end block portion 48 optionally has walls 54 extending approximating parallel to the face 52 in this or other embodiments. The stem 42 is depicted as having a side 62 defined by a spiral protrusion. A first end 44 of the stem portion 42 has a flange 56 and adapted to fixedly or removably engage an anchoring fastener optionally the like of those conventional to the art. In addition to a stem portion 42 having a circular cross section, it is appreciated that this cross section is readily distorted to form an ellipsoidal cross section.
Additionally, it is appreciated that the face 52 in addition to being planar is also formed to be arcuate to form either a concave or convex surface, optionally as illustrated in exemplary form in Figs. 3A-3C.
[0030] Owing to strength properties at elevated temperatures above 1000 Celsius and nonwetting properties relative to molten metals, phosphate bonded cements can be used as a substance from which an element is formed. It is appreciated that other cementitious materials can be used to form a refractory structural elements depending on the eventual exposure requirements of the element.
[0031] In some embodiments, a refractory structural element is made from a phosphate bonded cementitious material that is formed from a phosphate based component and an alkali earth component such as that described in U.S. Patent 7,503,974. The alkali earth ion component has as a majority source a calcium aluminate calcium ion source of dodeca-calcium hepta-aluminate, or tricalcium aluminate. Magnesium oxide that has been fused and crushed to a size of less than 200 microns, alone or in combination with the calcium aluminate calcium ion source is also provided as the alkali earth ion component.
[0032] An exemplary phosphate based component includes phosphoric acid, calcium phosphate, potassium phosphate, magnesium phosphate, sodium phosphate, aluminum phosphate, ammonium phosphate, zinc phosphate, boron phosphate, and combinations thereof.
[0033] An alkali earth ion component optionally includes magnesium oxide, dolomite, zinc oxide, aluminum oxide, calcium oxide, lithium carbonate, barium carbonate, barium sulfate, molybdenum oxide, calcium hydroxide, aluminum hydroxide, tin oxide, nickel oxide, nickel hydroxide, cobalt oxide, cobalt hydroxide, vanadium oxide, magnesium hydroxide, iron oxide, titanium oxide, chromium oxide, chromium hydroxide, dolomite, manganese oxide, zirconium oxide, zirconium hydroxide, NaOH, KOH, sodium carbonate, and potassium carbonate.
[0034] The alkali earth ion component may be predominantly dodeca-calcium hepta-aluminate (C1A7 or mayenite), tricalcium aluminate (C3A), or a combination thereof. The calcium aluminate optionally has a mean particle size of less than 100 microns, optionally 60 microns or less. Typical loadings of C12A7 in a fully formulated cementitious material inclusive of aggregate is from 0.5 to 5 total weight percent with C12A7 typically being present at about one-fourth the weight percent of CA and/or CA2 calcium aluminate used in other cementitious materials. C3A is typically present from 0.3 to 4 total dry weight percent of a cementitious material used to form a refractory structural element.
[0035] Other materials may be included in a cementitious material are illustratively, one or more tackifiers such as: carbohydrates such as saccharides and polysaccharides; starch and derivatives such as pregelatinized starch, dextrin, and corn syrup;
naphthalene sulfonate formaldehyde condensate polymers; melamine sulfonate formaldehyde condensate polymers;
polyhydroxy polycarboxylic compounds such as tartaric acid and mucic acid;
lignosulfonic acid;
and salts of any of the aforementioned acid moieties of tackifiers. A
tackifier is optionally present at 0.01 to 6 total dry weight percent. Plasticizers and strength enhancing agents such as insoluble phosphate are optionally included. Some embodiments include one or more dispersants such as polycarboxylates and conventional surfactants conventional to the field.
Optionally a cementitious material includes one or more deflocculants such as a polyalkylene glycol optionally at 0.05 to 1 weight percent.
[0036] A refractory structural element is optionally cured in a drum heater with internal heating units. A heating temperature in the range of 75 F (23 C) to 150 F
(66 C) is commonly used for this purpose. Heating also promotes the flowability of viscous material. Exemplary types of heaters include band heaters, immersion heaters, and heating cabinets. A band heater is equipped with aluminized steel shell which delivers up to 3,000 Watts of heating power with operating heating temperatures in the range of 60 F (75 C) to 400 F (205 Q. Additionally, an area blanket or quilt is used to insulate a drum heater. Optionally, a temperature shutoff device is installed with a heater for the purpose of preventing overheating of phosphate based component.
[0037] In other embodiments, a refractory structural element is formed from a cementitious material that includes a plurality of aggregate ceramic particles and a binder sintered to the plurality of aggregate ceramic particles, where the binder includes crystalline aluminum orthophosphate distributed in the binder as the result of reaction of aluminum metaphosphate with alumina. The plurality of aggregate ceramic particles optionally includes bauxite particles.
In some embodiments, the plurality of aggregate ceramic particles includes at least one of silicon carbide, fumed silica, or mullite.
[0038] With the refractory aggregate containing alumina, A1203 the aluminum metaphosphate reacts to form crystalline aluminum orthophosphate, A1PO4.
Aluminum orthophosphate is the thermodynamic product upon heating to a temperature greater than about 580 Celsius with a decomposition temperature of about 1650 Celsius. The resultant cementitious material is amenable to incorporation of reinforcing materials such as steel fibers and is operative with aggregate particulate including silicon carbide, mullite, alumina, titania, and combinations thereof. Such a cementitious material is readily formed with a density of greater than 90%, a theoretical density and cold crush strengths in excess of 88 Newtons per square millimeter. Through control of water content and conventional additives, the cast form of refractory structural element has sufficient green strength to be handled and optionally machined prior to firing to provide a refractory structural element with superior strength and alkali resistance, as compared to conventional materials.
[0039] A bindery for a cementitious material optionally includes aluminum metaphosphate that is mixed aggregate ceramic particles and processed under conditions to afford aluminum orthophosphate as a crystalline binder. The binder aluminum orthophosphate optionally has berlinite as a predominant phase. It is appreciated that aluminum metaphosphate as binder precursor is amenable to inclusion in a kit as aluminum metaphosphate is far less hygroscopic as compared to phosphoric acid, more pH neutral (around pH 5) and is commercially available in a variety of particle mesh sizes. The reaction of aluminum metaphosphate with alumina (synonymously termed bauxite herein) to form a crystalline binder phase of aluminum orthophosphate (synonymously referred to herein as berlinite) is detailed with respect to the following equation:
Al(PO3)3 + A1203 -* 3 AIPO4 (1) [0040] Aluminum orthophosphate appears to be a thermodynamically stable phase that is formed upon heating the reagents to a temperature above about 580 Celsius.
Aluminum orthophosphate is noted to have a decomposition temperature of about 1650 Celsius at ambient pressure. It is appreciated that the formation temperature of aluminum orthophosphate varies according to predictable thermodynamic relationships when the reaction proceeds at pressures other than atmospheric pressure. It is appreciated that formation of a refractory composition according to the present invention readily occurs through firing the green form of an article through hot isostatic pressing (HIP). It is appreciated that a mixed metal orthophosphate is readily formed according to the reaction:
Al(PO3)3 + Al2_RMO3 Al Al2_RMPO4 (11) where M is Sb, Bi, B, Cr (III), Er, Gd (III), In (III), Ni (III), Rh (III), Sm (III), Sc (III), Tb (III), Ti (III), W (III), V (III), Yb (III), or Y (III); and x is 0, 1, or 2.
[0041] The amount of aluminum metaphosphate present to form a matrix around refractory ceramic particulate depends on factors including size of the ceramic particulate, desired interparticle separation, morphology, size of primary crystals and oxide state. Optionally, aluminum metaphosphate is present between 2 and 20 total weight percent of the fully formulated cementitious material casting slurry. Alumina is optionally present in excess of molar stoichiometry of alumina metaphosphate. It is appreciated that alumina is present as aggregate ceramic particles or alternatively is added as a minor quantity of the ceramic particles for reaction with the alumina metaphosphate.
[0042] To facilitate mixing of ceramic particle aggregate and alumina metaphosphate as a binder precursor, a quantity of water or organic solvent is added to afford a slurry of a desired viscosity. Such organic solvents illustratively include alcohols, ketones, esters, ethers, amides, amines, glycols, alkanes, and the like. Optionally, such organic solvents are liquids below 200 Celsius, and optionally, are liquids at 20 Celsius. Loadings of water or solvents optionally range from 2-20 total weight percent of a fully formulated cementitious material slurry.
Optionally, additives are included that are consumed during berlinite formation, these additives provided to promote ease of handling. Such additives illustratively include surfactants;
polymerizable organic monomers or oligomers, deflocculants; polymers; and organic acids such as citric, and oxalic. While one of ordinary skill in the art can readily adjust slurry viscosity and green strength through the inclusion of such additives, typically each such additive is present from 0.01-5 total weight percent of a fully formulated refractory composition slurry. It is appreciated that the inclusion of organic monomeric or oligomeric polymerizable materials that upon cure can improve the green strength of the composition prior to firing or reaction according 5 to Equation (I) or (II). The resultant polymer is decomposed and therefore not present in the resultant refractory composition. Exemplary of such organic polymers are acrylic acids, acrylates, polyethylene glycols, and polycarboxylate ethers, which are added as polymeric precursors or slurry soluble preformed polymers.
[0043] Handling properties of a cementitious material slurry and the green strength of a 10 refractory structural element formed therefrom after drying are also optionally modified through inclusion of nonfacile additives. While the amount of such nonfacile additives is controlled by factors including desired green strength, refractory composition, working environment, temperature and corrosivity, desired cold crush strength, and setting time, working time and curing time, typical loadings of such nonfacile additives range from 0.1 to 10 total weight percent of a fully formulated cementitious material slurry. Representative nonfacile additives operative herein include calcium aluminate cement, sodium silicate, fumed silica, alkali metal or alkali earth polyphosphates, and organic salts like citric, oxalic or nitric acids, calcium silicate cement, potassium silicate, lithium silicate. Optionally, a nonfacile additive is present in a quantity such that the aluminum orthophosphate forms a continuous matrix phase.
[0044] Ceramic particle aggregate embedded within an aluminum orthophosphate binder according is limited only by the desired properties of the resultant cementitious material and compatibility with aluminum orthophosphate binder. Operative ceramic particle aggregates illustratively include bauxite, tabular alumina, mullite, silicon carbide, fused silica, rutile, and andalusite, sillimanite, magnesite, forsterite, kyanite, Mg spinell, and chromium oxide. Typical loadings of aggregate ceramic particles range from 50-95 weight percent of a fully formulated refractory composition slurry. Typical aggregate particle sizes range from 0.1 to 1000 microns.
It is appreciated that the aggregate particles can be in a variety of forms including spherical, polyhedral, irregular, and combinations thereof.
[0045] A cementitious material optionally includes strengthening fibers such as steel fibers as detailed in U.S. Patent Nos. 4,366,255. Additional, illustrative reinforcing fibers include nickel and chromium fibers and synthetic fibers such as polypropylene (PP), polyethylene (PE), and polyethylene terephthalate (PET). Optionally steel fibers are used containing aluminum within the steel alloy to form a protective layer of alumina on the steel fiber at elevated temperature. Optionally, the steel fiber has from 0.05 to 8 atomic percent aluminum content.
Other strengthening fiber fillers operative herein include carbon fibers with the recognition that firing occurs in a reducing atmosphere. Typical loadings of fibers are from 0 to 50 total weight percent of a refractory composition used to make a refractory structural element.
[0046] A cementitious material used to form a refractory structural element optionally includes one or more aggregate components. An aggregate component is typically present from 50 to 95 total dry weight percent. Typical aggregates illustratively include:
flint clay, mulcoa, basalt, olivine, diatomite, vermiculite, perlite, molochite, gibbsite, kyanite, mullite, chromite, tabular alumina, silicon oxide, silica, calcined bauxite, chrome oxide, zirconia, phosphate rock, and mixtures thereof.
[0047] A refractory structural element is optionally cast from a variety of cementitious materials other than those disclosed herein such as a variety commercially available materials from Stellar Materials, Inc., Boca Raton., FL. Illustrative examples of materials and methods of their production can be found in U.S. Patent Nos. 6,447,596; and 5,888,292.
[0048] The element, depending on particulars of the shape, is readily cast from two part or multiple part molds through techniques conventional to the art.
[0049] In operation, a refractive structural element forms a space created by projection of the flared end portion backwards towards the first end created by the smaller dimensions of the stem portion and the space surrounding the sides. This space is optionally filled with a fill material illustratively including ceramic fibers, perlite, vermiculite, and combinations thereof alone or retained within a bonded matrix. Space filling with one or more fill materials allows a user to adjust the radiative heat dissipation or insulative characteristics of a construct associated with one or more refractory structural elements to the user's needs.
[0050] One of skill in the art will appreciate that a refractory structural element affords more efficient use of cementitious material from which the element is formed and also through the use of a comparatively small dimension stem relative to the element face, and the ability to form cavities within the element so that adjustment of the operational properties of the element are readily controlled, as compared to conventional bricks.
[0051] The shape of a refractive structural element is optionally used to line the surface of a construct with one or more of many different surface geometries. Refractory structural elements are capable of forming planar or curved surface areas while retaining a desired tight association between the faces of multiple elements.
[0052] Various modifications of the present invention, in addition to those shown and described herein, will be apparent to those skilled in the art of the above description. Such modifications are also intended to fall within the scope of the appended claims.
[0053] It is appreciated that all materials are obtainable from sources known in the art unless otherwise specified.
[0054] Patents and publications mentioned in the specification are indicative of the levels of those skilled in the art to which the invention pertains. These patents and publications are incorporated herein by reference to the same extent as if each individual patent or publication was specifically and individually incorporated herein by reference.
[0055] The foregoing description is illustrative of particular embodiments of the invention, but is not meant to be a limitation upon the practice thereof. The following claims, including all equivalents thereof, are intended to define the scope of the invention.
curved wall optionally increases in angle from the edge to the stem portion, or decreases in angle from the edge to the stem portion. In some embodiments, a single wall is present such as a conical or globed wall that is continuous with the outer edges of the flared end block portion.
While the walls of FIG. 1A are substantially pyramidal in shape, it is appreciated that a flared end block portion need not have pyramidal sloped walls 24 or a face 22 that is planar.
Alternative flared end block portions relative to 18 are provided in Figs. 3A-3C.
5 [0024] The stem portion 12 has a side 32 optionally including protrusions shown generally at 34. The protrusions 34 decorate the side 32 or are integral with the side 32. The protrusions may take a variety of forms illustratively including undulations, spirals, ridges, regular or irregular scores, or combinations thereof. The protrusions, regardless of the form, function to increase the surface area of the side 32. This additional surface area on the side 32 allows for additional radiative heat dissipation as well as provides additional surface area for interlocking of element 10 with other joining pieces and/or mortar. In addition to the protrusions 34, other illustrative side profiles for such protrusions are depicted in Fig. 2 and Figs. 4A-4C. Optionally, any shape to the protrusions are operable so long as the presence of the shape increases the surface area of the side relative to a smooth cylinder.
[0025] As depicted in FIG. 1B, a stem portion 12 optionally has a first end 14 configured to be complementary to a fastener 28, either conventional or specific to the first end 14. A fastener 28 is fixedly or removably associated with an anchoring optionally formed from refractory brick that forms the inner surface of a construct. As depicted in FIG. 1B, a first end 14 optionally includes a flange 26 that is complementary to the fastener 28 to provide fixed or removable association of the element 28 with the fastener. While FIG. 1B illustrates a flange in a circular or ellipsoidal configuration, it is appreciated that other shapes are similarly operable such as a any pentagonal shape, or an irregular shape.
[0026] Optionally, the flared end block portion 18 has an edge 23 that has a contoured feature 25 to interlock with a complementary feature on another refractory article (not shown), the other refractory article optionally being another element 10, or an element with a shape complementary to the end block portion of the element 10, to better join an inventive element to neighboring elements and thereby form a more robust refractory construct. A
flared end block portion optionally has 3, 4, 5, 6, 7, 8, or more edges. A contour portion on a flared end block portion on a first edge is optionally a complementary feature to a contour portion on a different edge.
[0027] While contour feature 25 is shown as a protrusion, a complementary contour feature as a recess (e.g. groove) is depicted at 25. In addition to the tongue-and-groove contour features depicted in Fig. 1A, it is appreciated that other contour features are operative herein illustratively including dovetails, pin and socket, and other such complementary features conventional to the joinder arts. As such, a contour feature is optionally a tongue (optionally rectilinear or curved), groove (optionally rectilinear or curved), angular so as to form a dovetail joint, pin shape such as a tenon or cylindrical protrusion, or socket shape such as that of a mortise (rectangular or curved).
[0028] A edge optionally includes a plurality of contoured features, complementary features, or both. Contoured features and complementary features are optionally interdispersed, optionally to form an undulating surface for interlocking with another refractory structural element or other surface. The number of contoured features or complementary features is optionally 1, 2, 3, 4, 5, 6, or more.
[0029] FIG. 2 is a perspective view of an alternate embodiment of a structural element shown generally at 40. The element 40 is readily formed from the same materials and by the same techniques as element 10. Additionally, element 40 is also amenable to formation of the stem portion 42 and the flared end block portion 48 as unitary or joined portions consistent with the above description relative to element 10. The face 52 of element 40 is noted to be a regular hexagon in shape and also suitable for space filling to tile a plane or other shaped surface. The end block portion 48 optionally has walls 54 extending approximating parallel to the face 52 in this or other embodiments. The stem 42 is depicted as having a side 62 defined by a spiral protrusion. A first end 44 of the stem portion 42 has a flange 56 and adapted to fixedly or removably engage an anchoring fastener optionally the like of those conventional to the art. In addition to a stem portion 42 having a circular cross section, it is appreciated that this cross section is readily distorted to form an ellipsoidal cross section.
Additionally, it is appreciated that the face 52 in addition to being planar is also formed to be arcuate to form either a concave or convex surface, optionally as illustrated in exemplary form in Figs. 3A-3C.
[0030] Owing to strength properties at elevated temperatures above 1000 Celsius and nonwetting properties relative to molten metals, phosphate bonded cements can be used as a substance from which an element is formed. It is appreciated that other cementitious materials can be used to form a refractory structural elements depending on the eventual exposure requirements of the element.
[0031] In some embodiments, a refractory structural element is made from a phosphate bonded cementitious material that is formed from a phosphate based component and an alkali earth component such as that described in U.S. Patent 7,503,974. The alkali earth ion component has as a majority source a calcium aluminate calcium ion source of dodeca-calcium hepta-aluminate, or tricalcium aluminate. Magnesium oxide that has been fused and crushed to a size of less than 200 microns, alone or in combination with the calcium aluminate calcium ion source is also provided as the alkali earth ion component.
[0032] An exemplary phosphate based component includes phosphoric acid, calcium phosphate, potassium phosphate, magnesium phosphate, sodium phosphate, aluminum phosphate, ammonium phosphate, zinc phosphate, boron phosphate, and combinations thereof.
[0033] An alkali earth ion component optionally includes magnesium oxide, dolomite, zinc oxide, aluminum oxide, calcium oxide, lithium carbonate, barium carbonate, barium sulfate, molybdenum oxide, calcium hydroxide, aluminum hydroxide, tin oxide, nickel oxide, nickel hydroxide, cobalt oxide, cobalt hydroxide, vanadium oxide, magnesium hydroxide, iron oxide, titanium oxide, chromium oxide, chromium hydroxide, dolomite, manganese oxide, zirconium oxide, zirconium hydroxide, NaOH, KOH, sodium carbonate, and potassium carbonate.
[0034] The alkali earth ion component may be predominantly dodeca-calcium hepta-aluminate (C1A7 or mayenite), tricalcium aluminate (C3A), or a combination thereof. The calcium aluminate optionally has a mean particle size of less than 100 microns, optionally 60 microns or less. Typical loadings of C12A7 in a fully formulated cementitious material inclusive of aggregate is from 0.5 to 5 total weight percent with C12A7 typically being present at about one-fourth the weight percent of CA and/or CA2 calcium aluminate used in other cementitious materials. C3A is typically present from 0.3 to 4 total dry weight percent of a cementitious material used to form a refractory structural element.
[0035] Other materials may be included in a cementitious material are illustratively, one or more tackifiers such as: carbohydrates such as saccharides and polysaccharides; starch and derivatives such as pregelatinized starch, dextrin, and corn syrup;
naphthalene sulfonate formaldehyde condensate polymers; melamine sulfonate formaldehyde condensate polymers;
polyhydroxy polycarboxylic compounds such as tartaric acid and mucic acid;
lignosulfonic acid;
and salts of any of the aforementioned acid moieties of tackifiers. A
tackifier is optionally present at 0.01 to 6 total dry weight percent. Plasticizers and strength enhancing agents such as insoluble phosphate are optionally included. Some embodiments include one or more dispersants such as polycarboxylates and conventional surfactants conventional to the field.
Optionally a cementitious material includes one or more deflocculants such as a polyalkylene glycol optionally at 0.05 to 1 weight percent.
[0036] A refractory structural element is optionally cured in a drum heater with internal heating units. A heating temperature in the range of 75 F (23 C) to 150 F
(66 C) is commonly used for this purpose. Heating also promotes the flowability of viscous material. Exemplary types of heaters include band heaters, immersion heaters, and heating cabinets. A band heater is equipped with aluminized steel shell which delivers up to 3,000 Watts of heating power with operating heating temperatures in the range of 60 F (75 C) to 400 F (205 Q. Additionally, an area blanket or quilt is used to insulate a drum heater. Optionally, a temperature shutoff device is installed with a heater for the purpose of preventing overheating of phosphate based component.
[0037] In other embodiments, a refractory structural element is formed from a cementitious material that includes a plurality of aggregate ceramic particles and a binder sintered to the plurality of aggregate ceramic particles, where the binder includes crystalline aluminum orthophosphate distributed in the binder as the result of reaction of aluminum metaphosphate with alumina. The plurality of aggregate ceramic particles optionally includes bauxite particles.
In some embodiments, the plurality of aggregate ceramic particles includes at least one of silicon carbide, fumed silica, or mullite.
[0038] With the refractory aggregate containing alumina, A1203 the aluminum metaphosphate reacts to form crystalline aluminum orthophosphate, A1PO4.
Aluminum orthophosphate is the thermodynamic product upon heating to a temperature greater than about 580 Celsius with a decomposition temperature of about 1650 Celsius. The resultant cementitious material is amenable to incorporation of reinforcing materials such as steel fibers and is operative with aggregate particulate including silicon carbide, mullite, alumina, titania, and combinations thereof. Such a cementitious material is readily formed with a density of greater than 90%, a theoretical density and cold crush strengths in excess of 88 Newtons per square millimeter. Through control of water content and conventional additives, the cast form of refractory structural element has sufficient green strength to be handled and optionally machined prior to firing to provide a refractory structural element with superior strength and alkali resistance, as compared to conventional materials.
[0039] A bindery for a cementitious material optionally includes aluminum metaphosphate that is mixed aggregate ceramic particles and processed under conditions to afford aluminum orthophosphate as a crystalline binder. The binder aluminum orthophosphate optionally has berlinite as a predominant phase. It is appreciated that aluminum metaphosphate as binder precursor is amenable to inclusion in a kit as aluminum metaphosphate is far less hygroscopic as compared to phosphoric acid, more pH neutral (around pH 5) and is commercially available in a variety of particle mesh sizes. The reaction of aluminum metaphosphate with alumina (synonymously termed bauxite herein) to form a crystalline binder phase of aluminum orthophosphate (synonymously referred to herein as berlinite) is detailed with respect to the following equation:
Al(PO3)3 + A1203 -* 3 AIPO4 (1) [0040] Aluminum orthophosphate appears to be a thermodynamically stable phase that is formed upon heating the reagents to a temperature above about 580 Celsius.
Aluminum orthophosphate is noted to have a decomposition temperature of about 1650 Celsius at ambient pressure. It is appreciated that the formation temperature of aluminum orthophosphate varies according to predictable thermodynamic relationships when the reaction proceeds at pressures other than atmospheric pressure. It is appreciated that formation of a refractory composition according to the present invention readily occurs through firing the green form of an article through hot isostatic pressing (HIP). It is appreciated that a mixed metal orthophosphate is readily formed according to the reaction:
Al(PO3)3 + Al2_RMO3 Al Al2_RMPO4 (11) where M is Sb, Bi, B, Cr (III), Er, Gd (III), In (III), Ni (III), Rh (III), Sm (III), Sc (III), Tb (III), Ti (III), W (III), V (III), Yb (III), or Y (III); and x is 0, 1, or 2.
[0041] The amount of aluminum metaphosphate present to form a matrix around refractory ceramic particulate depends on factors including size of the ceramic particulate, desired interparticle separation, morphology, size of primary crystals and oxide state. Optionally, aluminum metaphosphate is present between 2 and 20 total weight percent of the fully formulated cementitious material casting slurry. Alumina is optionally present in excess of molar stoichiometry of alumina metaphosphate. It is appreciated that alumina is present as aggregate ceramic particles or alternatively is added as a minor quantity of the ceramic particles for reaction with the alumina metaphosphate.
[0042] To facilitate mixing of ceramic particle aggregate and alumina metaphosphate as a binder precursor, a quantity of water or organic solvent is added to afford a slurry of a desired viscosity. Such organic solvents illustratively include alcohols, ketones, esters, ethers, amides, amines, glycols, alkanes, and the like. Optionally, such organic solvents are liquids below 200 Celsius, and optionally, are liquids at 20 Celsius. Loadings of water or solvents optionally range from 2-20 total weight percent of a fully formulated cementitious material slurry.
Optionally, additives are included that are consumed during berlinite formation, these additives provided to promote ease of handling. Such additives illustratively include surfactants;
polymerizable organic monomers or oligomers, deflocculants; polymers; and organic acids such as citric, and oxalic. While one of ordinary skill in the art can readily adjust slurry viscosity and green strength through the inclusion of such additives, typically each such additive is present from 0.01-5 total weight percent of a fully formulated refractory composition slurry. It is appreciated that the inclusion of organic monomeric or oligomeric polymerizable materials that upon cure can improve the green strength of the composition prior to firing or reaction according 5 to Equation (I) or (II). The resultant polymer is decomposed and therefore not present in the resultant refractory composition. Exemplary of such organic polymers are acrylic acids, acrylates, polyethylene glycols, and polycarboxylate ethers, which are added as polymeric precursors or slurry soluble preformed polymers.
[0043] Handling properties of a cementitious material slurry and the green strength of a 10 refractory structural element formed therefrom after drying are also optionally modified through inclusion of nonfacile additives. While the amount of such nonfacile additives is controlled by factors including desired green strength, refractory composition, working environment, temperature and corrosivity, desired cold crush strength, and setting time, working time and curing time, typical loadings of such nonfacile additives range from 0.1 to 10 total weight percent of a fully formulated cementitious material slurry. Representative nonfacile additives operative herein include calcium aluminate cement, sodium silicate, fumed silica, alkali metal or alkali earth polyphosphates, and organic salts like citric, oxalic or nitric acids, calcium silicate cement, potassium silicate, lithium silicate. Optionally, a nonfacile additive is present in a quantity such that the aluminum orthophosphate forms a continuous matrix phase.
[0044] Ceramic particle aggregate embedded within an aluminum orthophosphate binder according is limited only by the desired properties of the resultant cementitious material and compatibility with aluminum orthophosphate binder. Operative ceramic particle aggregates illustratively include bauxite, tabular alumina, mullite, silicon carbide, fused silica, rutile, and andalusite, sillimanite, magnesite, forsterite, kyanite, Mg spinell, and chromium oxide. Typical loadings of aggregate ceramic particles range from 50-95 weight percent of a fully formulated refractory composition slurry. Typical aggregate particle sizes range from 0.1 to 1000 microns.
It is appreciated that the aggregate particles can be in a variety of forms including spherical, polyhedral, irregular, and combinations thereof.
[0045] A cementitious material optionally includes strengthening fibers such as steel fibers as detailed in U.S. Patent Nos. 4,366,255. Additional, illustrative reinforcing fibers include nickel and chromium fibers and synthetic fibers such as polypropylene (PP), polyethylene (PE), and polyethylene terephthalate (PET). Optionally steel fibers are used containing aluminum within the steel alloy to form a protective layer of alumina on the steel fiber at elevated temperature. Optionally, the steel fiber has from 0.05 to 8 atomic percent aluminum content.
Other strengthening fiber fillers operative herein include carbon fibers with the recognition that firing occurs in a reducing atmosphere. Typical loadings of fibers are from 0 to 50 total weight percent of a refractory composition used to make a refractory structural element.
[0046] A cementitious material used to form a refractory structural element optionally includes one or more aggregate components. An aggregate component is typically present from 50 to 95 total dry weight percent. Typical aggregates illustratively include:
flint clay, mulcoa, basalt, olivine, diatomite, vermiculite, perlite, molochite, gibbsite, kyanite, mullite, chromite, tabular alumina, silicon oxide, silica, calcined bauxite, chrome oxide, zirconia, phosphate rock, and mixtures thereof.
[0047] A refractory structural element is optionally cast from a variety of cementitious materials other than those disclosed herein such as a variety commercially available materials from Stellar Materials, Inc., Boca Raton., FL. Illustrative examples of materials and methods of their production can be found in U.S. Patent Nos. 6,447,596; and 5,888,292.
[0048] The element, depending on particulars of the shape, is readily cast from two part or multiple part molds through techniques conventional to the art.
[0049] In operation, a refractive structural element forms a space created by projection of the flared end portion backwards towards the first end created by the smaller dimensions of the stem portion and the space surrounding the sides. This space is optionally filled with a fill material illustratively including ceramic fibers, perlite, vermiculite, and combinations thereof alone or retained within a bonded matrix. Space filling with one or more fill materials allows a user to adjust the radiative heat dissipation or insulative characteristics of a construct associated with one or more refractory structural elements to the user's needs.
[0050] One of skill in the art will appreciate that a refractory structural element affords more efficient use of cementitious material from which the element is formed and also through the use of a comparatively small dimension stem relative to the element face, and the ability to form cavities within the element so that adjustment of the operational properties of the element are readily controlled, as compared to conventional bricks.
[0051] The shape of a refractive structural element is optionally used to line the surface of a construct with one or more of many different surface geometries. Refractory structural elements are capable of forming planar or curved surface areas while retaining a desired tight association between the faces of multiple elements.
[0052] Various modifications of the present invention, in addition to those shown and described herein, will be apparent to those skilled in the art of the above description. Such modifications are also intended to fall within the scope of the appended claims.
[0053] It is appreciated that all materials are obtainable from sources known in the art unless otherwise specified.
[0054] Patents and publications mentioned in the specification are indicative of the levels of those skilled in the art to which the invention pertains. These patents and publications are incorporated herein by reference to the same extent as if each individual patent or publication was specifically and individually incorporated herein by reference.
[0055] The foregoing description is illustrative of particular embodiments of the invention, but is not meant to be a limitation upon the practice thereof. The following claims, including all equivalents thereof, are intended to define the scope of the invention.
Claims (20)
1. A refractory structural element comprising:CLAIMS
a cementitious material in a shape having a stem portion, the stem portion having a first end and a second end, the second end associated with a flared end block portion, said flared end block portion including a face, said face having a cross sectional dimension that is greater than a cross sectional dimension of said stem portion.
a cementitious material in a shape having a stem portion, the stem portion having a first end and a second end, the second end associated with a flared end block portion, said flared end block portion including a face, said face having a cross sectional dimension that is greater than a cross sectional dimension of said stem portion.
2. The element of claim 1 wherein the flared end block portion is continuous with the stem portion.
3. The element of claim 1 wherein the stem portion has a side decorated with protrusions.
4. The element of claim 3 where the protrusions are undulations, spirals, ridges, irregular scores, or a combination thereof.
5. The element of claims 1 or 3 further comprising fill material surrounding the stem portion.
6. The element of claim 5 wherein said fill material is ceramic fiber, perlite, vermiculite, or combinations thereof.
7. The element of claims 1 or 3 wherein the first end of the stem portion includes a flange operable to engage a fastener for securement of the element to a substrate.
8. The element of claims 1 or 3 wherein said face is space filling.
9. The element of claims 1 or 3 wherein the face is planar or arcuate.
10. The element of claim 8 wherein the face is planar, convex arcuate, or concave arcuate.
11. The element of claims 1 or 3 wherein said flared end block portion has a first edge contoured with a contour feature, said contour feature shaped to interlock with a complementary feature of a complementary refractory structural element.
12. The element of claim 11 wherein said contour feature is shaped as a tongue, groove, pin, or socket.
13. The element of claim 11 wherein said element has a second edge with a complementary contour feature.
14. The element of claims 1 or 3 wherein said stem portion has a circular or ellipsoidal cross sectional shape.
15. The element of claims 1 or 3 wherein said stem portion has a polygonal cross sectional shape.
16. The element of claims 1 or 3 wherein said flared end block portion has a plurality of sloped walls, each wall extending from an edge of said flared end portion to the second end of said stem.
17. The element of claims 1 or 3 wherein said face has a central point and the thickness of the flared end block portion at said central point is greater than the thickness at an edge of said flared end block portion.
18. The element of claims 1 or 3 wherein said cementitious material is a phosphate-bonded cement.
19. The element of claims 1 or 3 formed of a cementitious material substantially as described herein.
20. A refractory structural element substantially as described herein.
Applications Claiming Priority (3)
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| US36248910P | 2010-07-08 | 2010-07-08 | |
| US61/362,489 | 2010-07-08 | ||
| PCT/US2011/043331 WO2012006507A2 (en) | 2010-07-08 | 2011-07-08 | Refractory structural element |
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| CA2804505A1 true CA2804505A1 (en) | 2012-01-12 |
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| CA2794146C (en) * | 2010-03-23 | 2020-07-14 | Stellar Materials, Incorporated | Refractory composition and process for forming article therefrom |
| KR101429675B1 (en) * | 2012-08-08 | 2014-08-13 | 주식회사 리배산업 | Insualtion block for ceiling of heating furnace and ceiling assembly using the same |
| WO2014092753A1 (en) * | 2012-12-14 | 2014-06-19 | Stellar Materials Incorporated | Refractory lining article and system |
| BR112016015610B1 (en) * | 2014-01-10 | 2021-02-09 | Jfe Steel Corporation | method for suppressing back face oxidation of carbon containing refractory, coating structure and carbon containing refractory |
| JP6775462B2 (en) * | 2017-04-10 | 2020-10-28 | 日本製鉄株式会社 | Anchor brick |
| KR102204086B1 (en) * | 2019-12-23 | 2021-01-18 | 에스원건설 주식회사 | Fire-resistance coating materials composition using waste recycling materials, comprising fire-resistance materials and multi-foam materials and Panel for fire-resistance coating using the same |
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| US1553004A (en) * | 1924-10-01 | 1925-09-08 | Int Comb Eng Corp | Furnace-wall structure |
| GB300980A (en) * | 1927-11-22 | 1929-07-18 | Alfred Numa De Saint Edme Born | Suspended ceilings chiefly for covering furnaces, fireboxes and the like |
| US3953009A (en) * | 1975-06-19 | 1976-04-27 | General Motors Corporation | Metallurgical vessel |
| US4473983A (en) * | 1981-03-12 | 1984-10-02 | United States Steel Corporation | Anchoring refractory materials to a refractory lining |
| DE3418195A1 (en) * | 1984-05-16 | 1985-11-21 | Krupp Polysius Ag, 4720 Beckum | CEILING AND WALL CONSTRUCTION |
| GB8700700D0 (en) * | 1987-01-13 | 1987-02-18 | Clinotherm Ltd | Refractories |
| US5601184A (en) * | 1995-09-29 | 1997-02-11 | Process Technologies, Inc. | Method and apparatus for use in photochemically oxidizing gaseous volatile or semi-volatile organic compounds |
| EP0895028B1 (en) * | 1997-07-28 | 2002-03-06 | Alstom | Ceramic lining |
| US6227127B1 (en) * | 1998-04-28 | 2001-05-08 | Kyocera Corporation | Furnace material, heat resisting protection tube and protective member using the same sintered material |
| DE59810637D1 (en) * | 1998-11-30 | 2004-02-26 | Alstom Switzerland Ltd | Ceramic lining for a combustion chamber |
| US6174388B1 (en) * | 1999-03-15 | 2001-01-16 | Lockheed Martin Energy Research Corp. | Rapid infrared heating of a surface |
| US6427610B1 (en) * | 2000-10-11 | 2002-08-06 | Merkle Engineers, Inc. | High temperature industrial furnace roof structure |
| US7503974B2 (en) * | 2006-03-22 | 2009-03-17 | Stellar Materials, Inc. | Cementitous material |
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2011
- 2011-07-08 CA CA 2804505 patent/CA2804505A1/en not_active Abandoned
- 2011-07-08 AU AU2011274532A patent/AU2011274532A1/en not_active Abandoned
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