US20020041928A1 - Method for coating substrate with metal oxide coating - Google Patents
Method for coating substrate with metal oxide coating Download PDFInfo
- Publication number
- US20020041928A1 US20020041928A1 US08/824,418 US82441897A US2002041928A1 US 20020041928 A1 US20020041928 A1 US 20020041928A1 US 82441897 A US82441897 A US 82441897A US 2002041928 A1 US2002041928 A1 US 2002041928A1
- Authority
- US
- United States
- Prior art keywords
- metal
- carboxylate composition
- liquid metal
- metal carboxylate
- cerium
- 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
- 238000000576 coating method Methods 0.000 title claims abstract description 82
- 238000000034 method Methods 0.000 title claims abstract description 81
- 239000011248 coating agent Substances 0.000 title claims abstract description 68
- 239000000758 substrate Substances 0.000 title claims abstract description 50
- 229910044991 metal oxide Inorganic materials 0.000 title claims abstract description 43
- 150000004706 metal oxides Chemical class 0.000 title claims abstract description 43
- 229910052751 metal Inorganic materials 0.000 claims abstract description 100
- 239000002184 metal Substances 0.000 claims abstract description 100
- 239000000203 mixture Substances 0.000 claims abstract description 97
- 150000007942 carboxylates Chemical class 0.000 claims abstract description 90
- 229910001338 liquidmetal Inorganic materials 0.000 claims abstract description 56
- 150000001735 carboxylic acids Chemical class 0.000 claims abstract description 31
- 239000000463 material Substances 0.000 claims abstract description 20
- 238000006243 chemical reaction Methods 0.000 claims abstract description 6
- 238000009834 vaporization Methods 0.000 claims abstract description 4
- 230000008016 vaporization Effects 0.000 claims abstract description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 23
- 239000002253 acid Substances 0.000 claims description 23
- 150000002739 metals Chemical class 0.000 claims description 23
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 20
- 229910052684 Cerium Inorganic materials 0.000 claims description 18
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 claims description 18
- 238000010438 heat treatment Methods 0.000 claims description 18
- 229910052804 chromium Inorganic materials 0.000 claims description 17
- 239000011651 chromium Substances 0.000 claims description 17
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 16
- 229910017052 cobalt Inorganic materials 0.000 claims description 15
- 239000010941 cobalt Substances 0.000 claims description 15
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 15
- 229910052759 nickel Inorganic materials 0.000 claims description 12
- 229910052742 iron Inorganic materials 0.000 claims description 10
- 150000007513 acids Chemical class 0.000 claims description 9
- 125000003178 carboxy group Chemical group [H]OC(*)=O 0.000 claims description 7
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 5
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 claims description 5
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 5
- 229910052802 copper Inorganic materials 0.000 claims description 5
- 239000010949 copper Substances 0.000 claims description 5
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 claims description 5
- 229910052737 gold Inorganic materials 0.000 claims description 5
- 239000010931 gold Substances 0.000 claims description 5
- 150000003839 salts Chemical class 0.000 claims description 5
- 229910052709 silver Inorganic materials 0.000 claims description 5
- 239000004332 silver Substances 0.000 claims description 5
- 229910052716 thallium Inorganic materials 0.000 claims description 5
- BKVIYDNLLOSFOA-UHFFFAOYSA-N thallium Chemical compound [Tl] BKVIYDNLLOSFOA-UHFFFAOYSA-N 0.000 claims description 5
- 229910052727 yttrium Inorganic materials 0.000 claims description 5
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims description 5
- 229910052726 zirconium Inorganic materials 0.000 claims description 5
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 claims description 4
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims description 4
- 229910052692 Dysprosium Inorganic materials 0.000 claims description 4
- 229910052691 Erbium Inorganic materials 0.000 claims description 4
- 229910052693 Europium Inorganic materials 0.000 claims description 4
- 229910052688 Gadolinium Inorganic materials 0.000 claims description 4
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 claims description 4
- 229910052689 Holmium Inorganic materials 0.000 claims description 4
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 claims description 4
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 4
- 229910052765 Lutetium Inorganic materials 0.000 claims description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 4
- 229910052779 Neodymium Inorganic materials 0.000 claims description 4
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 claims description 4
- 229910052777 Praseodymium Inorganic materials 0.000 claims description 4
- 229910052772 Samarium Inorganic materials 0.000 claims description 4
- 229910052771 Terbium Inorganic materials 0.000 claims description 4
- 229910052776 Thorium Inorganic materials 0.000 claims description 4
- 229910052775 Thulium Inorganic materials 0.000 claims description 4
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 4
- 229910052770 Uranium Inorganic materials 0.000 claims description 4
- 229910052769 Ytterbium Inorganic materials 0.000 claims description 4
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 4
- 229910052788 barium Inorganic materials 0.000 claims description 4
- DSAJWYNOEDNPEQ-UHFFFAOYSA-N barium atom Chemical compound [Ba] DSAJWYNOEDNPEQ-UHFFFAOYSA-N 0.000 claims description 4
- 229910052790 beryllium Inorganic materials 0.000 claims description 4
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims description 4
- 229910052797 bismuth Inorganic materials 0.000 claims description 4
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 claims description 4
- 229910052793 cadmium Inorganic materials 0.000 claims description 4
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 claims description 4
- 229910052792 caesium Inorganic materials 0.000 claims description 4
- TVFDJXOCXUVLDH-UHFFFAOYSA-N caesium atom Chemical compound [Cs] TVFDJXOCXUVLDH-UHFFFAOYSA-N 0.000 claims description 4
- 229910052791 calcium Inorganic materials 0.000 claims description 4
- 239000011575 calcium Substances 0.000 claims description 4
- KBQHZAAAGSGFKK-UHFFFAOYSA-N dysprosium atom Chemical compound [Dy] KBQHZAAAGSGFKK-UHFFFAOYSA-N 0.000 claims description 4
- UYAHIZSMUZPPFV-UHFFFAOYSA-N erbium Chemical compound [Er] UYAHIZSMUZPPFV-UHFFFAOYSA-N 0.000 claims description 4
- OGPBJKLSAFTDLK-UHFFFAOYSA-N europium atom Chemical compound [Eu] OGPBJKLSAFTDLK-UHFFFAOYSA-N 0.000 claims description 4
- UIWYJDYFSGRHKR-UHFFFAOYSA-N gadolinium atom Chemical compound [Gd] UIWYJDYFSGRHKR-UHFFFAOYSA-N 0.000 claims description 4
- 229910052733 gallium Inorganic materials 0.000 claims description 4
- 229910052735 hafnium Inorganic materials 0.000 claims description 4
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 claims description 4
- KJZYNXUDTRRSPN-UHFFFAOYSA-N holmium atom Chemical compound [Ho] KJZYNXUDTRRSPN-UHFFFAOYSA-N 0.000 claims description 4
- 229910052746 lanthanum Inorganic materials 0.000 claims description 4
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 claims description 4
- 229910052744 lithium Inorganic materials 0.000 claims description 4
- OHSVLFRHMCKCQY-UHFFFAOYSA-N lutetium atom Chemical compound [Lu] OHSVLFRHMCKCQY-UHFFFAOYSA-N 0.000 claims description 4
- 229910052749 magnesium Inorganic materials 0.000 claims description 4
- 239000011777 magnesium Substances 0.000 claims description 4
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 4
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 claims description 4
- 229910052700 potassium Inorganic materials 0.000 claims description 4
- 239000011591 potassium Substances 0.000 claims description 4
- PUDIUYLPXJFUGB-UHFFFAOYSA-N praseodymium atom Chemical compound [Pr] PUDIUYLPXJFUGB-UHFFFAOYSA-N 0.000 claims description 4
- 229910052701 rubidium Inorganic materials 0.000 claims description 4
- IGLNJRXAVVLDKE-UHFFFAOYSA-N rubidium atom Chemical compound [Rb] IGLNJRXAVVLDKE-UHFFFAOYSA-N 0.000 claims description 4
- KZUNJOHGWZRPMI-UHFFFAOYSA-N samarium atom Chemical compound [Sm] KZUNJOHGWZRPMI-UHFFFAOYSA-N 0.000 claims description 4
- 229910052706 scandium Inorganic materials 0.000 claims description 4
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 claims description 4
- 229910052708 sodium Inorganic materials 0.000 claims description 4
- 239000011734 sodium Substances 0.000 claims description 4
- 229910052712 strontium Inorganic materials 0.000 claims description 4
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 claims description 4
- 229910052715 tantalum Inorganic materials 0.000 claims description 4
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 4
- GZCRRIHWUXGPOV-UHFFFAOYSA-N terbium atom Chemical compound [Tb] GZCRRIHWUXGPOV-UHFFFAOYSA-N 0.000 claims description 4
- 229910052718 tin Inorganic materials 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- 239000010936 titanium Substances 0.000 claims description 4
- NAWDYIZEMPQZHO-UHFFFAOYSA-N ytterbium Chemical compound [Yb] NAWDYIZEMPQZHO-UHFFFAOYSA-N 0.000 claims description 4
- 229910052725 zinc Inorganic materials 0.000 claims description 4
- 239000011701 zinc Substances 0.000 claims description 4
- 238000009835 boiling Methods 0.000 claims description 3
- 239000000470 constituent Substances 0.000 claims description 2
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 claims 3
- 230000008569 process Effects 0.000 description 26
- 239000000654 additive Substances 0.000 description 17
- 230000000087 stabilizing effect Effects 0.000 description 16
- 239000012212 insulator Substances 0.000 description 14
- 238000004519 manufacturing process Methods 0.000 description 13
- 239000000919 ceramic Substances 0.000 description 11
- 239000007788 liquid Substances 0.000 description 10
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 10
- 230000015572 biosynthetic process Effects 0.000 description 9
- 239000002904 solvent Substances 0.000 description 8
- 238000002485 combustion reaction Methods 0.000 description 7
- 238000011109 contamination Methods 0.000 description 7
- 238000000354 decomposition reaction Methods 0.000 description 7
- 239000000243 solution Substances 0.000 description 7
- -1 2,2-dimethylbutyl Chemical group 0.000 description 5
- 230000000996 additive effect Effects 0.000 description 5
- 239000000446 fuel Substances 0.000 description 5
- 229930195733 hydrocarbon Natural products 0.000 description 5
- 150000002430 hydrocarbons Chemical class 0.000 description 5
- 229910052697 platinum Inorganic materials 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 4
- 229910052784 alkaline earth metal Inorganic materials 0.000 description 4
- 238000001704 evaporation Methods 0.000 description 4
- 230000008020 evaporation Effects 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 229910000464 lead oxide Inorganic materials 0.000 description 4
- 125000002496 methyl group Chemical group [H]C([H])([H])* 0.000 description 4
- UHOVQNZJYSORNB-UHFFFAOYSA-N Benzene Chemical compound C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 description 3
- 239000004215 Carbon black (E152) Substances 0.000 description 3
- YMWUJEATGCHHMB-UHFFFAOYSA-N Dichloromethane Chemical compound ClCCl YMWUJEATGCHHMB-UHFFFAOYSA-N 0.000 description 3
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 3
- OKKJLVBELUTLKV-UHFFFAOYSA-N Methanol Chemical compound OC OKKJLVBELUTLKV-UHFFFAOYSA-N 0.000 description 3
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 3
- 239000003570 air Substances 0.000 description 3
- 125000003342 alkenyl group Chemical group 0.000 description 3
- 125000000217 alkyl group Chemical group 0.000 description 3
- 125000000304 alkynyl group Chemical group 0.000 description 3
- 125000003118 aryl group Chemical group 0.000 description 3
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- 238000005229 chemical vapour deposition Methods 0.000 description 3
- 239000000571 coke Substances 0.000 description 3
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- YEXPOXQUZXUXJW-UHFFFAOYSA-N oxolead Chemical compound [Pb]=O YEXPOXQUZXUXJW-UHFFFAOYSA-N 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 238000004544 sputter deposition Methods 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- HEDRZPFGACZZDS-UHFFFAOYSA-N Chloroform Chemical compound ClC(Cl)Cl HEDRZPFGACZZDS-UHFFFAOYSA-N 0.000 description 2
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 2
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 2
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 2
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- FAPWRFPIFSIZLT-UHFFFAOYSA-M Sodium chloride Chemical compound [Na+].[Cl-] FAPWRFPIFSIZLT-UHFFFAOYSA-M 0.000 description 2
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- 239000000382 optic material Substances 0.000 description 2
- 125000001997 phenyl group Chemical group [H]C1=C([H])C([H])=C(*)C([H])=C1[H] 0.000 description 2
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- 229910052685 Curium Inorganic materials 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
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- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 150000002762 monocarboxylic acid derivatives Chemical class 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 125000001971 neopentyl group Chemical group [H]C([*])([H])C(C([H])([H])[H])(C([H])([H])[H])C([H])([H])[H] 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 239000010955 niobium Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 125000001400 nonyl group Chemical group [H]C([*])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])[H] 0.000 description 1
- 125000002347 octyl group Chemical group [H]C([*])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])[H] 0.000 description 1
- 239000003960 organic solvent Substances 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052763 palladium Inorganic materials 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 125000001147 pentyl group Chemical group C(CCCC)* 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- VQMWBBYLQSCNPO-UHFFFAOYSA-N promethium atom Chemical compound [Pm] VQMWBBYLQSCNPO-UHFFFAOYSA-N 0.000 description 1
- BDERNNFJNOPAEC-UHFFFAOYSA-N propan-1-ol Chemical compound CCCO BDERNNFJNOPAEC-UHFFFAOYSA-N 0.000 description 1
- 125000001436 propyl group Chemical group [H]C([*])([H])C([H])([H])C([H])([H])[H] 0.000 description 1
- 239000011253 protective coating Substances 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 238000004062 sedimentation Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- HPALAKNZSZLMCH-UHFFFAOYSA-M sodium;chloride;hydrate Chemical compound O.[Na+].[Cl-] HPALAKNZSZLMCH-UHFFFAOYSA-M 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 125000001424 substituent group Chemical group 0.000 description 1
- 125000000999 tert-butyl group Chemical group [H]C([H])([H])C(*)(C([H])([H])[H])C([H])([H])[H] 0.000 description 1
- 231100000331 toxic Toxicity 0.000 description 1
- 230000002588 toxic effect Effects 0.000 description 1
- DNYWZCXLKNTFFI-UHFFFAOYSA-N uranium Chemical compound [U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U] DNYWZCXLKNTFFI-UHFFFAOYSA-N 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/02—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition
- C23C18/12—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition characterised by the deposition of inorganic material other than metallic material
- C23C18/1204—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition characterised by the deposition of inorganic material other than metallic material inorganic material, e.g. non-oxide and non-metallic such as sulfides, nitrides based compounds
- C23C18/1208—Oxides, e.g. ceramics
- C23C18/1216—Metal oxides
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/02—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition
- C23C18/12—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by thermal decomposition characterised by the deposition of inorganic material other than metallic material
- C23C18/125—Process of deposition of the inorganic material
- C23C18/1291—Process of deposition of the inorganic material by heating of the substrate
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C26/00—Coating not provided for in groups C23C2/00 - C23C24/00
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12007—Component of composite having metal continuous phase interengaged with nonmetal continuous phase
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
- Y10T428/264—Up to 3 mils
- Y10T428/265—1 mil or less
Definitions
- the present invention relates generally to the field of surface coatings.
- the invention is a method for coating a wide variety of different substrates with a wide variety of metal oxide coatings.
- One known method for the formation of metal oxide coatings on substrates is via the electrochemical sedimentation of metal oxides from solution.
- this method can only used to coat electrically conductive substrates, a significant limitation where the substrate is non-conductive.
- Another method of forming metal oxide coatings on substrates is a sputtering process.
- a metal oxide powder is vaporized, using, for example, laser, plasma, flame or detonation methods.
- the vapors are carried in a gas carrier until they reach the surface to be coated. This surface is generally relatively cool, so that the vaporized metal oxide powder condenses on the surface.
- Detonation spraying is another possible method that could be used to produce coatings on various substrates.
- this method requires a large amount of catalyst material and specialized manufacturing equipment.
- CVD chemical vapor deposition
- toxic components include ⁇ -diketones and metal-carbonyl complexes.
- This process suffers from several drawbacks. First, it requires the use of a special furnace that contains a nonoxidizing atmosphere. In addition, the short heat treatment time produces a coating that has internal strains, leading to the lack of a well defined crystalline structure and creating a highly absorptive coating that can absorb water, gases or hydrocarbons. This absorption can make the coating conductive. Furthermore, the use of a single metal in the coating is undesirable because a number of metals, for example zirconium, do not form resistant coatings without additional additives. This would create weak coatings. Finally, this process only uses trivalent and tetravalent metals. As a result, desirable materials, such as nickel, copper and gold, can not be used therein.
- the above-referenced conventional coating processes suffer from a variety of disadvantages that would make them undesirable for the commercial-scale production of most substrates.
- the coatings produced by these methods are relatively thick, which can reduce their adhesion to the substrate and cause scaling or flaking off of the coating.
- the above methods require additional procedures to remove the coating from areas of the surface where no coating is desired.
- all of the above methods have high material consumption, increasing their cost.
- the present method overcomes the drawbacks described above in known techniques for coating substrates with metal oxides.
- the method generally comprises the steps of (a) applying a liquid metal carboxylate composition, or a solution thereof, to a substrate material, and (b) exposing the substrate material to an environment that will cause vaporization or dissipation of any excess carboxylic acids in the liquid metal carboxylate composition and conversion of the metal carboxylates to metal oxides.
- step (b) above is carried out by heating the substrate in a furnace, in normal air, at a temperature of at least about 300° C., and preferably of at least about 400° C., for at least about two minutes.
- the step can be accomplished by merely exposing the substrate to normal ambient conditions for a sufficiently long time to allow the metal oxide coating to form on the substrate.
- the invention also includes devices or structures coated with metal oxide coatings in accordance with the method described above.
- Suitable substrates for this process include metals, including steel alloys and aluminum, silica based materials (including optic and fiber optic materials), and various ceramic materials, that need to be protected from a range of environmental conditions, including atmospheres rich in corrosive fluids, combusted or partially combusted hydrocarbons (such as the combustion chambers of internal combustion engines, jet engines, and turbines, and in emission or pollution control systems attached thereto), saline conditions (such as in saline or brine conditioners), lead oxides, abrasive particles or degradative contaminants.
- sensors used in catalytic converters part of the required emission control systems for automobiles manufactured or sold in the United States, are commonly coated with platinum.
- the present coating could be used to replace the platinum coating, thereby offering a low-cost alternative.
- materials that could be coated in accordance with the present invention There are numerous other examples of materials that could be coated in accordance with the present invention.
- one embodiment of the present invention is to deposit a metal oxide coating onto various heating elements in heating or air conditioning elements, including condenser or heat exchanger tubes.
- Another embodiment of the present invention is to deposit a metal oxide coating onto a casting mold or press mold.
- press molds for rubber goods such as tires, gaskets, cups, and seals
- hydrocarbon and low alloy steels are made of hydrocarbon and low alloy steels.
- the lifetime of these machines can be significantly shortened by corrosion.
- a thin (up to 5 mcm) metal oxide coating can be applied onto the working surfaces of the press, in accordance with the present method, by heat decomposition of a liquid metal carboxylate composition at, for example, 370-390° C.
- Another embodiment of the present invention is to deposit a metal oxide coating onto a metal tool. For instance, formation of a metal oxide coating on the surface of hard-faced (carbide tip) cutting tools will increase the lifetime of cutting tips.
- Another embodiment of the present invention is to deposit a metal oxide coating onto salt water marine propellers.
- Another embodiment of the present invention is to deposit a metal oxide coating onto turbine blades.
- Another embodiment of the present invention is to deposit a metal oxide coating onto metallic moving parts in machinery, such as aluminum parts.
- Another embodiment of the present invention is to deposit a metal oxide coating onto steel castings used in air conditioners.
- Another embodiment of the present invention is to deposit a metal oxide coating onto silicon or silica based materials, including optic or fiber optic materials.
- Another embodiment of the present invention is to deposit a metal oxide coating onto various metal parts exposed to abrasion or continuous high temperatures or high impact conditions (such as tools, dies, stamping materials).
- Another embodiment of the present invention is to deposit a metal oxide coating onto boat hulls, for instance, to prevent corrosion and to prevent barnacle formation.
- Another embodiment of the present invention is to deposit a metal oxide coating onto molds used for molding nonferrous metals.
- a basic mold is first made with a size that is larger than the product to be made, by approximately 50-100 microns.
- the surface of the mold is then powder coated by a protective coating in such a way that the size of the mold corresponds to the size of the desired article.
- a primary drawback of this method is the necessity for double treatment of the metal mold, and the restricted resistance of the metal mold.
- the present invention can be used to form a protective film in the mold when the mold is manufactured, corresponding to the size of the corresponding articles.
- Another embodiment of the present invention is to deposit an oxide coating of yttrium or cerium on the surface of nichrome heating elements, such as that used in many irons, stoves and resistance furnaces. This will increase the maximum working temperature of a typical nichrome element from approximately 1100° C. to approximately 1220-1250° C. or higher, while increasing the life of the heating element.
- alkyl refers to a saturated straight, branched, or cyclic hydrocarbon, or a combination thereof, typically of C 1 to C 24 , and specifically includes methyl, ethyl, propyl, isopropyl, butyl, isobutyl, t-butyl, pentyl, cyclopentyl, isopentyl, neopentyl, hexyl, isohexyl, cyclohexyl, 3-methylpentyl, 2,2-dimethylbutyl, 2,3-dimethylbutyl, heptyl, octyl, nonyl, and decyl.
- alkenyl and alkynyl refers to a C 2 to C 24 straight or branched hydrocarbon with at least one double or triple bond, respectively.
- aryl or aromatic refers to phenyl, naphthyl, or substituted phenyl or naphthyl, wherein the substituent is alkyl, alkenyl, alkynyl or alkoxy.
- the liquid metal carboxylate composition is a solution of the carboxylic acid salts of one or more metals (“metal carboxylate”).
- Metal carboxylates are well known and can be produced by a variety of methods known to one skilled in the art. Non-limiting examples of methods for producing the metal carboxylate are shown in the following reaction schemes:
- the liquid metal carboxylate composition can contain a single metal, to form a single metal carboxylate, or a mixture of metals, to form a corresponding mixture of metal carboxylates.
- the liquid metal carboxylate composition contains a mixture of metals, as these compositions form mixed oxides having superior properties.
- the solvent used in the liquid metal carboxylate composition is an excess of a liquid carboxylic acid which was used to form the metal carboxylate.
- the solvent can be the solution of a carboxylic acid in another solvent, including, but not limited to, organic solvents such as acetone, ethanol, methanol, propanol, benzene, toluene, chloroform and dichloromethane.
- Carboxylic acids that are suitable for use to form the liquid metal carboxylate composition are those which: (1) can form a metal carboxylate, where the metal carboxylate is soluble in excess acid or another solvent; and (2) can be vaporized at a temperature which overlaps the oxide conversion temperature.
- the carboxylic acid should have a formula R-COOH, where R is alkyl, alkenyl, alkynyl or aryl.
- the liquid monocarboxylic acid comprises one or more carboxylic acids having the formula I below:
- R is selected from H and C 1 to C 24 alkyl groups
- R′ and R′′ are each independently selected from C 1 to C 24 alkyl groups.
- these alpha branched carboxylic acids have a molecular weight in the range 130 to 420. More preferably, the carboxylic acids have a molecular weight in the range 220 to 270.
- Either a single carboxylic acid or a mixture of carboxylic acids can be used to form the liquid metal carboxylate.
- a mixture of carboxylic acids is used.
- the use of a mixture provides several advantages. First, the mixture has a broader evaporation temperature range, making it more likely that the evaporation temperature of the acid mixture will overlap the metal carboxylate decomposition temperature, allowing the formation of an optimum oxide coating. Second, the production of purified individual acids is expensive. Thus, the use of an individual acid could unnecessarily raise the cost of this method.
- the carboxylic acid may be a mixture of tertiary and quaternary carboxylic acids of formula I.
- One preferred carboxylic acid mixture is a mixture manufactured by the Sterlitamakski Production Complex “KAUSTIK,” Bashkortostan, Sterlitamak City, Russia and other petrochemical enterprises, such as the Dneprodzerzhinski Complex in Dneprodzerzhinsk city, Ukraine. These materials are sold under the name “VIK acids.”
- the VIK acids are a material consisting of a mixture of carboxylic acids having the general formula CH 3 (CH 2 ) n C(CH 3 )(C 2 H 5 )—COOH, wherein n is 7 to 10.
- the average molecular weight of the acids contained in this mixture is from about 220 to 270.
- This mixture also contains the acid CH 3 CH 2 CH 2 CH(CH 3 )—COOH as its lowest boiling acid constituent.
- the VIK acids should have the properties set forth in Table 1.
- TABLE 1 CHARACTERISTIC NORM appearance transparent homogeneous liquid color less or low-yellow. Color, maximum 7.0 Density at 20 C. 0.90-0.93 g/cm 3 Acid Fraction composition: content of C 3 acids-maximum 1.0 b) content of C 5 -C 11 , acids and 90.0% higher-maximum Acid number, mg 300-350 KOH/gr Ether number, mg 20.0 KOH/gr-maximum Water content-maximum 0.5% Refraction coefficient, 1.42-1.43 ⁇ 20 C. 189779.1
- the critical properties of the VIK acid are the acid number, which should not be above 380 mg/g KOH and the appearance; the liquid should be clear.
- the liquid alpha-branched carboxylic acids can be used as received from the manufacturer and do not require any additional purification, such as the removal of alcohol, ethers or other organic impurities.
- Metals that are particularly suitable for use to form the liquid metal carboxylates include those selected from the group consisting of: Lithium, Beryllium, Sodium, Magnesium, Potassium, Calcium, Scandium, Titanium, Chromium, Manganese, Iron, Nickel, Cobalt, Copper, Zinc, Gallium, Rubidium, Strontium, Yttrium, Zirconium, Silver, Cadmium, Tin, Cesium, Cerium, Barium, Platinum, Lanthanum, Hafnium, Vanadium, Niobium, Molybdenum, Indium, Promethium, Plutonium, Curium, Californium, Tantalum, Gold, Thallium, Lead, Bismuth, Cerium, Praseodymium, Neodymium, Samarium, Europium, Gadolinium, Terbium, Dysprosium, Holmium, Erbium, Thulium, Ytterbium, Lutetium, Thorium and Plutonium and Uranium.
- any of the above metals or combinations thereof can be used to form coatings according to the present process.
- those skilled in the art can select appropriate metal mixtures to form the desired metal or metal oxide coating.
- the metals can be selected taking into consideration the nature of the substrate to be coated, the purpose of the substrate, and the environment to which the substrate is exposed.
- the above-named inventor is filing contemporaneously herewith an application directed to a method for coating the ceramic insulators of sparkplugs, just one of the many applications of the present invention.
- the oxide coating should not be electrically conductive.
- the partial reduction of iron, nickel and cobalt oxides is possible due to the interaction of these oxides with partially combusted fuel products.
- the amounts of these materials should be limited to that necessary to provide a stable coating.
- thermodynamically stable oxides such as chromium and cerium oxides should be the major components of the coating.
- chromium oxide should not be the sole component of the coating for a sparkplug, as it may form agglomerates or a crystalline structure with reduced resistance.
- chromium it is preferably used in combination with other oxides, such as cerium.
- divalent nickel with trivalent metals such as cobalt, iron or chromium, may cause the formation of electrically conductive spinels.
- the electrically conductive spinels are, of course, undesirable for use on sparkplug insulators, although they may have other applications. Accordingly, if sparkplugs are being coated, the use of nickel with trivalent metals should be carefully monitored.
- the liquid metal carboxylate composition preferably contains a mixture of metal carboxylates.
- This mixture preferably contains one metal carboxylate as its major component and one or more additional metal carboxylates as stabilizing additives.
- the stabilizing additives are preferably trivalent metal carboxylates.
- Preferred trivalent stabilizing additives include chromium, iron, manganese and nickel carboxylates.
- the liquid metal carboxylate composition contains both cerium and chromium carboxylates.
- the metal forming the metal carboxylate which is the major component of the liquid metal carboxylate composition is preferably present in an amount from about 65 to 97% by weight, relative to the total weight of the metal in the composition.
- the metal forming the metal carboxylate which is the major component is present in an amount from about 80-87% by weight.
- Another preferred amount for the metal forming the major component of the metal carboxylate composition is in the range from about 90-97% by weight.
- the stabilizing additives should be present, such that the total amount of the metal in metal carboxylates which are the stabilizing additives is at least 3% by weight, relative to the total weight of the metal in the liquid metal carboxylate composition. This can be achieved by using 3% of a single stabilizing additive, or less than 3% of more than one stabilizing additive, provided that the total weight of the metal in the stabilizing additives is greater than 3%.
- the total weight of the metal in the stabilizing additives is in a range from about 3% to about 35% by weight.
- Another preferred total weight range for the metal in the stabilizing additives is from about 3 to 30% by weight.
- One preferred total weight range for the metal in the stabilizing additives is from about 3 to 10 percent by weight.
- Non-limiting examples of liquid metal carboxylate compositions suitable for use in the present process are set forth below.
- weight range percentages for the metals are based on 100 percent total by weight of the metal in the liquid metal carboxylate composition.
- the minimum amount of the stabilizing additives, those defined below as being present in “up to” a certain amount, is a total stabilizing additive weight of at least 3 percent.
- the liquid metal carboxylate composition can have 3% of a single stabilizing additive or 1.5% of one stabilizing additives and 1.5% of another, or 2% of one stabilizing additive and 1% of the other.
- Non-limiting examples of suitable compositions are, particularly preferred in coating sparkplugs, are: up to 15% cobalt, up to 20% nickel, and the balance iron; up to 10% chromium, up to 20% cobalt, and the balance cerium; 3 through 5% cobalt, up to 20% chromium, and the balance cerium.
- the amount of metal in the liquid metal carboxylate composition should be enough to provide an adequate metal oxide coating. Preferably, this amount is in the range from about 20 to 150 grams of metal per kilogram of liquid metal carboxylate composition. A preferred amount of metal in the liquid metal carboxylate composition is 30 to 100 grams of metal per kilogram of liquid metal carboxylate composition. More preferably, the liquid metal carboxylate composition contains about 40-60 grams of metal per kg of composition.
- Amounts of metal less than 20 grams per kg of composition can be used. However, this low concentration requires that the process be repeated several times to provide an adequate coating.
- One preferred liquid metal carboxylate composition comprises VIK acids and the following metals (metal weight percentages are given relative to the total weight of metal in the liquid metal carboxylate composition): cerium - 94 to 96% chromium - 2 to 3% Iron - 2 to 3%
- the above metals are preferably present in the liquid metal carboxylate composition in an amount from about 30 to 40 grams of metal per kilogram of liquid metal carboxylate composition.
- Another preferred liquid metal carboxylate composition comprises VIK acids and the following metals (metal weight percentages are given relative to the total weight of metal in the liquid metal carboxylate composition): Cerium - 90% Chromium - 7% Cobalt - 3%
- the above metals are preferably present in the liquid metal carboxylate composition in an amount of 50 g of metal per kilogram of liquid metal carboxylate composition.
- the primary purpose of the disclosed method is the production of a metal oxide coating on the surface of a substrate.
- the method can be carried out on a variety of different structural products or components, whenever it is desirable to provide a metal oxide coating on the product or component.
- the coating can be applied to individual components prior to assembly into a multicomponent product, or can be applied to a finished multicomponent product.
- the liquid metal carboxylate composition can be applied to the substrate neat (without the use of an additional solvent) or in solution.
- the liquid metal carboxylate composition is applied without a solvent.
- any known method of application of the liquid metal carboxylate composition is suitable for use in the present process, so long as it provides an adequate coating of the liquid metal carboxylate composition on the substrate.
- the substrate component can be dipped into a container of the liquid metal carboxylate composition.
- a swab, sponge, dropper, pipet or other applicator can be used to apply the liquid metal carboxylate composition to the substrate.
- the liquid metal carboxylate composition should be applied at a temperature less than 500 C.
- the liquid metal carboxylate composition is applied to the substrate component at room temperature.
- the component is exposed to an environment sufficient to vaporize or dissipate excess carboxylic acid in the liquid metal carboxylate composition and to convert the metal carboxylates to metal oxides.
- the temperature for the treatment should be selected such that the temperature ranges for the evaporation of the carboxylic acid and the formation of the metal oxide overlap, and the temperature should not damage the component onto which the coating is being applied.
- this temperature is preferably greater than about 400° C.
- the upper limit for the heat treatment is dependent on the materials contained in the component being treated. The temperature should be selected so that it will not damage the component which is being coated.
- a preferred temperature range for most ceramic and metal components is from about 400 to 650° C. Another preferred temperature range is from about 400 to 550° C.
- the first process is the evaporation or decomposition of the excess carboxylic acid in the liquid metal carboxylate composition. This forms a metal carboxylate layer on the surface of the component.
- the second stage is the decomposition of the metal carboxylate layer to a metal oxide layer and fixation of that layer on the backing or substrate surface.
- Optimum oxide layer production occurs when the temperature at which the carboxylate decomposes and the acid evaporates overlap. That is, when the carboxylate decomposition stage commences, the removal and decomposition of the acid is not complete. Complete removal of the acid, prior to the commencement of carboxylate decomposition can reduce the adhesion of the oxide coating to the substrate.
- the heating can be conducted either by placing the coated component onto a rack or support and then into a furnace, which has been preheated to a desired temperature, or by placing the coated component into a furnace, followed by heating the furnace to the desired temperature.
- Any conventional furnace can be used, as no special heating equipment is required, provided, of course, that the furnace will accommodate the size and shape of the component being treated.
- the component should be heated for a time adequate to produce a uniform oxide coating.
- a preferred minimum time is at least about 2 min. If several different components are being treated simultaneously, uneven heating might take place. For example, the peripheral components will probably heat to working temperature faster than the components located in the center of the group. Accordingly, batches of components should be heated longer, depending on the type of furnace used and the nature of the components.
- the heat treatment should be carried out for at least two minutes at the desired temperature. More preferably, the heat treatment should be carried out for 15 to 20 minutes.
- the component should be allowed to cool to room temperature. Forced air cooling may be used to accelerate the cooling process.
- the component should not be cooled by treating it with a liquid coolant, as this could damage the coating or the component.
- the exposure step can also be carried out in some situations by exposing the substrate to ambient air conditions for sufficient time to fix the metal oxide coating to the substrate.
- the present process is carried out in a normal, i.e. ambient atmosphere. Accordingly, there is no need to provide any special atmosphere in the furnace during the heating process. However, should it be desired, the present process can also be conducted in specialized atmospheres. If a specialized atmosphere is used, it is preferably an oxidizing atmosphere, that is, one which is enriched with oxygen.
- sparkplugs in internal combustion engines, and igniters in gas turbines and jet engines, are used for igniting combustible mixtures of gases and vapors.
- sparkplugs used in internal combustion engines include a ceramic insulator, which surrounds a central electrode.
- the end portion of the sparkplug, including the end of the ceramic insulator is exposed to the interior of the combustion chamber of the engine.
- this contamination takes the form of electroconducting coke. This contamination can occur, for example, during engine idle when the engine has just been started and the fuel mixture is enriched, when the weather is cold, and when the engine is not properly tuned. It has been found that even when an engine is properly tuned, carbonization of the sparkplug can still take place, for example, when driving on a cold engine or using an enriched fuel mixture.
- the contamination can also take the form of lead-oxide, due to the presence of lead in leaded gasolines.
- the contamination of the sparkplug's ceramic insulator can interfere with the operation of the sparkplug.
- contamination with electroconductive coke or lead oxide reduces the sparking ability of the sparkplug, because the electrical current dissipates through the contaminant layer to the metal casing of the sparkplug.
- the present invention prevents or inhibits contamination of the sparkplug's ceramic insulator by carbon-based materials, such as coke, or by lead-oxide.
- the method can be used either during the sparkplug manufacturing process, for example, on an intermediate assembly, such as the ceramic insulator, or on the completed sparkplug.
- the present coating process can be used with any known process for manufacturing sparkplugs.
- the present oxide coating can be applied to the sparkplug's ceramic insulator prior to its assembly into the completed sparkplug.
- the coating can be applied to an assembled sparkplug.
- the present process can be used to form oxide coatings on sparkplugs which have been used in internal combustion engines, provided that the used sparkplug has been cleaned of any contaminants prior to formation of the oxide coating.
- metal carboxylate compositions used in Examples 1 to 3 were obtained from VserosBiiski Scientific Research Institute of Chemical Technologies, in Moscow, Russia.
- the upper electrode to which a sparkplug wire was attached was removed from a group of sparkplugs.
- the sparkplugs were then placed in a basket in a container over a boiling hydrocarbon solvent, in order to remove any grease or organic contamination which was present on the sparkplug.
- the basket containing the sparkplugs was removed from the degreasing chamber and was cooled to a temperature below 50° C.
- the degreased sparkplugs were placed in a holder, with the threaded portion of the sparkplug facing up, and were placed in a furnace which had been preheated to a temperature in the range 180 to 220° C. This treatment removed any solvent or moisture which had been absorbed onto the sparkplug. The sparkplugs were removed from the furnace and cooled to a temperature below 50° C.
- sparkplugs were placed in a furnace which had been heated to a temperature of 420° C. and were kept in the furnace for 30 minutes, forming the oxide coating. At the conclusion of the heat treatment, the sparkplugs were cooled to room temperature, and the upper electrode was reassembled into the sparkplug to provide the completed article.
- a Russian type All/1 sparkplug was prepared (degreased and dried) as set forth in Example 1, without the removal of the central electrode.
- the sparkplugs central insulator was dipped into the liquid carboxylate composition used in Example 1 to a depth between 10 to 15 mm.
- the sparkplug was then introduced into a furnace which had been preheated to 650° C., kept in the furnace for 10 minutes, removed and cooled to room temperature.
- Example 2 The procedure of Example 2 was repeated using a Russian All/l sparkplug which had been used in an internal combustion engine which had been run for 20,000 kilometers. A coated sparkplug was produced.
- sparkplugs manufactured according to the process set forth in Example 2 were used in a Lada automobile to determine their effects on the performance of the automobile, compared to uncoated sparkplugs.
- the use of the sparkplugs coated according to the present process significantly reduced the average time necessary to start the engine of a Lada automobile in cold weather from 2 min to 15-20 sec. In addition, the fuel consumption economy of the engine was improved by 5-7%.
- the present method can be used to coat numerous different substrates, with a variety of metal oxides. While the invention has been described by reference to various specific examples, it should be understood that the invention is not limited to those specific examples, and various modifications may be made to the embodiments described above without departing from the scope and spirite of the invention as claimed below.
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Abstract
The method is disclosed for coating or impregnating a substrate with a metal oxide. The method includes the steps of applying a liquid metal carboxylate composition, or a solution thereof, to a substrate material, and exposing the substrate material to an environment that will cause vaporization or dissipation of any excess carboxylic acids in the liquid metal carboxylate composition and conversion of the metal carboxylates to metal oxides.
Description
- The present invention relates generally to the field of surface coatings. In particular, the invention is a method for coating a wide variety of different substrates with a wide variety of metal oxide coatings.
- It is desirable in many situations to coat or impregnate the outer surface of a substrate with a coating, including a metal oxide coating.
- One method of coating substrates, such as a the ceramic insulator of a sparkplug, using active noble metals, such as silver, palladium or platinum, is disclosed in German Patent 3918272. The primary disadvantage of this method is its high cost. The use of platinum and other noble metals adds significantly to the cost of materials used to form the coating.
- One known method for the formation of metal oxide coatings on substrates is via the electrochemical sedimentation of metal oxides from solution. However, this method can only used to coat electrically conductive substrates, a significant limitation where the substrate is non-conductive.
- Another method of forming metal oxide coatings on substrates is a sputtering process. In this process, a metal oxide powder is vaporized, using, for example, laser, plasma, flame or detonation methods. The vapors are carried in a gas carrier until they reach the surface to be coated. This surface is generally relatively cool, so that the vaporized metal oxide powder condenses on the surface.
- The sputtering process is impractical and expensive to use for coating most substrates, making it commercially unreasonable. It requires the use of specialized manufacturing equipment to maintain the necessary vacuum conditions. These requirements increase the cost and difficulty of manufacturing the coated substrate product. Further, the materials used in the sputtering process, solid solutions of oxides, are expensive.
- Detonation spraying is another possible method that could be used to produce coatings on various substrates. However, this method requires a large amount of catalyst material and specialized manufacturing equipment.
- Another potential method for coating substrates is by deposition of metal oxides from aqueous solutions, followed by heat treatment. However, this method requires the use of a binder, such as phosphoric acid, in the metal oxide solution. The presence of phosphorus containing compounds in the catalytic layer reduces its catalytic activity.
- A further potential method is chemical vapor deposition (CVD) However, CVD requires the use of a carefully developed system of safety equipment, as toxic components are used in this process. These materials include β-diketones and metal-carbonyl complexes.
- Another known method for the deposition of a metal oxide coating on a substrate is described in U.S.S.R. Inventors Certificate No. 923232. This process uses a single trivalent metal salt formed by adding the metal to a solution of carboxylic acids. The salt is applied to a substrate and subjected to a temperature of 500 to 600° C. for 20 to 30 seconds in a nonoxidizing atmosphere.
- This process suffers from several drawbacks. First, it requires the use of a special furnace that contains a nonoxidizing atmosphere. In addition, the short heat treatment time produces a coating that has internal strains, leading to the lack of a well defined crystalline structure and creating a highly absorptive coating that can absorb water, gases or hydrocarbons. This absorption can make the coating conductive. Furthermore, the use of a single metal in the coating is undesirable because a number of metals, for example zirconium, do not form resistant coatings without additional additives. This would create weak coatings. Finally, this process only uses trivalent and tetravalent metals. As a result, desirable materials, such as nickel, copper and gold, can not be used therein.
- As noted above, the above-referenced conventional coating processes suffer from a variety of disadvantages that would make them undesirable for the commercial-scale production of most substrates. In addition, the coatings produced by these methods are relatively thick, which can reduce their adhesion to the substrate and cause scaling or flaking off of the coating. Further, the above methods require additional procedures to remove the coating from areas of the surface where no coating is desired. Finally, all of the above methods have high material consumption, increasing their cost.
- The present method overcomes the drawbacks described above in known techniques for coating substrates with metal oxides. The method generally comprises the steps of (a) applying a liquid metal carboxylate composition, or a solution thereof, to a substrate material, and (b) exposing the substrate material to an environment that will cause vaporization or dissipation of any excess carboxylic acids in the liquid metal carboxylate composition and conversion of the metal carboxylates to metal oxides.
- Usually, step (b) above is carried out by heating the substrate in a furnace, in normal air, at a temperature of at least about 300° C., and preferably of at least about 400° C., for at least about two minutes. However, for some items, such as large cast steel structures, the step can be accomplished by merely exposing the substrate to normal ambient conditions for a sufficiently long time to allow the metal oxide coating to form on the substrate.
- The invention also includes devices or structures coated with metal oxide coatings in accordance with the method described above.
- Suitable substrates for this process include metals, including steel alloys and aluminum, silica based materials (including optic and fiber optic materials), and various ceramic materials, that need to be protected from a range of environmental conditions, including atmospheres rich in corrosive fluids, combusted or partially combusted hydrocarbons (such as the combustion chambers of internal combustion engines, jet engines, and turbines, and in emission or pollution control systems attached thereto), saline conditions (such as in saline or brine conditioners), lead oxides, abrasive particles or degradative contaminants.
- For example, sensors used in catalytic converters, part of the required emission control systems for automobiles manufactured or sold in the United States, are commonly coated with platinum. To reduce the cost of these sensors, the present coating could be used to replace the platinum coating, thereby offering a low-cost alternative. There are numerous other examples of materials that could be coated in accordance with the present invention.
- For instance, one embodiment of the present invention is to deposit a metal oxide coating onto various heating elements in heating or air conditioning elements, including condenser or heat exchanger tubes.
- Another embodiment of the present invention is to deposit a metal oxide coating onto a casting mold or press mold. For instance, in some countries, press molds for rubber goods, such as tires, gaskets, cups, and seals, are made of hydrocarbon and low alloy steels. The lifetime of these machines can be significantly shortened by corrosion. To increase the life of such products, a thin (up to 5 mcm) metal oxide coating can be applied onto the working surfaces of the press, in accordance with the present method, by heat decomposition of a liquid metal carboxylate composition at, for example, 370-390° C.
- Another embodiment of the present invention is to deposit a metal oxide coating onto a metal tool. For instance, formation of a metal oxide coating on the surface of hard-faced (carbide tip) cutting tools will increase the lifetime of cutting tips.
- Another embodiment of the present invention is to deposit a metal oxide coating onto salt water marine propellers.
- Another embodiment of the present invention is to deposit a metal oxide coating onto turbine blades.
- Another embodiment of the present invention is to deposit a metal oxide coating onto metallic moving parts in machinery, such as aluminum parts.
- Another embodiment of the present invention is to deposit a metal oxide coating onto steel castings used in air conditioners.
- Another embodiment of the present invention is to deposit a metal oxide coating onto silicon or silica based materials, including optic or fiber optic materials.
- Another embodiment of the present invention is to deposit a metal oxide coating onto various metal parts exposed to abrasion or continuous high temperatures or high impact conditions (such as tools, dies, stamping materials).
- Another embodiment of the present invention is to deposit a metal oxide coating onto boat hulls, for instance, to prevent corrosion and to prevent barnacle formation.
- Another embodiment of the present invention is to deposit a metal oxide coating onto molds used for molding nonferrous metals. In the manufacture of such products, a basic mold is first made with a size that is larger than the product to be made, by approximately 50-100 microns. The surface of the mold is then powder coated by a protective coating in such a way that the size of the mold corresponds to the size of the desired article. A primary drawback of this method is the necessity for double treatment of the metal mold, and the restricted resistance of the metal mold. The present invention can be used to form a protective film in the mold when the mold is manufactured, corresponding to the size of the corresponding articles. This involves (1) manufacturing the mold with a size corresponding to the size of the article to be made, and (2) forming a protective surface of approximately 2 microns thickness on the surface of the mold. This provides a significant decrease in labor, and an increase in metal mold resistance at casting of at least 50%.
- Another embodiment of the present invention is to deposit an oxide coating of yttrium or cerium on the surface of nichrome heating elements, such as that used in many irons, stoves and resistance furnaces. This will increase the maximum working temperature of a typical nichrome element from approximately 1100° C. to approximately 1220-1250° C. or higher, while increasing the life of the heating element.
- While these are examples of various specific applications for the present invention, this list is by no means exhaustive, as the invention can be used to treat a wide variety of different components with a wide variety of different types and combinations of metal oxides.
- The term alkyl, as used herein, refer to a saturated straight, branched, or cyclic hydrocarbon, or a combination thereof, typically of C 1 to C24, and specifically includes methyl, ethyl, propyl, isopropyl, butyl, isobutyl, t-butyl, pentyl, cyclopentyl, isopentyl, neopentyl, hexyl, isohexyl, cyclohexyl, 3-methylpentyl, 2,2-dimethylbutyl, 2,3-dimethylbutyl, heptyl, octyl, nonyl, and decyl.
- The terms alkenyl and alkynyl, as used herein, refers to a C 2 to C24 straight or branched hydrocarbon with at least one double or triple bond, respectively.
- The term aryl or aromatic, as used herein, refers to phenyl, naphthyl, or substituted phenyl or naphthyl, wherein the substituent is alkyl, alkenyl, alkynyl or alkoxy.
- The liquid metal carboxylate composition is a solution of the carboxylic acid salts of one or more metals (“metal carboxylate”). Metal carboxylates are well known and can be produced by a variety of methods known to one skilled in the art. Non-limiting examples of methods for producing the metal carboxylate are shown in the following reaction schemes:
- RCOOH+Me→(RCOO) nMen+ 0.5nH2 (for alkaline earth metals, alkali earth metals and thallium);
- RCOOH+Me n+(OH)n→(RCOO)nMen+ H2O (for practically all metals having a solid hydroxide);
- RCOOH+Me n+(CO3)0.5n→(RCOO)nMen+ H2O CO2 (for alkaline earth metals, alkali earth metals and thalluim); and
- RCOOH+Me n+(X)n→(RCOO)nMen+ HmX (liquid extraction, usable for practically all metals having solid salts).
- The liquid metal carboxylate composition can contain a single metal, to form a single metal carboxylate, or a mixture of metals, to form a corresponding mixture of metal carboxylates. Preferably, the liquid metal carboxylate composition contains a mixture of metals, as these compositions form mixed oxides having superior properties.
- Preferably, the solvent used in the liquid metal carboxylate composition is an excess of a liquid carboxylic acid which was used to form the metal carboxylate. Alternatively, the solvent can be the solution of a carboxylic acid in another solvent, including, but not limited to, organic solvents such as acetone, ethanol, methanol, propanol, benzene, toluene, chloroform and dichloromethane.
- Carboxylic acids that are suitable for use to form the liquid metal carboxylate composition are those which: (1) can form a metal carboxylate, where the metal carboxylate is soluble in excess acid or another solvent; and (2) can be vaporized at a temperature which overlaps the oxide conversion temperature.
- The carboxylic acid should have a formula R-COOH, where R is alkyl, alkenyl, alkynyl or aryl.
- Preferably, the liquid monocarboxylic acid comprises one or more carboxylic acids having the formula I below:
- R—C(R″)(R′)—COOH (I)
- wherein:
- R is selected from H and C 1 to C24 alkyl groups; and
- R′ and R″ are each independently selected from C 1 to C24 alkyl groups.
- Preferably, these alpha branched carboxylic acids have a molecular weight in the range 130 to 420. More preferably, the carboxylic acids have a molecular weight in the range 220 to 270.
- Either a single carboxylic acid or a mixture of carboxylic acids can be used to form the liquid metal carboxylate. Preferably, a mixture of carboxylic acids is used. The use of a mixture provides several advantages. First, the mixture has a broader evaporation temperature range, making it more likely that the evaporation temperature of the acid mixture will overlap the metal carboxylate decomposition temperature, allowing the formation of an optimum oxide coating. Second, the production of purified individual acids is expensive. Thus, the use of an individual acid could unnecessarily raise the cost of this method.
- The carboxylic acid may be a mixture of tertiary and quaternary carboxylic acids of formula I. One preferred carboxylic acid mixture is a mixture manufactured by the Sterlitamakski Production Complex “KAUSTIK,” Bashkortostan, Sterlitamak City, Russia and other petrochemical enterprises, such as the Dneprodzerzhinski Complex in Dneprodzerzhinsk city, Ukraine. These materials are sold under the name “VIK acids.” The VIK acids are a material consisting of a mixture of carboxylic acids having the general formula CH 3(CH2)nC(CH3)(C2H5)—COOH, wherein n is 7 to 10. The average molecular weight of the acids contained in this mixture is from about 220 to 270. This mixture also contains the acid CH3CH2CH2CH(CH3)—COOH as its lowest boiling acid constituent.
- The VIK acids should have the properties set forth in Table 1.
TABLE 1 CHARACTERISTIC NORM appearance transparent homogeneous liquid color less or low-yellow. Color, maximum 7.0 Density at 20 C. 0.90-0.93 g/cm3 Acid Fraction composition: content of C3 acids-maximum 1.0 b) content of C5-C11, acids and 90.0% higher-maximum Acid number, mg 300-350 KOH/gr Ether number, mg 20.0 KOH/gr-maximum Water content-maximum 0.5% Refraction coefficient, 1.42-1.43 η 20 C. 189779.1 - The critical properties of the VIK acid are the acid number, which should not be above 380 mg/g KOH and the appearance; the liquid should be clear. The liquid alpha-branched carboxylic acids can be used as received from the manufacturer and do not require any additional purification, such as the removal of alcohol, ethers or other organic impurities.
- Metals that are particularly suitable for use to form the liquid metal carboxylates include those selected from the group consisting of: Lithium, Beryllium, Sodium, Magnesium, Potassium, Calcium, Scandium, Titanium, Chromium, Manganese, Iron, Nickel, Cobalt, Copper, Zinc, Gallium, Rubidium, Strontium, Yttrium, Zirconium, Silver, Cadmium, Tin, Cesium, Cerium, Barium, Platinum, Lanthanum, Hafnium, Vanadium, Niobium, Molybdenum, Indium, Promethium, Plutonium, Curium, Californium, Tantalum, Gold, Thallium, Lead, Bismuth, Cerium, Praseodymium, Neodymium, Samarium, Europium, Gadolinium, Terbium, Dysprosium, Holmium, Erbium, Thulium, Ytterbium, Lutetium, Thorium and Plutonium and Uranium.
- Any of the above metals or combinations thereof can be used to form coatings according to the present process. Depending on the particular use of the coating, those skilled in the art can select appropriate metal mixtures to form the desired metal or metal oxide coating. For example, the metals can be selected taking into consideration the nature of the substrate to be coated, the purpose of the substrate, and the environment to which the substrate is exposed.
- For example, the above-named inventor is filing contemporaneously herewith an application directed to a method for coating the ceramic insulators of sparkplugs, just one of the many applications of the present invention. By way of example, for the formation of a coating on the ceramic insulator of a sparkplug, the oxide coating should not be electrically conductive. In addition, if the engine is operating with a highly enriched fuel mixture, the partial reduction of iron, nickel and cobalt oxides is possible due to the interaction of these oxides with partially combusted fuel products. Thus, in these conditions, the amounts of these materials should be limited to that necessary to provide a stable coating. Preferably in these circumstances, thermodynamically stable oxides, such as chromium and cerium oxides should be the major components of the coating. Similarly, chromium oxide should not be the sole component of the coating for a sparkplug, as it may form agglomerates or a crystalline structure with reduced resistance. Thus, if chromium is used, it is preferably used in combination with other oxides, such as cerium. In addition, the use of divalent nickel with trivalent metals, such as cobalt, iron or chromium, may cause the formation of electrically conductive spinels. The electrically conductive spinels are, of course, undesirable for use on sparkplug insulators, although they may have other applications. Accordingly, if sparkplugs are being coated, the use of nickel with trivalent metals should be carefully monitored.
- In general, the liquid metal carboxylate composition preferably contains a mixture of metal carboxylates. This mixture preferably contains one metal carboxylate as its major component and one or more additional metal carboxylates as stabilizing additives. The stabilizing additives are preferably trivalent metal carboxylates. Preferred trivalent stabilizing additives include chromium, iron, manganese and nickel carboxylates. Preferably, the liquid metal carboxylate composition contains both cerium and chromium carboxylates.
- For most components in general, the metal forming the metal carboxylate which is the major component of the liquid metal carboxylate composition is preferably present in an amount from about 65 to 97% by weight, relative to the total weight of the metal in the composition. Preferably, the metal forming the metal carboxylate which is the major component is present in an amount from about 80-87% by weight. Another preferred amount for the metal forming the major component of the metal carboxylate composition is in the range from about 90-97% by weight.
- The stabilizing additives should be present, such that the total amount of the metal in metal carboxylates which are the stabilizing additives is at least 3% by weight, relative to the total weight of the metal in the liquid metal carboxylate composition. This can be achieved by using 3% of a single stabilizing additive, or less than 3% of more than one stabilizing additive, provided that the total weight of the metal in the stabilizing additives is greater than 3%. Preferably, the total weight of the metal in the stabilizing additives is in a range from about 3% to about 35% by weight. Another preferred total weight range for the metal in the stabilizing additives is from about 3 to 30% by weight. One preferred total weight range for the metal in the stabilizing additives is from about 3 to 10 percent by weight.
- Non-limiting examples of liquid metal carboxylate compositions suitable for use in the present process are set forth below. In these compositions, weight range percentages for the metals are based on 100 percent total by weight of the metal in the liquid metal carboxylate composition. As noted above, the minimum amount of the stabilizing additives, those defined below as being present in “up to” a certain amount, is a total stabilizing additive weight of at least 3 percent. For example, the liquid metal carboxylate composition can have 3% of a single stabilizing additive or 1.5% of one stabilizing additives and 1.5% of another, or 2% of one stabilizing additive and 1% of the other. Non-limiting examples of suitable compositions are, particularly preferred in coating sparkplugs, are: up to 15% cobalt, up to 20% nickel, and the balance iron; up to 10% chromium, up to 20% cobalt, and the balance cerium; 3 through 5% cobalt, up to 20% chromium, and the balance cerium.
- The amount of metal in the liquid metal carboxylate composition should be enough to provide an adequate metal oxide coating. Preferably, this amount is in the range from about 20 to 150 grams of metal per kilogram of liquid metal carboxylate composition. A preferred amount of metal in the liquid metal carboxylate composition is 30 to 100 grams of metal per kilogram of liquid metal carboxylate composition. More preferably, the liquid metal carboxylate composition contains about 40-60 grams of metal per kg of composition.
- Amounts of metal less than 20 grams per kg of composition can be used. However, this low concentration requires that the process be repeated several times to provide an adequate coating.
- Similarly, amounts of metal greater than 150 grams per kg of composition can be used, however, the use of more metal raises the cost of the present Method.
- One preferred liquid metal carboxylate composition comprises VIK acids and the following metals (metal weight percentages are given relative to the total weight of metal in the liquid metal carboxylate composition):
cerium - 94 to 96% chromium - 2 to 3% Iron - 2 to 3% - The above metals are preferably present in the liquid metal carboxylate composition in an amount from about 30 to 40 grams of metal per kilogram of liquid metal carboxylate composition.
- Another preferred liquid metal carboxylate composition comprises VIK acids and the following metals (metal weight percentages are given relative to the total weight of metal in the liquid metal carboxylate composition):
Cerium - 90% Chromium - 7% Cobalt - 3% - The above metals are preferably present in the liquid metal carboxylate composition in an amount of 50 g of metal per kilogram of liquid metal carboxylate composition.
- These liquid metal carboxylate compositions are commercially available from the state enterprise Vserossiiski Scientific Research Institute of Chemical Technologies, Moscow, Russia.
- As discussed above, the primary purpose of the disclosed method is the production of a metal oxide coating on the surface of a substrate. The method can be carried out on a variety of different structural products or components, whenever it is desirable to provide a metal oxide coating on the product or component. The coating can be applied to individual components prior to assembly into a multicomponent product, or can be applied to a finished multicomponent product.
- The liquid metal carboxylate composition can be applied to the substrate neat (without the use of an additional solvent) or in solution. Preferably, the liquid metal carboxylate composition is applied without a solvent.
- Any known method of application of the liquid metal carboxylate composition is suitable for use in the present process, so long as it provides an adequate coating of the liquid metal carboxylate composition on the substrate. For example, the substrate component can be dipped into a container of the liquid metal carboxylate composition. Alternatively, a swab, sponge, dropper, pipet or other applicator can be used to apply the liquid metal carboxylate composition to the substrate.
- The liquid metal carboxylate composition should be applied at a temperature less than 500 C. Preferably, the liquid metal carboxylate composition is applied to the substrate component at room temperature.
- Following application of the liquid metal carboxylate composition to the substrate, the component is exposed to an environment sufficient to vaporize or dissipate excess carboxylic acid in the liquid metal carboxylate composition and to convert the metal carboxylates to metal oxides. The temperature for the treatment should be selected such that the temperature ranges for the evaporation of the carboxylic acid and the formation of the metal oxide overlap, and the temperature should not damage the component onto which the coating is being applied.
- For sparkplugs and similar types of components, this temperature is preferably greater than about 400° C. The upper limit for the heat treatment is dependent on the materials contained in the component being treated. The temperature should be selected so that it will not damage the component which is being coated. A preferred temperature range for most ceramic and metal components is from about 400 to 650° C. Another preferred temperature range is from about 400 to 550° C.
- During the exposure step of the process, two processes take place. These processes can occur at different temperature levels. The first process is the evaporation or decomposition of the excess carboxylic acid in the liquid metal carboxylate composition. This forms a metal carboxylate layer on the surface of the component. The second stage is the decomposition of the metal carboxylate layer to a metal oxide layer and fixation of that layer on the backing or substrate surface.
- To create an oxide layer which is fixed to the substrate surface, it is preferred that there be an interaction between the substrate and the coating during the coating process. Optimum oxide layer production occurs when the temperature at which the carboxylate decomposes and the acid evaporates overlap. That is, when the carboxylate decomposition stage commences, the removal and decomposition of the acid is not complete. Complete removal of the acid, prior to the commencement of carboxylate decomposition can reduce the adhesion of the oxide coating to the substrate.
- Without wishing to be bound to any particular mechanism, it is believed that the following process occurs during the So production of the oxide coating. At high temperatures, it is believed that the carboxylic acid etches or otherwise interacts with the substrate, activating it. This allows interaction between the metal carboxylate and the activated substrate, resulting in the formation of a strong substrate-oxide link.
- The heating can be conducted either by placing the coated component onto a rack or support and then into a furnace, which has been preheated to a desired temperature, or by placing the coated component into a furnace, followed by heating the furnace to the desired temperature. Any conventional furnace can be used, as no special heating equipment is required, provided, of course, that the furnace will accommodate the size and shape of the component being treated.
- In general, the component should be heated for a time adequate to produce a uniform oxide coating. For a furnace which has been preheated to a temperature above 400° C., a preferred minimum time is at least about 2 min. If several different components are being treated simultaneously, uneven heating might take place. For example, the peripheral components will probably heat to working temperature faster than the components located in the center of the group. Accordingly, batches of components should be heated longer, depending on the type of furnace used and the nature of the components.
- Preferably, the heat treatment should be carried out for at least two minutes at the desired temperature. More preferably, the heat treatment should be carried out for 15 to 20 minutes.
- Following treatment, the component should be allowed to cool to room temperature. Forced air cooling may be used to accelerate the cooling process. The component should not be cooled by treating it with a liquid coolant, as this could damage the coating or the component.
- As noted above, while active heating to high temperatures is the preferred method of curing the coating, the exposure step can also be carried out in some situations by exposing the substrate to ambient air conditions for sufficient time to fix the metal oxide coating to the substrate.
- The present process is carried out in a normal, i.e. ambient atmosphere. Accordingly, there is no need to provide any special atmosphere in the furnace during the heating process. However, should it be desired, the present process can also be conducted in specialized atmospheres. If a specialized atmosphere is used, it is preferably an oxidizing atmosphere, that is, one which is enriched with oxygen.
- As noted above, one particular application of the present invention is for coating sparkplugs. Sparkplugs in internal combustion engines, and igniters in gas turbines and jet engines, are used for igniting combustible mixtures of gases and vapors.
- Typically, sparkplugs used in internal combustion engines include a ceramic insulator, which surrounds a central electrode. The end portion of the sparkplug, including the end of the ceramic insulator, is exposed to the interior of the combustion chamber of the engine. During normal operation of the engine, there are times when operating conditions contaminate the ceramic insulator of the sparkplug. Often, this contamination takes the form of electroconducting coke. This contamination can occur, for example, during engine idle when the engine has just been started and the fuel mixture is enriched, when the weather is cold, and when the engine is not properly tuned. It has been found that even when an engine is properly tuned, carbonization of the sparkplug can still take place, for example, when driving on a cold engine or using an enriched fuel mixture. The contamination can also take the form of lead-oxide, due to the presence of lead in leaded gasolines.
- The contamination of the sparkplug's ceramic insulator can interfere with the operation of the sparkplug. For example, contamination with electroconductive coke or lead oxide reduces the sparking ability of the sparkplug, because the electrical current dissipates through the contaminant layer to the metal casing of the sparkplug.
- The present invention prevents or inhibits contamination of the sparkplug's ceramic insulator by carbon-based materials, such as coke, or by lead-oxide. The method can be used either during the sparkplug manufacturing process, for example, on an intermediate assembly, such as the ceramic insulator, or on the completed sparkplug. The present coating process can be used with any known process for manufacturing sparkplugs. For example, the present oxide coating can be applied to the sparkplug's ceramic insulator prior to its assembly into the completed sparkplug. Alternatively, the coating can be applied to an assembled sparkplug. In addition, the present process can be used to form oxide coatings on sparkplugs which have been used in internal combustion engines, provided that the used sparkplug has been cleaned of any contaminants prior to formation of the oxide coating.
- The following examples illustrate the application of the present process to the coating of sparkplugs.
- The metal carboxylate compositions used in Examples 1 to 3 were obtained from VserosBiiski Scientific Research Institute of Chemical Technologies, in Moscow, Russia.
- The upper electrode to which a sparkplug wire was attached, was removed from a group of sparkplugs. The sparkplugs were then placed in a basket in a container over a boiling hydrocarbon solvent, in order to remove any grease or organic contamination which was present on the sparkplug. The basket containing the sparkplugs was removed from the degreasing chamber and was cooled to a temperature below 50° C.
- The degreased sparkplugs were placed in a holder, with the threaded portion of the sparkplug facing up, and were placed in a furnace which had been preheated to a temperature in the range 180 to 220° C. This treatment removed any solvent or moisture which had been absorbed onto the sparkplug. The sparkplugs were removed from the furnace and cooled to a temperature below 50° C.
- Two drops of a liquid metal carboxylate mixture were manually applied to the tip of the central electrode insulator of each spark plug. The metal carboxylate mixture had the following proportions of metal: 90% cerium, 7% chromium, and 3% cobalt. The carboxylic acid was VIK acid. The total metal concentration in the liquid carboxylate mixture was 50 g metal per kilogram of liquid carboxylate mixture.
- The sparkplugs were placed in a furnace which had been heated to a temperature of 420° C. and were kept in the furnace for 30 minutes, forming the oxide coating. At the conclusion of the heat treatment, the sparkplugs were cooled to room temperature, and the upper electrode was reassembled into the sparkplug to provide the completed article.
- A Russian type All/1 sparkplug was prepared (degreased and dried) as set forth in Example 1, without the removal of the central electrode. The sparkplugs central insulator was dipped into the liquid carboxylate composition used in Example 1 to a depth between 10 to 15 mm. The sparkplug was then introduced into a furnace which had been preheated to 650° C., kept in the furnace for 10 minutes, removed and cooled to room temperature.
- The procedure of Example 2 was repeated using a Russian All/l sparkplug which had been used in an internal combustion engine which had been run for 20,000 kilometers. A coated sparkplug was produced.
- The sparkplugs manufactured according to the process set forth in Example 2 were used in a Lada automobile to determine their effects on the performance of the automobile, compared to uncoated sparkplugs. The use of the sparkplugs coated according to the present process significantly reduced the average time necessary to start the engine of a Lada automobile in cold weather from 2 min to 15-20 sec. In addition, the fuel consumption economy of the engine was improved by 5-7%.
- As noted above, the present method can be used to coat numerous different substrates, with a variety of metal oxides. While the invention has been described by reference to various specific examples, it should be understood that the invention is not limited to those specific examples, and various modifications may be made to the embodiments described above without departing from the scope and spirite of the invention as claimed below.
Claims (17)
1. A method for forming a metal oxide coating on a substrate, comprising the steps of:
(a) applying metal carboxylate composition, or a solution thereof, to a substrate material, and
(b) exposing the substrate material to an environment that will cause vaporization or dissipation of any excess carboxylic acids in the liquid metal carboxylate composition and conversion of the metal carboxylates to metal oxides.
2. The method or claim 1 , wherein the liquid metal carboxylate composition comprises a solution of the metal salt of a carboxylic acid.
3. The method of claim 2 , wherein the carboxylic acid is an alpha-branched carboxylic acid having having the formula
R—C(R″)(R′)—COOH
wherein:
R is selected from H and C1 to C24 alkyl groups; and
R′ and R″ are each independently selected from C1 to C24 alkyl groups.
4. The method of claim 2 , wherein the carboxylic acid is a mixture of carboxylic acids having the formula CH3(CH2)nC(CH3)(C2H5)—COOH, wherein n is 7 to 10.
5. The method of claim 4 , wherein the average molecular weight of the acids contained in this mixture is from about 220 to 270.
6. The method of claim 5 , wherein the mixture of carboxylic acids contains the acid CH3CH2CH2CH(CH3)—COOH as its lowest boiling acid constituent.
7. The method of claim 2 , wherein the liquid metal carboxylate composition comprises a mixture of metals.
8. The method of claim 2 , wherein the liquid metal carboxylate composition comprises one or more metals selected from the group consisting of Lithium, Beryllium, Sodium, Magnesium, Potassium, Calcium, Scandium, Titanium, Chromium, Manganese, Iron, Nickel, Cobalt, Copper, Zinc, Gallium, Rubidium, Strontium, Yttrium, Zirconium, Silver, Cadmium, Tin, Cesium, Cerium, Barium, Lanthanum, Hafnium, Tantalum, Gold, Thallium, Lead, Bismuth, Cerium, Praseodymium, Neodymium, Samarium, Europium, Gadolinium, Terbium, Dysprosium, Holmium, Erbium, Thulium, Ytterbium, Lutetium, Thorium and Uranium.
9. The method of claim 3 , wherein the liquid metal carboxylate composition comprises one or more metals selected from the group consisting of Lithium, Beryllium, Sodium, Magnesium, Potassium, Calcium, Scandium, Titanium, Chromium, Manganese, Iron, Nickel, Cobalt, Copper, Zinc, Gallium, Rubidium, Strontium, Yttrium, Zirconium, Silver, Cadmium, Tin, Cesium, Cerium, Barium, Lanthanum, Hafnium, Tantalum, Gold, Thallium, Lead, Bismuth, Cerium, Praseodymium, Neodymium, Samarium, Europium, Gadolinium, Terbium, Dysprosium, Holmium, Erbium, Thulium, Ytterbium, Lutetium, Thorium and Uranium.
10. The method of claim 4 , wherein the liquid metal carboxylate composition comprises one or more metals selected from the group consisting of Lithium, Beryllium, Sodium, Magnesium, Potassium, Calcium, Scandium, Titanium, Chromium, Manganese, Iron, Nickel, Cobalt, Copper, Zinc, Gallium, Rubidium, Strontium, Yttrium, Zirconium, Silver, Cadmium, Tin, Cesium, Cerium, Barium, Lanthanum, Hafnium, Tantalum, Gold, Thallium, Lead, Bismuth, Cerium, Praseodymium, Neodymium, Samarium, Europium, Gadolinium, Terbium, Dysprosium, Holmium, Erbium, Thulium, Ytterbium, Lutetium, Thorium and Uranium.
11. The method of claim 2 , wherein the metal is a mixture comprising:
up to 15% by weight of cobalt;
up to 20% by weight of nickel; and
the balance iron;
wherein the minimum total amount of cobalt and nickel is at least 3%.
12. The method of claim 2 , wherein the metal is a mixture comprising:
up to 20% by weight of cobalt;
up to 10% by weight of chromium; and
the balance cerium;
wherein the minimum total amount of cobalt and chromium is at least 3%.
13. The method of claim 2 , wherein the metal is a mixture comprising:
3 through 5% by weight of cobalt,
0 through 20% by weight of chromium,
and the balance cerium.
14. The method of claim 1 wherein the vaporization or dissipation of any excess carboxylic acids in the liquid metal carboxylate composition and conversion of the metal carboxylates to metal oxides is carried out by heating the coated substrate.
15. The method of claim 14 , wherein the substrate is heated to a temperature greater than about 400° C.
16. The method of claim 2 , wherein the amount of metal in the liquid metal carboxylate composition is preferably in the range of 30-50 grams of metal per kilogram of liquid metal carboxylate composition.
17. The method of claim 2 , wherein the amount of metal in the liquid metal carboxylate composition is 30 to 40 grams of metal per kilogram of liquid metal carboxylate composition.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/824,418 US20020041928A1 (en) | 1997-03-26 | 1997-03-26 | Method for coating substrate with metal oxide coating |
| US10/440,802 US7718221B2 (en) | 1996-03-28 | 2003-05-19 | Coatings for metal casting parts |
| US10/868,417 US7211292B1 (en) | 1996-03-28 | 2004-06-15 | Coatings for metal cutting tools |
| US12/718,484 US20100159264A1 (en) | 1997-03-26 | 2010-03-05 | Coatings for metal casting parts |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/824,418 US20020041928A1 (en) | 1997-03-26 | 1997-03-26 | Method for coating substrate with metal oxide coating |
| US10/440,802 US7718221B2 (en) | 1996-03-28 | 2003-05-19 | Coatings for metal casting parts |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US83545301A Continuation-In-Part | 1996-03-28 | 2001-04-16 |
Publications (1)
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|---|---|
| US20020041928A1 true US20020041928A1 (en) | 2002-04-11 |
Family
ID=33476599
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US08/824,418 Abandoned US20020041928A1 (en) | 1996-03-28 | 1997-03-26 | Method for coating substrate with metal oxide coating |
| US10/440,802 Expired - Fee Related US7718221B2 (en) | 1996-03-28 | 2003-05-19 | Coatings for metal casting parts |
| US10/868,417 Expired - Fee Related US7211292B1 (en) | 1996-03-28 | 2004-06-15 | Coatings for metal cutting tools |
| US12/718,484 Abandoned US20100159264A1 (en) | 1997-03-26 | 2010-03-05 | Coatings for metal casting parts |
Family Applications After (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/440,802 Expired - Fee Related US7718221B2 (en) | 1996-03-28 | 2003-05-19 | Coatings for metal casting parts |
| US10/868,417 Expired - Fee Related US7211292B1 (en) | 1996-03-28 | 2004-06-15 | Coatings for metal cutting tools |
| US12/718,484 Abandoned US20100159264A1 (en) | 1997-03-26 | 2010-03-05 | Coatings for metal casting parts |
Country Status (4)
| Country | Link |
|---|---|
| US (4) | US20020041928A1 (en) |
| CA (1) | CA2526516C (en) |
| MX (1) | MXPA05012485A (en) |
| WO (1) | WO2004104261A1 (en) |
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Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
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Family Cites Families (38)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE295148C (en) | ||||
| GB1327760A (en) * | 1969-12-22 | 1973-08-22 | Imp Metal Ind Kynoch Ltd | Electrodes |
| US3962490A (en) * | 1974-01-24 | 1976-06-08 | Ferro Corporation | Preparation of nickel and chromium substrates for ceramic coating |
| JPS5949677B2 (en) | 1978-06-05 | 1984-12-04 | 株式会社豊田中央研究所 | Spark plug and its manufacturing method |
| DE2836002C2 (en) | 1978-08-17 | 1986-09-11 | Robert Bosch Gmbh, 7000 Stuttgart | Sensor for monitoring the absence of soot in exhaust gases |
| RU923232C (en) | 1980-07-14 | 1994-04-15 | Filippov E A | Method of obtaining oxide coatings |
| US4530340A (en) | 1981-05-01 | 1985-07-23 | Totman Millard C | Acid catalyzed combustion |
| JPS62226592A (en) | 1986-03-28 | 1987-10-05 | 日本特殊陶業株式会社 | Ignition plug |
| US4828934A (en) * | 1986-12-12 | 1989-05-09 | Vapor Technologies, Inc. | Method of protecting ceramic bodies against mechanical and thermal action |
| DE3706576A1 (en) | 1987-02-28 | 1988-09-08 | Bosch Gmbh Robert | IGNITION ARRANGEMENT WITH REDUCED IGNITION TEMPERATURE |
| DE3811395A1 (en) | 1987-04-06 | 1988-11-10 | Nippon Denso Co | Spark plug for an internal combustion engine |
| FR2617507B1 (en) | 1987-06-30 | 1989-12-08 | Inst Francais Du Petrole | METHOD FOR SURFACE MODIFICATION OF THE SURFACE OF A SUBSTRATE AND APPLICATION TO THE MANUFACTURE OF COATINGS AND CATALYSTS |
| DE3727526A1 (en) | 1987-08-18 | 1989-03-02 | Bosch Gmbh Robert | METHOD FOR PRODUCING A SPARK PLUG FOR INTERNAL COMBUSTION ENGINES |
| US4937484A (en) | 1988-05-16 | 1990-06-26 | Nippondenso Co., Ltd. | Sparking plug |
| US4881913A (en) | 1988-06-16 | 1989-11-21 | General Motors Corporation | Extended life spark plug/igniter |
| US4826462A (en) | 1988-08-19 | 1989-05-02 | Champion Spark Plug Company | Method for manufacturing a spark plug electrode |
| US4963390A (en) | 1988-10-05 | 1990-10-16 | The Aerospace Corporation | Metallo-organic solution deposition (MOSD) of transparent, crystalline ferroelectric films |
| US4935265A (en) | 1988-12-19 | 1990-06-19 | United Technologies Corporation | Method for coating fibers with an amorphous hydrated metal oxide |
| DE69006066T2 (en) | 1989-03-28 | 1994-08-11 | Ngk Spark Plug Co | Spark plug for an internal combustion engine. |
| US5073410A (en) | 1989-10-16 | 1991-12-17 | Eastman Kodak Company | Thin films of metal phosphates and the method of their formation |
| US5021398A (en) * | 1989-10-26 | 1991-06-04 | Amp Incorporated | Method of forming patterned oxide superconducting films |
| US5034550A (en) * | 1990-01-24 | 1991-07-23 | Akzo N.V. | Process for forming mixed heavy bimetal alkoxide-carboxylate compositions and novel compositions thereof |
| US5601869A (en) | 1991-12-13 | 1997-02-11 | Symetrix Corporation | Metal polyoxyalkylated precursor solutions in an octane solvent and method of making the same |
| US5612082A (en) | 1991-12-13 | 1997-03-18 | Symetrix Corporation | Process for making metal oxides |
| US5699035A (en) | 1991-12-13 | 1997-12-16 | Symetrix Corporation | ZnO thin-film varistors and method of making the same |
| US5274298A (en) | 1991-12-23 | 1993-12-28 | Ford Motor Company | Spark plug having an ablative coating for anticontaminat fouling |
| US5279111A (en) * | 1992-08-27 | 1994-01-18 | Inco Limited | Gas turbine cooling |
| US5312585A (en) * | 1993-06-28 | 1994-05-17 | The United States Of America As Represented By The Secretary Of The Navy | Corrosion inhibition in high temperature environment |
| CA2149567C (en) | 1994-05-31 | 2000-12-05 | William C. Russell | Coated cutting tool and method of making same |
| KR100406665B1 (en) | 1995-06-09 | 2004-03-26 | 미쓰비시 마테리알 가부시키가이샤 | Compositions for forming Ba1-xSrxTiyO3 thin films and methods for forming Ba1-xSrxTiyO3 thin films |
| US20020041928A1 (en) | 1997-03-26 | 2002-04-11 | Leonid V. Budaragin | Method for coating substrate with metal oxide coating |
| US5952769A (en) * | 1996-03-29 | 1999-09-14 | Sparco, Inc. | Method for coating sparkplugs |
| JP3856891B2 (en) | 1997-03-11 | 2006-12-13 | 本田技研工業株式会社 | Method for surface modification of hard material and cutting tool |
| US5981088A (en) * | 1997-08-18 | 1999-11-09 | General Electric Company | Thermal barrier coating system |
| SE517046C2 (en) | 1997-11-26 | 2002-04-09 | Sandvik Ab | Plasma-activated CVD method for coating fine-grained alumina cutting tools |
| US6294261B1 (en) | 1999-10-01 | 2001-09-25 | General Electric Company | Method for smoothing the surface of a protective coating |
| US6620456B2 (en) * | 2001-02-26 | 2003-09-16 | Eastman Kodak Company | Forming a dielectric layer by thermal decomposition of a metallo-organic material |
| US6663983B1 (en) * | 2002-07-26 | 2003-12-16 | General Electric Company | Thermal barrier coating with improved strength and fracture toughness |
-
1997
- 1997-03-26 US US08/824,418 patent/US20020041928A1/en not_active Abandoned
-
2003
- 2003-05-19 US US10/440,802 patent/US7718221B2/en not_active Expired - Fee Related
-
2004
- 2004-05-06 MX MXPA05012485A patent/MXPA05012485A/en active IP Right Grant
- 2004-05-06 WO PCT/US2004/014178 patent/WO2004104261A1/en not_active Ceased
- 2004-05-06 CA CA2526516A patent/CA2526516C/en not_active Expired - Fee Related
- 2004-06-15 US US10/868,417 patent/US7211292B1/en not_active Expired - Fee Related
-
2010
- 2010-03-05 US US12/718,484 patent/US20100159264A1/en not_active Abandoned
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| US20090166259A1 (en) * | 2007-12-28 | 2009-07-02 | Steven Bradley | Metal-based coatings for inhibiting metal catalyzed coke formation in hydrocarbon conversion processes |
| US8623301B1 (en) | 2008-04-09 | 2014-01-07 | C3 International, Llc | Solid oxide fuel cells, electrolyzers, and sensors, and methods of making and using the same |
| US9670586B1 (en) | 2008-04-09 | 2017-06-06 | Fcet, Inc. | Solid oxide fuel cells, electrolyzers, and sensors, and methods of making and using the same |
| US20100061902A1 (en) * | 2008-09-05 | 2010-03-11 | Bradley Steven A | Metal-Based Coatings for Inhibiting Metal Catalyed Coke Formation in Hydrocarbon Conversion Processes |
| US8128887B2 (en) | 2008-09-05 | 2012-03-06 | Uop Llc | Metal-based coatings for inhibiting metal catalyzed coke formation in hydrocarbon conversion processes |
| US10344389B2 (en) | 2010-02-10 | 2019-07-09 | Fcet, Inc. | Low temperature electrolytes for solid oxide cells having high ionic conductivity |
| US12071697B2 (en) | 2010-02-10 | 2024-08-27 | Fcet, Inc. | Low temperature electrolytes for solid oxide cells having high ionic conductivity |
| US11560636B2 (en) | 2010-02-10 | 2023-01-24 | Fcet, Inc. | Low temperature electrolytes for solid oxide cells having high ionic conductivity |
| US20130298531A1 (en) * | 2011-01-20 | 2013-11-14 | Ihi Corporation | Deposition prevention method and turbocharger |
| US9322313B2 (en) * | 2011-01-20 | 2016-04-26 | Ihi Corporation | Deposition prevention method and turbocharger |
| US10707511B2 (en) | 2013-07-15 | 2020-07-07 | Fcet, Inc. | Low temperature solid oxide cells |
| US9905871B2 (en) | 2013-07-15 | 2018-02-27 | Fcet, Inc. | Low temperature solid oxide cells |
| US11814730B2 (en) * | 2017-06-02 | 2023-11-14 | Warner Babcock Institute For Green Chemistry, Llc | Methods for producing metal oxide films |
Also Published As
| Publication number | Publication date |
|---|---|
| US20100159264A1 (en) | 2010-06-24 |
| US7718221B2 (en) | 2010-05-18 |
| MXPA05012485A (en) | 2006-07-03 |
| CA2526516A1 (en) | 2004-12-02 |
| CA2526516C (en) | 2010-06-29 |
| US20040253438A1 (en) | 2004-12-16 |
| US7211292B1 (en) | 2007-05-01 |
| WO2004104261A1 (en) | 2004-12-02 |
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