GB2402399A - A silver-germanium-copper alloy - Google Patents
A silver-germanium-copper alloy Download PDFInfo
- Publication number
- GB2402399A GB2402399A GB0312693A GB0312693A GB2402399A GB 2402399 A GB2402399 A GB 2402399A GB 0312693 A GB0312693 A GB 0312693A GB 0312693 A GB0312693 A GB 0312693A GB 2402399 A GB2402399 A GB 2402399A
- Authority
- GB
- United Kingdom
- Prior art keywords
- alloy
- dialkyl
- silver
- alkanethiol
- thioglycollate
- 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.)
- Granted
Links
- 229910000881 Cu alloy Inorganic materials 0.000 title claims description 8
- ZHWDKWFGZPWVMU-UHFFFAOYSA-N [Ge].[Cu].[Ag] Chemical compound [Ge].[Cu].[Ag] ZHWDKWFGZPWVMU-UHFFFAOYSA-N 0.000 title description 3
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 86
- 239000000956 alloy Substances 0.000 claims abstract description 86
- 229910052709 silver Inorganic materials 0.000 claims abstract description 51
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 claims abstract description 50
- 239000004332 silver Substances 0.000 claims abstract description 49
- 229910052732 germanium Inorganic materials 0.000 claims abstract description 32
- 239000010949 copper Substances 0.000 claims abstract description 31
- QJAOYSPHSNGHNC-UHFFFAOYSA-N octadecane-1-thiol Chemical compound CCCCCCCCCCCCCCCCCCS QJAOYSPHSNGHNC-UHFFFAOYSA-N 0.000 claims abstract description 26
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 24
- -1 alkyl thioglycollate Chemical compound 0.000 claims abstract description 24
- 229910052802 copper Inorganic materials 0.000 claims abstract description 23
- 239000000203 mixture Substances 0.000 claims abstract description 19
- 229910052796 boron Inorganic materials 0.000 claims abstract description 18
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 17
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 16
- UCKMPCXJQFINFW-UHFFFAOYSA-N Sulphide Chemical compound [S-2] UCKMPCXJQFINFW-UHFFFAOYSA-N 0.000 claims abstract description 15
- 239000003599 detergent Substances 0.000 claims abstract description 14
- BWGNESOTFCXPMA-UHFFFAOYSA-N Dihydrogen disulfide Chemical compound SS BWGNESOTFCXPMA-UHFFFAOYSA-N 0.000 claims abstract description 11
- 239000003960 organic solvent Substances 0.000 claims abstract description 9
- 239000004744 fabric Substances 0.000 claims abstract description 8
- 239000012535 impurity Substances 0.000 claims abstract description 8
- 239000000344 soap Substances 0.000 claims abstract description 6
- CYNYIHKIEHGYOZ-UHFFFAOYSA-N 1-bromopropane Chemical compound CCCBr CYNYIHKIEHGYOZ-UHFFFAOYSA-N 0.000 claims abstract description 5
- ORTRWBYBJVGVQC-UHFFFAOYSA-N hexadecane-1-thiol Chemical compound CCCCCCCCCCCCCCCCS ORTRWBYBJVGVQC-UHFFFAOYSA-N 0.000 claims abstract description 4
- GNPVGFCGXDBREM-UHFFFAOYSA-N germanium atom Chemical compound [Ge] GNPVGFCGXDBREM-UHFFFAOYSA-N 0.000 claims description 22
- 239000002904 solvent Substances 0.000 claims description 19
- 229910002058 ternary alloy Inorganic materials 0.000 claims description 11
- 238000005266 casting Methods 0.000 claims description 10
- 229910000927 Ge alloy Inorganic materials 0.000 claims description 9
- 238000005498 polishing Methods 0.000 claims description 7
- 238000004381 surface treatment Methods 0.000 claims description 4
- 238000007865 diluting Methods 0.000 claims 1
- 239000006185 dispersion Substances 0.000 claims 1
- 230000007935 neutral effect Effects 0.000 claims 1
- 229910001316 Ag alloy Inorganic materials 0.000 abstract description 15
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 abstract description 3
- 239000005864 Sulphur Substances 0.000 abstract description 2
- 125000000913 palmityl 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])C([H])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])C([H])([H])[H] 0.000 abstract description 2
- 239000000243 solution Substances 0.000 description 23
- 238000011282 treatment Methods 0.000 description 17
- 239000007788 liquid Substances 0.000 description 14
- 238000004519 manufacturing process Methods 0.000 description 14
- 238000000137 annealing Methods 0.000 description 12
- 230000015572 biosynthetic process Effects 0.000 description 12
- 229910001118 argentium sterling silver Inorganic materials 0.000 description 11
- 238000012360 testing method Methods 0.000 description 11
- 230000005496 eutectics Effects 0.000 description 10
- 238000002844 melting Methods 0.000 description 10
- 230000009467 reduction Effects 0.000 description 10
- 239000010410 layer Substances 0.000 description 9
- 238000000034 method Methods 0.000 description 9
- QGZKDVFQNNGYKY-UHFFFAOYSA-O Ammonium Chemical compound [NH4+] QGZKDVFQNNGYKY-UHFFFAOYSA-O 0.000 description 8
- 238000004140 cleaning Methods 0.000 description 8
- 229920001021 polysulfide Polymers 0.000 description 8
- 239000010944 silver (metal) Substances 0.000 description 8
- 239000011877 solvent mixture Substances 0.000 description 8
- 229910000898 sterling silver Inorganic materials 0.000 description 8
- 239000010934 sterling silver Substances 0.000 description 8
- 239000012298 atmosphere Substances 0.000 description 7
- 230000008018 melting Effects 0.000 description 7
- 238000005494 tarnishing Methods 0.000 description 7
- RWSOTUBLDIXVET-UHFFFAOYSA-N Dihydrogen sulfide Chemical compound S RWSOTUBLDIXVET-UHFFFAOYSA-N 0.000 description 6
- 239000003570 air Substances 0.000 description 6
- 238000010438 heat treatment Methods 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 230000001681 protective effect Effects 0.000 description 6
- 230000002829 reductive effect Effects 0.000 description 6
- 238000005096 rolling process Methods 0.000 description 6
- QPLDLSVMHZLSFG-UHFFFAOYSA-N Copper oxide Chemical compound [Cu]=O QPLDLSVMHZLSFG-UHFFFAOYSA-N 0.000 description 5
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 5
- 229910052793 cadmium Inorganic materials 0.000 description 5
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 5
- 239000003795 chemical substances by application Substances 0.000 description 5
- 239000007789 gas Substances 0.000 description 5
- YBMRDBCBODYGJE-UHFFFAOYSA-N germanium dioxide Chemical compound O=[Ge]=O YBMRDBCBODYGJE-UHFFFAOYSA-N 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 4
- 229920000742 Cotton Polymers 0.000 description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- 229910052760 oxygen Inorganic materials 0.000 description 4
- 239000001301 oxygen Substances 0.000 description 4
- 238000012545 processing Methods 0.000 description 4
- 239000003223 protective agent Substances 0.000 description 4
- 238000005476 soldering Methods 0.000 description 4
- 238000009987 spinning Methods 0.000 description 4
- 239000002344 surface layer Substances 0.000 description 4
- 238000003466 welding Methods 0.000 description 4
- UOCLXMDMGBRAIB-UHFFFAOYSA-N 1,1,1-trichloroethane Chemical compound CC(Cl)(Cl)Cl UOCLXMDMGBRAIB-UHFFFAOYSA-N 0.000 description 3
- ZWEHNKRNPOVVGH-UHFFFAOYSA-N 2-Butanone Chemical compound CCC(C)=O ZWEHNKRNPOVVGH-UHFFFAOYSA-N 0.000 description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 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
- NEIHULKJZQTQKJ-UHFFFAOYSA-N [Cu].[Ag] Chemical compound [Cu].[Ag] NEIHULKJZQTQKJ-UHFFFAOYSA-N 0.000 description 3
- 238000009835 boiling Methods 0.000 description 3
- 238000005219 brazing Methods 0.000 description 3
- 238000005336 cracking Methods 0.000 description 3
- 229960004643 cupric oxide Drugs 0.000 description 3
- 230000003247 decreasing effect Effects 0.000 description 3
- 238000011161 development Methods 0.000 description 3
- 238000001704 evaporation Methods 0.000 description 3
- 230000008020 evaporation Effects 0.000 description 3
- 238000005304 joining Methods 0.000 description 3
- 230000007774 longterm Effects 0.000 description 3
- 150000002898 organic sulfur compounds Chemical class 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 238000007665 sagging Methods 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- 239000004094 surface-active agent Substances 0.000 description 3
- 239000008399 tap water Substances 0.000 description 3
- 235000020679 tap water Nutrition 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 239000005751 Copper oxide Substances 0.000 description 2
- KFZMGEQAYNKOFK-UHFFFAOYSA-N Isopropanol Chemical compound CC(C)O KFZMGEQAYNKOFK-UHFFFAOYSA-N 0.000 description 2
- 125000000217 alkyl group Chemical group 0.000 description 2
- 239000012080 ambient air Substances 0.000 description 2
- 239000003945 anionic surfactant Substances 0.000 description 2
- 239000003125 aqueous solvent Substances 0.000 description 2
- 239000010953 base metal Substances 0.000 description 2
- VQLYBLABXAHUDN-UHFFFAOYSA-N bis(4-fluorophenyl)-methyl-(1,2,4-triazol-1-ylmethyl)silane;methyl n-(1h-benzimidazol-2-yl)carbamate Chemical compound C1=CC=C2NC(NC(=O)OC)=NC2=C1.C=1C=C(F)C=CC=1[Si](C=1C=CC(F)=CC=1)(C)CN1C=NC=N1 VQLYBLABXAHUDN-UHFFFAOYSA-N 0.000 description 2
- DKPFZGUDAPQIHT-UHFFFAOYSA-N butyl acetate Chemical compound CCCCOC(C)=O DKPFZGUDAPQIHT-UHFFFAOYSA-N 0.000 description 2
- ZCCIPPOKBCJFDN-UHFFFAOYSA-N calcium nitrate Chemical compound [Ca+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O ZCCIPPOKBCJFDN-UHFFFAOYSA-N 0.000 description 2
- 125000004432 carbon atom Chemical group C* 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 238000009749 continuous casting Methods 0.000 description 2
- 229910000431 copper oxide Inorganic materials 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 150000002019 disulfides Chemical class 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
- 235000019441 ethanol Nutrition 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 239000003517 fume Substances 0.000 description 2
- 150000008282 halocarbons Chemical class 0.000 description 2
- 238000005495 investment casting Methods 0.000 description 2
- 150000002894 organic compounds Chemical class 0.000 description 2
- 238000005554 pickling Methods 0.000 description 2
- XOKSLPVRUOBDEW-UHFFFAOYSA-N pinane of uncertain configuration Natural products CC1CCC2C(C)(C)C1C2 XOKSLPVRUOBDEW-UHFFFAOYSA-N 0.000 description 2
- 230000009993 protective function Effects 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 229910000679 solder Inorganic materials 0.000 description 2
- 238000001179 sorption measurement Methods 0.000 description 2
- 238000010186 staining Methods 0.000 description 2
- 125000004079 stearyl 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])C([H])([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 2
- 239000000126 substance Substances 0.000 description 2
- 150000004763 sulfides Chemical class 0.000 description 2
- 150000003505 terpenes Chemical class 0.000 description 2
- 235000007586 terpenes Nutrition 0.000 description 2
- 150000003573 thiols Chemical class 0.000 description 2
- 238000005406 washing Methods 0.000 description 2
- 238000004383 yellowing Methods 0.000 description 2
- XOKSLPVRUOBDEW-IWSPIJDZSA-N (1r,4r,5r)-4,6,6-trimethylbicyclo[3.1.1]heptane Chemical compound C[C@@H]1CC[C@H]2C(C)(C)[C@@H]1C2 XOKSLPVRUOBDEW-IWSPIJDZSA-N 0.000 description 1
- XOKSLPVRUOBDEW-DJLDLDEBSA-N (1r,4s,5r)-4,6,6-trimethylbicyclo[3.1.1]heptane Chemical compound C[C@H]1CC[C@H]2C(C)(C)[C@@H]1C2 XOKSLPVRUOBDEW-DJLDLDEBSA-N 0.000 description 1
- FRCHKSNAZZFGCA-UHFFFAOYSA-N 1,1-dichloro-1-fluoroethane Chemical compound CC(F)(Cl)Cl FRCHKSNAZZFGCA-UHFFFAOYSA-N 0.000 description 1
- RBACIKXCRWGCBB-UHFFFAOYSA-N 1,2-Epoxybutane Chemical compound CCC1CO1 RBACIKXCRWGCBB-UHFFFAOYSA-N 0.000 description 1
- WNXJIVFYUVYPPR-UHFFFAOYSA-N 1,3-dioxolane Chemical compound C1COCO1 WNXJIVFYUVYPPR-UHFFFAOYSA-N 0.000 description 1
- 229910002699 Ag–S Inorganic materials 0.000 description 1
- 229910017944 Ag—Cu Inorganic materials 0.000 description 1
- 229910000521 B alloy Inorganic materials 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 229910017821 Cu—Ge Inorganic materials 0.000 description 1
- 239000005909 Kieselgur Substances 0.000 description 1
- LSDPWZHWYPCBBB-UHFFFAOYSA-N Methanethiol Chemical compound SC LSDPWZHWYPCBBB-UHFFFAOYSA-N 0.000 description 1
- 206010028980 Neoplasm Diseases 0.000 description 1
- XOJVVFBFDXDTEG-UHFFFAOYSA-N Norphytane Natural products CC(C)CCCC(C)CCCC(C)CCCC(C)C XOJVVFBFDXDTEG-UHFFFAOYSA-N 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 1
- XSTXAVWGXDQKEL-UHFFFAOYSA-N Trichloroethylene Chemical group ClC=C(Cl)Cl XSTXAVWGXDQKEL-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 150000007824 aliphatic compounds Chemical class 0.000 description 1
- 150000004996 alkyl benzenes Chemical class 0.000 description 1
- 150000001356 alkyl thiols Chemical class 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 125000000129 anionic group Chemical group 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 238000003556 assay Methods 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- FZQBLSFKFKIKJI-UHFFFAOYSA-N boron copper Chemical compound [B].[Cu] FZQBLSFKFKIKJI-UHFFFAOYSA-N 0.000 description 1
- 229910000585 britannia silver Inorganic materials 0.000 description 1
- 239000010945 britannia silver Substances 0.000 description 1
- 201000011510 cancer Diseases 0.000 description 1
- 125000002091 cationic group Chemical group 0.000 description 1
- 239000012459 cleaning agent Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- BERDEBHAJNAUOM-UHFFFAOYSA-N copper(I) oxide Inorganic materials [Cu]O[Cu] BERDEBHAJNAUOM-UHFFFAOYSA-N 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- KRFJLUBVMFXRPN-UHFFFAOYSA-N cuprous oxide Chemical compound [O-2].[Cu+].[Cu+] KRFJLUBVMFXRPN-UHFFFAOYSA-N 0.000 description 1
- 229940112669 cuprous oxide Drugs 0.000 description 1
- 238000005238 degreasing Methods 0.000 description 1
- 239000008367 deionised water Substances 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 239000012153 distilled water Substances 0.000 description 1
- 150000002148 esters Chemical class 0.000 description 1
- 230000003203 everyday effect Effects 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 230000007062 hydrolysis Effects 0.000 description 1
- 238000006460 hydrolysis reaction Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 239000003112 inhibitor Substances 0.000 description 1
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 1
- 150000002576 ketones Chemical class 0.000 description 1
- 231100000053 low toxicity Toxicity 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- OKKJLVBELUTLKV-UHFFFAOYSA-N methanol Natural products OC OKKJLVBELUTLKV-UHFFFAOYSA-N 0.000 description 1
- 125000002496 methyl group Chemical group [H]C([H])([H])* 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- LYGJENNIWJXYER-UHFFFAOYSA-N nitromethane Chemical compound C[N+]([O-])=O LYGJENNIWJXYER-UHFFFAOYSA-N 0.000 description 1
- 229910000510 noble metal Inorganic materials 0.000 description 1
- 230000009972 noncorrosive effect Effects 0.000 description 1
- 239000002736 nonionic surfactant Substances 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- PVADDRMAFCOOPC-UHFFFAOYSA-N oxogermanium Chemical compound [Ge]=O PVADDRMAFCOOPC-UHFFFAOYSA-N 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000005077 polysulfide Substances 0.000 description 1
- 150000008117 polysulfides Polymers 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- BDERNNFJNOPAEC-UHFFFAOYSA-N propan-1-ol Chemical compound CCCO BDERNNFJNOPAEC-UHFFFAOYSA-N 0.000 description 1
- 239000011253 protective coating Substances 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 238000000197 pyrolysis Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 239000013545 self-assembled monolayer Substances 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 229910000108 silver(I,III) oxide Inorganic materials 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- PGWMQVQLSMAHHO-UHFFFAOYSA-N sulfanylidenesilver Chemical compound [Ag]=S PGWMQVQLSMAHHO-UHFFFAOYSA-N 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 235000011149 sulphuric acid Nutrition 0.000 description 1
- 239000001117 sulphuric acid Substances 0.000 description 1
- 238000006557 surface reaction Methods 0.000 description 1
- 238000010301 surface-oxidation reaction Methods 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- CWERGRDVMFNCDR-UHFFFAOYSA-M thioglycolate(1-) Chemical compound [O-]C(=O)CS CWERGRDVMFNCDR-UHFFFAOYSA-M 0.000 description 1
- 231100000331 toxic Toxicity 0.000 description 1
- 230000002588 toxic effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- UBOXGVDOUJQMTN-UHFFFAOYSA-N trichloroethylene Natural products ClCC(Cl)Cl UBOXGVDOUJQMTN-UHFFFAOYSA-N 0.000 description 1
- 238000004506 ultrasonic cleaning Methods 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- 238000012795 verification Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C5/00—Alloys based on noble metals
- C22C5/06—Alloys based on silver
-
- 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
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F11/00—Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent
- C23F11/08—Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent in other liquids
- C23F11/10—Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent in other liquids using organic inhibitors
- C23F11/16—Sulfur-containing compounds
-
- 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
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F11/00—Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent
- C23F11/08—Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent in other liquids
- C23F11/10—Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent in other liquids using organic inhibitors
- C23F11/16—Sulfur-containing compounds
- C23F11/161—Mercaptans
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Preventing Corrosion Or Incrustation Of Metals (AREA)
- Cleaning And De-Greasing Of Metallic Materials By Chemical Methods (AREA)
- Manufacture And Refinement Of Metals (AREA)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
- Conductive Materials (AREA)
- Chemical Treatment Of Metals (AREA)
Abstract
A silver alloy containing (by weight): more than 93.5 - 95.5 % silver, 0.5-3 % Ge, with the balance, apart from grain refiner and impurities being copper. The grain refiner may be 1-40 ppm of boron. The surface of the alloy is treated with an alkanethiol, alkyl thioglycollate, dialkyl sulfide or dialkyl disulfide, for example stearyl mercaptan, cetyl mercaptan (octadecyl mercaptan), stearyl thioglycollate or cetyl thioglocollate. The sulphur containing molecule may be dissolved in an organic solvent such as n-propyl bromide, contained in a polish or impregnated into a cloth. Alternatively it may be dissolved in an organic solvent and then adding a relatively concentrated aqueous soap or detergent. The resulting mixture may then be diluted with water.
Description
SILVER TERNARY ALLOY
FIELD OF THE INVENTION
s The present invention relates to a ternary alloy of silver, copper and germanium, to finished or semi-finished shaped articles made from the alloy, and to the use for the surface treatment of the alloy with alkanethiol, alkyl thioglycollate, dialkyl sulfide or dialkyl disulfide.
BACKGROUND TO THE INVENTION
Since ancient times it has been appreciated that unalloyed 'fine' silver is too soft to withstand normal usage, and it has been the practice to add a proportion of a base metal to increase hardness and strength. In the UK, legislation that has existed since the fourteenth century specifies a minimum silver content of articles for sale at 92.5% (the Sterling standard) or 96% (the Britannia standard), but does not specify the base metal constituents. Experience convinced early silversmiths that copper was the most suitable of the metals available to them. Modern silver-sheet manufacturers generally adhere to this composition, although sometimes a proportion of copper is replaced by cadmium to attain even greater ductility. Sterling with a 2.5% cadmium content is permitted to be used in the UK for spinning and stamping, although the use of cadmium is becoming less widespread because when the alloy is in the molten state fumes of cadmium are given off and are toxic. For that reason, a specific alloy composition is produced in continental Europe that contains 93.5 wt% silver. It is sold as a sterling grade alloy with enhanced forming properties for deep drawing or spinning operations. The high silver content reduces the hardness of the alloy, but not to a level where a finished item would be too soft and subject to excessive damage from handling. It therefore can provide a cadmium-free spinning grade, sold to perform similar forming operations to the cadmium-containing silver grades available in the UK.
l Àe A: e.e e. À. e.: The relatively high value assigned to silver compared to the other alloying constituents in the different grades has meant that manufacturers have aimed to produce their alloys as closely as possible to the minimum legal silver content.
This has also resulted in a system in the UK of ensuring that the minimum silver content is assured by means of independent external verification the Assay Office System.
In all but the largest manufacturing companies, most of the annealing and 0 soldering required to assemble finished or semi-finished articles is carried out with the flame of an air-gas blowtorch. The oxidising or reducing nature of the flame and the temperature of the articles are controlled only by the skill of the silversmith. Pure silver allows oxygen to pass easily through it, particularly when the silver is heated to above red heat. Silver does not oxidise in air, but the copper in a silver/copper alloy is oxidised to cuprous or cupric oxide. Pickling of the oxidised surface of the article in hot dilute sulphuric acid removes the superficial but not the deeper seated copper oxide so that the surface consists of fine or unalloyed silver covering a layer of silver/copper oxide mixture. The pure silver is easily permeated during further heating, allowing copper located deeper below the surface to become oxidised. Successive annealing, cold working and pickling produces a surface that exhibits the pure lustre of silver when lightly polished but with heavier polishing reveals dark and disfiguring stains known as 'fire-stain' or fire'. Soldering operations are much more productive of deep fire-stain because of the higher temperatures involved. When the depth of the fire-stain exceeds about 0.025mm (0.010 inches) the alloy is additionally prone to cracking and difficult to solder because an oxide surface is not wetted by solder so that a proper metallurgical bond is not formed.
Secondly, it is a well-known fact that with exposure to everyday atmospheric conditions, silver and silver alloys develop a lustredestroying dark film known as tarnish. : ;. - 3
The addition of germanium to silver alloys was found to offer a solution to both these problems. Patent GB-B-2255348 (Rateau, Albert and Johns; Metaleurop Recherche) disclosed a novel silver alloy that maintained the properties of hardness and lustre inherent in Ag-Cu alloys while reducing problems resulting from the tendency of the copper content to oxidise. The alloys were ternary Ag-Cu-Ge alloys containing at least 92.5 wt% Ag, 0.5-3 wt% Ge and the balance, apart from impurities, copper. The alloys were stated to be stainless in ambient air during conventional production, transformation and finishing operations, to be easily deformable when cold, to be easily brazed and 0 not to give rise to significant shrinkage on casting. They were also stated to exhibit superior ductility and tensile strength and to be annealable to a required hardness. Gemmanium was stated to exert a protective function that was responsible for the advantageous combination of properties exhibited by the new alloys, and was in solid solution in both the silver and the copper phases. The microstructure of the alloy was said to be constituted by two phases, a solid solution of germanium and copper in silver surrounded by a filamentous solid solution of gemmanium and silver and copper. The germanium in the copper-rich phase was said to inhibit surface oxidation of that phase by forming a thin GeO or GeO2 protective coating which prevented the appearance of fire-stain during brazing and flame annealing which results from the oxidation of copper at high temperatures. Furthemmore the development of tarnish was appreciably delayed by the addition of gemmanium, the surface turned slightly yellow rather than black and famish products were easily removed by ordinary tap water. The alloy was said to be useful inter alla in jewellery. However, the alloy disclosed in the above patent suffers limitations insofar as it can exhibit large grain size, leading to poor deformation properties and formation of large pools from low-melting eutectics resulting in localised surface melting when the alloy is subject to the heat of an air torch.
Furthermore, patents US-A-6168071 and EP-B-0729398 (Johns) disclosed a silver/germanium alloy which comprised a silver content of at least 77 wt % and Àe.. A. e: l I I a. ee Àe À À À À . . - 4 - a germanium content of between 0.4 and 7%, the remainder principally being copper apart from any impurities, which alloy contained elemental boron as a grain refiner at a concentration of greater than O ppm and less than 20ppm. The boron content of the alloy could be achieved by providing the boron in a master copper/boron alloy having 2 wt % elemental boron. It was reported that such low concentrations of boron surprisingly provided excellent grain refining in a silver/germanium alloy, imparting greater strength and ductility to the alloy compared with a silver/germanium alloy without boron. The boron in the alloy inhibited grain growth even at temperatures used in the jewellery trade for lo soldering, and samples of the alloy were reported to have resisted pitting even upon heating repeatedly to temperatures where in the previously suggested alloys a briefly mentioned copper/germanium eutectic in the alloy would melt. Strong and aesthetically pleasing joints between separate elements of the alloy could be obtained without using a filler material between the free surfaces of the two elements and a butt or lap joint could be formed by a diffusion process or resistance or laser welding techniques. Compared to a weld in Sterling silver, a weld in the above-described alloy had a much smaller average grain size that improved the formability and ductility of the welds, and an 830 alloy had been welded by laser welding and polished without the need for grinding. It may be noted with regard to the above mentioned eutectic that although its adverse effects are reduced by the reduction in grain size, the ability of the eutectic to form and become molten on post-formation thermal treatment is retained because that is governed by the chemical composition of the alloy rather than its crystal structure.
Silver alloy according to the teaching of GB-B-2255348 and EP-B 0729398 is now commercially available in Europe and in the USA under the trade name Argentium, and the word "Argentium" as used herein refers to these alloys.
The 925 grade Argentium alloy comprises 92.5 wt% (minimum) Ag, 1.1-1.3 wt% Ge, 6 ppm B. the balance being copper and impurities. The alloy shows excellent resistance to tarnishing even under very arduous conditions. A passive layer is À Àe.Àe.. ee: À e. À:- À. À:: À.e À:: À 5 formed by the germanium, which significantly slows the formation of silver sulphide, the main cause of tarnishing on conventional silver alloys. Even in a hydrogen sulphide atmosphere the degree and depth of tarnish is significantly less compared to a conventional silver alloy or a silver plated item. The same mechanism that creates the tarnish resistance also results in the formation of a passive layer which significantly reduces the depth of 'fire-staining' or the 'fire layer' that is produced in this alloy when torch annealing in air. Trials have shown that the depth of the 'fire-staining' to be up to three times greater in conventional silver alloys compared to the Argentium silver alloys. This reduces lo the amount of polishing that the alloy requires and can result in other considerable cost savings in manufacturing.
Despite the advantages of existing Argentium alloy grades, there is a need for further improvement of the alloy with respect to its stability under thermal processing and in particular to its resistance to pitting and/or sagging when heated for the purposes of annealing or joining. There is also a need for alloys that combine these favourable properties with hardness and resistance to tarnishing.
There is a further need for alloys that on investment casting has a reduced propensity to formation of "hot short" (cracking) defects.
As a further matter, so far as long-term tarnish resistance is concerned, various proposals have been made for cleaning or protecting Sterling silver and other known grades of silver to remove tarnish and/or to inhibit the formation of tarnish. GB-A-1130540 is concerned with the protection of a finished surface of Sterling or Britannia silver as a step in a production run, and discloses a process that comprises the steps of: welting a clean silver surface of an article with a solution comprising 99 parts by weight of a volatile organic solvent, for example trichloroethylene or 1,1,1-trichloroethane and from 0.1-1.8 parts by weight of an organic solute containing a -SH group and capable of forming a transparent colourless À À. .. .-. be: Àe À:. À. À:: Àe À:: - 6 protective layer on the silver surface, for example stearyl and cetyl mercaptan or thioglycollate; allowing the solution to react with the surface to form such a layer and allowing the solvent to evaporate; and washing the surface with a detergent solution, rinsing the surface with hot water and allowing it to dry. The above process is stated to provide a "long-term finish" intended to last the intended shelf-life until the article reaches the user.
Treatments of the above kind are believed to result in the formation of a lo self-assembled coating derived from the thiol compounds in which the sulphur atoms are bound onto the metal surface and the alkyl tails are directed away from the metal surface, see US-A-6183815 (Enick). Yousong Kim et al, http://www.electrochem. org/meetings/past/200/abstracts/symposia/hl/1026.pdf reported that the adsorption of thiols onto silver proceeds through an anodic oxidation reaction that produces a shift of the open circuit potential of the substrate metal in the negative direction or if the potential is fixed an anodic current peak: RSH + M(0) RS-M(I) + H+ + e(M) (M = Au or Ag) Kwan Kim, Adsorption and Reaction of Thiols and Sulfides on Noble Metals, Raman SRS-2000, 14-17 August 2000, Xaimen, Fujian, China, http://pcoss. org/icorsxm/paper/knankim.pdf, also discloses the formation of self assembled monolayers and discloses that alkanethiols, dialkyl sulfides and dialkyl disulfides self-assemble on silver surfaces with aliphatic dithiols forming dithoiolates by forming two Ag-S bonds. In contrast, the literature on formation of alkylthiols of germanium is relatively sparse. The reaction of alkanethiols with Ge to form a high quality monolayer has been reported in the context of semiconductor and nanotechnology by Han et al, J. Am. Chem. Soc., 123, 2422 (2001). In the experiment described, a Ge(111) wafer is sonicated in acetone to dissolve organic contaminants and immersed in concentrated HF to remove residual oxide and produce a hydrogen-terminated surface, after which the wafer À:. À: À..e À:e:e - 7 is immersed in an alknaethiol solution in isopropanol, sonicated in propanol and dried.
SUMMARY OF THE INVENTION
Although GB-B-2255348 discloses a range of silver content from Sterling to Britannia grades, as previously explained a skilled person would not contemplate using a silver content above the legal minimum for the intended grade because of the cost of the silver. He is not given by the disclosure of that lo patent or that of the subsequent patents relating to the ternary alloys any incentive to adopt intemmediate silver contents. However, it has now been found that silver copper-gemmanium ternary alloys having silver contents between those of the Sterling and Britannia grades possess valuable properties that facilitate both casting, welding and other themmal treatments used in the manufacture of silver articles.
In particular, the applicants have become aware of the desirability of reducing or avoiding the fommationand/or melting of the above mentioned binary copper-gemmanium eutectic which melts at 554 C. During the production of e.g. 925 Argentium silver alloys, the fommation of this phase can be avoided by careful control of the casting conditions since under equilibrium cooling conditions the crystallization is complete at below 640 C. However, this binary phase can create problems during subsequent themmal treatment of the alloys, e.g. using brazing alloys which typically have melting points in the range 680-750 and torch annealing which typically involves heating a workpiece to a dull red heat at 700 750 C. On heating the workpiece to or beyond these temperatures incipient melting occurs with a small amount of material corresponding to this binary phase becoming molten while the bulk remains stable. When the workpiece returns to ambient temperature, porosity develops where the alloy has liquefied. This contributes brittleness and e.g. as noted in GBB-2255348 there is a tendency for the alloy to sag when heated for joining or annealing operations. Although the use À À. .. .. be: À.e À:- À. À:: -e À:: - 8 - of the boron grain refiner of US-A-6168071 and EP-B-0729398 significantly reduces the pitting and sagging consequent on formation and melting of the binary eutectic, the formation and melting of that eutectic is, as previously mentioned, not elimated and there is still scope for the further development of the ternary alloy to improve its pitting and sagging properties. By increasing the silver content above the level for Sterling but less than that for Britannia it is possible to produce an alloy in which the above binary eutectic either does not form or gives rise to reduced problems in subsequent heat treatment. This provides alloys with a much greater inherent stability under thermal processing.
ID The germanium addition prevents the reduction in hardness that would be seen in a silver-copper alloy of this composition. The alloy also shows resistance to tarnishing, even under very arduous test conditions. i The invention therefore provides a ternary alloy of silver, copper and germanium containing from more than 93.5 wt% to 95.5 wt% Ag, from 0.5 to 3 wt% Ge and the remainder, apart from impurities and grain refiner, copper.
A typical alloy that has been found to be suitable contains about 94.5 wt% Ag, about 4.3 wt% Cu and about 1.2 wt% Ge. In the above alloy the weight ratio I of Cu to Ge is about 3.6: I whereas in the existing 925 grade Argentium the ratio can be from 5.8:1 (1.1 wt% Ge) to 4.8:1 (1.3 wt% Ge). The applicants consider that it is the reduction in the Cu:Ge weight ratio that is responsible for the reduced thermal processing problems, the CuGe eutectic either not forming or forming in a significantly reduced amount during post-melt thermal processing. In particular the ratio is preferably from 4:1 to 3:1, more preferably about 3.5:1. Above 4:1 the alloy is more likely to exhibit firestain, whereas below 3:1 the high germanium content gives rise to formability problems.
In the above alloy, preferred Ag contents range from about 94.0 to about 95.5 wt%, lower values being preferred for reducing the expense of the silver I used. It has been found, surprisingly, that if the Ag content is increased to 96 wt% ' À Àe I. .. e.: À e. it:- Àe À:: Àe À:: - 9 - it is difficult to avoid firestain even at high Ge contents. As regards Ge, contents of from 1.0 to 2.0 wt% are preferred. Below 1.0 wt% Ge, consistent resistance to firestain and tarnish may not be obtained, whereas above 2 wt% Ge there is an increasing risk of embrittlement of the alloy. Furthermore, Ge is expensive and its expense makes it desirable to reduce its content to a minimum. The applicants have found that consistent resistance to firestain and tarnish are obtained at Ge contents of from 1.1 to 1.3 wt%. The alloy will preferably further comprise boron in an amount effective for grain refinement, typically 1- 40 ppm and preferably 5 ppm. Excessive amounts of boron may give rise to boron hard spots, but in the lo case of alloys supplied for casting it will often be desirable to incorporate relatively large amounts of boron to compensate for losses on re-melting.
The alloy may be produced by continuous casting. The initial casting conditions may be as for an equivalent silver-copper grade except that the germanium addition will give solidus and liquidus temperatures approximately 1 5 C lower than the equivalent silver-copper alloys. The germanium content also alters the emissivity of the alloy. This will affect the rate at which heat can be removed from the die (if continuous casting) or standing time (if static casting). It may also be desirable to re- calibrate optical (infra-red) pyrometers when casting the present tertiary alloys. This is because the germanium content gives the alloys a different emissivity. Typically the sensors would give a much lower reading than the actual temperature if they were not adjusted. During billet production from continuously cast slabs it is a requirement to remove the surface layer, which has been in contact with the die. This is the layer that acted as the starting point for solidification of the metal and it contains the most impurities. To remove this layer a minimum of 0.01 mm should be removed from each side of the cast slab by either a mechanical or an abrasive technique.
To produce a sheet with an internal structure suitable for further use by the silversmith a rolling regime which contains a minimum of two 50% reductions and two anneals is recommended. This will remove the 'as-cast' grain structure À À. me.. be: À.i À - Àe.: À.e e: - 10 and prevent any orange peel effects when the sheet is being formed by the silversmith. As an example, to produce sheet at 2.5 mm thick the following would be the minimum rolling requirements: Starting size 10 mm thick Roll to 5.0 mm thick (50% reduction) Anneal Roll to 2.5 mm thick (50% reduction) Anneal When cross-rolling to increase the width of sheets, at the end of the cross- rolling regime the sheet should be annealed prior to the commencement of the normal rolling schedule.
When drawing the alloy into wire, the required drawing sequence depends on the internal grain structure of the starting material. This is because the wire could be from two possible sources, either a cold or warm working operation (e.g. extrusion) or from an 'as-cast' wire size (e.g. a 'mini' casting system). For material that has come from a previous cold worked source the only constraint is that the material has a minimum of 25% cold work prior to each anneal. This will prevent excessive grain growth. A maximum of 60% cold work between each anneal is recommended. For example, the following work procedures would apply to wire from a previously cold worked source: Starting size 6 mm diameter Draw to 5.2 mm diameter (25% reduction) Or Starting size 6 mm diameter Draw to 3.8 mm diameter (60% reduction) Anneal Draw to 2.4 mm diameter (60% reduction) Anneal etc. :..: A. À:e:e - 11 For material that is from a cast source then a drawing sequence involving two reductions of a minimum of 50% and two anneals recommended to give a grain size suitable for further work by the silversmith. Work procedures would be similar to those given above.
When annealing the alloy, it is important that the furnace gas, although protective, does not deplete the surface layer of germanium, as this will reduce the tarnish resistance of the alloy and its resistance to "fire stain". It is the ability 0 of the surface layer of germanium to form a germanium oxide which then acts as a barrier preventing any further penetration of the oxide layer or build up of tarnishing products. For this reason a furnace atmosphere based on cracked ammonia is not recommended. To prevent depletion of the germanium from the surface of the alloy the presence of a small amount of oxygen or a slightly "wet" furnace atmosphere is beneficial. Typically the furnace atmosphere should contain approximately 0.1-0.5% oxygen and have a dew point of 200 C. The exact balance of these values depends on the type of furnace being used. It is important that the balance is not set to far in the opposite direction as this may result in oxidation of the copper content of the alloy. The annealing temperature may be within the range 620 - 650 C and should preferably not exceed a maximum temperature of 650 C. The annealing time for this temperature range is to 45 minutes.
As regards cleaning procedures, although GB-A-1130540 was alleged to provide a long-term finish, in the inventor's experience this type of treatment does not fully solve the difficulties created by tarnish in the period between manufacture and supply to the ultimate purchaser or user and suffers from a number of shortcomings. Although a silver product might arrive at the retailer in an untarnished state, it was largely the result of the wrapping applied by the manufacturer, which protected the article from air. Once the wrapping was removed and the article was displayed in a retail environment such as a display À À. .e.. ee: a. i.. À:. a. À. .: À À . . - 12 - case in a hotel where it was subject to ambient air and the heat of artificial lighting, an article of conventional Sterling silver would require re-polishing after one week and after two weeks would normally be so tarnished as to be un saleable. At an exhibition, the life of an article on display before significant tarnish sets in may be as short as 3-4 days. Re-polishing produces wear and fine handling scratches, so that unless the article can be sold quickly it looses its pristine appearance. The need to polish display silver at frequent intervals adds to the labour cost of a jeweller or other retail establishment, whose management take the view that its staff should be employed to sell products and not to clean stock.
lo Tarnish at point of sale is therefore a serious problem that reduces the willingness of those in the distribution chain to stock and display silver products, and which has not yet been adequately solved.
When the product reaches the ultimate purchaser, it is of course desirable that the task of tarnish removal should be made as infrequent and undemanding as possible.
It has now been found that an alkanethiol, alkyl thioglycollate, dialkyl sulphide or dialkyl disulphide can be used for the surface treatment of the above described alloys, preferably so as to reduce or further reduce tarnishing of the alloy such that a sample can be subjected to hydrogen sulphide gas above a 20% solution of ammonium polysulphide for at least 30 minutes and typically 45-60 minutes while retaining a generally untarnished appearance.
The invention also therefore includes the use of an organic compound containing -SH or-S-S- bonds e.g a C'2-C24 alkanethiol, alkyl thioglycollate, dialkyl sulphide or dialkyl disulphide in the preparation of a tarnish inhibitor for an article of a the silver-copper-germanium alloy described above.
À e. .e.. cc: s e. À:e À. À:: À.. À:: - 13 - The invention further provides an alloy of silver as described above, or a shaped article formed of said alloy, that has been treated with a C-C:.
alkanethiol, alkyl thioglycollate, dialkyl sulphide or dialkyl disulphide.
In an accelerated tarnish test in which the article is subject to hydrogen sulphide gas from the ammonium polysulphide solution above which it is suspended at a height of e.g. 30mm corresponds to a period of a year or more in a retail environment where an article is on display and exposed to ambient atmosphere and may be subject to elevated temperatures. It is the combination of the protective function of the germanium content of the alloy with the further protection from the organo-sulphur compound that is believed to be responsible for the observed increase in tarnish resistance. The period during which the article retains its untarnished appearance under these severe conditions may be three or more times the corresponding period for an article that has not been treated with an organo-sulphur compound, which is unexpected because the same accelerated tarnish test carried out under the same conditions on a conventional Sterling silver article not containing protective germanium does not reveal a significant increase in untarnished lifetime between its untreated and organo-sulfur treated states.
Accelerated tarnishing tests with Argentium Sterling using ammonium polysulphide have been reported by the Society of American Silversmiths, see http://www.silversmithing.com/l argentium4.htm and in a comparative test the Argentium Sterling remained untarnished after one hour whereas conventional Sterling became tarnished after less than 15 minutes.
However, in this test 0.5ml of 20% ammonium polysulfide solution is mixed with 200ml of distilled water, so that the test is greatly less severe than when samples are exposed to the 20% solution itself. In WO 02/095082, samples were suspended above 20% ammonium polysulphide, but the exposure times were relatively short, and onset of yellowing was reported for AgCu-Ge alloys after 3 5 minutes exposure. Other tests reported in that specification involve placing 1. . 14 - samples in a desiccator containing flowers of sulphur and calcium nitrate and are less severe than the ammonium polysulphide test.
As protective agent there may be used a compound containing a long chain alkyl group and a-SH or-S-S- group, e.g. an alkanethiol, dialkyl sulfide or dialkyl disulfides in which the chain is preferably at least 10 carbon atoms long and may be C'2-C24. The -SH or WAS- compounds that many be used include straight chain saturated aliphatic compounds containing 16- 24 carbon atoms in the chain, for example stearyl mercaptan, cetyl mercaptan (octadecyl mercaptan) lo and stearyl and cetyl thioglycollates whose formulae appear below.
HI - - -
HS
SH o
SH
Stearyl mercaptan is a white to pale yellow waxy solid that is insoluble in water. The protective agent may be used in solution in a solvent e.g. a non-polar; organic solvent such as an alcohol e.g. methyl or ethyl alcohol, a ketone e.g. acetone or methyl ethyl ketone, an ether e.g. diethyl ether, an ester e.g. n-butyl acetate, a hydrocarbon, a halocarbon e.g. methylene chloride, 1,1,1 trichloroethane, trichloroethylene, perchloroethylene or HCFC 141b. The I protective agent may comprise 0.1-1 wt% of the solvent. Solvents based on n propyl bromide are presently preferred on the ground of the short atmospheric life i 2s of thatcompound, its relatively low toxicity compared to other halocarbons, its ce. .s: - 15 - favourable chemical and physical properties and its boiling point, specific heat and latent heat of vaporization.
US-A-5616549 discloses a solvent mixture comprising: 90 percent to s about 96.5 percent n-propyl bromide; 0 percent to about 6.5 percent of a mixture of terpenes, the terpene mixture comprising 35 percent to about 50 percent cis pinane and 35 percent to about 50 percent trans-pinane; and 3.5 percent to about 5 percent of a mixture of low boiling solvents, the low boiling solvent mixture comprising 0.5 percent to I percent nitromethane, 0.5 percent to I percent 1,2 butylene oxide and 2.5 percent to 3 percent 1,3-dioxolane. The solvent mixture has the following advantages: (i) it is properly stabilized against any free acid that might result from oxidation of the mixture in the presence of air, from hydrolysis of the mixture in the presence of water, and from pyrolysis of the mixture under the influence of is high temperatures; (ii) it is non-flanmable and non-corrosive; (iii) the various components of the solvent mixture are not regulated by the U.S. Clean Air Act; and (iv) none of the various components of the solvent mixture are known cancer causing agents (i.e., the various components are not listed by N.T. I., I.A.R.C. and California Proposition 65, nor are they regulated by OSHA).
Moreover, the solvent mixture has a high solvency with a kauri-butanol value I above 120 and, more preferably, above 125. In addition, the solvent mixture has an evaporation rate of at least 0.96 where 1,1,1Trichloroethane=l. Upon 2s evaporation, the solvent mixture leaves a non-volatile residue (NVR) of less than 2.5 mg and, more preferably, no residue. Solvents made in accordance with the above patent are available from Enviro-Tech Intemational, Inc of Melrose Park, I Illinois, USA under the trade name EnSolv.
The surface treatment may be carried out after the manufacturing stages for a shaped article made of the alloy have been completed. The article may be of .' ase. cee. e.; .e ce: - 16 - flatware, hollowware or jewellery. Fabrication steps may include spinning, pressing, forging, casting, chasing, hammering from sheet, planishing, joining by soldering brazing or welding, annealing and polishing using buffs/mops and aluminium oxide or rouge. An article to be treated may be de-greased ultrasonically in a treatment bath, dipped into a bath containing the treatment agent e.g. 1 wt% stearyl mercaptan in solvent e. g. EnSolv, rinsed in one or more baths of the solvent and allowed to dry by evaporation. The solvent should leave no or substantially no residue, so that subsequent washing with water or aqueous solvents should be unnecessary and the article can be allowed to dry. The article lo may then be packed for delivery into the distribution chain. This may include wrapping the article in one or more protective sheets, placing it in a presentation box, and wrapping the presentation box in a protective wrapping e.g. of heat shrunk plastics film. Articles which have been treated with an organic compound containing -SH or-S-S- groups as aforesaid and packaged should not only reach their point of sale in good condition but should if displayed e.g. on a shelf or in a cabinet for an extended period, expected to be at least 6 months and possibly 12 months or more, remain without development of significant tarnish.
For many purposes, e.g. light industrial applications, it may be preferred to carry out the anti-tarnish treatment using a predominantly aqueous solvent system. For this purpose, the protective agent may be dissolved in a water immiscible organic solvent, for example a solvent based on n-propyl bromide, the resulting solution may be mixed with a relatively concentrated water-based soap or detergent composition which acts as a "carrier", after which water is added to the resulting mixture to provide an aqueous treatment dip or combined degreasing and treatment solution. Thus an aqueous dip has the advantages that a solvent decreasing system is not necessary, the dip is easily made and may be used cold, all areas of immersed articles can come into contact with the stearyl mercaptan or other treatment agent, the present alloy only requires 2 minutes in the dip, rinsing and drying of articles are made easy as water droplets are repelled from the À Àe.- .. be: Àe À:e Àe À:: Àe À:: surface of the polished salloy, and the dip can be easily used in a manufacturing environment before articles are sent to retailers.
Preferred water-based detergents may be based on anionic, alkoxylated nonionic or water-soluble cationic surface active agents or mixtures of them and preferably have a pH at or close to 7. Anionic surfactants may be based on alkyl sulphates and alkyl benzene sulphonates, whose harshness on prolonged skin exposure may be reduced by the co-presence or use of alkyl ethoxy sulphates (US-A-3793233, Rose et al.; 4024078 Gilbert, 4316824 Pancherni). Other known 0 surfactants e.g. betaines may also be present, see e.g. US-A-4555360 (Bissett). A suitable formulation containing 5-15 wt% non-ionic surfactants and 15-30 wt% anionic surfactants is available commercially in the UK under the trade name Fairy Liquid (Proctor & Gamble).
An aqueous liquid may also be made by dissolving the treatment agent in a non-organic solvent and adding a relatively concentrated aqueous detergent liquid, for example undiluted Fairy Liquid. This provides a detergent liquid that has a number of advantages: the soapy liquid is easily made, the liquid is easily applied to the articles of the present alloy with a damp sponge/cotton wool/cloth etc. the liquid and lather enables the stearyl mercaptan or other treatment agent to get into those awkward areas on an article where a cloth may not be able to reach, rinsing and drying of articles are made easy as water droplets are repelled from the surface of the polished silver, the process can be easily used in a manufacturing environment before articles are sent to retailers and can also be easily used in a retail or domestic environment.
The articles may alternatively simply be polished with a polish containing 1-5wt% of the organo-sulphur compound e.g. stearyl mercaptan together surfactants and a cleaning agent e.g. diatomaceous earth in a solvent. As a further alternative, they may be simply polished with a cloth impregnated with the sogano-sulphur compound e.g. stearyl mercaptan. The advantages of a cleaning À À. A. .. ec: À.e À:e Àe À:: À.. À:: - 18 cloth are that it is easily manufactured, can be easily used in a retail or domestic environment and is good for general upkeep of articles of the present alloy (if required).
The invention will now be further described, by way of illustration only, with reference to the following examples. Throughout the examples, the term "enhanced tarnish resistance" of samples treated with stearyl mercaptan refers to the comparison with samples of Argentium Silver which have not had any treatment except for polishing and cleaning in EnSolv 765.
Example 1
(Production and properties of continuously cast alloy) A ternary silvercopper-germanium alloy (Ag = 94.5 wt%, Ge = 1.2 wt%, Cu = 4.1 wt%, B = 0. 0008 wt% (8 ppm) is prepared by melting silver, copper and germanium together at 1050 C under an atmosphere of nitrogen, and adding the boron as a copper-boron master alloy at the last possible moment. The molten mixture is then continuously cast into strip of width 50mm and of thickness 10 mm, after which an impurity-rich surface layer of at least 0. 1 mm is scalped off the surface of the cast strip by a metal planer. The cast strip is then cold rolled to Smm thickness, annealed at 620-650 C for 30-45 minutes in a slightly wet protective gas atmosphere containing 0.1 -0.5% oxygen and having a dew point of 20-40 C, these conditions being selected to promote formation of GeO2 without oxidizing copper to copper oxides, then subjected to a second rolling to a thickness of 2.5 mm and a second annealing, after which the "as cast" grain structure has been substantially removed and the sheet can be formed by a silversmith without exhibiting objectionable orange- peel effects.
The rolled annealed sheet has a measured hardness of 64 HV which is comparable to values for Sterling silver. A sample of the rolled sheet can be annealed by heating to about 600 C followed by quenching, and the procedure can be repeated six times, after which the sample is in good condition apart from À Àe.e.-. Be: Àe À:. Àe À:: À. À:: - 19 slight edge cracking and exhibits no fire-stain. This behaviour differs from that of normal Sterling silver which tends to crack if quenched from red heat, and also from that of 925 Argentium whose low-melting (554 C) ternary silver-copper germanium eutectic would be liquid at the quenching temperature and would s cause the alloy to shatter when quenched.
Example 2
(Production and properties of investment cast strip) lo The molten alloy of Example 1 is formed into strip by investment casting.
The resulting strip is substantially free of "hot short" defects and brittleness, and has a hardness of 63.5 HV.
Example 3
Solvent dip cleaning (solvent degreased samples) Solutions are made up containing stearyl mercaptan (0.1, 0.5 and 1.0 gram) in EnSolv 765 (100 ml). Samples of the rolled annealed ternary alloy sheet of Example 1 which have been polished and ultrasonically decreased in EnSolv 765 for 2 minutes are each immersed in one of the stearyl mercaptan solutions for periods of 2 minutes, 5 minutes and 15 minutes. The samples are then buffed with clean cotton wool.
In order to evaluate tarnish resistance, the alloy samples are supported on a glass slide in a fume cupboard about 25mm above the surface of 20% ammonium polysulphide solution so as to be exposed to the hydrogen sulphide that arises from that solution. All of the samples demonstrate good tarnish resistance during a one-hour test, with very slight yellowing after 45 minutes exposure to the hydrogen sulphide. The light film on the samples is easily removed with a cleaning cloth impregnated with stearyl mercaptan.
À À. A. .. it: À-e À:. À. À:: À. À:: - 20 By way of comparison, a standard Sterling silver sample starts to discolour as soon as it is subjected to the above test and after one hour had forms a heavy black famish which can not be removed with a cleaning cloth impregnated with stearyl mercaptan.
Example 4
Effect of post-treatment solvent cleaning Example 3 is repeated for the ternary alloy samples except that instead of lo buffmg with cotton wool after the mercaptan treatment, the samples are ultrasonically decreased in EnSolv 765 for 2 minutes. The samples are then famish tested as described in Example 3 and all show enhanced famish resistance.
The ability of the protective effect of the stearyl mercaptan treatment to survive ultrasonic cleaning in EnSolv suggests that the tarnish resistance is achieved by a surface reaction involving the stearyl mercaptan and possibly the germanium in the present alloy, and not by formation of a grease or oil layer on the surface of the present alloy.
Example 5
Aqueous dip application (solvent degreased samples) An anti-famish treatment solution is prepared using the following ingredients: Stearyl mercaptan lg EnSolv 765 5 ml Detergent (Fairy Liquid) 40 ml De-ionised water 100 ml The Stearyl Mercaptan is dissolved into the EnSolv 765 after which the resulting solution is mixed with detergent (Fairy Liquid) and diluted with water to À:e a.: À. ee. À:e:e - 21 provide an aqueous dip. Samples of the ternary alloy of Example I are polished and ultrasonically degreased in EnSolv 765 for 2 minutes, immersed into the above aqueous dip for 2 minutes at ambient temperatures and then rinsed under running tap water It may be noted the water is immediately repelled from the polished surface, which leaves the samples dry. Samples may be tarnish tested as described in Example 3 and all show enhanced tarnish resistance.
Example 6
lo Direct "Sponge" Application - Neat Detergent Solutions (solvent degreased/ aqueous degreased samples) The following solutions are prepared: - I gram stearyl mercaptan - 5 ml EnSolv 765 - 40ml detergent (Fairy Liquid) (Preferred quantities) - 1 gram stearyl mercaptan - 5 ml EnSolv 765 - 40ml soap (liquid hand soap) The stearyl mercaptan is initially dissolved into the EnSolv. The detergent l is then mixed into the solutions. Samples of the rolled annealed alloy of Example 1 are polished and ultrasonically degreased in EnSolv 765 for 2 minutes. The ' stearyl mercaptan/EnSolv/detergent solutions are then directly applied to the surface of the samples using damp cotton wool and massaged into lather. The 2s samples are then rinsed under running tap water. In each case, it is noted that water is repelled off of the polished surface, leaving the samples dry. Samples are tarnish tested as in Example 3 by being exposed to neat ammonium polysulphide solution over a period of 1 hour. They all show enhanced tarnish resistance. The above direct "sponging" method for applying the Stearyl Mercaptan is tested on ternary alloy strip samples degreased in a 2% Fairy Liquid aqueous solution. l Enhanced tarnish resistance is again achieved. '
Claims (19)
1. A ternary alloy of silver, copper and germanium containing from more than 93.5 wt% to 95.5 wt% Ag, from 0.5 to 3 wt% Ge and the remainder, apart from impurities and grain refiner, copper.
2. The alloy of claim 1, wherein the weight ratio of Cu to Ge is from 4:1 to 3:1.
lo
3. The alloy of claim 2, wherein the weight ratio of Cu to Ge is about 3.5:1.
4. The alloy of any preceding claim, containing from 1.0 to 1.5 wt% Ge.
5. The alloy of claim 4, containing about 94.5 wt% Ag, about 4.3 wt% Cu l and about 1.2 wt% Ge.
6. The alloy of any preceding claim, further comprising boron in an amount i effective for grain refinement.
7. The alloy of any preceding claim, containing 1-40 ppm of boron. l
8. The alloy of any preceding claim, containing 5-20 ppm of boron.
9. A finished or semi-finished shaped article of the alloy of any preceding claim.
10. The article of claim 9, which is formed by casting.
The article of claim 9, which is at least partly produced from sheet or strip.
i i i.: e.e is.- À i:e - 23 -
12. Use of an alkanethiol, alkyl thioglycollate, dialkyl sulfide or dialkyl disulfide for the surface treatment of an alloy according to any of claims 1-8.
13. The use of claim 12, wherein the alkanethiol, alkyl thioglycollate, dialkyl sulfide or dialkyl disulfide has C2-C24 alkyl groups.
14. The use of claim 12 or 13, wherein the alkanethiol, alkyl thioglycollate, I dialkyl sulfide or dialkyl disulfide is in an organic solvent.
lo
15. The use of claim 14, wherein the solvent containing the alkanethiol, alkyl thioglycollate, dialkyl sulfide or dialkyl disulfide is generally neutral.
16. The use of claim 14 or 15, wherein the alkanethiol, alkyl thioglycollate, dialkyl sulfide or dialkyl disulfide is in a solvent based on n-propyl bromide.
17. The use of claim 12 or 13, wherein the alkanethiol, alkyl thioglycollate, dialkyl sulfide or dialkyl disulfide is in (a) a composition obtainable by dissolving said alkanethiol, alkyl thioglycollate, dialkyl sulfide or dialkyl disulfide in an organic solvent and adding to said solution a relatively concentrated aqueous soap or detergent, or (b) an aqueous dispersion obtainable by dissolving said alkanethiol, alkyl thioglycollate, dialkyl sulfide or dialkyl disulfide in an organic solvent, adding to said solution a relatively concentrated aqueous soap or detergent, and diluting the resulting mixture with water.
18. The use of claim 12 or 13, wherein the alkanethiol, alkyl thioglycollate, dialkyl sulfide or dialkyl disulfide is contained in a polish or impregnated into a polishing cloth.
19. The use of any of claims 12-18, wherein the alkanethiol or alkylthioglycolate is selected from stearyl mercaptan, cetyl mercaptan (octadecyl mercaptan), stearyl thioglycollate and cetyl thioglycollate.
Priority Applications (15)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0312693A GB2402399B (en) | 2003-06-03 | 2003-06-03 | Silver ternary alloy |
PCT/GB2004/002317 WO2004106567A1 (en) | 2003-06-03 | 2004-06-01 | Silver ternary alloy |
CN201210188563.9A CN102690969B (en) | 2003-06-03 | 2004-06-01 | The alloy of the method for alloying and silver, copper and germanium |
AU2004243654A AU2004243654A1 (en) | 2003-06-03 | 2004-06-01 | Silver ternary alloy |
AT04735594T ATE420980T1 (en) | 2003-06-03 | 2004-06-01 | SILVER TERNARY ALLOY |
CA002527430A CA2527430A1 (en) | 2003-06-03 | 2004-06-01 | Silver ternary alloy |
CNA2004800154108A CN1846007A (en) | 2003-06-03 | 2004-06-01 | Silver ternary alloy |
EP04735594A EP1631692B1 (en) | 2003-06-03 | 2004-06-01 | Silver ternary alloy |
PT04735594T PT1631692E (en) | 2003-06-03 | 2004-06-01 | Silver ternary alloy |
JP2006508380A JP2007535616A (en) | 2003-06-03 | 2004-06-01 | Silver ternary alloy |
DE602004019080T DE602004019080D1 (en) | 2003-06-03 | 2004-06-01 | SILBERTERNÄRLEGIERUNG |
ES04735594T ES2322465T3 (en) | 2003-06-03 | 2004-06-01 | SILVER TERNARY ALLOY. |
EA200501875A EA011015B1 (en) | 2003-06-03 | 2004-06-01 | Silver ternary alloy |
US10/559,092 US20070009375A1 (en) | 2003-06-03 | 2004-06-01 | Silver ternary alloy |
US12/766,312 US20100239454A1 (en) | 2003-06-03 | 2010-04-23 | Silver ternary alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0312693A GB2402399B (en) | 2003-06-03 | 2003-06-03 | Silver ternary alloy |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0312693D0 GB0312693D0 (en) | 2003-07-09 |
GB2402399A true GB2402399A (en) | 2004-12-08 |
GB2402399B GB2402399B (en) | 2005-10-12 |
Family
ID=9959219
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0312693A Expired - Fee Related GB2402399B (en) | 2003-06-03 | 2003-06-03 | Silver ternary alloy |
Country Status (13)
Country | Link |
---|---|
US (1) | US20070009375A1 (en) |
EP (1) | EP1631692B1 (en) |
JP (1) | JP2007535616A (en) |
CN (2) | CN102690969B (en) |
AT (1) | ATE420980T1 (en) |
AU (1) | AU2004243654A1 (en) |
CA (1) | CA2527430A1 (en) |
DE (1) | DE602004019080D1 (en) |
EA (1) | EA011015B1 (en) |
ES (1) | ES2322465T3 (en) |
GB (1) | GB2402399B (en) |
PT (1) | PT1631692E (en) |
WO (1) | WO2004106567A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2428045A (en) * | 2005-07-07 | 2007-01-17 | Middlesex Silver Co Ltd | Silver-copper-germanium alloy |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2412666B (en) * | 2004-03-30 | 2008-10-08 | Paul Gilbert Cole | Water-based metal treatment composition |
GB2485374B (en) | 2010-11-11 | 2013-07-24 | Argentium Internat Ltd | Alloy for investment casting |
US9222150B2 (en) | 2004-06-02 | 2015-12-29 | Peter Gamon Johns | Process for making finished or semi-finished articles of silver alloy |
GB2426250A (en) * | 2005-05-20 | 2006-11-22 | Middlesex Silver Co Ltd | Silver alloys |
EP1888797A1 (en) * | 2005-05-20 | 2008-02-20 | Middlesex Silver Co. Limited | Silver-copper-germanium alloy manufacturing |
GB0517166D0 (en) * | 2005-08-23 | 2005-09-28 | Middlesex Silver Co Ltd | Silver wire |
IT1398698B1 (en) * | 2010-02-24 | 2013-03-08 | Mesa S A S Di Malimpensa Simona E Davide E C | METHOD FOR THE PROTECTION OF SILVER SURFACES AND ITS UNDERSTANDING ALLOYS. |
GB2561376A (en) * | 2017-04-12 | 2018-10-17 | Argentium International Ltd | Silver alloys, investment casting using the alloys and casting grain |
CN111910524A (en) * | 2020-08-19 | 2020-11-10 | 山东鼎鲁建筑有限公司 | Supporting equipment for bridge engineering construction |
DE102022106410A1 (en) | 2022-03-18 | 2023-09-21 | Leonhard Kurz Stiftung & Co. Kg | Multilayer body, method for producing a multilayer body, use of a multilayer body and use of a heat application device |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2841501A (en) * | 1957-04-17 | 1958-07-01 | James G Murphy | Silver polish |
GB1130540A (en) * | 1966-02-18 | 1968-10-16 | Goddard & Sons Ltd J | Protecting silver against tarnish |
GB1217414A (en) * | 1968-06-29 | 1970-12-31 | Goddard & Sons Ltd J | Long term silver dip |
GB2255348A (en) * | 1991-04-29 | 1992-11-04 | Metaleurop Rech | Novel silver-based ternary alloy |
GB2283933A (en) * | 1993-11-18 | 1995-05-24 | Peter Gamon Johns | A method of joining materials together by a diffusion process using silver/germanium alloys |
US5972131A (en) * | 1992-03-25 | 1999-10-26 | Tanaka Kikinzoku Kogyo K.K. | Ag-Cu alloy for a sliding contact |
US6168071B1 (en) * | 1994-11-17 | 2001-01-02 | Peter Gamon Johns | Method for joining materials together by a diffusion process using silver/germanium alloys and a silver/germanium alloy for use in the method |
WO2002095082A2 (en) * | 2001-05-23 | 2002-11-28 | Peter Gamon Johns | Method of producing silver-copper alloys |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0617167A (en) * | 1992-06-30 | 1994-01-25 | Ishifuku Metal Ind Co Ltd | High hardness and high corrosion resistant silver alloy |
WO1995014112A1 (en) * | 1993-11-15 | 1995-05-26 | Apecs Investment Castings Pty. Ltd. | Silver alloy compositions |
US6183815B1 (en) * | 1994-04-01 | 2001-02-06 | University Of Pittsburgh | Method and composition for surface treatment of metals |
US5616549A (en) * | 1995-12-29 | 1997-04-01 | Clark; Lawrence A. | Molecular level cleaning of contaminates from parts utilizing an envronmentally safe solvent |
GB9926313D0 (en) * | 1999-11-05 | 2000-01-12 | Johns Peter G | A silver/copper/germanium alloy composition |
-
2003
- 2003-06-03 GB GB0312693A patent/GB2402399B/en not_active Expired - Fee Related
-
2004
- 2004-06-01 CN CN201210188563.9A patent/CN102690969B/en not_active Expired - Fee Related
- 2004-06-01 DE DE602004019080T patent/DE602004019080D1/en not_active Expired - Lifetime
- 2004-06-01 ES ES04735594T patent/ES2322465T3/en not_active Expired - Lifetime
- 2004-06-01 CA CA002527430A patent/CA2527430A1/en not_active Abandoned
- 2004-06-01 JP JP2006508380A patent/JP2007535616A/en not_active Withdrawn
- 2004-06-01 WO PCT/GB2004/002317 patent/WO2004106567A1/en active Application Filing
- 2004-06-01 US US10/559,092 patent/US20070009375A1/en not_active Abandoned
- 2004-06-01 PT PT04735594T patent/PT1631692E/en unknown
- 2004-06-01 EP EP04735594A patent/EP1631692B1/en not_active Expired - Lifetime
- 2004-06-01 EA EA200501875A patent/EA011015B1/en not_active IP Right Cessation
- 2004-06-01 AU AU2004243654A patent/AU2004243654A1/en not_active Abandoned
- 2004-06-01 AT AT04735594T patent/ATE420980T1/en not_active IP Right Cessation
- 2004-06-01 CN CNA2004800154108A patent/CN1846007A/en active Pending
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2841501A (en) * | 1957-04-17 | 1958-07-01 | James G Murphy | Silver polish |
GB1130540A (en) * | 1966-02-18 | 1968-10-16 | Goddard & Sons Ltd J | Protecting silver against tarnish |
GB1217414A (en) * | 1968-06-29 | 1970-12-31 | Goddard & Sons Ltd J | Long term silver dip |
GB2255348A (en) * | 1991-04-29 | 1992-11-04 | Metaleurop Rech | Novel silver-based ternary alloy |
US5972131A (en) * | 1992-03-25 | 1999-10-26 | Tanaka Kikinzoku Kogyo K.K. | Ag-Cu alloy for a sliding contact |
GB2283933A (en) * | 1993-11-18 | 1995-05-24 | Peter Gamon Johns | A method of joining materials together by a diffusion process using silver/germanium alloys |
US6168071B1 (en) * | 1994-11-17 | 2001-01-02 | Peter Gamon Johns | Method for joining materials together by a diffusion process using silver/germanium alloys and a silver/germanium alloy for use in the method |
WO2002095082A2 (en) * | 2001-05-23 | 2002-11-28 | Peter Gamon Johns | Method of producing silver-copper alloys |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2428045A (en) * | 2005-07-07 | 2007-01-17 | Middlesex Silver Co Ltd | Silver-copper-germanium alloy |
Also Published As
Publication number | Publication date |
---|---|
CA2527430A1 (en) | 2004-12-09 |
PT1631692E (en) | 2009-04-16 |
CN102690969B (en) | 2016-05-04 |
DE602004019080D1 (en) | 2009-03-05 |
GB0312693D0 (en) | 2003-07-09 |
EP1631692A1 (en) | 2006-03-08 |
US20070009375A1 (en) | 2007-01-11 |
ES2322465T3 (en) | 2009-06-22 |
CN1846007A (en) | 2006-10-11 |
WO2004106567A1 (en) | 2004-12-09 |
CN102690969A (en) | 2012-09-26 |
GB2402399B (en) | 2005-10-12 |
EP1631692B1 (en) | 2009-01-14 |
JP2007535616A (en) | 2007-12-06 |
EA011015B1 (en) | 2008-12-30 |
ATE420980T1 (en) | 2009-01-15 |
AU2004243654A1 (en) | 2004-12-09 |
EA200501875A1 (en) | 2006-06-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1631692B1 (en) | Silver ternary alloy | |
US20070039665A1 (en) | Enhancing silver tarnish-resistance | |
US20100239454A1 (en) | Silver ternary alloy | |
US20070277906A1 (en) | Water-Based Metal Treatment Composition | |
ES2318490T3 (en) | PROCEDURE FOR THE PRODUCTION OF FINISHED OR SEMI-FINISHED ITEMS BASED ON SILVER ALLOY BASED ON COPPER AND GERMANIUM. | |
US20080069722A1 (en) | Metal alloy manufacturing | |
WO2006123190A1 (en) | Silver-copper-germanium alloy manufacturing | |
MXPA05012991A (en) | Silver ternary alloy | |
JP3221179B2 (en) | High hardness wire drawn wire for gold ornaments with excellent hardness stability | |
WO2007007121A1 (en) | Silver alloy | |
GB2414739A (en) | Process for making finished or semi-finished articles of silver alloy | |
JP2007534836A (en) | Silver chain manufacture | |
FR2791363A1 (en) | Sulfidation-resistant, pink silver-copper alloys for decorative articles contain palladium and optionally indium or contain gold | |
MXPA06010964A (en) | Water-based metal treatment composition | |
JPS62130245A (en) | Silver material for ornament | |
JPS616221A (en) | Silver material for accessory |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
COOA | Change in applicant's name or ownership of the application |
Owner name: MIDDLESEX SILVER CO. LIMITED Free format text: FORMER APPLICANT(S): COLE, PAUL G |
|
732E | Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977) |
Free format text: REGISTERED BETWEEN 20090219 AND 20090225 |
|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20220603 |