MX2007005565A - Fabric structure comprising silver-germanium-copper alloy - Google Patents
Fabric structure comprising silver-germanium-copper alloyInfo
- Publication number
- MX2007005565A MX2007005565A MXMX/A/2007/005565A MX2007005565A MX2007005565A MX 2007005565 A MX2007005565 A MX 2007005565A MX 2007005565 A MX2007005565 A MX 2007005565A MX 2007005565 A MX2007005565 A MX 2007005565A
- Authority
- MX
- Mexico
- Prior art keywords
- alloy
- silver
- structure according
- wire
- weight
- Prior art date
Links
- 239000004744 fabric Substances 0.000 title claims abstract description 17
- 229910000881 Cu alloy Inorganic materials 0.000 title claims description 7
- -1 silver-germanium-copper Chemical compound 0.000 title description 7
- 229910052709 silver Inorganic materials 0.000 claims abstract description 53
- BQCADISMDOOEFD-UHFFFAOYSA-N silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 claims abstract description 53
- 239000004332 silver Substances 0.000 claims abstract description 53
- 229910001316 Ag alloy Inorganic materials 0.000 claims abstract description 34
- 238000000034 method Methods 0.000 claims abstract description 17
- 229910000927 Ge alloy Inorganic materials 0.000 claims abstract description 11
- 238000001556 precipitation Methods 0.000 claims abstract description 11
- 238000010438 heat treatment Methods 0.000 claims abstract description 9
- 229910045601 alloy Inorganic materials 0.000 claims description 73
- 239000000956 alloy Substances 0.000 claims description 73
- REDXJYDRNCIFBQ-UHFFFAOYSA-N aluminium(3+) Chemical class [Al+3] REDXJYDRNCIFBQ-UHFFFAOYSA-N 0.000 claims description 51
- 229910052796 boron Inorganic materials 0.000 claims description 41
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 40
- 239000010949 copper Substances 0.000 claims description 27
- RYGMFSIKBFXOCR-UHFFFAOYSA-N copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 21
- 229910052802 copper Inorganic materials 0.000 claims description 21
- 230000015572 biosynthetic process Effects 0.000 claims description 20
- 238000005755 formation reaction Methods 0.000 claims description 20
- GNPVGFCGXDBREM-UHFFFAOYSA-N germanium Chemical compound [Ge] GNPVGFCGXDBREM-UHFFFAOYSA-N 0.000 claims description 20
- 229910052732 germanium Inorganic materials 0.000 claims description 20
- 150000001639 boron compounds Chemical class 0.000 claims description 16
- 238000009940 knitting Methods 0.000 claims description 16
- 238000004519 manufacturing process Methods 0.000 claims description 15
- 239000011701 zinc Substances 0.000 claims description 14
- 239000012535 impurity Substances 0.000 claims description 8
- 239000010410 layer Substances 0.000 claims description 6
- 238000009941 weaving Methods 0.000 claims description 5
- HCHKCACWOHOZIP-UHFFFAOYSA-N zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 5
- 229910052725 zinc Inorganic materials 0.000 claims description 5
- 239000002356 single layer Substances 0.000 claims description 4
- YOQDYZUWIQVZSF-UHFFFAOYSA-N sodium borohydride Substances [BH4-].[Na+] YOQDYZUWIQVZSF-UHFFFAOYSA-N 0.000 claims description 4
- 229910000033 sodium borohydride Inorganic materials 0.000 claims description 3
- 238000010348 incorporation Methods 0.000 claims description 2
- ODGROJYWQXFQOZ-UHFFFAOYSA-N sodium;boron(1-) Chemical compound [B-].[Na+] ODGROJYWQXFQOZ-UHFFFAOYSA-N 0.000 claims description 2
- 239000012298 atmosphere Substances 0.000 description 23
- 229910052751 metal Inorganic materials 0.000 description 22
- 239000002184 metal Substances 0.000 description 22
- 238000000137 annealing Methods 0.000 description 20
- IJGRMHOSHXDMSA-UHFFFAOYSA-N nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 20
- 239000000835 fiber Substances 0.000 description 18
- 239000007789 gas Substances 0.000 description 12
- 239000001257 hydrogen Substances 0.000 description 12
- 229910052739 hydrogen Inorganic materials 0.000 description 12
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 11
- 229910052757 nitrogen Inorganic materials 0.000 description 10
- 230000001590 oxidative Effects 0.000 description 10
- 239000000463 material Substances 0.000 description 9
- 239000012159 carrier gas Substances 0.000 description 8
- 239000010934 sterling silver Substances 0.000 description 8
- 229910000898 sterling silver Inorganic materials 0.000 description 8
- 238000001816 cooling Methods 0.000 description 7
- 150000002431 hydrogen Chemical class 0.000 description 7
- 239000000203 mixture Substances 0.000 description 7
- 239000007787 solid Substances 0.000 description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 7
- UORVGPXVDQYIDP-UHFFFAOYSA-N Borane Chemical class B UORVGPXVDQYIDP-UHFFFAOYSA-N 0.000 description 6
- 239000007788 liquid Substances 0.000 description 6
- 150000002739 metals Chemical class 0.000 description 6
- 239000012071 phase Substances 0.000 description 6
- 229910052697 platinum Inorganic materials 0.000 description 6
- 230000002829 reduced Effects 0.000 description 6
- 239000010944 silver (metal) Substances 0.000 description 6
- 229910001118 argentium sterling silver Inorganic materials 0.000 description 5
- YBMRDBCBODYGJE-UHFFFAOYSA-N germanium dioxide Inorganic materials O=[Ge]=O YBMRDBCBODYGJE-UHFFFAOYSA-N 0.000 description 5
- KDLHZDBZIXYQEI-UHFFFAOYSA-N palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 5
- 238000007792 addition Methods 0.000 description 4
- XKRFYHLGVUSROY-UHFFFAOYSA-N argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- 239000002775 capsule Substances 0.000 description 4
- 239000003054 catalyst Substances 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 4
- 238000001914 filtration Methods 0.000 description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 4
- 239000011261 inert gas Substances 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 239000006104 solid solution Substances 0.000 description 4
- 230000000576 supplementary Effects 0.000 description 4
- 229910000521 B alloy Inorganic materials 0.000 description 3
- 229910017821 Cu—Ge Inorganic materials 0.000 description 3
- 240000006133 Fittonia albivenis Species 0.000 description 3
- 229910000085 borane Inorganic materials 0.000 description 3
- 229910000090 borane Inorganic materials 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 238000009749 continuous casting Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical group [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 3
- 229910052737 gold Inorganic materials 0.000 description 3
- 239000010931 gold Substances 0.000 description 3
- 229910002804 graphite Inorganic materials 0.000 description 3
- 239000010439 graphite Substances 0.000 description 3
- 239000000314 lubricant Substances 0.000 description 3
- 229910052987 metal hydride Inorganic materials 0.000 description 3
- 150000004681 metal hydrides Chemical class 0.000 description 3
- 229910052763 palladium Inorganic materials 0.000 description 3
- 230000001681 protective Effects 0.000 description 3
- 238000003756 stirring Methods 0.000 description 3
- 229910017944 Ag—Cu Inorganic materials 0.000 description 2
- WTEOIRVLGSZEPR-UHFFFAOYSA-N Boron trifluoride Chemical compound FB(F)F WTEOIRVLGSZEPR-UHFFFAOYSA-N 0.000 description 2
- 229910001260 Pt alloy Inorganic materials 0.000 description 2
- 229920002472 Starch Polymers 0.000 description 2
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 2
- 239000000443 aerosol Substances 0.000 description 2
- QGZKDVFQNNGYKY-UHFFFAOYSA-N ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- 230000000844 anti-bacterial Effects 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 229910002092 carbon dioxide Inorganic materials 0.000 description 2
- 239000001569 carbon dioxide Substances 0.000 description 2
- UGFAIRIUMAVXCW-UHFFFAOYSA-N carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 2
- 229910002091 carbon monoxide Inorganic materials 0.000 description 2
- 229910052803 cobalt Inorganic materials 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 238000000354 decomposition reaction Methods 0.000 description 2
- DMJZZSLVPSMWCS-UHFFFAOYSA-N diborane Chemical compound B1[H]B[H]1 DMJZZSLVPSMWCS-UHFFFAOYSA-N 0.000 description 2
- VLKZOEOYAKHREP-UHFFFAOYSA-N hexane Chemical compound CCCCCC VLKZOEOYAKHREP-UHFFFAOYSA-N 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 239000011133 lead Substances 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 238000005461 lubrication Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 229910001512 metal fluoride Inorganic materials 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N oxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 239000010970 precious metal Substances 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 238000004881 precipitation hardening Methods 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 239000011253 protective coating Substances 0.000 description 2
- 238000007670 refining Methods 0.000 description 2
- 239000011819 refractory material Substances 0.000 description 2
- KEAYESYHFKHZAL-UHFFFAOYSA-N sodium Chemical compound [Na] KEAYESYHFKHZAL-UHFFFAOYSA-N 0.000 description 2
- 229910052708 sodium Inorganic materials 0.000 description 2
- 239000011734 sodium Substances 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 235000019698 starch Nutrition 0.000 description 2
- 239000008107 starch Substances 0.000 description 2
- PPBRXRYQALVLMV-UHFFFAOYSA-N styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 2
- 238000005494 tarnishing Methods 0.000 description 2
- WYURNTSHIVDZCO-UHFFFAOYSA-N tetrahydrofuran Chemical compound C1CCOC1 WYURNTSHIVDZCO-UHFFFAOYSA-N 0.000 description 2
- 239000004753 textile Substances 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N tin hydride Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- 239000002759 woven fabric Substances 0.000 description 2
- 229910001020 Au alloy Inorganic materials 0.000 description 1
- 229920000742 Cotton Polymers 0.000 description 1
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 230000036499 Half live Effects 0.000 description 1
- 210000001503 Joints Anatomy 0.000 description 1
- 229920000914 Metallic fiber Polymers 0.000 description 1
- 229910001252 Pd alloy Inorganic materials 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 239000005092 Ruthenium Substances 0.000 description 1
- LALRXNPLTWZJIJ-UHFFFAOYSA-N Triethylborane Chemical compound CCB(CC)CC LALRXNPLTWZJIJ-UHFFFAOYSA-N 0.000 description 1
- 229910052769 Ytterbium Inorganic materials 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 1
- 229940072056 alginate Drugs 0.000 description 1
- 229920000615 alginic acid Polymers 0.000 description 1
- 235000010443 alginic acid Nutrition 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000003712 anti-aging Effects 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- 230000001580 bacterial Effects 0.000 description 1
- 229910052788 barium Inorganic materials 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- 229910002056 binary alloy Inorganic materials 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- CROBTXVXNQNKKO-UHFFFAOYSA-N borohydride Chemical compound [BH4-] CROBTXVXNQNKKO-UHFFFAOYSA-N 0.000 description 1
- 238000009954 braiding Methods 0.000 description 1
- 230000005587 bubbling Effects 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000003197 catalytic Effects 0.000 description 1
- 238000006555 catalytic reaction Methods 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 238000004320 controlled atmosphere Methods 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 239000011889 copper foil Substances 0.000 description 1
- QPLDLSVMHZLSFG-UHFFFAOYSA-N copper oxide Chemical class [Cu]=O QPLDLSVMHZLSFG-UHFFFAOYSA-N 0.000 description 1
- 230000003111 delayed Effects 0.000 description 1
- 230000001809 detectable Effects 0.000 description 1
- 230000001627 detrimental Effects 0.000 description 1
- FESAXEDIWWXCNG-UHFFFAOYSA-N diethyl(methoxy)borane Chemical compound CCB(CC)OC FESAXEDIWWXCNG-UHFFFAOYSA-N 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 238000000635 electron micrograph Methods 0.000 description 1
- 230000001747 exhibiting Effects 0.000 description 1
- 230000002349 favourable Effects 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 239000010946 fine silver Substances 0.000 description 1
- 239000008246 gaseous mixture Substances 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- PVADDRMAFCOOPC-UHFFFAOYSA-N germanium monoxide Inorganic materials [Ge]=O PVADDRMAFCOOPC-UHFFFAOYSA-N 0.000 description 1
- 229910000447 germanium oxide Inorganic materials 0.000 description 1
- 150000004820 halides Chemical class 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium(0) Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 239000008079 hexane Substances 0.000 description 1
- 125000004435 hydrogen atoms Chemical group [H]* 0.000 description 1
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 1
- 229910052738 indium Inorganic materials 0.000 description 1
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 1
- 229910052741 iridium Inorganic materials 0.000 description 1
- 229910052745 lead Inorganic materials 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 239000002932 luster Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 229910001507 metal halide Inorganic materials 0.000 description 1
- 150000005309 metal halides Chemical class 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000010417 needlework Methods 0.000 description 1
- GRYLNZFGIOXLOG-UHFFFAOYSA-N nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 1
- QJGQUHMNIGDVPM-UHFFFAOYSA-N nitrogen group Chemical group [N] QJGQUHMNIGDVPM-UHFFFAOYSA-N 0.000 description 1
- 229910000510 noble metal Inorganic materials 0.000 description 1
- 239000003960 organic solvent Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000035699 permeability Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920002451 polyvinyl alcohol Polymers 0.000 description 1
- 235000019422 polyvinyl alcohol Nutrition 0.000 description 1
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 1
- 239000011591 potassium Substances 0.000 description 1
- 229910052700 potassium Inorganic materials 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000000197 pyrolysis Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 239000003638 reducing agent Substances 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 description 1
- 239000010948 rhodium Substances 0.000 description 1
- 229910052703 rhodium Inorganic materials 0.000 description 1
- KJTLSVCANCCWHF-UHFFFAOYSA-N ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 description 1
- 229910052707 ruthenium Inorganic materials 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- 239000011265 semifinished product Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000007790 solid phase Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000010301 surface-oxidation reaction Methods 0.000 description 1
- 239000008399 tap water Substances 0.000 description 1
- 235000020679 tap water Nutrition 0.000 description 1
- 229910002058 ternary alloy Inorganic materials 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 230000001131 transforming Effects 0.000 description 1
- ZMPKTELQGVLZTD-UHFFFAOYSA-N tripropylborane Chemical compound CCCB(CCC)CCC ZMPKTELQGVLZTD-UHFFFAOYSA-N 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- 229920002554 vinyl polymer Polymers 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Abstract
A woven, braided or knitted fabric structure comprises wires of silver alloy, preferably a precipitation-hardenable Ag Cu Ge alloy. The process for making a fabric structure may comprise providing silver wire having a temper of more than fully soft but less than half hardness, forming said wire into said structure and heating the structure to precipitation harden the wire.
Description
WOVEN STRUCTURE COMPRISING AN ALLOY OF SILVER-GERMANIUM-COPPER Field of the Invention This invention relates to woven structures based on silver threads, which may comprise all or part of the structures. Background of the Invention The literature on the production of silver threads is relatively scarce. For example, patent US 6627149 (Tayama et al.) Describes the production of silver wire of a relatively large diameter and of high purity for use in recording or image transmission applications. The literature that refers to the silver-based woven structures is also scarce. Such woven structures have been based mainly on braided strips, cords or filaments together, see, US-A-240096 (Crane), US-A-253587 (Crane) and US-A-5203182 (Wiriath). However, US-A-2708788 (Cassman et al) discloses a mesh or sheet of silver through which the material will be evaporated during the manufacture of television tubes, the mesh is stiffened by the deposition of gold over the same and by the alloy of silver and gold to cause shrinkage of the mesh. US-A-5122185 (Hochella) discloses a precious metal mesh used as the so-called "vacuum tuners" in the recovery of platinum from Ref. 182126 from a gas stream from the oxidation of ammonia. The mesh is preferably pure palladium, but may also be a palladium alloy with one or more metals selected from nickel, cobalt, platinum, ruthenium, iridium, gold, silver and copper. Knitting by wire or metal fiber stitches is already known, for example, as in US-A-2274684 (Goodloe), but the existing knitted, metallic knits are predominantly ferrous alloys. US-A-5188813 (Fairey et al., Johnson Matthey) describes woven fabrics of stitches by stitch consisting essentially of interlock loops of precious metal fibers selected from the metals of the group of platinum, gold, and alloys thereof using circular bed or flat bed knitting machines, with platinum or with platinum alloys, for use as metallic catalytic sieves that are preferred. Fairey et al found that strands of platinum alloy or metals with similar mechanical properties could not be knitted effectively and that attempts to do so led to a break in the fiber and clogging of the machine. cause that the tensile strength of the metal fibers was insufficient to withstand the frictional forces in the knitting process. The solution described was to feed the metallic fiber with a supplementary fiber that acted as a lubricant, the supplementary fiber preferably being in the form of multiple cords instead of a monofilament, and the cords surround the metallic wire to minimize contact of the metal with the metal. After knitting, the supplementary fiber can be removed by dissolving in a solvent or by pyrolysis. WO 92/02301 (Heywood) discloses a woven fabric of warp stitches of platinum, palladium or rhodium threads, using for example the knitted fabric of knitting, raschel or jacquard to give metal screens catalysts that are more flexible or open than the knits. woven metal sieves and that are less likely to twist under thermal stress. The knitter by points is facilitated either by the lubrication of the wire with a lubricant such as starch or wax or by feeding a supplementary fiber. A particular structure of the fine mesh warp knitted fabric, based on noble metal threads and for use as a catalyst, is described in US-A-6089051 (Gorywoda et al). None of the above references discloses or suggests the formation of dot-woven structures based on fine silver or silver alloy, and our experience is that standard Sterling silver has insufficient tensile strength for weaving by effective points on the machine.
GB-B-2255348 (Rateau, Albert and Johns, Metaleurop Recherche) discloses a novel silver alloy that maintains the hardness and luster properties inherent in Ag-Cu alloys while reducing the resulting problems of the tendency of the copper content to oxidize. The alloys are ternary alloys of Ag-Cu-Ge containing at least 92.5% by weight of Ag, 0.5-3% by weight of Ge and the rest, apart from the impurities, of copper. The alloys are stainless in the air of the environment during the operations of production, transformation and conventional finishing, they are deformable easily when they are cold, they are easily brazed and they do not cause a significant shrinkage during the casting. They also exhibit superior ductility and tensile strength. Germanium is established to exert a protective function that was responsible for the advantageous combination of the properties exhibited by the new alloys, and is in a solid solution in the phases of both silver and copper. The microstructure of the alloy consists of two phases, a solid solution of germanium and copper in silver surrounded by a solid filament solution of germanium and silver in copper that contains by itself a few dispersoids of the intermetallic CuGe phase. Germanium in the copper-rich phase is said to inhibit the surface oxidation of this phase by the formation of a protective coating of GeO and / or thin Ge02 that prevented the appearance of a purple spot during brassizing and annealing by the flame. In addition, the tarnish development was appreciably delayed by the addition of germanium, the surface became slightly yellow instead of black and the tarnish products were easily removed by ordinary tap water. US-A-6168071 (Johns) and EP-B-0729398 (Johns) describe a silver / germanium alloy comprising a silver content of at least 77% by weight and a germanium content of between 0.4 and 7% , the rest is mainly copper apart from some impurities, such alloy contained elemental boron as a grain refiner at a concentration greater than 0 ppm and less than 20 ppm. The boron content of the alloy could be achieved by providing the boron in a master copper-boron alloy having 2% by weight of elemental boron. It was reported that such low boron concentrations surprisingly provided excellent refining of the grain in a silver / germanium alloy, imparting greater strength and ductility to the alloy, compared to a silver / germanium alloy without boron. Silver sterling Argentium (trademark) comprises Ag 92.5% by weight and Ge 1.2% by weight, the rest is copper and approximately 4 ppm of boron as a grain refiner. The Society of the American Goldsmiths maintains a web site for the commercial modalities of the aforementioned alloys known as Argentium (registered trademark) at the address of the network http: // www. silversmithing. com / largent ium. htm US-A-6726877 (Eccles) discloses inter alia a silver alloy composition for jewelry hardenable by mechanical means, resistant to the formation of purple spots, comprising 81-95.409% by weight of Ag, 0.5-6% by weight. Cu weight, 0.05-5% by weight of Zn, 0.02-2% by weight of Si, 0.01-2% by weight of B, 0.01-1.5% by weight of In and 0.01 not greater than 2.0% by weight of Ge . The germanium content is alleged to lead to alloys that have mechanical hardening characteristics of a kind exhibited by conventional 0.925 silver alloys, along with resistance to the formation of a purple stain from alloys that are allegedly resistant to the formation of a purple spot, known prior to June 1994. The amounts of Ge in the alloy from about 0.04 to 2.0% by weight are alleged to provide hardening properties by mechanical means, modified in relation to the alloys of the resistant class to the formation of a purple stain that do not include germanium, but the operation of the hardening is not linear with the increase of the germanium nor the hardening is linear with the degree of the hardening by mechanical means. The Zn content of the alloy has a support in the color of the alloy as well as in the operation as a reducing agent for the silver and copper oxides and is preferably 2.0-4.0% by weight. The Si content of the alloy is preferably adjusted in relation to the proportion of Zn used and is preferably 0.15 to 0.2% by weight. The hardening by precipitation after annealing is not described, and there is no description or suggestion that the problems of distortion and damage to welded joints in the almost finished work made of this alloy can be avoided. By way of background, US-A-4810308 (Eagar et al.; Leach & Garner) describes a hardenable silver alloy comprising not less than 90% silver; not less than 2.0% copper; and at least one metal selected from the group consisting of lithium, tin and antimony. The silver alloy may also contain up to 0.5% by weight of bismuth. Preferably, the metals comprising the alloy are combined and heated to a temperature of not less than 676-760 ° C (1250-1450 ° F) for example for about 2 hours to anneal the alloy in a solid solution, a temperature of 732 ° C. C (1350 ° F) is used in the examples. The annealed alloy is then cooled rapidly to room temperature by quenching. It can then be hardened over time by reheating to 149-371 ° C (300-700 ° F) for a predetermined period of time followed by cooling of the hardened alloy with the passage of time at room temperature. The hardened alloy over time demonstrates a substantially higher hardness than that of traditional sterling silver, typically 100 HVN (Vickers hardness number), and can be returned by elevated temperatures to a state relatively soft. The description of US-A-4869757 (Eagar et al., Leach &Garner) is similar. In both cases, the annealing temperature described is higher than that of Argentium, and no reference describes alloys resistant to the formation of a purple stain or tarnish. The inventor has no knowledge of the process described in these patents that is used for commercial production, and again there is no description or suggestion that the hardening can be achieved in almost completed work. A silver alloy called Steralite is said to be covered by US-A-5817195 (Davitz); 5882441 (Davitz), and exhibiting high resistance to corrosion and tarnish. The alloy of US-A-5817195 (Davitz) contains 90-92.5% by weight of Ag, 5.75-5.5% by weight of Zn, 0.25 to less than 1% by weight of Cu, 0.25-0.5% by weight of Ni, 0.1- 0.25% by weight of Si and 0.0-0.05% by weight of In. The alloy of US-A-5882441 (Davitz) contains 90-94% by weight of Ag, 3.5-7.35% by weight of Zn, 1-3% by weight of Cu and 0.1-2.5% by weight of Si. An alloy of low copper content-high zinc content, like, is described in US-A-4973446 (Bernhard et al) and is said to exhibit reduced purple spot formation, reduced porosity and reduced grain scale . It has now been found that silver wire can be formed by machining into woven structures by processes such as weaving, knitting or braiding and that sufficient strength can be imparted to the wire by the formation itself by machining if the wire is hardened by the hardening by mechanical means from its fully annealed state prior to the formation of the fabric, at the same time that a further hardening by mechanical means is allowed to take place in the fabric forming process and still allowing the development of a hardness additional by hardening by precipitation. Argentium wire and other silver / copper / germanium alloy wires, in particular, have a particularly desirable combination of physical properties that allow them to be knitted or otherwise formed into woven or cable structures or lacing structures braided.
BRIEF DESCRIPTION OF THE INVENTION The invention provides a woven structure comprising yarns of a silver alloy which may be knitted, woven, braided, woven with hooks or otherwise formed and which may comprise fibers that are total, partial or predominantly silver. The invention also provides a process for manufacturing a woven structure as mentioned above which comprises providing a silver wire having a temper greater than that of the fully softened material but less than the material half the hardness, shaping the wire into the structure woven, and heat the structure for hardening by precipitation of the wire. In a further aspect, the invention provides a woven structure (for example a structure formed by knitted fabric, hooked fabric or other interlock loops of the wire) comprising (as all of the filaments or yarns in the structure) or as some of the filaments or threads in the structure) threads of a silver alloy having a grain structure refined by incorporation into the molten silver alloy from which the wire is formed, of a boron compound that It can decompose. Detailed Description of the Invention Alloys for forming the wire The wire used to form the present structures can be any grade of silver curable by precipitation and by mechanical means, but preferably it is an alloy of silver, copper and germanium, for example an alloy consisting of , apart from impurities and any grain refiner, 80-96% in silver, 0.1-5% germanium and 1-19.9% copper, by weight of the alloy. Sterling grade alloys of the above type may comprise, apart from impurities and the grain refiner, 92.5-98% silver, 0.3-3% germanium, and 1-7.2% copper, by weight of the alloy, together with 1-200 ppm for example 1-40 ppm boron as a grain refiner. A particularly preferred group of such alloys consists, apart from the impurities and the grain refiner, of 92.5-96% silver, 0.5-2% germanium, and 1-7% by weight of copper, by weight of the alloy, together with 1-40 ppm boron as the grain refiner. The alloy may further comprise zinc, preferably in a proportion, by weight, with respect to copper of not more than 1: 1. Accordingly, the alloy may comprise 81-95.49% by weight of Ag, 0.5-6% by weight of Cu, 0.05-5% by weight of Zn, 0.02-2% by weight of Si, 0.01-2% by weight of B, optionally 0.01-1.5% by weight of In, optionally 0.25-6% by weight of Sn and 0.01-not greater than 2.0% by weight of Ge. The alloy from which the present wire is formed may contain one or more incidental ingredients known per se in the production of silver alloys in amounts (for example in total up to 0.5% by weight) which are not detrimental to the strength mechanical, tarnish resistance and other material properties. Cadmium can also be added in similar amounts although its use is not currently preferred. Tin can be beneficial, typically in an amount of 0.5% by weight. The indium can be added in small amounts for example as a grain refiner and to improve the wettability of the alloy. Other elements of possible incidental ingredients, selected from Al, Ba, Be, Co, Cr, Er, Ga, Mg, Ni, Pb, Pd, Pt, Si, Ti, V, Y, Yb, and Zr, provided the effect of germanium in terms of providing resistance to the formation of a purple spot and tarnish so that it is not unduly affected. Refining the grain of the alloys Boron can be incorporated into the silver alloys used to make the wire for the present purposes as a grain refiner. It can be added, for example, to the molten silver alloy as a master alloy of copper / boron, at 2% by weight of B. However, it has recently been found that alloys having improved mechanical properties (including for example tensile strength) can be made by introducing the boron into the alloy as a boron compound selected from the compounds of alkyl boron, boron hydrides, halides of boron, metal hydrides containing boron, metal halides containing boron and mixtures thereof. The use of wire made of molten silver treated with boron compounds that can be decomposed as mentioned above, is advantageous for the present invention since the mechanical properties thereof are more consistent and the strength can be higher both prior to forming of the woven structure as after over-heating the woven structure to effect hardening. In some embodiments, the refined grain silver by means of a decomposable boron compound is detectable for example on an electron micrograph examination because of its fine grain structure. The boron compound can be introduced into the molten silver alloy in the gas phase, advantageously mixed with a carrier gas which helps to create a stirring action in the molten alloy and to disperse the boron content of the gas mixture within said alloy . Suitable carrier gases include, for example, hydrogen, nitrogen and argon. The gaseous boron compound and the carrier gas can be introduced from above into a container containing the molten silver, for example a crucible in a silver melting furnace, a casting boiler or a tundish using a metallurgical lancet. which may be an elongated tubular body of refractory material for example of graphite or may be a metallic tube lining in the refractory material and is immersed in its lower end in the molten metal. The lancet is preferably of sufficient length to allow the injection of the gaseous boron compound and the carrier gas deep into the molten silver alloy. Alternatively, the gas containing the boron can be introduced into the molten silver from one side or from below using for example a permeable gas bubble cap or a submerged injection nozzle. For example, Rautomead International of Dundee, Scotland, manufactures continuous casting machines, horizontal, in the RMK series for the continuous casting of semi-finished products in silver. The alloy to be heated is placed in a solid graphite crucible, protected by an inert gas atmosphere which can be, for example, oxygen-free nitrogen containing <; 5 ppm of oxygen and < 2 ppm moisture and is heated by heating with an electrical resistance using graphite blocks. Such furnaces have an integrated facility for the bubbling of inert gas through the molten material. The addition of small amounts of the gas that contains the thermally decomposable boron to the inert gas that is bubbled through the mixture easily provides a boron content of some ppm or a few tenths of a ppm, desired. The introduction of the boron compound into the alloy as a stream of gas diluted over a period of time, the carrier gas of the gas stream serving to stir the molten metal or alloy, rather than in one or more relatively large amounts , it is believed that it will be favorable from the point of view of avoiding the development in the metal or the alloy of boron hard points. Compounds that can be introduced into the molten silver or alloys thereof in this manner, include boron trifluoride, diborane or trimethylboro which are available in pressurized cylinders diluted with hydrogen, argon, nitrogen or helium, diborane is preferred to Because apart from boron, the only other element that is introduced into the alloy is hydrogen. A still further possibility is to bubble the carrier gas through the molten silver to effect agitation thereof and to add a solid boron compound, for example, NaBH4 or aBF4 in the fluidized gas stream as a finely divided powder forming a aerosol. A boron compound can also be introduced into the molten silver alloy in the liquid phase, either as such or in an inert organic solvent. Compounds which can be introduced in this manner include alkylborane or alkoxy alkyl borane such as triethylborane, tripropylborane, tri-n-butyl-imborane and methoxydiethylborane which by their safe handling can be dissolved in hexane or THF. The liquid boron compound can be filled and sealed in silver or copper foil containers that resemble a capsule or envelope using the known envelope / liquid or capsule / liquid filling machinery and using a protective atmosphere to provide the envelopes with filled capsules or other small containers typically of 0.5-5 ml capacity, more typically approximately 1-1.5 ml. Capsules or envelopes filled in an appropriate number can then be submerged individually or as one or more groups in the molten silver or an alloy thereof. A still further possibility is to atomize the liquid boron-containing compound into a stream of a carrier gas which is used to stir the molten silver as described above. The droplets may take the form of an aerosol in the stream of the carrier gas, or they may become evaporated therein. Preferably, the boron compound is introduced into the molten silver alloy in the solid phase, using for example a solid borane eg decaborane Bi0H14 (mp 100 ° C, e.g. 213 ° C). However, boron is preferably added in the form of either a metal hydride containing boron or a boron containing metal fluoride.
When a metal hydride containing boron is used, suitable metals include sodium, lithium, potassium, calcium, zinc and mixtures thereof. When a boron containing metal fluoride is used, sodium is the preferred metal. Sodium borohydride, NaBH 4 which has a molecular weight of 37.85 and contains 28.75% boron, is even more preferred. The boron can be bonded to the molten silver alloy both in the first casting and at intervals during the storage of the alloy in the molten state and subsequently to compensate for the loss of boron if the alloy is kept in the molten state for a period of time. time, as in a continuous casting process by grain. Surprisingly it has been found that when a decomposable boron compound such as a borane or a borohydride is added, more than 20 ppm can be incorporated into a silver alloy without the development of boron hard spots. This is advantageous because boron is rapidly lost from the molten silver: according to one experiment, the boron content in the molten silver decomposes with a half-life of about 2 minutes. The mechanism of this decomposition is not clear, but it can be an oxidizing process. It is therefore desirable to incorporate more than 20 ppm of boron in an alloy as a first cast, and amounts for example up to 50 ppm, typically up to 80 ppm, and in some cases up to 800 or even 1000 ppm can be incorporated. Thus, a grain from the silver melt containing approximately 40 ppm boron could be produced. Due to the loss of boron during subsequent re-melting and wire formation, the boron content of the finished wire may be closer to 1-20 ppm, but the ability to achieve relatively high initial boron concentrations means that It can achieve improved consistency and improved mechanical properties. Formation of the wire from the alloys The formation of the germanium-containing silver in a wire for the formation of a fabric according to the invention can be carried out using conventional wire-making processes. In certain embodiments of the invention, the metal is cast to form ingots that are wound on a roller mill to form a wire rod. The resulting bar is stretched successively through a series of diameter dies that are progressively reduced to give the required size. Stretching may be in single block machines, or the wire may be stretched over continuous wire stretching machines having a series of guides through which the wire passes in a continuous manner. Lubrication can be provided when necessary. In the final stage, and when required in the intermediate stages, the wire can be annealed to restore ductility. Preferably this step is carried out in an atmosphere that is not too reductive or that is mildly oxidizing. The corrosion resistance of the present AgCuCe alloys depends on the presence of the oxide films, and these are reduced for example by an atmosphere of 50% hydrogen, 50% nitrogen with some loss of tarnish resistance. In each step, it is desirable that the annealing atmosphere should be an inert gas, generally nitrogen, with less than 10% hydrogen, typically 3-10%, preferably about 3-5%. If the atmosphere of the furnace is thermofractioned ammonia, it is preferred that the hydrogen content should not be greater than the range indicated above. It has been found that it is possible to have mildly oxidizing conditions during annealing, that is, partial temperatures and pressures of oxygen, which allow the Ag-Cu- (Zn) -Ge alloys to be processed in such a way that the Ge will react to form Ge02 without Cu forming CuC > 2. However, the restrictions on the maximum processing temperature and time on the temperature rise from the normal commercial annealing temperature and the time used for the production of silver-copper alloys such as Sterling Silver., typically approximately 625 ° C or 650 ° C. It has been established that the Ag-Cu- (Zn) -Ge alloys can be processed even at annealing temperatures such as 625 ° C and 650 ° C to selectively oxidize the Ge to Ge02, using a controlled atmosphere. Preferably, the annealing atmosphere is a selectively oxidizing, wet atmosphere. By "wet" is this context is meant an atmosphere containing moisture (H20), such that the atmosphere exhibits a dew point of at least +1 ° C, preferably at least +25 ° C, more preferably at minus +40 ° C. Preferably, the dew point is considered to be within the range of +1 ° C to +80 ° C, more preferably in the range of +2 ° C to +50 ° C. The dew point can be defined as the temperature at which an atmosphere containing water vapor must be cooled so that saturation occurs, whereby an additional cooling below the dew point temperature leads to dew formation. A more comprehensive definition is given in "Handbook of Chemistry and Physics," 65th Ed. (1985-85), CRC Press Inc., USA, page F-75. It is preferred that the selectively oxidizing atmosphere comprises hydrogen and moisture, for example an atmosphere of nitrogen, hydrogen and water vapor, such as a gaseous mixture of 95% nitrogen / 5% hydrogen (v / v) containing water vapor , or a furnace atmosphere of nitrogen, hydrogen, carbon monoxide, carbon dioxide, methane, and water vapor. In practice, it is preferred to produce the selectively oxidizing, wet annealing atmosphere by controlling the addition of water vapor to a dry, or inert, substantially dry kiln atmosphere, for example to a furnace atmosphere predominantly nitrogen or nitrogen and hydrogen, and which typically comprises nitrogen, hydrogen, carbon monoxide, carbon dioxide and methane. The dew point in the furnace can be measured by conventional means such as a dew point meter or a probe in the furnace, and the mixing ratios of the gas are adjusted accordingly to control the selectively oxidizing atmosphere. As explained above, in some embodiments of the invention, the annealing of the wire is carried out under the selectively oxidizing atmosphere. If, as usual, the annealing is carried out as successive annealing steps, for example with interleaved stretching steps, then at least the final annealing step must be carried out under a selectively oxidizing atmosphere. In the further embodiments of the invention, one or more of the annealing steps preceding the final annealing step are carried out under a reducing atmosphere. However, in other embodiments of the invention, all of the annealing steps are carried out under a selectively oxidizing atmosphere. In the embodiments of the invention, the annealing of the wire is carried out at a temperature in the range from 400 ° C to 750 ° C, typically in the range from 400 ° C to 700 ° C, preferably in the range from 500 ° C. C up to 675 ° C, more preferably in the range from 600 ° C to 650 ° C, and in particular at about 625 ° C. In the embodiments of the invention, the annealing is carried out for a total period in the range from 5 minutes, at the highest annealing temperatures, up to 5 hours, at the lower annealing temperatures, and preferably in the range of 15 minutes. minutes up to 2 hours. A further improvement in tarnishing resistance can be obtained by heating the post-production of the wire, ie after the alloy has been stretched and annealed to provide a finished wire. The heating may be in an atmosphere of air or steam at a temperature in the range from 40 ° C to 220 ° C, preferably in the range of 50 ° C to 200 ° C, more preferably in the range of 60 ° C to 180 ° C. Preferably, postproduction heat treatment is carried out for a period in the range from 1 minute to 24 hours, preferably in the range of 10 minutes to 4 hours. Accordingly, the protective coating of germanium oxide can be further developed within the surface of the alloy. Advantageously, this post-production treatment also covers the protection of the alloy against tarnishing, which is particularly important for the fine wire because of its high surface area in relation to its mass. The structures of the invention may consist wholly or mainly of silver threads, or the silver wire may be a minor component, for example when incorporated in bandages to take advantage of the bacterial properties of silver. The wire is a solid section different from the strip, and can be provided in a reel or in a reel or in a roll. The wire used to manufacture the present woven structures may be circular in cross section, but other sections may be employed, for example, oval, polygonal, strip or flat wire depending on the desired appearance for the finished chain. The wire will typically be circular in section. It may be of diameter or size of 0.05-2.0 mm, typically 0.1-1 mm. The wire may be a single cord or may comprise a plurality of twisted cords together. Hardness of the wire to form the woven structures Prior to the formation of the present structures, the wire of the invention should preferably be more than fully softened but less than half the hardness. These expressions have well understood meanings in the jewelry trade. In the jewelery wire, the hardness or malleability is graduated as soft or extra soft, of a quarter of hardness, half hardness, hard, and flexible hardness. The numbers instead of the names can also designate the hardness of the wire. The numbering system, which ranges from zero to 10 or greater, is based on the number of times the wire has been stretched through progressively smaller holes in a drawing plate. Each increase in the number designates a duplication of the preceding number. The soft or extra-soft wire is as it was annealed, has not been subsequently stretched through a plate and has a zero number. It is malleable and can easily be bent by hand in a large number of ways but does not retain its shape under tension. The wire that is hard to a quarter has been stretched through a single plate, the medium hard wire has been stretched twice and the hard wire has been stretched four times. The wire used to form the present structures is preferably a quarter-hardness wire, which imparts the necessary bending and breaking strength required for the fabric in the machine or the knitted fabric in the machine, but leaves sufficient material in the solid solution for both hardening by mechanical means during weaving or spot weaving and for subsequent hardening by precipitation. Structures that can be formed from the wire The wire can be knitted in the weft on a circular or flat bed knitting machine to produce for example a knitted structure in single layer knit stitches, or layer structures doubles, or more structures similar to a network, open, which can be tubular or can be flat sheets. In particular, wire-like, tubular, single-layer structures, based on a single layer or two layers, can be used as a substitute for conventional chains in the manufacture of jewelry such as bracelets and necklaces, and have the advantage of an attractive appearance and luminosity. The wire can also be warp knitted. The wire can be further shaped into braided cable structures, for example by twisting together a plurality of single silver filaments to form pleated yarns which are then braided, see for example US-A-4170921 and US-A-6070434 (Figure 6) for example to form a braided silver shirt surrounding the core that can be made of silver, of another metal or for example of plastic filaments. An additional possibility is to form the wire in a hook-woven structure. "Crochet" as used herein, means a manufacturing process of a needlework comprising loop stitches formed from a single strand or filament, for example a silver / copper / germanium alloy using a needle with Hook shape and includes both the formation of a base row that may be useful per se as a chain of jewelry and the manufacture of a flat woven structure or open work from successive rows of knitted fabrics. You can make structures of the type of band and lace. The embodiments of the invention for knitting or knitting with hooks also employ a sacrificial thread mounted substantially parallel and adjacent to the silver alloy wire during the operations involved in knitting or knitting with a hook and fed simultaneously with the same. The sacrificial strand can be formed of any suitable material that can be removed after the knitted structure has been formed. For example, suitable materials for the sacrificial strand may include cotton, an easily soluble metal, and polymers, natural or synthetic, including polyamides, polyesters, cellulosic fibers, acrylic styrene polymers, PVA and other vinyl polymers, alginate, and the like . Multiple strand fibers or cords and monofilament fibers or cords can be used. One of the advantages of a sacrificial strand is to provide a spacer to control the spacing in the structure of the knitted fiber. Accordingly, the thickness of the sacrificial strand can be used as a way to increase or decrease the volume of space between the adjacent portions of the knitted wire. Typically, the sacrificial strand may have a diameter that is approximately the same as the wire. As mentioned above, it may be desirable to decompose or dissolve the sacrificial strand, and the selection of the sacrificial strand is conveniently made to allow decomposition or facilitated dissolution after the woven structure has been formed. Most organic fibers, for example, can be pyrolyzed and / or oxidized to leave a small residue or no waste, or a strong acid such as sulfuric acid or nitric acid can be used. Additionally or as an alternative to a sacrificial strand, a lubricant, for example starch, may be used to reduce friction in the knitting or knitting process with a hook. After the formation of a knitted, braided, woven with hook or woven structure, it may be subjected to a curing treatment by heating in an oven for example at about 300 ° C for about 30-45 minutes followed by gradual cooling. A surprising difference in properties exists between conventional Sterling silver alloys and other binary alloys of Ag-Cu on the one hand and silver alloys of Ag-Cu-Ge on the other hand, on which the gradual cooling of the alloys of the Sterling binary type leads to coarse or coarse precipitates and a small hardening by precipitation, while the gradual cooling of the Ag-Cu-Ge alloys leads to fine precipitates and a hardening by useful precipitation, particularly where the silver alloy contains a effective amount of the grain refiner. further, the addition of germanium to Sterling silver changes the thermal conductivity of the silver alloy, compared to standard Sterling silver. The International Annealed Copper Scale (IACS) is a measure of conductivity in metals. On this scale, the copper value is 100%, pure silver is 106%, and standard Sterling silver is 96%, while a Sterling alloy containing 1.1% germanium has a conductivity of 56%. The significance of this is that sterling argentium alloys and other germanium-containing silver alloys do not dissipate heat as rapidly as standard sterling silver or its germanium-free equivalents, a piece will take a longer time to cool, and the Precipitation hardening to a commercially useful level (preferably up to a Vickers hardness of 110 or greater, more preferably up to 115 or greater) can be carried out during cooling with natural air or during cooling with controlled, slow air. A number of Ag-Cu-Ge-Zn alloys of the boron refined grain using a copper-boron master alloy or using a decomposable boron compound also exhibits a precipitation hardening under the conditions indicated above. The present structures can be used to make articles that can be used, for example chains, bracelets, necklaces, earrings, key rings and the like. The silver wire can be incorporated, in the embodiments of the invention, into a variety of additional structures for example for use in catalysis or a water treatment. Accordingly, it can be incorporated into a backing material for example for carpets, as a minor component in woven or knitted garments, for example for protective clothing or in fashionable garments, in textile fabrics general, knitted, circular or flat fabrics, warp knitted fabrics, sleeves, ribbons, felts perforated with needles or other felts, and twisted or braided cords or cords. The silver wire, either alone or mixed with other metallic or natural or synthetic organic fibers or filaments, can be formed in a porous medium, for example three-dimensional non-woven structures, for example for filtration (for example of water where the anti-aging properties). -bacterial silver can be an advantage) or in catalyst support applications. It can be incorporated as a component of a bandage taking into account its antibacterial properties. In the further embodiments, the silver wire can be formed into a high porosity, non-woven matrix of sintered metal fibers, which exhibits high gas permeability, or a layer that can be folded. The sintered metal fibers can be formed into a medium having a plurality of layers, for example 1-3 layers optionally with an internal or surface support mesh or screen for a variety of filtration applications and other applications including catalysts, filtration gas-solid and / or gas / liquid and / or odor removal and liquid / solid filtration. Because of the high porosity that can be achieved, filter media made using the fibers according to the invention can exhibit a relatively low pressure drop. They can be used as such or incorporated as minor components in textile products, for example in bandages to provide antibacterial properties. It is noted that in relation to this date, the best method known to the applicant to carry out the aforementioned invention, is that which is clear from the present description of the invention.
Claims (34)
- Claims Having described the invention as above, the content of the following claims is claimed as property. A woven structure, characterized in that it comprises silver alloy wires.
- 2. The structure according to claim 1, characterized in that the alloy is an alloy of silver, copper and germanium.
- 3. The structure according to claim 2, characterized in that the alloy consists, apart from the impurities and any grain refiner, of 80-96% silver, 0.1-5% germanium and 1-19.9% copper, in Alloy weight. .
- The structure according to claim 3, characterized in that the alloy comprises, apart from the impurities and the grain refiner, 92.5-98% silver, 0.3-3% germanium, and 1-7.2% copper, by weight of the alloy, together with 1-40 ppm boron as the grain refiner.
- 5. The structure according to claim 4, characterized in that the alloy consists, apart from the impurities and the grain refiner, of 92.5-96% silver, 0.5-2% germanium, and 1-7% copper, by weight of the alloy, together with 1-40 ppm of boron as the grain refiner.
- 6. The structure according to any preceding claim, characterized in that the alloy further comprises zinc.
- 7. The structure according to claim 6, characterized in that the zinc is present in a proportion, by weight, with respect to copper of not more than 1: 1.
- The structure according to any preceding claim, characterized in that the alloy comprises 81-95,409% by weight of Ag, 0.5-6% by weight of Cu, 0.05-5% by weight of Zn, 0.02-2% by weight of Yes, 0.01-2% by weight of B, optionally 0.01-1.5% by weight of In, optionally 0.25-6% by weight of Sn and 0.01-not more than 2.0% by weight of Ge.
- The structure according to any preceding claim, characterized in that it consists essentially of silver wire.
- 10. The structure according to any preceding claim, characterized in that the wire is of a diameter of 0.05-2.0 mm.
- The structure according to claim 10, characterized in that the wire is of a diameter of 0.1-1 mm.
- 12. The structure according to any preceding claim, characterized in that the silver wire is of a single cord.
- The structure according to any of claims 1-12, characterized in that the silver wire comprises a plurality of cords.
- 14. The structure according to any preceding claim, characterized in that it is woven.
- 15. The structure according to any of claims 1-13, characterized in that it is knitted by stitches.
- 16. The structure according to claim 15, characterized in that it comprises a single layer.
- 17. The structure according to claim 15, characterized in that it comprises two or more layers of loops knitted together.
- 18. The structure according to claims 15, 16 or 17, characterized in that it is knitted from stitches per frame.
- 19. The structure according to claims 15, 16 or 17, characterized in that it is woven of warp stitches.
- 20. The structure according to any of claims 15-19, characterized in that it is tubular or similar to a cable.
- 21. The structure according to any of claims 15-19, characterized in that it is a flat sheet.
- 22. The structure according to any preceding claim, characterized in that it can be obtained by the formation of a quarter-hardness wire.
- 23. The structure according to any preceding claim, characterized in that it is hardened by precipitation after the structure has been formed.
- 24. The structure according to claim 23, characterized in that it is hardened by precipitation by heating to about 300 ° C for about 30 minutes.
- 25. A process for manufacturing a woven structure, characterized in that it comprises providing a silver wire having a greater temper than fully softened but less than half the hardness, forming the wire within the structure and heating the structure to harden the wire by precipitation.
- 26. The process according to claim 25, characterized in that the wire before dot weaving is one quarter hard.
- 27. The process according to claim 25 or 26, characterized in that the woven structure is formed by the knitting of the wire.
- 28. The process according to claim 27, characterized in that the structure is formed by the fabric of stitches per frame.
- 29. The process according to claim 27, characterized in that the structure is formed by the knitting of warp stitches.
- 30. The process according to any of claims 25-29, characterized in that the wire is of a precipitation-curable Ag Cu Ge alloy, containing at least 80% by weight of Ag.
- 31. The process in accordance with the claim 30, characterized in that the alloy has an effective amount of boron as a grain refiner and up to 20 ppm.
- 32. A woven structure, characterized in that it comprises silver alloy yarns having a grain structure refined by incorporation into the molten silver alloy from which the wire is formed of a decomposable boron compound.
- 33. The structure according to claim 32, characterized in that the decomposable boron compound is sodium borohydride.
- 34. The structure according to claim 32 or 33, characterized in that it is formed by knitting in a machine.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0425152.6 | 2004-11-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
MX2007005565A true MX2007005565A (en) | 2008-10-03 |
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