GB2402399A - A silver-germanium-copper alloy - Google Patents

A silver-germanium-copper alloy Download PDF

Info

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
Application number
GB0312693A
Other versions
GB0312693D0 (en
GB2402399B (en
Inventor
Peter Gamon Johns
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Middlesex Silver Co Ltd
Original Assignee
COLE PAUL GILBERT
Middlesex Silver Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by COLE PAUL GILBERT, Middlesex Silver Co Ltd filed Critical COLE PAUL GILBERT
Priority to GB0312693A priority Critical patent/GB2402399B/en
Publication of GB0312693D0 publication Critical patent/GB0312693D0/en
Priority to PT04735594T priority patent/PT1631692E/en
Priority to DE602004019080T priority patent/DE602004019080D1/en
Priority to AU2004243654A priority patent/AU2004243654A1/en
Priority to AT04735594T priority patent/ATE420980T1/en
Priority to CA002527430A priority patent/CA2527430A1/en
Priority to CNA2004800154108A priority patent/CN1846007A/en
Priority to EP04735594A priority patent/EP1631692B1/en
Priority to PCT/GB2004/002317 priority patent/WO2004106567A1/en
Priority to JP2006508380A priority patent/JP2007535616A/en
Priority to CN201210188563.9A priority patent/CN102690969B/en
Priority to ES04735594T priority patent/ES2322465T3/en
Priority to EA200501875A priority patent/EA011015B1/en
Priority to US10/559,092 priority patent/US20070009375A1/en
Publication of GB2402399A publication Critical patent/GB2402399A/en
Application granted granted Critical
Publication of GB2402399B publication Critical patent/GB2402399B/en
Priority to US12/766,312 priority patent/US20100239454A1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C5/00Alloys based on noble metals
    • C22C5/06Alloys based on silver
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23FNON-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
    • C23F11/00Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent
    • C23F11/08Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent in other liquids
    • C23F11/10Inhibiting 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
    • C23F11/16Sulfur-containing compounds
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23FNON-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
    • C23F11/00Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent
    • C23F11/08Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent in other liquids
    • C23F11/10Inhibiting 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
    • C23F11/16Sulfur-containing compounds
    • C23F11/161Mercaptans

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)

Àe A. A. en: À. .. i.. .:e e.. À e: À À À . . - 22 - CLAIMS
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.
GB0312693A 2003-06-03 2003-06-03 Silver ternary alloy Expired - Fee Related GB2402399B (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (8)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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