EP3121297A1 - Herstellungsverfahren einer schmuckkomponente aus platinlegierung - Google Patents
Herstellungsverfahren einer schmuckkomponente aus platinlegierung Download PDFInfo
- Publication number
- EP3121297A1 EP3121297A1 EP16177653.9A EP16177653A EP3121297A1 EP 3121297 A1 EP3121297 A1 EP 3121297A1 EP 16177653 A EP16177653 A EP 16177653A EP 3121297 A1 EP3121297 A1 EP 3121297A1
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- EP
- European Patent Office
- Prior art keywords
- hardness
- semi
- finished product
- alloy
- process according
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 59
- 229910001260 Pt alloy Inorganic materials 0.000 title description 11
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 claims abstract description 47
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 34
- 239000000956 alloy Substances 0.000 claims abstract description 34
- 239000011265 semifinished product Substances 0.000 claims abstract description 29
- 229910052697 platinum Inorganic materials 0.000 claims abstract description 22
- 238000003754 machining Methods 0.000 claims abstract description 10
- 238000005482 strain hardening Methods 0.000 claims abstract description 8
- 239000002994 raw material Substances 0.000 claims abstract description 4
- 238000010438 heat treatment Methods 0.000 claims description 17
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 8
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 claims description 8
- 229910052802 copper Inorganic materials 0.000 claims description 8
- 239000010949 copper Substances 0.000 claims description 8
- 238000011282 treatment Methods 0.000 claims description 7
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 claims description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 6
- 229910052733 gallium Inorganic materials 0.000 claims description 6
- 238000011084 recovery Methods 0.000 claims description 6
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 6
- 229910052721 tungsten Inorganic materials 0.000 claims description 6
- 239000010937 tungsten Substances 0.000 claims description 6
- KJTLSVCANCCWHF-UHFFFAOYSA-N Ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 claims description 5
- 229910052707 ruthenium Inorganic materials 0.000 claims description 5
- 238000007493 shaping process Methods 0.000 claims description 5
- 229910052763 palladium Inorganic materials 0.000 claims description 4
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 3
- 229910052729 chemical element Inorganic materials 0.000 claims description 3
- 229910017052 cobalt Inorganic materials 0.000 claims description 3
- 239000010941 cobalt Substances 0.000 claims description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 3
- 238000007906 compression Methods 0.000 claims description 3
- 125000004122 cyclic group Chemical group 0.000 claims description 3
- 238000001125 extrusion Methods 0.000 claims description 3
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 claims description 3
- 229910052737 gold Inorganic materials 0.000 claims description 3
- 239000010931 gold Substances 0.000 claims description 3
- 229910052735 hafnium Inorganic materials 0.000 claims description 3
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 claims description 3
- 229910052738 indium Inorganic materials 0.000 claims description 3
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 claims description 3
- 229910052741 iridium Inorganic materials 0.000 claims description 3
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- 229910052703 rhodium Inorganic materials 0.000 claims description 3
- 239000010948 rhodium Substances 0.000 claims description 3
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium atom Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 claims description 3
- 229910052706 scandium Inorganic materials 0.000 claims description 3
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 claims description 3
- 238000005275 alloying Methods 0.000 claims description 2
- 238000001556 precipitation Methods 0.000 claims description 2
- 239000000463 material Substances 0.000 description 6
- 229910052684 Cerium Inorganic materials 0.000 description 3
- ZMIGMASIKSOYAM-UHFFFAOYSA-N cerium Chemical compound [Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce] ZMIGMASIKSOYAM-UHFFFAOYSA-N 0.000 description 3
- 239000010970 precious metal Substances 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 239000006185 dispersion Substances 0.000 description 2
- 238000005498 polishing Methods 0.000 description 2
- 238000009419 refurbishment Methods 0.000 description 2
- 230000003252 repetitive effect Effects 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 210000004027 cell Anatomy 0.000 description 1
- 210000002421 cell wall Anatomy 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009760 electrical discharge machining Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 230000002706 hydrostatic effect Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000004807 localization Effects 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000010297 mechanical methods and process Methods 0.000 description 1
- 230000005226 mechanical processes and functions Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 229910000510 noble metal Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 238000007725 thermal activation Methods 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 238000007514 turning Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/14—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of noble metals or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C5/00—Alloys based on noble metals
- C22C5/04—Alloys based on a platinum group metal
Definitions
- the present invention relates to a method for obtaining a platinum alloy ornament component containing at least 80% by weight of platinum, having a particularly high hardness and can be machined by the usual methods.
- the component is intended for applications in watchmaking, jewelery, jewelery, eyewear, writing instruments, luxury accessories, and other decorative or functional applications in which the visual aspect is also important.
- the document EP0621349 describes a process for curing platinum at the surface by a surface layer containing boron.
- the process described only allows the treatment of a finished part, and tends to affect the aesthetic aspect of the latter (hue and temperature).
- the surface can be damaged. Refurbishment or refurbishment of such a room requires a specific post-restoration process that can be conducted only under very specific conditions and is therefore not within the reach of restoration workshops equipped with conventional means.
- the document GB2279967 proposes a high purity platinum alloy containing cerium in a small amount.
- This alloy makes it possible to achieve hardness comparable to, or even slightly greater than, that of a standard platinum alloy.
- cerium is a very sensitive element to oxidation, the preparation of the alloy must be carried out under vacuum or under an inert gas, making the process complex.
- cerium has a medium solid solubility in platinum, which also limits the homogeneity of the alloy obtained.
- the document GB578956 proposes a platinum alloy cured by the addition of oxides by means of a sintering process.
- the process is complex and is dependent on the size of the powders and the homogeneity of the compound to be obtained.
- the document JP1988145759 proposes a platinum alloy containing in particular iron, palladium and copper, and the hardening is obtained in part by a plastic deformation operation to the shape of the part to be obtained and by a heat treatment operation after the steps of setting in shape.
- This solution is therefore limited on the one hand by expensive matrix tools, and on the other hand by the heat treatment step which could promote recrystallization of the material, or even cause surface texture to appear.
- the document EP0947595 discloses a platinum alloy cured by dispersion reinforcement. This alloy uses dispersion oxides to oxidize the non-noble metal. On the other hand, the dispersing elements tend not only to disadvantage the wear of the tools, but they also make difficult the polishing steps.
- Heat treatment hardening processes on finished platinum alloy components are, on the other hand, known. They have the disadvantage that the grain structure is modified, which affects the texture of the polished surfaces.
- EP2705170A1 proposes a process for obtaining a platinum alloy with very high hardness through an amorphous structure, namely a metal glass.
- This high hardness involves a material and a method of shaping very particular and also require very specific tools and associated costs very high.
- the application of this technology to a wide range of products, highly diversified in their geometries, is therefore not the most suitable from an industrial point of view.
- the component obtained by the process of the invention has a hardness typically 25% to 50% higher than the hardness of the starting alloy.
- the method makes it possible to obtain the component in its final form and hardness without the need for heat treatment on the final component to modify its hardness.
- the purpose of the severe plastic deformation cycle (s) of the hardening step is to transform the crystallographic structure of the platinum alloy into an ultrafine grained ( UFG) structure.
- ultrafine grain structure we mean a structure whose grain size is at least less than 1 ⁇ m in at least one grain orientation.
- the grain size of the ultrafine grain structure may be less than 500 nm, and even less than 200 nm, see 100 nm.
- the deformation (or the relative elongation, noted ⁇ ) can be up to 5, or more.
- the alloy comprises at least 80.0% platinum and one or more of the following chemical elements: between 0% and 4% indium; between 0% and 6% ruthenium; between 0% and 5% copper; between 0% and 5% cobalt; between 0% and 20% of iridium; between 0% and 10% nickel; between 0% and 20% hafnium; between 0% and 20% tin; between 0% and 20% tungsten; between 0% and 15% of palladium; between 0% and 3% gallium; between 0% and 20% rhodium; between 0% and 20% scandium; between 0% and 8% of tungsten; and between 0% and 5% gold.
- the severe plastic deformation cycle (s) can be realized using one of the methods, or a combination of these methods, including: equal channel angular pressing (ECAP ), angular extrusion according to equal channels (ECAP- accordance), high pressure torsion (high pressure torsion tube twisting orhigh pressure, HPT or HPTT), accumulative roll-bonding (accumulative roll bonding, ARB), repetitive corrugation and straightening (straightening and repetitive corrugation, RCS) , asymmetric rolling (asymmetric rolling, ASR), cyclic extrusion-compression (cyclic extrusion compression CEC), roll drawing (rotary swaging), or any other suitable method for obtaining said ultrafine-grained structure.
- ECAP equal channel angular pressing
- ECAP- accordance high pressure torsion
- HPT or HPTT high pressure torsion tube twisting orhigh pressure, HPT or HPTT
- accumulative roll-bonding accumulative roll bonding
- ARB repetitive corrugation and straightening
- RCS
- the method comprises a step of shaping the alloy so as to give the semi-finished product a particular shape.
- the semi-finished product may take the form of a plate, a bar, an ingot, a billet, or any other advantageous form for the subsequent machining step.
- the method also comprises a step comprising one or more heat recovery treatments.
- Restoration heat treatment can be performed after the severe plastic deformation cycle, or between severe plastic deformation cycles.
- the parameters of the recovery heat treatment are adjusted so as not to completely relax the platinum alloy, so as not to degrade the second hardness obtained during the work hardening step.
- the (or) heat recovery treatment is performed at a temperature below 600 ° C beyond which the mechanical properties of the alloy drop rapidly and the ductility increases.
- the heat treatment (s) is preferably carried out at a temperature above 250 ° C and below 600 ° C. Indeed, below 250 ° C, the restoration heat treatment may have little or no effect for treatment times that are less than 1 hour, the thermal activation is not sufficient.
- the figure 1 reports the evolution of the elastic limit (Rm in MPa) and the maximum stress (Rp0.2 in MPa) for an alloy comprising at least 80.0% platinum as a function of temperature.
- the figure 2 reports the evolution of the hardness (HV) of the same alloy as a function of temperature.
- the (or) heat treatment of restoration is preferably carried out at a temperature between 250 ° C and 500 ° C, or even between 250 ° C and 400 ° C.
- the recovery heat treatment time may be one hour or less than one hour.
- the process comprises one or more heat treatment cures.
- the heat treatment or treatments for hardening further increase the second hardness of the semi-finished product by the precipitation of the alloying elements.
- the process of the invention provides the semi-finished product with a second hardness which is at least 25% and even 50% higher than the first hardness of the starting alloy.
- the machining step may include a material removal process such as turning, milling, grinding, spark erosion, cutting, laser or water jet cutting, or any other suitable method.
- the machining step may also include a method of shaping by deformation or assembly.
- the machining step can also include one or more finishing treatments, such as machining, satin finishing, polishing, sanding, microbilling, etching or any other suitable mechanical process.
- the machining step makes it possible to obtain the component in its final shape and hardness. It is therefore not necessary to perform heat treatment on the component obtained by the present process to modify its hardness. Indeed, the second hardness obtained for the semi-finished product by the hardening step corresponds to the desired hardness of the component.
- the ornamentation component may comprise a watch component, for example a component of the movement, the bracelet or a dressing component such as the case, the bezel, the bottom.
- the ornamentation component may also include a component for jewelery, eyewear, writing instruments, luxury accessories (key chains, lighters, cufflinks, tie bars, etc.) and others. decorative or functional applications in which the visual aspect is also important.
- an alloy comprising about 95% platinum and about 5% ruthenium, having a first nominal hardness of about 120Hv.
- the alloy is subjected to the first shaping step and the work hardening step having at least one severe plastic deformation cycle, so as to increase the second hardness of the semi-finished product to a value of at least 250 Hv.
- the cured semi-finished product has a second hardness of about 250 Hv.
- the hardening step is performed by the high-pressure torsion method, the semi-finished product has a second hardness greater than 400 Hv.
- an alloy comprising approximately 95% of platinum, between 1% and 4% of copper and between 1% and 4% of gallium (for a total of approximately 5% of copper and gallium) is provided.
- first nominal hardness of at least 200Hv.
- the semi-finished product when the work hardening step is performed by the accumulative bonding method, the semi-finished product has a second hardness of about 300 Hv.
- the semi-finished product can then be subjected to a subsequent curing heat treatment step to increase the second hardness to about 400 Hv.
- the hardening step comprising at least one severe plastic deformation cycle which may be followed by at least one heat recovery treatment, as described above.
- the process for obtaining an ornamental component described herein applies to any alloy comprising at least 80% by weight platinum, and may contain one or more of the following chemical elements: between 0% and 4% indium; between 0% and 6% ruthenium; between 0% and 5% copper; between 0% and 5% cobalt; between 0% and 20% of iridium; between 0% and 10% nickel; between 0% and 20% hafnium; between 0% and 20% tin; between 0% and 20% tungsten; between 0% and 15% of palladium; between 0% and 3% gallium; between 0% and 20% rhodium; between 0% and 20% scandium; between 0% and 8% of tungsten; and between 0% and 5% gold.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Adornments (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH10732015 | 2015-07-23 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3121297A1 true EP3121297A1 (de) | 2017-01-25 |
EP3121297B1 EP3121297B1 (de) | 2020-12-16 |
Family
ID=53723960
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16177653.9A Active EP3121297B1 (de) | 2015-07-23 | 2016-07-01 | Herstellungsverfahren einer schmuckkomponente aus platinlegierung |
Country Status (1)
Country | Link |
---|---|
EP (1) | EP3121297B1 (de) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107058788A (zh) * | 2017-04-12 | 2017-08-18 | 深圳市星光达珠宝首饰实业有限公司 | 一种多元铂钌合金及其制备方法 |
CN107671159A (zh) * | 2017-10-18 | 2018-02-09 | 大连理工大学 | 超声振动辅助脱模的限制性模压模具及晶粒细化方法 |
CN107893201A (zh) * | 2017-11-17 | 2018-04-10 | 合肥工业大学 | 制备超细晶材料的往复挤扭镦等径角成形方法 |
WO2022074363A1 (en) * | 2020-10-05 | 2022-04-14 | Alloyed Limited | A platinum alloy composition |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB578956A (en) | 1942-02-07 | 1946-07-18 | Lodge Plugs Ltd | Improvements relating to sparking plug electrodes |
US4165983A (en) * | 1977-02-23 | 1979-08-28 | Johnson, Matthey & Co., Limited | Jewelry alloys |
JPS63145759A (ja) | 1986-12-09 | 1988-06-17 | Citizen Watch Co Ltd | 装飾用白金合金の熱処理方法 |
EP0621349A1 (de) | 1993-04-23 | 1994-10-26 | Degussa Aktiengesellschaft | Oberflächengehärtete Gegenstände aus Platin- und Palladiumlegierungen und Verfahren zu deren Herstellung |
GB2279967A (en) | 1993-07-14 | 1995-01-18 | Nagahori Kk | Platinum alloy |
US5846352A (en) * | 1996-11-22 | 1998-12-08 | Kretchmer; Steven | Heat treatment of a platinum-gallium alloy for jewelry |
EP0947595A2 (de) | 1998-03-28 | 1999-10-06 | W.C. Heraeus GmbH & Co. KG | Verfahren zur Herstellung eines aus dispersionsverfestigtem Platinwerkstoff bestehenden, geschweissten Formkörpers, insbesondere eines Rohres |
US6562158B1 (en) * | 1998-12-01 | 2003-05-13 | Steven Kretchmer | Heat-treatable platinum-gallium-palladium alloy for jewelry |
WO2006024928A1 (en) * | 2004-09-02 | 2006-03-09 | University Of Cape Town | Hardening of metal alloys |
WO2012150558A1 (en) * | 2011-05-02 | 2012-11-08 | École Polytechnique Fédérale De Lausanne (Epfl) | Platinum based alloys |
-
2016
- 2016-07-01 EP EP16177653.9A patent/EP3121297B1/de active Active
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB578956A (en) | 1942-02-07 | 1946-07-18 | Lodge Plugs Ltd | Improvements relating to sparking plug electrodes |
US4165983A (en) * | 1977-02-23 | 1979-08-28 | Johnson, Matthey & Co., Limited | Jewelry alloys |
JPS63145759A (ja) | 1986-12-09 | 1988-06-17 | Citizen Watch Co Ltd | 装飾用白金合金の熱処理方法 |
EP0621349A1 (de) | 1993-04-23 | 1994-10-26 | Degussa Aktiengesellschaft | Oberflächengehärtete Gegenstände aus Platin- und Palladiumlegierungen und Verfahren zu deren Herstellung |
GB2279967A (en) | 1993-07-14 | 1995-01-18 | Nagahori Kk | Platinum alloy |
US5846352A (en) * | 1996-11-22 | 1998-12-08 | Kretchmer; Steven | Heat treatment of a platinum-gallium alloy for jewelry |
EP0947595A2 (de) | 1998-03-28 | 1999-10-06 | W.C. Heraeus GmbH & Co. KG | Verfahren zur Herstellung eines aus dispersionsverfestigtem Platinwerkstoff bestehenden, geschweissten Formkörpers, insbesondere eines Rohres |
US6562158B1 (en) * | 1998-12-01 | 2003-05-13 | Steven Kretchmer | Heat-treatable platinum-gallium-palladium alloy for jewelry |
WO2006024928A1 (en) * | 2004-09-02 | 2006-03-09 | University Of Cape Town | Hardening of metal alloys |
WO2012150558A1 (en) * | 2011-05-02 | 2012-11-08 | École Polytechnique Fédérale De Lausanne (Epfl) | Platinum based alloys |
EP2705170A1 (de) | 2011-05-02 | 2014-03-12 | Ecole Polytechnique Fédérale de Lausanne (EPFL) | Legierungen auf platinbasis |
Non-Patent Citations (1)
Title |
---|
BIGGS T ET AL: "THE HARDENING OF PLATINUM ALLOYS FOR POTENTIAL JEWELLERY APPLICATION", PLATINIUM METALS REVIEW, JOHNSON MATTHEY PLC, LONDON, GB, vol. 49, no. 1, 1 January 2005 (2005-01-01), pages 2 - 15, XP009055328, ISSN: 0032-1400, DOI: 10.1595/147106705X24409 * |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107058788A (zh) * | 2017-04-12 | 2017-08-18 | 深圳市星光达珠宝首饰实业有限公司 | 一种多元铂钌合金及其制备方法 |
CN107671159A (zh) * | 2017-10-18 | 2018-02-09 | 大连理工大学 | 超声振动辅助脱模的限制性模压模具及晶粒细化方法 |
CN107671159B (zh) * | 2017-10-18 | 2020-02-18 | 大连理工大学 | 超声振动辅助脱模的限制性模压模具及晶粒细化方法 |
CN107893201A (zh) * | 2017-11-17 | 2018-04-10 | 合肥工业大学 | 制备超细晶材料的往复挤扭镦等径角成形方法 |
WO2022074363A1 (en) * | 2020-10-05 | 2022-04-14 | Alloyed Limited | A platinum alloy composition |
GB2599462B (en) * | 2020-10-05 | 2023-06-14 | Anglo Platinum Marketing Ltd | A platinum alloy composition |
Also Published As
Publication number | Publication date |
---|---|
EP3121297B1 (de) | 2020-12-16 |
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