US20060086441A1 - Particle reinforced noble metal matrix composite and method of making same - Google Patents
Particle reinforced noble metal matrix composite and method of making same Download PDFInfo
- Publication number
- US20060086441A1 US20060086441A1 US10/974,229 US97422904A US2006086441A1 US 20060086441 A1 US20060086441 A1 US 20060086441A1 US 97422904 A US97422904 A US 97422904A US 2006086441 A1 US2006086441 A1 US 2006086441A1
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- US
- United States
- Prior art keywords
- noble metal
- particle
- matrix composite
- carbide
- metal matrix
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Links
- 229910000510 noble metal Inorganic materials 0.000 title claims abstract description 155
- 239000002245 particle Substances 0.000 title claims abstract description 123
- 239000011156 metal matrix composite Substances 0.000 title claims abstract description 65
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 14
- 239000000463 material Substances 0.000 claims abstract description 68
- 238000010438 heat treatment Methods 0.000 claims abstract description 39
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 claims abstract description 37
- 239000010931 gold Substances 0.000 claims abstract description 37
- 229910052737 gold Inorganic materials 0.000 claims abstract description 37
- 239000004332 silver Substances 0.000 claims abstract description 30
- 238000000034 method Methods 0.000 claims abstract description 29
- 229910052709 silver Inorganic materials 0.000 claims abstract description 29
- 239000011159 matrix material Substances 0.000 claims abstract description 19
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 17
- 239000000956 alloy Substances 0.000 claims abstract description 17
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 claims description 29
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 claims description 20
- 229910039444 MoC Inorganic materials 0.000 claims description 15
- 229910052751 metal Inorganic materials 0.000 claims description 15
- 239000002184 metal Substances 0.000 claims description 15
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 claims description 15
- QIJNJJZPYXGIQM-UHFFFAOYSA-N 1lambda4,2lambda4-dimolybdacyclopropa-1,2,3-triene Chemical compound [Mo]=C=[Mo] QIJNJJZPYXGIQM-UHFFFAOYSA-N 0.000 claims description 14
- 238000002844 melting Methods 0.000 claims description 10
- 230000008018 melting Effects 0.000 claims description 10
- 238000001816 cooling Methods 0.000 claims description 7
- 229910052697 platinum Inorganic materials 0.000 claims description 6
- 229910001316 Ag alloy Inorganic materials 0.000 claims description 5
- 239000012298 atmosphere Substances 0.000 claims description 4
- 239000002131 composite material Substances 0.000 abstract description 60
- 239000000945 filler Substances 0.000 abstract description 5
- 230000008569 process Effects 0.000 abstract description 5
- 239000000843 powder Substances 0.000 description 20
- 230000008595 infiltration Effects 0.000 description 15
- 238000001764 infiltration Methods 0.000 description 15
- 229910052721 tungsten Inorganic materials 0.000 description 12
- 239000010937 tungsten Substances 0.000 description 12
- 229910001020 Au alloy Inorganic materials 0.000 description 11
- 239000003353 gold alloy Substances 0.000 description 11
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 10
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 8
- 239000002905 metal composite material Substances 0.000 description 7
- -1 whiskers Substances 0.000 description 7
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- 229910052802 copper Inorganic materials 0.000 description 6
- 239000010949 copper Substances 0.000 description 6
- 229910052703 rhodium Inorganic materials 0.000 description 6
- 239000010948 rhodium Substances 0.000 description 6
- KJTLSVCANCCWHF-UHFFFAOYSA-N Ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 description 5
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 5
- 229910052736 halogen Inorganic materials 0.000 description 5
- 229910052741 iridium Inorganic materials 0.000 description 5
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 5
- 229910052762 osmium Inorganic materials 0.000 description 5
- SYQBFIAQOQZEGI-UHFFFAOYSA-N osmium atom Chemical compound [Os] SYQBFIAQOQZEGI-UHFFFAOYSA-N 0.000 description 5
- 229910052763 palladium Inorganic materials 0.000 description 5
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium atom Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 description 5
- 229910052707 ruthenium Inorganic materials 0.000 description 5
- 239000000523 sample Substances 0.000 description 5
- 229910052725 zinc Inorganic materials 0.000 description 5
- 239000011701 zinc Substances 0.000 description 5
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 4
- 229910001338 liquidmetal Inorganic materials 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 239000011148 porous material Substances 0.000 description 4
- 230000002787 reinforcement Effects 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 3
- 239000012300 argon atmosphere Substances 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 229910001092 metal group alloy Inorganic materials 0.000 description 3
- 229910052750 molybdenum Inorganic materials 0.000 description 3
- 239000011733 molybdenum Substances 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- 239000008188 pellet Substances 0.000 description 3
- 230000003014 reinforcing effect Effects 0.000 description 3
- 239000012779 reinforcing material Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 238000012512 characterization method Methods 0.000 description 2
- 239000008367 deionised water Substances 0.000 description 2
- 229910003460 diamond Inorganic materials 0.000 description 2
- 239000010432 diamond Substances 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 229910002804 graphite Inorganic materials 0.000 description 2
- 239000010439 graphite Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 238000009736 wetting Methods 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 241001443715 Fusarium oxysporum f. sp. conglutinans Species 0.000 description 1
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- UJXVAJQDLVNWPS-UHFFFAOYSA-N [Al].[Al].[Al].[Fe] Chemical compound [Al].[Al].[Al].[Fe] UJXVAJQDLVNWPS-UHFFFAOYSA-N 0.000 description 1
- OQPDWFJSZHWILH-UHFFFAOYSA-N [Al].[Al].[Al].[Ti] Chemical compound [Al].[Al].[Al].[Ti] OQPDWFJSZHWILH-UHFFFAOYSA-N 0.000 description 1
- IUHFWCGCSVTMPG-UHFFFAOYSA-N [C].[C] Chemical class [C].[C] IUHFWCGCSVTMPG-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000005054 agglomeration Methods 0.000 description 1
- 230000002776 aggregation Effects 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
- 229910052786 argon Inorganic materials 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- UOUJSJZBMCDAEU-UHFFFAOYSA-N chromium(3+);oxygen(2-) Chemical class [O-2].[O-2].[O-2].[Cr+3].[Cr+3] UOUJSJZBMCDAEU-UHFFFAOYSA-N 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 229910021641 deionized water Inorganic materials 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000007772 electroless plating Methods 0.000 description 1
- 229910001254 electrum Inorganic materials 0.000 description 1
- 230000003203 everyday effect Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000010940 green gold Substances 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229910021326 iron aluminide Inorganic materials 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 238000009862 microstructural analysis Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000004570 mortar (masonry) Substances 0.000 description 1
- 229910000907 nickel aluminide Inorganic materials 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 239000012763 reinforcing filler Substances 0.000 description 1
- 229910001112 rose gold Inorganic materials 0.000 description 1
- 238000007873 sieving Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229910000601 superalloy Inorganic materials 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 229910021324 titanium aluminide Inorganic materials 0.000 description 1
- 239000010938 white gold Substances 0.000 description 1
- 229910000832 white gold Inorganic materials 0.000 description 1
- 239000010930 yellow gold Substances 0.000 description 1
- 229910001097 yellow gold Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C5/00—Alloys based on noble metals
- C22C5/02—Alloys based on gold
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/10—Alloys containing non-metals
- C22C1/1036—Alloys containing non-metals starting from a melt
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C32/00—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
- C22C32/0047—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents
- C22C32/0052—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only carbides
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/25—Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
- Y10T428/256—Heavy metal or aluminum or compound thereof
Definitions
- the present invention pertains generally to metal matrix composite materials and, more particularly, to particle reinforced noble metal matrix composites and a method of making the same.
- composite materials consist of a bulk or base material, i.e. a matrix, and a filler reinforcement material, such as fibers, whiskers, or particles.
- the composite materials can be classified into three categories: 1) polymer, 2) metal, and 3) ceramic depending on the matrix employed, and can be further divided depending on the type of reinforcement material provided. These further divisions include dispersion strengthened, particle reinforced, or fiber reinforced type composites.
- two or more materials such as a metal and a particle material
- a metal and a particle material may be combined together in a certain order on a macroscopic level to form a new material with potentially different and attractive properties.
- attractive properties may include improved hardness, conductivity, density yield, etc.
- a composite is developed for use in a desired industry, such as the jewelry industry, with an eye toward improving at least one or more of the above noted properties and/or improving the method of making thereof, for example, by reducing production time to reduce costs.
- Methods for fabricating metal matrix composites vary and can include conventional powder metallurgy, in-situ using laser technology, electroless plating, hot pressing, and liquid metal infiltration. Each process includes advantages and disadvantages that may change dependent upon the material(s) used in making the metal composite. New and improved metal composites may be developed through new methods or by adapting existing methods, which may themselves be improved. For example, tungsten carbide reinforced copper matrix composites have been made, utilizing liquid metal infiltration, via an infrared heating process to produce a metal matrix composite having good hardness, conductivity, and density.
- Infrared processing also has been successfully used for joining advanced materials such as titanium-matrix composites, titanium aluminide, iron aluminide, nickel aluminide, titanium alloys, nickel based superalloys, carbon-carbon composites, and silicon carbide and carbon fiber reinforced titanium and aluminum matrix composites.
- infrared heating technology has been developing over about the last decade or so and is based on the generation of radiation by means of tungsten halogen lamps with a filament temperature of about 3000° C. Due to the selective absorption of infrared radiations and its cold wall process, it provides faster heating and cooling rates and has proved to be a quick, efficient, and energy conserving heating source.
- tungsten carbide reinforced copper matrix composites and other metal composites are known, to-date it appears unknown to produce particle reinforced noble metal matrix composites via infrared heating.
- These particle reinforced noble metal matrix composites include a noble metal, as the base, and a particle filler material, such as a carbide, that is added to improve the properties of the resulting composite.
- Noble metals also referred to as noble metals, are understood to include silver, gold, the six platinum-group metals (platinum, palladium, ruthenium, rhodium, osmium, and iridium), and alloys thereof. These noble metals are seen in our everyday lives and are used extensively in jewelry, tableware, electrical contacts, etc.
- Each of the above noted noble metals in general, include distinct individual characteristics from metals that must be considered when producing a particle reinforced noble metal matrix composite via infrared heating. These characteristics coupled with the understanding that the infrared heating process itself includes at least two parameters that appear to be critical to form a metal composite: 1) temperature, which is critical for superheating and for sufficient viscosity of the metal, and 2) pressure, which is important in forcing liquid metal into the particle material, results in great efforts when attempting to produce, via infrared heating, a particle reinforced noble metal matrix composite of sufficient quality.
- the jewelry industry is one industry that stands to benefit from particle reinforced noble metal composites that are provided with at least sufficient wear resistance and that are produced in a manner that reduces the labor and time required for processing thereof thereby reducing overall production and purchase costs.
- the auto, aviation, and power industries similarly are always seeking improved materials, such as for use in electrical contacts, which offer low resistance/high conductivity and which also are produced in a cost effective manner.
- a particle reinforced noble metal matrix composite having desired properties, such as good hardness and/or low resistivity, that reduces the labor and time required for processing thereof thereby reducing overall production costs
- the composite may be used in the jewelry industry, such as for making watches, rings, and other jewelry, and/or in the power, automobile, and aircraft industries, such as for making electrical contact materials.
- the present invention provides for particle reinforced noble metal matrix composites having sufficient hardness, i.e. good wear resistance, and low resistivity, and a method of making the same.
- Particle reinforced noble metal matrix composites including a noble metal, as the base, and a particle filler material, such as a carbide, are formed via an infrared heating process that includes the infiltration of a liquid noble metal within the interstitial spaces of a porous particle material preform, and subsequent solidification thereof.
- this group can include silver, gold, platinum, palladium, ruthenium, rhodium, osmium, iridium, and alloys thereof.
- the particle filler material includes carbides, such as tungsten and molybdenum carbide, having particle sizes greater than 0.1 ⁇ m but less than about 1000 ⁇ m.
- silver alloys should include at least about 50% silver, advantageously no less than about 90%.
- the gold alloys should include no less than about 41% gold, advantageously no less than about 58%.
- each of the platinum group metal alloys should include no less than about 50% of platinum, palladium, ruthenium, rhodium, osmium, or iridium, advantageously no less than about 93%.
- the particle reinforced noble metal matrix composites of the present invention include desirable properties, such as sufficient hardness, low resistivity, and/or high density, and are prepared generally according to the following method.
- a noble metal and a precast particle material are heated by infrared heating to a temperature above the melting point of the noble metal thereby producing a molten noble metal.
- the particle material is contacted with the molten noble metal in an inert atmosphere at standard atmospheric pressure for a period of time sufficient to allow the molten noble metal to infiltrate the particle material.
- the molten metal then is solidified within the interstitial spaces of the preform by cooling the particle reinforced noble metal matrix composite to about room temperature.
- the liquid noble metal infiltration is carried out without the application of any pressure on the liquid metal.
- the threshold pressure at the infiltration front is overcome due to the wetting characteristics between the carbide materials and the noble metals.
- the particle reinforced noble metal matrix composite includes a noble metal content of at least 56% by weight.
- the particle reinforced noble metal matrix composite includes gold or alloys thereof, advantageously red, green, yellow, or white gold alloys, and the particle reinforcement material includes either tungsten or molybdenum carbide.
- the composites are produced by the infrared heating process generally discussed above wherein a precast carbide material is contacted with the noble metal at a temperature above the melting point of the noble metal to form the composite. More specifically, the gold and gold alloys are heated in a chamber by a tungsten halogen lamp to a temperature of about 1250° C. at a rate of no greater than about 100° C./sec to produce a molten metal. The molten metal is allowed to contact and infiltrate the carbide material for about 240 seconds to form a composite material.
- the particle reinforced gold or gold alloy matrix composites include a resistivity of no greater than about 1.3E-04 ohm centimeters, a Vickers hardness of at least 171, and a density value of at least 97% of a theoretical density value.
- various colored composites such as pink, green, yellow, and white, are produced as a result of the gold or gold alloy.
- the particle reinforced noble metal matrix composite include silver or alloys thereof and the particle reinforcement material includes tungsten carbide.
- the composites are produced by the infrared heating process discussed below wherein a precast tungsten carbide material is contacted with the noble metal at a temperature above the melting point of the noble metal to form the composite. More specifically, the silver and silver alloys similarly are heated in a chamber by a tungsten halogen lamp to a temperature of about 1250° C. at a rate of no greater than about 100° C./sec and allowed to contact and infiltrate the tungsten carbide material for about 240 seconds to form the composite. The composite then is cooled down to room temperature such as at about a rate of 20° C./sec.
- particle reinforced pure silver matrix composites include a resistivity of no greater than about 4.9E-06 ohm centimeters, a Vickers hardness of at least 251, and a density value of at least 97% of a theoretical density value.
- a particle reinforced noble metal matrix composite having at least sufficient hardness and/or low resistivity such that the composite may be used in the jewelry industry, such as for making watches, rings, and other jewelry, and/or in the power, automobile, and aircraft industries, such as for making electrical contact materials, and a method of making the same.
- the present invention provides for particle reinforced noble metal matrix composites having desired properties, such as sufficient hardness and/or low resistivity, and a method of making the same.
- an infrared heating process is used to prepare the particle reinforced noble metal matrix composites having a noble metal, as a base, and a particle reinforcing filler material, such as a carbide material, advantageously tungsten or molybdenum carbide.
- the noble metals include silver, gold, platinum, palladium, ruthenium, rhodium, osmium, iridium, and alloys thereof, advantageously gold, silver, and alloys thereof, more advantageously, silver and gold alloys.
- silver alloys should include at least about 50% silver, advantageously no less than about 90%.
- the gold alloys should include no less than about 41% gold, advantageously no less than about 58%.
- each of the platinum group metal alloys should include no less than about 50% of platinum, palladium, ruthenium, rhodium, osmium, or iridium, advantageously no less than about 93%.
- the particle materials may include oxides, such as iron, nickel, manganese, zinc, and chromium oxides, and the like, and the carbide materials may further include silicon, and calcium carbides, and the like.
- the particle material should include particle sizes greater than 0.1 ⁇ m but less than about 1000 ⁇ m.
- this process includes heating, or superheating, a noble metal and a precast particle material, such as a carbide preform, in a furnace chamber using an infrared heat source, such as a tungsten halogen lamp.
- the infrared light may include any infrared wavelength, and advantageously a wavelength of from about 0.6 ⁇ m to about 10 ⁇ m.
- the infrared heating is performed in an inert atmosphere, advantageously a nitrogen, helium, or argon atmosphere, most advantageously an argon atmosphere, at standard atmospheric pressure, and at a rate of no greater than about 100° C./sec to a temperature greater than the melting point of the noble metal, advantageously 1150° C. to 1350° C., more advantageously 1,200° C. to 1300° C., most advantageously 1250° C., to produce a molten noble metal.
- the noble metal is allowed to contact the preform at the temperature above the melting point of the noble metal for a period of sufficient to infiltrate the particle material to form the particle reinforced noble metal matrix composite.
- this period of time is about 60 to 600 seconds, more advantageously 120 to 480 seconds, and most advantageously 240 seconds.
- infiltration of the preform is progressive because the noble metal first fills large pores then small pores in the preform.
- surface energy differences act to promote infiltration, i.e. wetting of the particle material, at the infiltration front of the molten metal.
- the capillary forces of the preform act as the driving force for the infiltration of the noble metal into the preform.
- the molten metal of the composite is solidified within the interstitial spaces of the preform by cooling the particle reinforced noble metal matrix composite to about room temperature.
- the resulting particle reinforced noble metal matrix composite includes a noble metal content of at least 56% by weight, advantageously about 56% to 75% by weight, and desirable characteristics as discussed below.
- Each of the noble metal matrix materials used in the examples below was obtained from the Stueller Settings company of Lafayette, LA, in the form of casting grains.
- Five different noble metal matrix materials, identified as A, B, C, D, E, and F, are described in Table 1 below. These noble metals were used in producing the particle reinforced noble metal matrix composites listed in Tables 2-7, which respectively also are identified as A, B, C, D, E, and F based on the noble metal contained therein.
- Noble metal Composition and Characteristics A Gold alloy 14 k gold with 39.00% copper, 2.00% silver, and 0.40% zinc M.P. 931° C.
- gold purity may be indicated by the karat, which is a unit of fineness equal to 1/24 th part of pure gold.
- 24 karat (24 k) gold is pure gold; 18 k is 18/24 ths or about 75% gold; 14 k is 14/24 ths or about 58.33% gold; and 10 k is 10/24 ths or about 41.67% gold.
- the specific particle reinforcing materials used in the below discussed composites, as included in Tables 2-7, are molybdenum carbide and tungsten carbide.
- the tungsten carbide was obtained from Alfa Aesar of Ward Hill, Mass., in the form of a powder.
- Two different tungsten carbide powders hereinafter referred to as Powders #1 and #2, were obtained and used.
- Powder #1 includes a purity of 99.5% and has an average particle size of no greater than 1 ⁇ m.
- Powder #2 includes a purity of 99.75 and has particles sizes in the range of 44 to 149 ⁇ m. It is specifically noted that Powder #1 is used in each of the Table 2 composites while a 50/50 mixture by weight of Powder #1 and Powder #2 is used in each of the Table 3 composites.
- the molybdenum carbide material similarly is obtained from Alfa Aesar of Ward Hill, Mass., in the form of a powder.
- the molybdenum carbide powder includes 99.5% purity and has particles sizes in no greater than 44 ⁇ m.
- the particle powder material i.e. the tungsten or molybdenum carbide powder
- the particle powder material is cast to form a generally cylindrically shaped preform. More specifically, agglomerations of the powder are broken down using sieving, the mortar and pestle grinder, or any other commonly known technique. About 1.40 grams to 2.00 grams of powder, as indicated in Tables 2, 3, and 4, is weighed out using a digital balance to an accuracy of plus or minus 0.01 grams. The weighed powder is poured into a cylindrical die made of steel that has been thoroughly cleaned with acetone, dried, and lubricated with silicone lubricant to provide a smooth surface for the powder to be compacted.
- the die, containing the powder, is then subjected to cold hand pressing followed by mechanical compaction at a pressure of about 44,792 psi to produce cylindrical preforms having a diameter of about 0.377 inches and a height of about 0.150 inches.
- the particular green density for each preform was determined, by methods commonly known in the art, and is indicated in each of Tables 2, 3, and 4.
- each noble metal is cast into a block, by methods commonly known in the art, and the weight thereof is determined and indicated in Table 2, 3, and 4 below.
- a graphite crucible of 9.7 mm inner diameter is used to hold the preform and noble metal block.
- the preform first is loaded carefully into the graphite crucible to avoid cracking.
- the noble metal block is polished to remove an oxide layer, if applicable, then cleaned with acetone and deionized water, ultrasonically, and placed on top of the preform.
- the entire assembly then is placed in an infrared furnace and subjected to pressureless infrared heating, i.e. infrared heating at a standard atmospheric pressure of 1 atm, under an argon atmosphere.
- the furnace chamber is heated, or superheated, by a tungsten halogen lamp at a rate of no greater than about 100° C./sec, advantageously about 80° C./sec, from about room temperature to about 1250° C. to produce a molten noble metal.
- the infrared light advantageously has a wavelength of from about 0.6 to about 10 ⁇ m.
- the temperature during the process is monitored and controlled by using an S-type or a Pt/Pt-10% Rh thermocouple that is secured to the bottom of the crucible.
- the capillary forces of the preform act as the driving force for the infiltration of the noble metal into the preform.
- the noble metal is allowed to infiltrate the carbide preform at about 1250° C.
- the furnace chamber is provided with a vent to evacuate the argon gas when the molten metal flows down through the porous preform. Then, the composite is cooled to about room temperature, advantageously at a rate of about 20° C./sec.
- the composites include a noble metal content of at least 56% by weight, and were subjected to various characterization techniques immediately after infiltration for determination of density, hardness, and resistivity as discussed below with results being illustrated in Tables 5, 6, and 7.
- each composite consisted of a certain color as a result of the noble metal used therein. More specifically, composite A was pink, B was green, C was yellow, D was white, E was yellow, and F was silver in color.
- Group 1 Tungsten Carbide (WC) Particle Reinforced Noble Metal Matrix Composite TABLE 2 Particle Pre- Reinforced Mass of Infiltration Noble metal Noble Mass (Green) Pellet Matrix metal of WC Density Temperature Time Composite (gm) (gm) (gm/cc) (° C.) (sec.)
- gm Tungsten Carbide
- Green Pellet Matrix metal of WC Density Temperature Time Composite
- gm (gm) (gm/cc) (° C.) (sec.)
- Group 2 Mixed Tungsten Carbide Particle Reinforced Noble Metal Matrix Composite TABLE 3 Particle Pre- Reinforced Mass Infiltration Noble metal of Noble Mass (Green) Pellet Matrix metal of WC Density Temperature Time Composite (gm) (gm) (gm/cc) (° C.) (sec.)
- gm gm/cc
- Group 3 Molybdenum Carbide Particle Reinforced Noble Metal Matrix Composite TABLE 4 Particle Pre- Reinforced Mass Infiltration Noble metal of Noble Mass of (Green) Pellet Matrix metal MoC Density Temperature Time Composite (gm) (gm) (gm/cc) (° C.) (sec.) A 2.0459 1.4525 5.294 1250 240 B 2.1273 1.4484 5.279 1250 240 C 2.0347 1.4654 5.341 1250 240 D 2.1692 1.9697 5.384 1250 240 E 2.5500 1.4500 5.290 1250 240 Control Group 4: Noble Metals (A-F) With No Reinforcing Material
- Control Group 4 includes the noble metals (A-F), as characterized in Table 1, minus the particle reinforcing material.
- A-F the noble metals
- Each of the Group 4 noble metals and metal alloys are subjected to the same processing steps as above described.
- each prepared composite from Table 2 (Group 1), Table 3 (Group 2), and Table 4 (Group 3) are listed in Table 5 below.
- Table 5 The densities of each prepared composite from Table 2 (Group 1), Table 3 (Group 2), and Table 4 (Group 3) are listed in Table 5 below.
- each composite is cut into a rectangular block by a high-speed saw having a diamond blade. Prior to characterization, excess noble metal on the composite surface was removed with cutting and grinding. Density was determined using Archimedes principle of water displacement using a Mettler H54AR suspension balance. Each composite was weighed in air, then in de-ionized water. The weight difference between the air and water was used to calculate the sample volume. The water density was taken to be 1 gm/cm 3 .
- the composites showed good resulting density as determined by microstructural examination using means, e.g. optical microscope means, commonly known in the art. Micro images indicated that infiltration was essentially complete and that resulting pores sizes were negligible. In addition, good resulting density can be shown in relation to theoretical densities by utilizing the rule of mixtures for composites, as is commonly known in the art. Overall, the density values of the particle reinforced noble metal matrix composites as determined by microstructural analysis is believed to be at least about 97% and greater of the theoretical density value.
- each prepared composite from Table 2 (Group 1), Table 3 (Group 2), and Table 4 (Group 3) is listed in Table 6 below.
- Hardness was considered to be a measure of wear resistance which was measured using a Vicker's hardness tester, M-400-H1 obtained from Leco of St. Joseph, Mich., at a constant load of 100 gm and dwelling time of 15 seconds for each composite. At least 10 measurements were done for each sample. The average value was taken after removing the highest and lowest value.
- the hardness value is about 216 VHN and 251 VHN respectively.
- composites E (pure gold) and F (pure silver) in Group 1 show a significant improvement in hardness over pure gold and pure silver respectively.
- the hardness value, or wear resistance, of the other composites (A-D) in Groups 1, 2, and 3 is significantly greater than pure gold or pure silver as well as their corresponding composite in Control Group 4.
- almost all of the gold alloy composites in Groups 1-3 show greater than a 100% increase of hardness over pure gold and silver.
- each prepared composite from Table 2 (Group 1), Table 3 (Group 2), and Table 4 (Group 3) is listed in Table 7 below.
- Table 7 The electrical resistivity is assessed using a four-point-probe technique, and more specifically a C4S-64/5S four-point probe, at a constant current of 2 Amp. The spacing between the probes is 0.159 cm.
- the resistivity is about 2.2 ⁇ 10 ⁇ 6 ⁇ -cm and 1.6 ⁇ 10 ⁇ 6 ⁇ -cm respectively.
- the resulting resistivity of the particle reinforced noble metal composites for all Groups is similar to the resistivity of their respective pure noble metal. This similarity suggests that pores in the composite do little to affect the electrical properties thereof and confirms the homogenous microstructure and presence of a continuous network of noble metal matrix surrounding the carbide particles.
- the infrared heating process of the present invention produces a particle reinforced noble metal matrix composite having desirable properties, such as sufficient hardness and/or low resistivity.
- the resulting composites advantageously can be prepared in a short period of time and can be used in the jewelry industry, such as for making watches, rings, and other jewelry, and/or in the power, automobile, and aircraft industries, such as for making electrical contact materials.
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Abstract
The present invention relates to particle reinforced noble metal matrix composites and a method of making the same. The composites include a noble metal such as silver, gold, and alloys thereof, as a base or matrix, and a particle reinforced filler material, such as a carbide. A pressureless infrared heating, or superheating, process is used to produce the particle reinforced noble metal matrix composites thereby providing a composite with at least sufficient hardness, i.e. wear resistance, and/or low resistivity. The composites may be used in the jewelry industry, such as for making watches, rings, and other jewelry, and/or in the power, automobile, and aircraft industries, such as for making electrical contact materials.
Description
- 1. Field of the Invention
- The present invention pertains generally to metal matrix composite materials and, more particularly, to particle reinforced noble metal matrix composites and a method of making the same.
- 2. Description of Related Art
- Generally, composite materials consist of a bulk or base material, i.e. a matrix, and a filler reinforcement material, such as fibers, whiskers, or particles. The composite materials can be classified into three categories: 1) polymer, 2) metal, and 3) ceramic depending on the matrix employed, and can be further divided depending on the type of reinforcement material provided. These further divisions include dispersion strengthened, particle reinforced, or fiber reinforced type composites.
- In the production of particle reinforced metal matrix composites, two or more materials, such as a metal and a particle material, may be combined together in a certain order on a macroscopic level to form a new material with potentially different and attractive properties. These attractive properties may include improved hardness, conductivity, density yield, etc. Generally, a composite is developed for use in a desired industry, such as the jewelry industry, with an eye toward improving at least one or more of the above noted properties and/or improving the method of making thereof, for example, by reducing production time to reduce costs.
- Methods for fabricating metal matrix composites vary and can include conventional powder metallurgy, in-situ using laser technology, electroless plating, hot pressing, and liquid metal infiltration. Each process includes advantages and disadvantages that may change dependent upon the material(s) used in making the metal composite. New and improved metal composites may be developed through new methods or by adapting existing methods, which may themselves be improved. For example, tungsten carbide reinforced copper matrix composites have been made, utilizing liquid metal infiltration, via an infrared heating process to produce a metal matrix composite having good hardness, conductivity, and density. Infrared processing also has been successfully used for joining advanced materials such as titanium-matrix composites, titanium aluminide, iron aluminide, nickel aluminide, titanium alloys, nickel based superalloys, carbon-carbon composites, and silicon carbide and carbon fiber reinforced titanium and aluminum matrix composites.
- Notably, infrared heating technology has been developing over about the last decade or so and is based on the generation of radiation by means of tungsten halogen lamps with a filament temperature of about 3000° C. Due to the selective absorption of infrared radiations and its cold wall process, it provides faster heating and cooling rates and has proved to be a quick, efficient, and energy conserving heating source.
- While tungsten carbide reinforced copper matrix composites and other metal composites, as well as the production thereof by infrared heating, are known, to-date it appears unknown to produce particle reinforced noble metal matrix composites via infrared heating. These particle reinforced noble metal matrix composites include a noble metal, as the base, and a particle filler material, such as a carbide, that is added to improve the properties of the resulting composite. Noble metals, also referred to as noble metals, are understood to include silver, gold, the six platinum-group metals (platinum, palladium, ruthenium, rhodium, osmium, and iridium), and alloys thereof. These noble metals are seen in our everyday lives and are used extensively in jewelry, tableware, electrical contacts, etc.
- Each of the above noted noble metals, in general, include distinct individual characteristics from metals that must be considered when producing a particle reinforced noble metal matrix composite via infrared heating. These characteristics coupled with the understanding that the infrared heating process itself includes at least two parameters that appear to be critical to form a metal composite: 1) temperature, which is critical for superheating and for sufficient viscosity of the metal, and 2) pressure, which is important in forcing liquid metal into the particle material, results in great efforts when attempting to produce, via infrared heating, a particle reinforced noble metal matrix composite of sufficient quality.
- The jewelry industry is one industry that stands to benefit from particle reinforced noble metal composites that are provided with at least sufficient wear resistance and that are produced in a manner that reduces the labor and time required for processing thereof thereby reducing overall production and purchase costs. In addition, the auto, aviation, and power industries similarly are always seeking improved materials, such as for use in electrical contacts, which offer low resistance/high conductivity and which also are produced in a cost effective manner.
- There is thus a need for a particle reinforced noble metal matrix composite having desired properties, such as good hardness and/or low resistivity, that reduces the labor and time required for processing thereof thereby reducing overall production costs wherein the composite may be used in the jewelry industry, such as for making watches, rings, and other jewelry, and/or in the power, automobile, and aircraft industries, such as for making electrical contact materials.
- The present invention provides for particle reinforced noble metal matrix composites having sufficient hardness, i.e. good wear resistance, and low resistivity, and a method of making the same.
- Particle reinforced noble metal matrix composites including a noble metal, as the base, and a particle filler material, such as a carbide, are formed via an infrared heating process that includes the infiltration of a liquid noble metal within the interstitial spaces of a porous particle material preform, and subsequent solidification thereof. With respect to noble metals, this group can include silver, gold, platinum, palladium, ruthenium, rhodium, osmium, iridium, and alloys thereof. In addition, the particle filler material includes carbides, such as tungsten and molybdenum carbide, having particle sizes greater than 0.1 μm but less than about 1000 μm.
- Concerning the noble metal alloys, silver alloys should include at least about 50% silver, advantageously no less than about 90%. The gold alloys should include no less than about 41% gold, advantageously no less than about 58%. And, each of the platinum group metal alloys should include no less than about 50% of platinum, palladium, ruthenium, rhodium, osmium, or iridium, advantageously no less than about 93%.
- The particle reinforced noble metal matrix composites of the present invention include desirable properties, such as sufficient hardness, low resistivity, and/or high density, and are prepared generally according to the following method. A noble metal and a precast particle material are heated by infrared heating to a temperature above the melting point of the noble metal thereby producing a molten noble metal. The particle material is contacted with the molten noble metal in an inert atmosphere at standard atmospheric pressure for a period of time sufficient to allow the molten noble metal to infiltrate the particle material. The molten metal then is solidified within the interstitial spaces of the preform by cooling the particle reinforced noble metal matrix composite to about room temperature. The liquid noble metal infiltration is carried out without the application of any pressure on the liquid metal. Notably, the threshold pressure at the infiltration front is overcome due to the wetting characteristics between the carbide materials and the noble metals. Advantageously, the particle reinforced noble metal matrix composite includes a noble metal content of at least 56% by weight.
- In exemplary embodiments, the particle reinforced noble metal matrix composite includes gold or alloys thereof, advantageously red, green, yellow, or white gold alloys, and the particle reinforcement material includes either tungsten or molybdenum carbide. The composites are produced by the infrared heating process generally discussed above wherein a precast carbide material is contacted with the noble metal at a temperature above the melting point of the noble metal to form the composite. More specifically, the gold and gold alloys are heated in a chamber by a tungsten halogen lamp to a temperature of about 1250° C. at a rate of no greater than about 100° C./sec to produce a molten metal. The molten metal is allowed to contact and infiltrate the carbide material for about 240 seconds to form a composite material. The composite then is cooled down to room temperature such as at about a rate of 20° C./sec. Advantageously, the particle reinforced gold or gold alloy matrix composites include a resistivity of no greater than about 1.3E-04 ohm centimeters, a Vickers hardness of at least 171, and a density value of at least 97% of a theoretical density value. In addition, various colored composites, such as pink, green, yellow, and white, are produced as a result of the gold or gold alloy.
- In another exemplary embodiment, the particle reinforced noble metal matrix composite include silver or alloys thereof and the particle reinforcement material includes tungsten carbide. The composites are produced by the infrared heating process discussed below wherein a precast tungsten carbide material is contacted with the noble metal at a temperature above the melting point of the noble metal to form the composite. More specifically, the silver and silver alloys similarly are heated in a chamber by a tungsten halogen lamp to a temperature of about 1250° C. at a rate of no greater than about 100° C./sec and allowed to contact and infiltrate the tungsten carbide material for about 240 seconds to form the composite. The composite then is cooled down to room temperature such as at about a rate of 20° C./sec. Advantageously, particle reinforced pure silver matrix composites include a resistivity of no greater than about 4.9E-06 ohm centimeters, a Vickers hardness of at least 251, and a density value of at least 97% of a theoretical density value.
- By virtue of the foregoing, there is thus provided a particle reinforced noble metal matrix composite having at least sufficient hardness and/or low resistivity such that the composite may be used in the jewelry industry, such as for making watches, rings, and other jewelry, and/or in the power, automobile, and aircraft industries, such as for making electrical contact materials, and a method of making the same.
- The features and objectives of the present invention will become more readily apparent from the following Detailed Description
- The present invention provides for particle reinforced noble metal matrix composites having desired properties, such as sufficient hardness and/or low resistivity, and a method of making the same.
- To this end, an infrared heating process is used to prepare the particle reinforced noble metal matrix composites having a noble metal, as a base, and a particle reinforcing filler material, such as a carbide material, advantageously tungsten or molybdenum carbide.
- The noble metals include silver, gold, platinum, palladium, ruthenium, rhodium, osmium, iridium, and alloys thereof, advantageously gold, silver, and alloys thereof, more advantageously, silver and gold alloys. Concerning the noble metal alloys, silver alloys should include at least about 50% silver, advantageously no less than about 90%. The gold alloys should include no less than about 41% gold, advantageously no less than about 58%. And, each of the platinum group metal alloys should include no less than about 50% of platinum, palladium, ruthenium, rhodium, osmium, or iridium, advantageously no less than about 93%. In addition, the particle materials may include oxides, such as iron, nickel, manganese, zinc, and chromium oxides, and the like, and the carbide materials may further include silicon, and calcium carbides, and the like. The particle material should include particle sizes greater than 0.1 μm but less than about 1000 μm.
- Concerning the infrared heating process, this process includes heating, or superheating, a noble metal and a precast particle material, such as a carbide preform, in a furnace chamber using an infrared heat source, such as a tungsten halogen lamp. The infrared light may include any infrared wavelength, and advantageously a wavelength of from about 0.6 μm to about 10 μm. The infrared heating is performed in an inert atmosphere, advantageously a nitrogen, helium, or argon atmosphere, most advantageously an argon atmosphere, at standard atmospheric pressure, and at a rate of no greater than about 100° C./sec to a temperature greater than the melting point of the noble metal, advantageously 1150° C. to 1350° C., more advantageously 1,200° C. to 1300° C., most advantageously 1250° C., to produce a molten noble metal.
- The noble metal is allowed to contact the preform at the temperature above the melting point of the noble metal for a period of sufficient to infiltrate the particle material to form the particle reinforced noble metal matrix composite. Advantageously, this period of time is about 60 to 600 seconds, more advantageously 120 to 480 seconds, and most advantageously 240 seconds. In general, infiltration of the preform is progressive because the noble metal first fills large pores then small pores in the preform. Notably, surface energy differences act to promote infiltration, i.e. wetting of the particle material, at the infiltration front of the molten metal. The capillary forces of the preform act as the driving force for the infiltration of the noble metal into the preform.
- Finally, the molten metal of the composite is solidified within the interstitial spaces of the preform by cooling the particle reinforced noble metal matrix composite to about room temperature. The resulting particle reinforced noble metal matrix composite includes a noble metal content of at least 56% by weight, advantageously about 56% to 75% by weight, and desirable characteristics as discussed below.
- Accordingly, various exemplary embodiments of the particle reinforced noble metal matrix composites of the present invention will now be described along with the infrared heating process used for making them.
- Materials
- Each of the noble metal matrix materials used in the examples below was obtained from the Stueller Settings company of Lafayette, LA, in the form of casting grains. Five different noble metal matrix materials, identified as A, B, C, D, E, and F, are described in Table 1 below. These noble metals were used in producing the particle reinforced noble metal matrix composites listed in Tables 2-7, which respectively also are identified as A, B, C, D, E, and F based on the noble metal contained therein.
TABLE 1 Composition and Characteristics of Noble metals Used Group No. Noble metal Composition and Characteristics A Gold alloy 14 k gold with 39.00% copper, 2.00% silver, and 0.40% zinc M.P. 931° C. Red in color B Gold alloy 14 k gold with 2.00% copper, 39.00% silver, and 0.40% zinc M.P. 958° C. Green in color C Gold alloy 14 k gold with with 29.00% copper, 8.00% silver, and 4.50% zinc M.P. 861° C. Bright yellow in color D Gold alloy 14 k gold with with 25.50% copper, 9.00% zinc, and 7.50% nickel M.P. 946° C. Yellowish white in color E Pure gold 24 k M.P. 1064.4° C. Yellow in color F Pure Silver 99.99% Silver M.P. 961.8° C. Silver in color - With specific reference to gold, as is commonly understood in the art, gold purity may be indicated by the karat, which is a unit of fineness equal to 1/24th part of pure gold. As such, 24 karat (24 k) gold is pure gold; 18 k is 18/24 ths or about 75% gold; 14 k is 14/24 ths or about 58.33% gold; and 10 k is 10/24 ths or about 41.67% gold.
- Particle Material
- The specific particle reinforcing materials used in the below discussed composites, as included in Tables 2-7, are molybdenum carbide and tungsten carbide.
- The tungsten carbide was obtained from Alfa Aesar of Ward Hill, Mass., in the form of a powder. Two different tungsten carbide powders, hereinafter referred to as Powders #1 and #2, were obtained and used. Powder #1 includes a purity of 99.5% and has an average particle size of no greater than 1 μm. Powder #2 includes a purity of 99.75 and has particles sizes in the range of 44 to 149 μm. It is specifically noted that Powder #1 is used in each of the Table 2 composites while a 50/50 mixture by weight of Powder #1 and Powder #2 is used in each of the Table 3 composites.
- The molybdenum carbide material similarly is obtained from Alfa Aesar of Ward Hill, Mass., in the form of a powder. The molybdenum carbide powder includes 99.5% purity and has particles sizes in no greater than 44 μm.
- Experimental Methodology
- Each of the particle reinforced noble metal composites (A-F), identified in Tables 2-7, are made according to the below described experimental methodology.
- Preform Casting and Noble Metal Preparation
- In preparation for composite formation, the particle powder material, i.e. the tungsten or molybdenum carbide powder, is cast to form a generally cylindrically shaped preform. More specifically, agglomerations of the powder are broken down using sieving, the mortar and pestle grinder, or any other commonly known technique. About 1.40 grams to 2.00 grams of powder, as indicated in Tables 2, 3, and 4, is weighed out using a digital balance to an accuracy of plus or minus 0.01 grams. The weighed powder is poured into a cylindrical die made of steel that has been thoroughly cleaned with acetone, dried, and lubricated with silicone lubricant to provide a smooth surface for the powder to be compacted. The die, containing the powder, is then subjected to cold hand pressing followed by mechanical compaction at a pressure of about 44,792 psi to produce cylindrical preforms having a diameter of about 0.377 inches and a height of about 0.150 inches. The particular green density for each preform was determined, by methods commonly known in the art, and is indicated in each of Tables 2, 3, and 4.
- Concerning the noble metal grains characterized above in Table 1, each noble metal is cast into a block, by methods commonly known in the art, and the weight thereof is determined and indicated in Table 2, 3, and 4 below.
- Heating, and Cooling
- For composite formation, a graphite crucible of 9.7 mm inner diameter is used to hold the preform and noble metal block. The preform first is loaded carefully into the graphite crucible to avoid cracking. The noble metal block is polished to remove an oxide layer, if applicable, then cleaned with acetone and deionized water, ultrasonically, and placed on top of the preform. The entire assembly then is placed in an infrared furnace and subjected to pressureless infrared heating, i.e. infrared heating at a standard atmospheric pressure of 1 atm, under an argon atmosphere.
- The furnace chamber is heated, or superheated, by a tungsten halogen lamp at a rate of no greater than about 100° C./sec, advantageously about 80° C./sec, from about room temperature to about 1250° C. to produce a molten noble metal. The infrared light advantageously has a wavelength of from about 0.6 to about 10 μm. The temperature during the process is monitored and controlled by using an S-type or a Pt/Pt-10% Rh thermocouple that is secured to the bottom of the crucible. The capillary forces of the preform act as the driving force for the infiltration of the noble metal into the preform. The noble metal is allowed to infiltrate the carbide preform at about 1250° C. for a period of about 240 seconds to form the particle reinforced noble metal matrix composite. The furnace chamber is provided with a vent to evacuate the argon gas when the molten metal flows down through the porous preform. Then, the composite is cooled to about room temperature, advantageously at a rate of about 20° C./sec.
- The composites, thus obtained, include a noble metal content of at least 56% by weight, and were subjected to various characterization techniques immediately after infiltration for determination of density, hardness, and resistivity as discussed below with results being illustrated in Tables 5, 6, and 7. In addition, each composite consisted of a certain color as a result of the noble metal used therein. More specifically, composite A was pink, B was green, C was yellow, D was white, E was yellow, and F was silver in color.
- Group 1: Tungsten Carbide (WC) Particle Reinforced Noble Metal Matrix Composite
TABLE 2 Particle Pre- Reinforced Mass of Infiltration Noble metal Noble Mass (Green) Pellet Matrix metal of WC Density Temperature Time Composite (gm) (gm) (gm/cc) (° C.) (sec.) A 3.0105 2.0016 8.046 1250 240 B 3.0105 2.0020 8.047 1250 240 C 2.5169 2.0050 8.059 1250 240 D 2.5074 2.0035 8.053 1250 240 E 1.5904 1.6741 8.028 1250 240 F 2.5500 1.6500 8.040 1250 240 - Group 2: Mixed Tungsten Carbide Particle Reinforced Noble Metal Matrix Composite
TABLE 3 Particle Pre- Reinforced Mass Infiltration Noble metal of Noble Mass (Green) Pellet Matrix metal of WC Density Temperature Time Composite (gm) (gm) (gm/cc) (° C.) (sec.) A 2.5354 1.9614 9.748 1250 240 B 2.5152 1.9440 9.750 1250 240 C 2.5282 1.9430 9.745 1250 240 D 2.5232 1.9410 9.735 1250 240 E 2.5570 1.5870 8.033 1250 240 - Group 3: Molybdenum Carbide Particle Reinforced Noble Metal Matrix Composite
TABLE 4 Particle Pre- Reinforced Mass Infiltration Noble metal of Noble Mass of (Green) Pellet Matrix metal MoC Density Temperature Time Composite (gm) (gm) (gm/cc) (° C.) (sec.) A 2.0459 1.4525 5.294 1250 240 B 2.1273 1.4484 5.279 1250 240 C 2.0347 1.4654 5.341 1250 240 D 2.1692 1.9697 5.384 1250 240 E 2.5500 1.4500 5.290 1250 240
Control Group 4: Noble Metals (A-F) With No Reinforcing Material - The density, hardness, and resistivity of each of the prepared particle reinforced noble metal matrix composites is further compared in Tables 5, 6, and 7 against control Group 4. Control Group 4 includes the noble metals (A-F), as characterized in Table 1, minus the particle reinforcing material. Each of the Group 4 noble metals and metal alloys are subjected to the same processing steps as above described.
- Methods Used to Determine Physical Properties of Composite Density
- The densities of each prepared composite from Table 2 (Group 1), Table 3 (Group 2), and Table 4 (Group 3) are listed in Table 5 below. To measure the density, each composite is cut into a rectangular block by a high-speed saw having a diamond blade. Prior to characterization, excess noble metal on the composite surface was removed with cutting and grinding. Density was determined using Archimedes principle of water displacement using a Mettler H54AR suspension balance. Each composite was weighed in air, then in de-ionized water. The weight difference between the air and water was used to calculate the sample volume. The water density was taken to be 1 gm/cm3.
- The composites showed good resulting density as determined by microstructural examination using means, e.g. optical microscope means, commonly known in the art. Micro images indicated that infiltration was essentially complete and that resulting pores sizes were negligible. In addition, good resulting density can be shown in relation to theoretical densities by utilizing the rule of mixtures for composites, as is commonly known in the art. Overall, the density values of the particle reinforced noble metal matrix composites as determined by microstructural analysis is believed to be at least about 97% and greater of the theoretical density value.
- Resulting Properties of Particle Reinforced Noble metal Matrix Composites
TABLE 5 DENSITY (gm/cc) Particle Group 2 Reinforced Group 1 (tungsten Control Noble metal (tungsten carbide, Group 3 Group 4 Matrix carbide, mixed (molybdenum (no reinforcing Composite Powder #1) 50/50) carbide) material) A 12.698 14.730 10.490 — B 13.610 14.980 11.090 — C 12.701 14.920 10.530 — D 12.973 14.320 10.190 — E 15.308 16.486 11.320 19.3 F 13.150 — — 10.5
Hardness - The hardness of each prepared composite from Table 2 (Group 1), Table 3 (Group 2), and Table 4 (Group 3) is listed in Table 6 below. To measure the hardness, each composite is cut into a rectangular block by a high-speed saw having a diamond blade. Hardness was considered to be a measure of wear resistance which was measured using a Vicker's hardness tester, M-400-H1 obtained from Leco of St. Joseph, Mich., at a constant load of 100 gm and dwelling time of 15 seconds for each composite. At least 10 measurements were done for each sample. The average value was taken after removing the highest and lowest value.
- With specific reference to pure gold and pure silver, the hardness value is about 216 VHN and 251 VHN respectively. In comparison, composites E (pure gold) and F (pure silver) in Group 1 show a significant improvement in hardness over pure gold and pure silver respectively. In addition, the hardness value, or wear resistance, of the other composites (A-D) in Groups 1, 2, and 3 is significantly greater than pure gold or pure silver as well as their corresponding composite in Control Group 4. In fact, almost all of the gold alloy composites in Groups 1-3 show greater than a 100% increase of hardness over pure gold and silver.
TABLE 6 HARDNESS (VHN) Particle Group 2 Reinforced Group 1 (tungsten Noble metal (tungsten carbide, Group 3 Group 4 Matrix carbide, mixed (molybdenum (no reinforcing Composite Powder #1) 50/50) carbide) material) A 517.15 517.15 409.34 139.60 B 407.01 407.01 341.20 83.17 C 532.39 532.39 455.95 137.87 D 582.35 582.35 483.51 152.53 E 245.34 — 171.24 82.73 F 366.94 — — 86.42
Resistivity - The resistivity of each prepared composite from Table 2 (Group 1), Table 3 (Group 2), and Table 4 (Group 3) is listed in Table 7 below. To measure the resistivity, each composite is machined so as to form a square bar having the following dimensions: 0.9×0.35×0.25 cm. The electrical resistivity is assessed using a four-point-probe technique, and more specifically a C4S-64/5S four-point probe, at a constant current of 2 Amp. The spacing between the probes is 0.159 cm. The resistivity was calculated by the following equation:
ρ=π×V/ln 2×I
where ρ is the resistivity (Ω-cm), V is the output voltage (V), and I is the input current (Amp). About seven readings were taken with each composite and the average value was calculated after removing the highest and lowest value. - With specific reference to pure gold and pure silver, the resistivity is about 2.2×10−6 Ω-cm and 1.6×10−6 Ω-cm respectively. Notably, the resulting resistivity of the particle reinforced noble metal composites for all Groups is similar to the resistivity of their respective pure noble metal. This similarity suggests that pores in the composite do little to affect the electrical properties thereof and confirms the homogenous microstructure and presence of a continuous network of noble metal matrix surrounding the carbide particles.
TABLE 7 RESISTIVITY (Ω-cm) Particle Reinforced Group 1 Group 2 Noble metal (tungsten (tungsten Group 3 Group 4 Matrix carbide, carbide, mixed (molybdenum (no reinforcing Composite Powder #1) 50/50) carbide) material) A 4.31679E−05 3.60896E−05 8.2149E−05 2.652E−05 B 4.67570E−05 4.55606E−05 6.8092E−05 2.791E−05 C 5.31374E−05 6.80917E−05 8.7333E−05 3.370E−05 D 7.44722E−05 8.43420E−05 1.3249E−04 7.328E−05 E 2.67183E−05 — 5.5032E−05 1.376E−05 F 4.98000E−06 — — 9.380E−06 - Accordingly, the infrared heating process of the present invention produces a particle reinforced noble metal matrix composite having desirable properties, such as sufficient hardness and/or low resistivity. The resulting composites advantageously can be prepared in a short period of time and can be used in the jewelry industry, such as for making watches, rings, and other jewelry, and/or in the power, automobile, and aircraft industries, such as for making electrical contact materials.
- While the present invention has been illustrated by a description of various versions, and while the illustrative versions have been described in considerable detail, it is not the intention of the inventor(s) to restrict or in any way limit the scope of the appended claims to such detail. Additional advantages and modifications will readily appear to those skilled in the art. The invention in its broader aspects is therefore not limited to the specific details, representative apparatus and methods, and illustrative examples shown and described. Accordingly, departures may be made from such details without departing from the spirit or scope of the inventor's (inventors') general inventive concept.
Claims (28)
1. A method of making a particle reinforced noble metal matrix composite, comprising the steps of:
heating a noble metal and a particle material by infrared heating to a temperature above the melting point of the noble metal thereby producing a molten noble metal; and
contacting the particle material with the molten noble metal for a period of time sufficient to allow the molten noble metal to infiltrate the particle material to form a particle reinforced noble metal matrix composite.
2. The method of claim 1 wherein the noble metal is silver, gold, or alloys thereof and the particle material includes a carbide.
3. The method of claim 2 wherein the carbide includes either molybdenum carbide or tungsten carbide.
4. The method of claim 1 wherein the heating step includes heating the noble 5metal and the particle material by infrared heating at a rate not greater than about 100° C. per second to the temperature above the melting point of the noble metal.
5. The method of claim 1 wherein the heating step includes heating the noble metal and the particle material by infrared heating at a wavelength of about 0.6 μm to 10 μm.
6. The method of claim 1 wherein the contacting step includes contacting the particle material with the molten noble metal at the temperature above the melting point of the noble metal for about 60 seconds to about 600 seconds to allow the molten noble metal to infiltrate the particle material.
7. The method of claim 1 wherein the contacting step is performed in an inert atmosphere and at no greater than a pressure of about 1 atm.
8. A method of making a particle reinforced noble metal matrix composite, comprising the steps of:
heating a noble metal selected from the group consisting of silver, gold, and alloys thereof and either tungsten carbide or molybdenum carbide by infrared heating to a temperature above the melting point of the noble metal thereby producing a molten noble metal;
contacting the tungsten carbide or molybdenum carbide with the molten noble metal for a period of time sufficient to allow the molten noble metal to infiltrate the carbide material to form a particle reinforced noble metal matrix composite; and
cooling the particle reinforced noble metal matrix to about room temperature.
9. The method of claim 9 wherein the heating step includes heating the noble metal and the carbide material by infrared heating at a rate not greater than about 100° C. per second to a temperature of about 1200° C. to 1300° C.
10. The method of claim 9 wherein the heating step includes heating the noble metal and the particle material by infrared heating at a wavelength of about 0.6 μm to 10 μm.
11. The method of claim 9 wherein the contacting step is performed in an inert atmosphere and at no greater than a pressure of about 1 atm.
12. The method of claim 9 wherein the contacting step includes contacting the carbide material with the molten noble metal at the temperature above the melting point of the noble metal for about 200 to 300 seconds to allow the molten noble metal to infiltrate the carbide material.
13. The method of claim 9 wherein the step of cooling the particle reinforced noble metal matrix composite to about room temperature includes cooling at a rate of no less than about 20° C. per second to about room temperature.
14. A particle reinforced noble metal matrix composite, comprising:
a noble metal and a particle material, wherein the particle reinforced noble metal matrix composite includes a noble metal content of at least about 56% by weight and a Vickers hardness of at least about 171.
15. The particle reinforced noble metal matrix composite of claim 14 wherein the noble metal is silver, gold, or alloys thereof and the particle material includes a carbide.
16. The particle reinforced noble metal matrix composite of claim 15 wherein the carbide includes tungsten carbide or molybdenum carbide.
17. The particle reinforced noble metal matrix composite of claim 14 wherein the noble metal is silver and the particle material includes a carbide, and wherein the particle reinforced noble metal matrix composite includes a Vickers hardness of at least 251.
18. The particle reinforced noble metal matrix composite of claim 14 wherein the noble metal is gold or an alloy thereof and the particle material includes a carbide, and wherein the particle reinforced noble metal matrix composite includes a Vickers hardness of at least about 216.
19. The particle reinforced noble metal matrix composite of claim wherein a density value of the particle reinforced noble metal matrix composite is at least about 97% of a theoretical density value.
20. A particle reinforced noble metal matrix composite, comprising:
a noble metal and a particle material, wherein the particle reinforced noble metal matrix composite includes a noble metal content of at least 56% by weight and a resistivity of no greater than about 1.3E-04 ohm centimeters.
21. The particle reinforced noble metal matrix composite of claim 20 wherein the noble metal is silver, gold, or alloys thereof and the particle material includes a carbide.
22. The particle reinforced noble metal matrix composite of claim 21 wherein the carbide includes tungsten carbide or molybdenum carbide.
23. The particle reinforced noble metal matrix composite of claim 20 wherein the noble metal is a silver alloy and the particle material includes a carbide, and wherein the particle reinforced noble metal matrix composite includes a resistivity of no greater than about 4.9E-06 ohm centimeters.
24. The particle reinforced noble metal matrix composite of claim 20 wherein the noble metal is gold or an alloy thereof and the particle material includes tungsten carbide, and wherein the particle reinforced noble metal matrix composite includes a resistivity of no greater than about 8.4E-05 ohm centimeters.
25. The particle reinforced noble metal matrix composite of claim 20 wherein a density value of the particle reinforced noble metal matrix composite is at least about 97% of a theoretical density value.
26. A particle reinforced noble metal matrix composite, comprising:
a particle material; and
a noble metal selected from the group consisting of gold, silver, platinum, and alloys thereof wherein the particle reinforced noble metal matrix composite includes a noble metal content of at least about 56% by weight.
27. The particle reinforced noble metal matrix composite of claim 26 wherein the particle material includes a carbide.
28. The particle reinforced noble metal matrix composite of claim 27 wherein the carbide includes tungsten carbide or molybdenum carbide.
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US10/974,229 US20060086441A1 (en) | 2004-10-27 | 2004-10-27 | Particle reinforced noble metal matrix composite and method of making same |
EP05857824A EP1825015A4 (en) | 2004-10-27 | 2005-10-26 | Particle reinforced noble metal matrix composite and method of making same |
PCT/US2005/038671 WO2006110179A2 (en) | 2004-10-27 | 2005-10-26 | Particle reinforced noble metal matrix composite and method of making same |
US12/035,798 US7608127B2 (en) | 2004-10-27 | 2008-02-22 | Particle reinforced noble metal matrix composite and method of making same |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
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US20050129091A1 (en) * | 2003-12-16 | 2005-06-16 | Habboosh Samir W. | Extended temperature range EMF device |
DE102010026930A1 (en) * | 2010-07-12 | 2012-01-12 | C. Hafner Gmbh + Co. Kg | Ideally white precious metal-jewelry alloy, useful for preparing clocks, jewelry or its articles and/or writing instruments, comprises specified amount of rhodium and platinum |
US20150158081A1 (en) * | 2012-05-21 | 2015-06-11 | Teijin Limited | Manufacturing Method for Resin Shaped Product Including Casted Metal |
US9695090B2 (en) * | 2011-03-08 | 2017-07-04 | Hublot Sa | Composite material comprising a precious metal, manufacturing process and use of such material |
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Citations (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3459915A (en) * | 1967-05-03 | 1969-08-05 | Mallory & Co Inc P R | Electrical discharge machining electrode comprising tungsten particles in a silver matrix |
US3460920A (en) * | 1966-10-10 | 1969-08-12 | Whittaker Corp | Filament reinforced metal composites for gas turbine blades |
US3685134A (en) * | 1970-05-15 | 1972-08-22 | Mallory & Co Inc P R | Method of making electrical contact materials |
US3827883A (en) * | 1972-10-24 | 1974-08-06 | Mallory & Co Inc P R | Electrical contact material |
US3969570A (en) * | 1972-03-08 | 1976-07-13 | Smith Baynard R | Composition and method of bonding gold to a ceramic substrate and a bonded gold article |
US4309458A (en) * | 1978-10-16 | 1982-01-05 | Nihon Kogyo Kabushiki Kaisha | Process of producing composite powder coated with noble metal |
US4374086A (en) * | 1981-04-27 | 1983-02-15 | The United States Of America As Represented By The Secretary Of The Navy | Gold based material for electrical contact materials |
US4409037A (en) * | 1982-04-05 | 1983-10-11 | Macdermid Incorporated | Adhesion promoter for printed circuits |
US4450135A (en) * | 1982-01-04 | 1984-05-22 | Gte Laboratories Incorporated | Method of making electrical contacts |
US4512818A (en) * | 1983-05-23 | 1985-04-23 | Shipley Company Inc. | Solution for formation of black oxide |
US4530875A (en) * | 1982-10-13 | 1985-07-23 | Toyota Jidosha Kabushiki Kaisha | Silicon carbide whisker composite material with low non whisker particle content and method of manufacture thereof |
US4551596A (en) * | 1982-03-26 | 1985-11-05 | Hitachi, Ltd. | Surge-absorberless vacuum circuit interrupter |
US5045972A (en) * | 1990-08-27 | 1991-09-03 | The Standard Oil Company | High thermal conductivity metal matrix composite |
US5059255A (en) * | 1989-06-27 | 1991-10-22 | Ludwig Muller S.A. | Coloring a gold alloy |
US5139739A (en) * | 1989-02-28 | 1992-08-18 | Agency Of Industrial Science And Technology | Gold alloy for black coloring, processed article of black colored gold alloy and method for production of the processed article |
US5180551A (en) * | 1991-10-30 | 1993-01-19 | Leach & Garner Co. | Gold alloys of exceptional yellow color and reversible hardness |
US5681617A (en) * | 1993-10-01 | 1997-10-28 | University Of Cincinnati | Large scale metal coating of continuous ceramic fibers |
US5697421A (en) * | 1993-09-23 | 1997-12-16 | University Of Cincinnati | Infrared pressureless infiltration of composites |
US6174388B1 (en) * | 1999-03-15 | 2001-01-16 | Lockheed Martin Energy Research Corp. | Rapid infrared heating of a surface |
US6312495B1 (en) * | 1999-04-09 | 2001-11-06 | Louis Renner Gmbh | Powder-metallurgically produced composite material and method for its production |
US6868848B2 (en) * | 2000-05-18 | 2005-03-22 | The Commonwealth Of Australia Commonwealth Scientific And Industrial Research Organization | Cutting tool and method of using same |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3069759A (en) * | 1960-04-27 | 1962-12-25 | Grant | Production of dispersion strengthened metals |
GB1005461A (en) * | 1961-06-02 | 1965-09-22 | Stackpole Carbon Co | Electrical contact |
US3158469A (en) * | 1962-08-08 | 1964-11-24 | Stackpole Carbon Co | Electrical contact |
US4088480A (en) * | 1976-09-10 | 1978-05-09 | Gte Laboratories Incorporated | Process for preparing refractory metal-silver-cadmium alloys |
US4137076A (en) * | 1977-02-24 | 1979-01-30 | Westinghouse Electric Corp. | Electrical contact material of TiC, WC and silver |
-
2004
- 2004-10-27 US US10/974,229 patent/US20060086441A1/en not_active Abandoned
-
2005
- 2005-10-26 WO PCT/US2005/038671 patent/WO2006110179A2/en active Application Filing
- 2005-10-26 EP EP05857824A patent/EP1825015A4/en not_active Withdrawn
-
2008
- 2008-02-22 US US12/035,798 patent/US7608127B2/en not_active Expired - Fee Related
Patent Citations (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3460920A (en) * | 1966-10-10 | 1969-08-12 | Whittaker Corp | Filament reinforced metal composites for gas turbine blades |
US3459915A (en) * | 1967-05-03 | 1969-08-05 | Mallory & Co Inc P R | Electrical discharge machining electrode comprising tungsten particles in a silver matrix |
US3685134A (en) * | 1970-05-15 | 1972-08-22 | Mallory & Co Inc P R | Method of making electrical contact materials |
US3969570A (en) * | 1972-03-08 | 1976-07-13 | Smith Baynard R | Composition and method of bonding gold to a ceramic substrate and a bonded gold article |
US3827883A (en) * | 1972-10-24 | 1974-08-06 | Mallory & Co Inc P R | Electrical contact material |
US4309458A (en) * | 1978-10-16 | 1982-01-05 | Nihon Kogyo Kabushiki Kaisha | Process of producing composite powder coated with noble metal |
US4374086A (en) * | 1981-04-27 | 1983-02-15 | The United States Of America As Represented By The Secretary Of The Navy | Gold based material for electrical contact materials |
US4450135A (en) * | 1982-01-04 | 1984-05-22 | Gte Laboratories Incorporated | Method of making electrical contacts |
US4551596A (en) * | 1982-03-26 | 1985-11-05 | Hitachi, Ltd. | Surge-absorberless vacuum circuit interrupter |
US4409037A (en) * | 1982-04-05 | 1983-10-11 | Macdermid Incorporated | Adhesion promoter for printed circuits |
US4530875A (en) * | 1982-10-13 | 1985-07-23 | Toyota Jidosha Kabushiki Kaisha | Silicon carbide whisker composite material with low non whisker particle content and method of manufacture thereof |
US4512818A (en) * | 1983-05-23 | 1985-04-23 | Shipley Company Inc. | Solution for formation of black oxide |
US5139739A (en) * | 1989-02-28 | 1992-08-18 | Agency Of Industrial Science And Technology | Gold alloy for black coloring, processed article of black colored gold alloy and method for production of the processed article |
US5164026A (en) * | 1989-06-27 | 1992-11-17 | Ludwig Muller S.A. | Coloring a gold alloy |
US5059255A (en) * | 1989-06-27 | 1991-10-22 | Ludwig Muller S.A. | Coloring a gold alloy |
US5045972A (en) * | 1990-08-27 | 1991-09-03 | The Standard Oil Company | High thermal conductivity metal matrix composite |
US5180551A (en) * | 1991-10-30 | 1993-01-19 | Leach & Garner Co. | Gold alloys of exceptional yellow color and reversible hardness |
US5180551B1 (en) * | 1991-10-30 | 1995-09-19 | Swiss Bank Corp | ible hardness Gold alloys of exceptional yellow color and revers |
US5180551B2 (en) * | 1991-10-30 | 1999-02-09 | Fleet Precious Metals Inc | Gold alloys of exceptional yellow color and reversible hardness |
US5697421A (en) * | 1993-09-23 | 1997-12-16 | University Of Cincinnati | Infrared pressureless infiltration of composites |
US5681617A (en) * | 1993-10-01 | 1997-10-28 | University Of Cincinnati | Large scale metal coating of continuous ceramic fibers |
US6174388B1 (en) * | 1999-03-15 | 2001-01-16 | Lockheed Martin Energy Research Corp. | Rapid infrared heating of a surface |
US6312495B1 (en) * | 1999-04-09 | 2001-11-06 | Louis Renner Gmbh | Powder-metallurgically produced composite material and method for its production |
US6868848B2 (en) * | 2000-05-18 | 2005-03-22 | The Commonwealth Of Australia Commonwealth Scientific And Industrial Research Organization | Cutting tool and method of using same |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050129091A1 (en) * | 2003-12-16 | 2005-06-16 | Habboosh Samir W. | Extended temperature range EMF device |
US7131768B2 (en) * | 2003-12-16 | 2006-11-07 | Harco Laboratories, Inc. | Extended temperature range EMF device |
DE102010026930A1 (en) * | 2010-07-12 | 2012-01-12 | C. Hafner Gmbh + Co. Kg | Ideally white precious metal-jewelry alloy, useful for preparing clocks, jewelry or its articles and/or writing instruments, comprises specified amount of rhodium and platinum |
US9695090B2 (en) * | 2011-03-08 | 2017-07-04 | Hublot Sa | Composite material comprising a precious metal, manufacturing process and use of such material |
US20150158081A1 (en) * | 2012-05-21 | 2015-06-11 | Teijin Limited | Manufacturing Method for Resin Shaped Product Including Casted Metal |
US20240206048A1 (en) * | 2018-02-02 | 2024-06-20 | Kuprion Inc. | Thermal Management in Circuit Board Assemblies |
WO2022017697A3 (en) * | 2020-07-22 | 2022-03-24 | The Swatch Group Research And Development Ltd | Component for a timepiece or jewellery item made of cermet |
Also Published As
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WO2006110179A3 (en) | 2007-04-05 |
EP1825015A2 (en) | 2007-08-29 |
US7608127B2 (en) | 2009-10-27 |
US20080176063A1 (en) | 2008-07-24 |
WO2006110179A2 (en) | 2006-10-19 |
EP1825015A4 (en) | 2008-02-27 |
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