US20050166401A1 - Wear-resistant composite rings for jewelry, medical or industrial devices and manufacturing method therefor - Google Patents
Wear-resistant composite rings for jewelry, medical or industrial devices and manufacturing method therefor Download PDFInfo
- Publication number
- US20050166401A1 US20050166401A1 US10/769,356 US76935604A US2005166401A1 US 20050166401 A1 US20050166401 A1 US 20050166401A1 US 76935604 A US76935604 A US 76935604A US 2005166401 A1 US2005166401 A1 US 2005166401A1
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- precious metal
- groove
- annular
- blank
- metal wire
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- 238000004519 manufacturing process Methods 0.000 title abstract description 12
- 239000002131 composite material Substances 0.000 title description 17
- 238000000034 method Methods 0.000 abstract description 41
- 239000010970 precious metal Substances 0.000 abstract description 41
- 229910052751 metal Inorganic materials 0.000 abstract description 24
- 239000002184 metal Substances 0.000 abstract description 24
- 238000005229 chemical vapour deposition Methods 0.000 abstract description 19
- 238000003466 welding Methods 0.000 abstract description 9
- 238000005520 cutting process Methods 0.000 abstract description 6
- 238000005096 rolling process Methods 0.000 abstract description 5
- 238000003825 pressing Methods 0.000 abstract description 4
- 238000005299 abrasion Methods 0.000 abstract description 3
- 150000002736 metal compounds Chemical class 0.000 abstract description 3
- 238000005266 casting Methods 0.000 abstract description 2
- 238000000151 deposition Methods 0.000 abstract description 2
- 230000008021 deposition Effects 0.000 abstract description 2
- 238000009987 spinning Methods 0.000 abstract description 2
- 239000000463 material Substances 0.000 description 14
- 238000000576 coating method Methods 0.000 description 13
- 238000005240 physical vapour deposition Methods 0.000 description 12
- 239000000758 substrate Substances 0.000 description 12
- 238000000227 grinding Methods 0.000 description 9
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 description 8
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 8
- 238000002788 crimping Methods 0.000 description 6
- 150000002739 metals Chemical class 0.000 description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 5
- 239000011230 binding agent Substances 0.000 description 5
- 238000007906 compression Methods 0.000 description 5
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 5
- 229910052737 gold Inorganic materials 0.000 description 5
- 239000010931 gold Substances 0.000 description 5
- 239000002245 particle Substances 0.000 description 5
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 230000006835 compression Effects 0.000 description 4
- 229910052697 platinum Inorganic materials 0.000 description 4
- 239000000843 powder Substances 0.000 description 4
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 3
- 150000001247 metal acetylides Chemical class 0.000 description 3
- 229910052709 silver Inorganic materials 0.000 description 3
- 239000004332 silver Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-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
- KJTLSVCANCCWHF-UHFFFAOYSA-N Ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 description 2
- 150000001722 carbon compounds Chemical class 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 229910003460 diamond Inorganic materials 0.000 description 2
- 239000010432 diamond Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 229910052763 palladium Inorganic materials 0.000 description 2
- 238000000623 plasma-assisted chemical vapour deposition Methods 0.000 description 2
- 238000004663 powder metallurgy Methods 0.000 description 2
- 229910052707 ruthenium Inorganic materials 0.000 description 2
- 238000004544 sputter deposition Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- -1 titanium nitride Chemical class 0.000 description 2
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- CXOWYMLTGOFURZ-UHFFFAOYSA-N azanylidynechromium Chemical compound [Cr]#N CXOWYMLTGOFURZ-UHFFFAOYSA-N 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000005524 ceramic coating Methods 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000000774 hypoallergenic effect Effects 0.000 description 1
- 150000002484 inorganic compounds Chemical class 0.000 description 1
- 229910010272 inorganic material Inorganic materials 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 229910052741 iridium Inorganic materials 0.000 description 1
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- NFFIWVVINABMKP-UHFFFAOYSA-N methylidynetantalum Chemical compound [Ta]#C NFFIWVVINABMKP-UHFFFAOYSA-N 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 229910052755 nonmetal Inorganic materials 0.000 description 1
- 150000002843 nonmetals Chemical class 0.000 description 1
- 150000002894 organic compounds Chemical class 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 239000012254 powdered material Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 229910052703 rhodium Inorganic materials 0.000 description 1
- 239000010948 rhodium Substances 0.000 description 1
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium atom Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910003468 tantalcarbide Inorganic materials 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 238000002207 thermal evaporation Methods 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
Images
Classifications
-
- A—HUMAN NECESSITIES
- A44—HABERDASHERY; JEWELLERY
- A44C—PERSONAL ADORNMENTS, e.g. JEWELLERY; COINS
- A44C27/00—Making jewellery or other personal adornments
- A44C27/001—Materials for manufacturing jewellery
- A44C27/002—Metallic materials
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49588—Jewelry or locket making
- Y10T29/4959—Human adornment device making
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49588—Jewelry or locket making
- Y10T29/4959—Human adornment device making
- Y10T29/49591—Bracelet making
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49588—Jewelry or locket making
- Y10T29/4959—Human adornment device making
- Y10T29/49593—Finger ring making
Definitions
- the sintered composite materials generally comprise, as the principal component, very hard powdered materials with high melting points, such as tungsten carbide, silicon carbide, aluminum oxide and ceramic materials, in combination with a much smaller amount of a softer binder metal, such as nickel, cobalt, palladium, platinum, ruthenium, iridium and gold, or alloys thereof, which has a lower melting point.
- very hard powdered materials with high melting points such as tungsten carbide, silicon carbide, aluminum oxide and ceramic materials
- a softer binder metal such as nickel, cobalt, palladium, platinum, ruthenium, iridium and gold, or alloys thereof, which has a lower melting point.
- soft metals such as gold, silver and platinum, which are malleable, as well as castable and fusible at relatively low temperatures.
- soft metals have very little resistance to abrasion.
- relief, detail and edges of soft metal jewelry tend to wear rapidly. This is particularly true if the jewelry is worn so that it comes in contact with hard objects and abrasive surfaces and particles.
- Sintered, or cemented, composite materials comprising at least one metal carbide and a metallic binder have long been used for the manufacture of cutting tools as a result of their immense hardness and durability.
- Such materials are made, using conventional well-known powder metallurgy, by bonding hard tungsten, tantalum, titanium, or chromium nitride particles with one or metals such as iron, cobalt, and nickel.
- the carbide particles which are typically about 20-150 ⁇ m in size, generally comprise between 75 and 85 percent, by weight of the cemented material.
- Nitrides and carbonitrides of the same metals may also be used as hard particles in cemented materials.
- Cemented materials may also be formed using a combination of two or more types of hard particles and binder metals such as ruthenium, rhodium, palladium, platinum, silver and gold.
- a composite material is manufactured, for example, by mixing tungsten carbide powder, tantalum carbide powder, cobalt powder and nickel powder according to a predertermined alloy composition, molding the material powder of mixed alloy composition by pressing the powder, and finally sintering the obtained molded pieces.
- the major challenge of fabricating articles made of cemented metal carbides is that of finishing the raw sintered components. Because the molded pieces are formed using a high-pressure press, complex shapes may be impossible to fabricate and dimensional precision may be difficult or impossible to achieve directly. For example, products having shapes that can be formed in one axis direction only can be formed by die compaction. However, even if a cold isostatic press (CIP) technique is used to form three-dimensional shapes, high precision generally cannot be achieved because the items are molded inside rubber molds.
- CIP cold isostatic press
- U.S. Pat. No. 5,403,374 discloses a process for manufacturing an exterior part for a watch having a three-dimensional curved surfaced and a small hole, without applying secondary machining operations.
- U.S. Pat. No. 6,062,045 discloses a finger ring having five facets having surface angles within a range of from 1 to 40 degrees.
- a related U.S. Pat. No. 6,553,667 discloses a system, apparatus and method for making composite jewelry items, such as finger rings, bracelets, earrings, body jewelry and the like.
- the focus of the patent is multiple methods of manufacture, the first of which includes the steps of preheating an annular substrate, contacting a depression in a surface of the substrate with a second material, heating the second material at a point contact with the substrate, causing the second material to liquify and flow into the depression, and moving the point of contact along the depression while continuously feeding the second material and heating the second material at the point contact with the substrate to cause it to substantially fill the depression.
- the second method includes the steps of providing an annular composite article having an annular groove therein, forming a seamless ring from a metal wire that slides over the annular composite article, placing the annular composite article on a mandrel, and forcing the ring into the groove with a collet.
- the methods covered by this patent are costly and not particularly adapted to mass production.
- the present invention includes a method for manufacturing finger rings, bracelets, annular earrings, annular body jewelry and the like, which have at least one curved surface, from sintered, or cemented, composite materials comprising at least one metal carbide and a metallic binder.
- the annular jewelry piece may be inlaid with a precious metal and/or it may be subjected to a physical vapor deposition (PVD), chemical vapor deposition (CVD), or plasma chemical vapor deposition (PCVD) process in order to deposit thereon either a metal compound, such as titanium nitride, or a diamond-like carbon compound.
- PVD physical vapor deposition
- CVD chemical vapor deposition
- PCVD plasma chemical vapor deposition
- the ring blanks are placed in a spinning fixture and subjected to abrasion against at least one curved abrasive surface.
- the inner surface is formed as a continuous curve.
- the precious metal is inserted in either a straight-wall, dovetail, or notched groove.
- the precious metal is inlaid in the groove by one of several processes, which may include hammering, rolling, or pressing.
- the inlaying process may include the laser welding of joints and removal of any excess inlaid metal above the level of the mouth of the groove with a cutting tool affixed to a lathe in which the ring has been rotatably chucked.
- the may be tack welded, torch welded, or soldered, or the precious metal may be burnished and subsequently cut back with a cutting tool.
- a malleable precious metal wire of generally rectangular cross section may be used.
- a dovetail or notched groove it is necessary to deform the precious metal wire as it is hammered, rolled or pressed into the groove so that it expands to fill the slightly wider space below the mouth of the groove.
- the wire may also be hammered, pressed or rolled in order to secure a tighter fit of the precious metal against the sidewalls of the groove.
- the preferred method for inlaying a ductile metal in a groove involves the use of a press.
- the inlay band is formed as a ring either by laser welding the ends of a looped wire of rectangular cross section, or by stamping.
- the inlay ring is then pressed into the groove using a circular press. Any excess metal is then removed with a cutting tool in combination with a lathe.
- FIG. 1 is an isometric view of a finger ring blank after a groove and facets have been ground on the outer surface and a comfort surface has been ground on the inner surface thereof;
- FIG. 2 is a cross-sectional view of the ring blank of FIG. 1 , taken through its axis of symmetry;
- FIG. 3 is a cross-sectional view of a ring blank similar to that of FIG. 1 , but having a dovetail groove therein;
- FIG. 4 is a cross-sectional view of a ring blank similar to that of FIG. 1 , but having a notched groove therein;
- FIG. 5 is an isometric view of a precious metal strip which has been formed into a hoop, but having a gap between the two ends thereof;
- FIG. 6 is an isometric view of the precious metal strip of FIG. 5 following closing of the gap;
- FIG. 7 is an isometric view of the precious metal strip of FIG. 6 following the laser welding of the abutting ends;
- FIG. 8 is an isometric view of the assembly comprising the ring blank of FIG. 1 and the precious metal hoop of FIG. 7 , the latter having been slipped over the former so that it is positioned above the groove of the blank;
- FIG. 9 is a front elevational view of the radial compression head of a hydraulic crimping and swaging machine, in which the ring and hoop have been positioned on a mandrel;
- FIG. 10 is a cross-sectional view of the assembly of FIG. 8 , but with the notched groove of FIG. 4 , taken through its axis of symmetry;
- FIG. 11 is a cross-sectional view of the assembly of FIG. 10 following the compression of the hoop in the head of the crimping and swaging machine so that it is positioned within the groove of the ring blank;
- FIG. 12 is a cross-sectional view of the assembly of FIG. 11 following further compression in the head of the crimping and swaging machine so that the hoop is squeezed into the notches of the groove of the ring blank;
- FIG. 13 is a side elevational view of a ring blank secured on the mandrel of a rolling machine, showing a precious metal strip being rolled into the groove in the ring blank;
- FIG. 14 is a side elevational view of a ring blank secured on the mandrel of a hammering machine, showing a precious metal strip being hammered into the groove in the ring blank;
- FIG. 15 is a cross-sectional view of a ring blank secured within a chuck and showing a process used to grind the comfort surface inside the ring blank;
- FIG. 16 is a cross sectional view of the ring blank of FIGS. 1 and 2 after its mounting on a mandrel and following the grinding of a notch in one sidewall of the groove thereof;
- FIG. 17 is a cross-sectional view of the ring blank of FIG. 16 following the grinding of a notch in the other sidewall of the groove thereof.
- annular finger ring blank 100 made of sintered composite material has a pair of angled conical facets 102 , an annular groove 103 , and an interior comfort surface 101 .
- the finger ring blank 100 is shown in a cross-sectional view, which shows the parallel, vertical walls 201 of annular groove 103 and the curved interior comfort surface 101 .
- the finger ring blank 100 of FIGS. 1 and 2 has been modified so that the parallel, vertical walls 201 thereof have been replaced with slanted walls 302 , which form a dovetail groove 301 .
- the dovetail groove ensures that precious metal inlaid therein will be securely affixed to the ring. As a practical matter, it is very difficult to grind the slanted walls of a dovetail groove. Thus, the ring blank shown in FIG. 4 is a more practical design.
- the finger ring blank 100 of FIGS. 1 and 2 has been modified so that the parallel, vertical walls 201 thereof have been replaced with notched vertical walls 402 .
- the resulting groove 401 functions almost as well as, and is much more manufacturable than the dovetail groove 301 .
- the method of forming the notched groove 401 will be subsequently disclosed.
- FIGS. 5 through 12 depict the process used to form and press a precious metal hoop into the groove of a ring blank 300 .
- a precious metal strip 501 which may be gold, silver, platinum or other precious ductile metal, has been formed into a hoop, but having a gap between the two ends 502 A and 502 B thereof.
- the two ends 502 A and 502 B of precious metal strip 501 have been laser welded together to form an endless hoop 701 .
- the laser welding step may be replaced with a tack welding, torch welding or soldering step.
- An endless hoop may also be produced in a number of other ways, which include stamping and casting.
- the precious metal hoop 701 of FIG. 7 has been slipped over a sintered composite material ring blank 100 , 200 or 300 so that the precious metal hoop 701 is positioned directly above the groove 103 , 301 or 401 , respectively.
- FIG. 9 the assembly of FIG. 8 is shown mounted on a mandrel 905 that is axially positioned within the head 901 of a Finn-Power crimping and swaging machine.
- the head 901 has eight radially movable collet members 902 .
- the collet members are movable via hydraulic pressure applied to hydraulic fittings 903 via hydraulic lines 904 .
- the machine was designed especially for crimping or swaging tubular collars used to secure fittings to the end of flexible lines and tubes, the machine can be used to compress or squeeze the precious metal hoop 701 into the groove of a ring blank 100 200 or 300 .
- FIG. 10 the assembly of FIG. 8 is shown before the compression process is effected in the Finn-Power crimping and swaging machine.
- the precious metal hoop 701 has been compressed so that its diameter has shrunk to the extent that it is now annularly positioned within the groove 103 , 301 or 401 .
- groove 401 is actually shown in this drawing figure.
- compression of the precious metal hoop 701 is continued until metal from the hoop 701 has squeezed into the notches of notched walls 402 , thereby securing the metal hoop in the groove 300 .
- Any excess inlaid metal above the level of the mouth of the groove may be removed with a cutting tool affixed to a lathe in which the ring has been rotatably chucked.
- FIG. 13 a first alternative inlay method is shown, whereby a precious metal strip 1302 is rolled into the groove 103 , 301 or 401 of a ring blank 100 , 200 or 300 , respectively.
- the ring blank 100 , 200 or 300 is positioned on a mandrel 1301 that is rotatable about a central axis 1304 .
- a roller 1303 pressed against the ring blank 100 , 200 or 300 and forces the precious metal strip 302 into the groove 103 , 301 or 401 .
- the ends of the precious metal strip may be laser welded together or the precious metal strip 1302 , once it is inlaid in the groove 103 , 301 or 401 , may be burnished in order to conceal the joint where the ends of the precious metal strip 302 meet.
- a is a second alternative inlay method is shown, whereby a precious metal strip 1302 is hammered into the groove 103 , 301 or 401 of a ring blank 100 , 200 or 300 , respectively.
- the ring blank 100 , 200 or 300 is positioned on a mandrel 1301 that is rotatable about a central axis 1304 .
- a reciprocating hammer head 1401 forces the precious metal strip 302 into the groove 103 , 301 or 401 .
- the ends of the precious metal strip may be laser welded together or the precious metal strip 1302 , once it is inlaid in the groove 103 , 301 or 401 , may be burnished in order to conceal the joint where the ends of the precious metal strip 302 meet.
- a ring blank 300 is secured by jaws 1502 within a chuck 1501 that spins about a central axis 1503 .
- a grinding wheel 1504 having a concave cross-sectional profile spins about an axis of symmetry 1505 .
- the grind wheel 1504 grinds the comfort surface 101 in a grinding operation.
- FIGS. 16 and 17 the method of grinding the vertical sidewalls 201 of groove 103 (see FIG. 2 ) to form a groove 401 having notched sidewalls 402 (see FIG. 4 ) is shown.
- the ring blank 100 is secured on a mandrel 1601 that spins on a ring rotation axis 1602 .
- a grinding wheel 1603 having diamond grit embedded therein is rotated on a grinding axis 1604 that makes an acute angle with and preferably intersects the ring rotation axis 1602 .
- the notches may be cut one at a time by either reversing the ring for the second notch or in each wall 201 by simply reversing the ring by moving the tool to the other side.
- the notches in the sidewalls 201 of groove 103 may be ground simultaneously with the equipment set up as shown and employing two grind wheels 1603 A and 1603 B.
- the ring Prior to the metal inlay process, the ring may be subjected to a physical vapor deposition (PVD), chemical vapor deposition (CVD), or plasma chemical vapor deposition (PCVD) process in order to deposit thereon either a metal compound, such as titanium nitride, or a diamond-like carbon compound.
- a metal compound such as titanium nitride, or a diamond-like carbon compound.
- Titanium nitride is a gold coloured ceramic coating having a face-centered cubic crystal structure that is applied, most typically, by physical vapor deposition (PVD). Titanium nitride is characterized by extreme density, non-porosity, extreme hardness (approximately 85 Rc) that is greater than that of carbide compounds, and a low coefficient of friction.
- titanium nitride films can be subjected to temperatures of up to 600° C. without damage, are highly conformal (i.e., the deposited film follows the contour of the substrate), able to withstand high temperatures, and form an outstanding bond to the substrate that will not blister, flake, or chip.
- Titanium nitride coatings may be applied by PVD, CVD or PCVD. Each of these processes will be briefly addressed.
- Physical Vapor Deposition, or PVD involves the atom-by-atom, molecule-by-molecule, or ion deposition of various materials on solid substrates in vacuum systems. Two types of physical vapor deposition are currently used.
- Thermal evaporation uses the atomic cloud formed by the evaporation of the coating material in a vacuum environment to coat all the surfaces in the line of sight between the substrate and the target (source).
- Sputtering applies high-technology coatings such as ceramics, metal alloys, organic and inorganic compounds by connecting the workpiece and the substance to a high-voltage DC power supply in an argon vacuum system (10-2-10-3 mmHg).
- a plasma is established between the substrate (workpiece) and the target (donor) and transposes the sputtered off-target atoms to the surface of the substrate.
- RF radio-frequency
- CVD Chemical Vapor Deposition
- metals and non-metals such as glass and plastic. Contrasting to the PVD coating in the “line of sight”, the CVD can coat all surfaces of the substrate.
- Plasma-Assisted Chemical Vapor Deposition is a technique for producing hard wear-resistant surface coatings on tools and wear parts.
- the difference between Plasma-Assisted CVD and conventional CVD lies mainly in a process temperature of about 500° C., as opposed to the 1000-1100° C. temperatures of a conventional CVD process.
- Diamond-like-carbon is an amorphous coating with an extremely low coefficient of friction and extreme hardness.
- DLC coatings are typically applied by either CVD or PCVD processes.
- DLC CVD processes are generally limited to materials which will not soften at temperatures within a range of 700-750° C. Cemented carbides certainly fall in this category.
- the PCVD DLC coating process can be performed at lower temperature than the DLC CVD processes.
- inventive aspect is the coating of the cemented carbide ring blanks with those coatings in order to enhance their appearance, provide a more wear resistant surface, and render them hypoallergenic.
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Abstract
A method for manufacturing finger rings, bracelets, earrings, body jewelry and the like which have at least one curved surface, and which are inlaid with a precious metal or which have which have been subjected to deposition thereon of a metal compound via chemical vapor deposition. Ring blanks are placed in a spinning fixture and subjected to abrasion against at least one curved abrasive surface. For comfort rings, the inner surface is formed as a continuous curve. For rings having inlaid malleable precious metal, the precious metal is inserted in either a straight-wall or undercut wall. Ring blanks having straight-wall grooves can be formed using conventional casting processes. The precious metal is inlaid in the groove by one of several processes, which may include hammering, rolling, or pressing. For a preferred embodiment of the process, the inlaying process involves laser welding of joints and burnishing of the inlaid metal, and cutting the inlaid metal in a lathe to about the level of the mouth of the groove.
Description
- 1. Field of the Invention
- This invention relates generally to articles manufactured from sintered composite materials and methods for their manufacture. The sintered composite materials generally comprise, as the principal component, very hard powdered materials with high melting points, such as tungsten carbide, silicon carbide, aluminum oxide and ceramic materials, in combination with a much smaller amount of a softer binder metal, such as nickel, cobalt, palladium, platinum, ruthenium, iridium and gold, or alloys thereof, which has a lower melting point.
- 2. History of the Prior Art
- For millennia, jewelry has been fabricated from soft metals, such as gold, silver and platinum, which are malleable, as well as castable and fusible at relatively low temperatures. Unfortunately, soft metals have very little resistance to abrasion. Thus, relief, detail and edges of soft metal jewelry tend to wear rapidly. This is particularly true if the jewelry is worn so that it comes in contact with hard objects and abrasive surfaces and particles.
- Sintered, or cemented, composite materials comprising at least one metal carbide and a metallic binder have long been used for the manufacture of cutting tools as a result of their incredible hardness and durability. Such materials are made, using conventional well-known powder metallurgy, by bonding hard tungsten, tantalum, titanium, or chromium nitride particles with one or metals such as iron, cobalt, and nickel. The carbide particles, which are typically about 20-150 μm in size, generally comprise between 75 and 85 percent, by weight of the cemented material. Nitrides and carbonitrides of the same metals may also be used as hard particles in cemented materials. Cemented materials may also be formed using a combination of two or more types of hard particles and binder metals such as ruthenium, rhodium, palladium, platinum, silver and gold.
- A composite material is manufactured, for example, by mixing tungsten carbide powder, tantalum carbide powder, cobalt powder and nickel powder according to a predertermined alloy composition, molding the material powder of mixed alloy composition by pressing the powder, and finally sintering the obtained molded pieces.
- The major challenge of fabricating articles made of cemented metal carbides is that of finishing the raw sintered components. Because the molded pieces are formed using a high-pressure press, complex shapes may be impossible to fabricate and dimensional precision may be difficult or impossible to achieve directly. For example, products having shapes that can be formed in one axis direction only can be formed by die compaction. However, even if a cold isostatic press (CIP) technique is used to form three-dimensional shapes, high precision generally cannot be achieved because the items are molded inside rubber molds.
- As a consequence of the need for more durable jewelry, jewelry manufacturers began fabricating watch cases and bands from cemented, or sintered, metal carbides, several decades ago. These early pieces were obtained using conventional processes, whereby relatively simple shapes formed by normal powder metallurgy methods were subjected to secondary machining, diamond grinding and electrical discharge operations to realize the complicated shapes required for watch cases and watch band pieces, which typically have curved surfaces, small holes and mirror-polished surfaces.
- Accordingly, U.S. Pat. No. 5,403,374 discloses a process for manufacturing an exterior part for a watch having a three-dimensional curved surfaced and a small hole, without applying secondary machining operations.
- The manufacturing of composite jewelry has expanded from watches to annular items. U.S. Pat. No. 6,062,045 discloses a finger ring having five facets having surface angles within a range of from 1 to 40 degrees. A related U.S. Pat. No. 6,553,667, discloses a system, apparatus and method for making composite jewelry items, such as finger rings, bracelets, earrings, body jewelry and the like. The focus of the patent is multiple methods of manufacture, the first of which includes the steps of preheating an annular substrate, contacting a depression in a surface of the substrate with a second material, heating the second material at a point contact with the substrate, causing the second material to liquify and flow into the depression, and moving the point of contact along the depression while continuously feeding the second material and heating the second material at the point contact with the substrate to cause it to substantially fill the depression. The second method includes the steps of providing an annular composite article having an annular groove therein, forming a seamless ring from a metal wire that slides over the annular composite article, placing the annular composite article on a mandrel, and forcing the ring into the groove with a collet. The methods covered by this patent are costly and not particularly adapted to mass production.
- What is needed is a simplified process for manufacturing finger rings, bracelets, earrings, body jewelry and the like, which are more suited to high volume low-cost production.
- The present invention includes a method for manufacturing finger rings, bracelets, annular earrings, annular body jewelry and the like, which have at least one curved surface, from sintered, or cemented, composite materials comprising at least one metal carbide and a metallic binder. The annular jewelry piece may be inlaid with a precious metal and/or it may be subjected to a physical vapor deposition (PVD), chemical vapor deposition (CVD), or plasma chemical vapor deposition (PCVD) process in order to deposit thereon either a metal compound, such as titanium nitride, or a diamond-like carbon compound.
- For all rings which are the subject of the present invention, the ring blanks are placed in a spinning fixture and subjected to abrasion against at least one curved abrasive surface. For comfort rings, the inner surface is formed as a continuous curve.
- For rings having inlaid malleable precious metal, the precious metal is inserted in either a straight-wall, dovetail, or notched groove. The precious metal is inlaid in the groove by one of several processes, which may include hammering, rolling, or pressing. For embodiments of the process involving hammering and rolling of the inlay into the groove, the inlaying process may include the laser welding of joints and removal of any excess inlaid metal above the level of the mouth of the groove with a cutting tool affixed to a lathe in which the ring has been rotatably chucked. As an alternative to laser welding of the joint, the may be tack welded, torch welded, or soldered, or the precious metal may be burnished and subsequently cut back with a cutting tool. If the precious metal is inlaid in a groove of either rectangular or dovetail cross section, a malleable precious metal wire of generally rectangular cross section may be used. For a dovetail or notched groove, it is necessary to deform the precious metal wire as it is hammered, rolled or pressed into the groove so that it expands to fill the slightly wider space below the mouth of the groove. For the straight-wall groove of rectangular cross section the wire may also be hammered, pressed or rolled in order to secure a tighter fit of the precious metal against the sidewalls of the groove.
- The preferred method for inlaying a ductile metal in a groove involves the use of a press. The inlay band is formed as a ring either by laser welding the ends of a looped wire of rectangular cross section, or by stamping. The inlay ring is then pressed into the groove using a circular press. Any excess metal is then removed with a cutting tool in combination with a lathe.
-
FIG. 1 is an isometric view of a finger ring blank after a groove and facets have been ground on the outer surface and a comfort surface has been ground on the inner surface thereof; -
FIG. 2 is a cross-sectional view of the ring blank ofFIG. 1 , taken through its axis of symmetry; -
FIG. 3 is a cross-sectional view of a ring blank similar to that ofFIG. 1 , but having a dovetail groove therein; -
FIG. 4 is a cross-sectional view of a ring blank similar to that ofFIG. 1 , but having a notched groove therein; -
FIG. 5 is an isometric view of a precious metal strip which has been formed into a hoop, but having a gap between the two ends thereof; -
FIG. 6 is an isometric view of the precious metal strip ofFIG. 5 following closing of the gap; -
FIG. 7 is an isometric view of the precious metal strip ofFIG. 6 following the laser welding of the abutting ends; -
FIG. 8 is an isometric view of the assembly comprising the ring blank ofFIG. 1 and the precious metal hoop ofFIG. 7 , the latter having been slipped over the former so that it is positioned above the groove of the blank; -
FIG. 9 is a front elevational view of the radial compression head of a hydraulic crimping and swaging machine, in which the ring and hoop have been positioned on a mandrel; -
FIG. 10 is a cross-sectional view of the assembly ofFIG. 8 , but with the notched groove ofFIG. 4 , taken through its axis of symmetry; -
FIG. 11 is a cross-sectional view of the assembly ofFIG. 10 following the compression of the hoop in the head of the crimping and swaging machine so that it is positioned within the groove of the ring blank; -
FIG. 12 is a cross-sectional view of the assembly ofFIG. 11 following further compression in the head of the crimping and swaging machine so that the hoop is squeezed into the notches of the groove of the ring blank; -
FIG. 13 is a side elevational view of a ring blank secured on the mandrel of a rolling machine, showing a precious metal strip being rolled into the groove in the ring blank; -
FIG. 14 is a side elevational view of a ring blank secured on the mandrel of a hammering machine, showing a precious metal strip being hammered into the groove in the ring blank; -
FIG. 15 is a cross-sectional view of a ring blank secured within a chuck and showing a process used to grind the comfort surface inside the ring blank; -
FIG. 16 is a cross sectional view of the ring blank ofFIGS. 1 and 2 after its mounting on a mandrel and following the grinding of a notch in one sidewall of the groove thereof; and -
FIG. 17 is a cross-sectional view of the ring blank ofFIG. 16 following the grinding of a notch in the other sidewall of the groove thereof. - The method for manufacturing finger rings, bracelets, annular earrings, annular body jewelry and the like from sintered, or cemented, composite materials comprising at least one metal carbide and a metallic binder will now be described in detail with reference to the attached drawing figures.
- There are multiple aspects of the present invention. One involves forming at least one curved surface on the sintered composite material blank. Another involves the process of inlaying a precious metal in a groove in the sintered composite material blank using pressing, rolling or hammering. Still another involves subjecting the sintered composite material blank to a chemical vapor deposition process in order to deposit thereon a layer of nonallergenic material such as titanium nitride or diamond-like carbon. Yet another involves the grinding of notches in inlay grooves for improved anchoring of the precious metal inlay. These various aspects of the invention will now be described in detail with reference to the attaching drawing figures.
- Referring now to
FIG. 1 , an annular finger ring blank 100 made of sintered composite material has a pair of angledconical facets 102, anannular groove 103, and aninterior comfort surface 101. - Referring now to
FIG. 2 , the finger ring blank 100 is shown in a cross-sectional view, which shows the parallel,vertical walls 201 ofannular groove 103 and the curvedinterior comfort surface 101. - Referring now to
FIG. 3 , thefinger ring blank 100 ofFIGS. 1 and 2 has been modified so that the parallel,vertical walls 201 thereof have been replaced with slantedwalls 302, which form adovetail groove 301. The dovetail groove ensures that precious metal inlaid therein will be securely affixed to the ring. As a practical matter, it is very difficult to grind the slanted walls of a dovetail groove. Thus, the ring blank shown inFIG. 4 is a more practical design. - Referring now to
FIG. 4 , thefinger ring blank 100 ofFIGS. 1 and 2 has been modified so that the parallel,vertical walls 201 thereof have been replaced with notchedvertical walls 402. The resultinggroove 401 functions almost as well as, and is much more manufacturable than thedovetail groove 301. The method of forming the notchedgroove 401 will be subsequently disclosed. -
FIGS. 5 through 12 depict the process used to form and press a precious metal hoop into the groove of aring blank 300. - Referring now to
FIG. 5 , aprecious metal strip 501, which may be gold, silver, platinum or other precious ductile metal, has been formed into a hoop, but having a gap between the two 502A and 502B thereof.ends - Referring now to
FIG. 6 , the gap between the two 502A and 502B ofends precious metal strip 501 has been closed in preparation for welding. - Referring now to
FIG. 7 , the two 502A and 502B ofends precious metal strip 501 have been laser welded together to form anendless hoop 701. The laser welding step may be replaced with a tack welding, torch welding or soldering step. An endless hoop may also be produced in a number of other ways, which include stamping and casting. - Referring now to
FIG. 8 , theprecious metal hoop 701 ofFIG. 7 has been slipped over a sintered composite material ring blank 100, 200 or 300 so that theprecious metal hoop 701 is positioned directly above the 103, 301 or 401, respectively.groove - Referring now to
FIG. 9 , the assembly ofFIG. 8 is shown mounted on amandrel 905 that is axially positioned within thehead 901 of a Finn-Power crimping and swaging machine. Thehead 901 has eight radiallymovable collet members 902. The collet members are movable via hydraulic pressure applied tohydraulic fittings 903 viahydraulic lines 904. Although the machine was designed especially for crimping or swaging tubular collars used to secure fittings to the end of flexible lines and tubes, the machine can be used to compress or squeeze theprecious metal hoop 701 into the groove of a ring blank 100 200 or 300. - Referring now to
FIG. 10 , the assembly ofFIG. 8 is shown before the compression process is effected in the Finn-Power crimping and swaging machine. - Referring now to
FIG. 11 , theprecious metal hoop 701 has been compressed so that its diameter has shrunk to the extent that it is now annularly positioned within the 103, 301 or 401. As an example of a preferred embodiment of the invention,groove groove 401 is actually shown in this drawing figure. - Referring now to
FIG. 12 , compression of theprecious metal hoop 701 is continued until metal from thehoop 701 has squeezed into the notches of notchedwalls 402, thereby securing the metal hoop in thegroove 300. Any excess inlaid metal above the level of the mouth of the groove may be removed with a cutting tool affixed to a lathe in which the ring has been rotatably chucked. - Referring now to
FIG. 13 , a first alternative inlay method is shown, whereby aprecious metal strip 1302 is rolled into the 103, 301 or 401 of a ring blank 100, 200 or 300, respectively. The ring blank 100, 200 or 300 is positioned on agroove mandrel 1301 that is rotatable about acentral axis 1304. As the ring blank 100, 200 or 300 is rotated onmandrel 1301, aroller 1303 pressed against the ring blank 100, 200 or 300 and forces theprecious metal strip 302 into the 103, 301 or 401. The ends of the precious metal strip may be laser welded together or thegroove precious metal strip 1302, once it is inlaid in the 103, 301 or 401, may be burnished in order to conceal the joint where the ends of thegroove precious metal strip 302 meet. - Referring now to
FIG. 14 , a is a second alternative inlay method is shown, whereby aprecious metal strip 1302 is hammered into the 103, 301 or 401 of a ring blank 100, 200 or 300, respectively. The ring blank 100, 200 or 300 is positioned on agroove mandrel 1301 that is rotatable about acentral axis 1304. As the ring blank 100, 200 or 300 is rotated onmandrel 1301, areciprocating hammer head 1401 forces theprecious metal strip 302 into the 103, 301 or 401. The ends of the precious metal strip may be laser welded together or thegroove precious metal strip 1302, once it is inlaid in the 103, 301 or 401, may be burnished in order to conceal the joint where the ends of thegroove precious metal strip 302 meet. - Referring now to
FIG. 15 , a ring blank 300 is secured byjaws 1502 within achuck 1501 that spins about acentral axis 1503. Agrinding wheel 1504 having a concave cross-sectional profile spins about an axis ofsymmetry 1505. Thegrind wheel 1504 grinds thecomfort surface 101 in a grinding operation. - Referring now to
FIGS. 16 and 17 , the method of grinding thevertical sidewalls 201 of groove 103 (seeFIG. 2 ) to form agroove 401 having notched sidewalls 402 (seeFIG. 4 ) is shown. The ring blank 100 is secured on amandrel 1601 that spins on aring rotation axis 1602. Agrinding wheel 1603 having diamond grit embedded therein is rotated on a grindingaxis 1604 that makes an acute angle with and preferably intersects thering rotation axis 1602. As shown inFIGS. 16 and 17 , the notches may be cut one at a time by either reversing the ring for the second notch or in eachwall 201 by simply reversing the ring by moving the tool to the other side. - Referring now to
FIG. 18 , the notches in thesidewalls 201 ofgroove 103 may be ground simultaneously with the equipment set up as shown and employing two 1603A and 1603B.grind wheels - Prior to the metal inlay process, the ring may be subjected to a physical vapor deposition (PVD), chemical vapor deposition (CVD), or plasma chemical vapor deposition (PCVD) process in order to deposit thereon either a metal compound, such as titanium nitride, or a diamond-like carbon compound. Titanium nitride is a gold coloured ceramic coating having a face-centered cubic crystal structure that is applied, most typically, by physical vapor deposition (PVD). Titanium nitride is characterized by extreme density, non-porosity, extreme hardness (approximately 85 Rc) that is greater than that of carbide compounds, and a low coefficient of friction. As it is a highly inert compound, it has excellent chemical resistance and hypoallergenicity. It is typically applied in thicknesses ranging from about 3 to 12 microns. Deposited titanium nitride films can be subjected to temperatures of up to 600° C. without damage, are highly conformal (i.e., the deposited film follows the contour of the substrate), able to withstand high temperatures, and form an outstanding bond to the substrate that will not blister, flake, or chip.
- Titanium nitride coatings may be applied by PVD, CVD or PCVD. Each of these processes will be briefly addressed. Physical Vapor Deposition, or PVD, involves the atom-by-atom, molecule-by-molecule, or ion deposition of various materials on solid substrates in vacuum systems. Two types of physical vapor deposition are currently used. Thermal evaporation uses the atomic cloud formed by the evaporation of the coating material in a vacuum environment to coat all the surfaces in the line of sight between the substrate and the target (source). Sputtering, on the other hand, applies high-technology coatings such as ceramics, metal alloys, organic and inorganic compounds by connecting the workpiece and the substance to a high-voltage DC power supply in an argon vacuum system (10-2-10-3 mmHg). A plasma is established between the substrate (workpiece) and the target (donor) and transposes the sputtered off-target atoms to the surface of the substrate. When the substrate is non-conductive, radio-frequency (RF) sputtering is used.
- Chemical Vapor Deposition, or CVD, is capable of producing thick, dense, ductile, and good adhesive coatings on metals and non-metals such as glass and plastic. Contrasting to the PVD coating in the “line of sight”, the CVD can coat all surfaces of the substrate.
- Plasma-Assisted Chemical Vapor Deposition, or PCVD, is a technique for producing hard wear-resistant surface coatings on tools and wear parts. The difference between Plasma-Assisted CVD and conventional CVD lies mainly in a process temperature of about 500° C., as opposed to the 1000-1100° C. temperatures of a conventional CVD process.
- Diamond-like-carbon (DLC) is an amorphous coating with an extremely low coefficient of friction and extreme hardness. DLC coatings are typically applied by either CVD or PCVD processes. DLC CVD processes are generally limited to materials which will not soften at temperatures within a range of 700-750° C. Cemented carbides certainly fall in this category. The PCVD DLC coating process can be performed at lower temperature than the DLC CVD processes.
- As the patent and technical literature is replete with processes for PVD, CVD and PCVD for titanium nitride coatings, as well as processes for CVD and PCVD for diamond-like carbon coatings, no attempt will be made to provide detailed coverage, as the processes themselves are considered prior art. The inventive aspect is the coating of the cemented carbide ring blanks with those coatings in order to enhance their appearance, provide a more wear resistant surface, and render them hypoallergenic.
- Although only several embodiments of the present invention have been disclosed herein, it will be obvious to those having ordinary skill in the art that changes and modifications may be made thereto without departing from the scope and spirit of the invention as hereinafter claimed.
Claims (20)
1. A method of method for manufacturing finger rings, bracelets, earrings, and other annular body jewelry from sintered, or cemented, composite materials comprising at least one metal carbide and a metallic binder, comprises the steps of:
placing an annular blank of sintered material in a spinning fixture; and
abrading the annular blank against at least one curved abrasive surface so that the annular blank acquires a curved surface about its circumference.
2. The method of claim 1 , which further comprises the steps of:
providing an annular blank having at least one annular groove therein on an outer surface thereof;
forcing a piece of precious metal wire into each groove, beginning at one end thereof and continuing to the opposite end thereof so that both ends of the precious metal wire adjoin one another; and
removing excess precious metal to the level of the outer surface of the blank.
3. The method of claim 2 , which further comprises the step of joining together the ends of the precious metal wire.
4. The method of claim 2 , which further comprises the step of burnishing the precious metal in the groove.
5. The method of claim 2 , wherein the precious metal wire is hammered into the groove.
6. The method of claim 2 , wherein the precious metal wire is rolled into the groove.
7. The method of claim 1 , which further comprises the steps of:
providing an annular blank having at least one annular groove therein on an outer surface thereof;
forming an endless hoop of precious metal wire for each annular groove;
pressing an endless hoop into each groove using a radial crimping/swaging machine; and
removing excess precious metal to the level of the outer surface of the blank.
8. The method of claim 7 , which further comprises the steps of:
undercutting the walls of the groove with an abrasive tool prior to pressing an endless hoop into an annular groove.
9. The method of claim 1 , wherein the annular blank is subjected to a thin film deposition process selected from the group consisting of physical vapor deposition, chemical vapor deposition and plasma-assisted chemical vapor deposition, in which a coating selected from the group consisting of titanium nitride and diamond like carbon is applied thereto.
10. A method for manufacturing finger rings, bracelets, earrings, and other annular body jewelry from sintered, or cemented, composite materials comprising at least one metal carbide and a metallic binder, comprises the steps of:
providing an annular blank having at least one annular groove therein on an outer surface thereof;
forcing a piece of precious metal wire into each annular groove; and
removing excess precious metal to the level of the outer surface of the blank.
11. The method of claim 10 , which further comprises the step of laser welding together the ends of the precious metal wire.
12. The method of claim 10 , which further comprises the step of burnishing the precious metal in the annular groove.
13. The method of claim 10 , wherein the precious metal wire is hammered into the annular groove.
14. The method of claim 10 , wherein the precious metal wire is rolled into the annular groove.
15. The method of claim 10 , wherein:
the precious metal wire is formed into an endless hoop for each annular groove; and
an endless hoop is pressed into each annular groove using a radial crimping/swaging machine.
16. The method of claim 10 , which further comprises the steps of:
undercutting the walls of the groove with an abrasive tool prior to forcing a piece of precious metal wire into each annular groove.
17. A method for manufacturing finger rings, bracelets, earrings, and other annular body jewelry from sintered, or cemented, composite materials comprising at least one metal carbide and a metallic binder, comprises the steps of:
providing an annular blank having an annular groove therein on an outer surface thereof;
forming an endless hoop of precious metal;
pressing the endless hoop into the groove using a radial crimping/swaging machine; and
removing excess precious metal to the level of the outer surface of the blank.
18. The method of claim 17 , which further comprises the steps of undercutting the walls of the groove with an abrasive tool while the blank is chucked in the spinning fixture, and before the precious metal hoop is forced into the groove.
19. The method of claim 17 , wherein the annular blank is subjected to a thin film deposition process selected from the group consisting of physical vapor deposition, chemical vapor deposition and plasma-assisted chemical vapor deposition, in which a coating selected from the group consisting of titanium nitride and diamond like carbon is applied thereto.
20. The method of claim 17 , which further comprises the steps of:
securing the annular blank in a spinning fixture;
abrading the annular blank against at least one curved abrasive surface so that the annular blank acquires a curved surface about its circumference.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/769,356 US20050166401A1 (en) | 2004-01-30 | 2004-01-30 | Wear-resistant composite rings for jewelry, medical or industrial devices and manufacturing method therefor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/769,356 US20050166401A1 (en) | 2004-01-30 | 2004-01-30 | Wear-resistant composite rings for jewelry, medical or industrial devices and manufacturing method therefor |
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| Publication Number | Publication Date |
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| US20050166401A1 true US20050166401A1 (en) | 2005-08-04 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/769,356 Abandoned US20050166401A1 (en) | 2004-01-30 | 2004-01-30 | Wear-resistant composite rings for jewelry, medical or industrial devices and manufacturing method therefor |
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| US (1) | US20050166401A1 (en) |
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| EP1813385A1 (en) * | 2006-01-27 | 2007-08-01 | Comadur S.A. | Method of burnishing a hard material and decorated workpiece made from a hard, burnished material |
| WO2011112162A1 (en) * | 2010-03-11 | 2011-09-15 | Mert Kuyumculuk Sanayi Ve Ticaret Limited Sirketi | Ring and the manufacturing method for the same providing different advantages in assembly |
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| WO2012167080A1 (en) * | 2011-06-01 | 2012-12-06 | Frederick Goldman, Inc. | Methods for producing a design in a sintered product |
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