Coupling for a multi-part dental implant system
US-8968002-B2 · Mar 3, 2015 · US
US11053572B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11053572-B2 |
| Application number | US-201916277173-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 15, 2019 |
| Priority date | Jul 3, 2013 |
| Publication date | Jul 6, 2021 |
| Grant date | Jul 6, 2021 |
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Disclosed herein is an article comprising a metal alloy; where the metal alloy comprises a base metal, a second element and a third element; where the base metal is magnesium, calcium, strontium, zinc, or a combination thereof; where the second element is chemically different from the third element; and where the second element and the third element are scandium, yttrium, gadolium, cerium, neodymium, dysporium, or a combination thereof; and a protective layer disposed upon the metal alloy and is reactively bonded to the metal alloy; where the protective layer comprises a base non-metallic derivative, a second non-metallic derivative and a third non-metallic derivative of metals present in the metal alloy; and where the base non-metallic derivative, the second non-metallic derivative and the third non-metallic derivative are all chemically different from one another.
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What is claimed is: 1. A method comprising: blending three or more metals to form a metal alloy, where the metal alloy comprises a base metal, a second element and a third element; where the base metal is magnesium, calcium, strontium, zinc, or a combination thereof; where the second element is chemically different from the third element; and where the second element and the third element are scandium, yttrium, gadolium, cerium, neodymium, dysporium, or a combination thereof; molding the metal alloy; and annealing the metal alloy at a temperature and in an atmosphere effective to produce a protective layer on the metal alloy; where the protective layer is reactively bonded to the metal alloy and where the protective layer is non-metallic, where the protective layer comprises a base non-metallic derivative, a second non-metallic derivative and a third non-metallic derivative of metals present in the metal alloy; and where the base non-metallic derivative, the second non-metallic derivative and the third non-metallic derivative are all chemically different from one another. 2. The method of claim 1 , where the metal alloy is annealed at a temperature of about 25 to about 800° C. 3. The method of claim 1 , where the atmosphere contains oxygen, carbon, boron, silicon, selenium, fluorine, bromine, iodine, tellurium, sulfur, nitrogen, or a combination thereof. 4. The method of claim 1 , where the metal alloy comprises a base metal, a second element and a third element; where the base metal is magnesium, calcium, strontium, zinc, or a combination thereof; where the second element is chemically different from the third element; and where the second element and the third element are scandium, gadolium, cerium, neodymium, dysporium, or a combination thereof; and where the protective layer comprises a base non-metallic derivative, a second non-metallic derivative and a third non-metallic derivative of metals present in the metal alloy; and where the base non-metallic derivative, the second non-metallic derivative and the third non-metallic derivative are all chemically different from one another. 5. The method of claim 4 , where the protective layer comprises a plurality of layers; with an outermost layer comprising an oxide of magnesium, calcium, strontium, or a combination thereof; while an inner layer comprises an oxide of scandium, gadolium, cerium, neodymium, dysporium, or a combination thereof. 6. The method of claim 4 , where the protective layer has a thickness of 0.1 nanometers to 500 nanometers. 7. The method of claim 4 , wherein the base metal is magnesium. 8. The method of claim 4 , wherein the base metal is calcium. 9. The method of claim 4 , wherein the base metal is strontium. 10. The method of claim 4 , wherein the base metal is zinc. 11. The method of claim 4 , wherein the base metal is magnesium, the second element is scandium, and the third element is cerium. 12. The method of claim 1 , where the metal alloy comprises a base metal, a second element and a third element; where the base metal is calcium, strontium, zinc, or a combination thereof where the second element is chemically different from the third element; and where the second element and the third element are scandium, yttrium, gadolium, cerium, neodymium, dysporium, or a combination thereof; and where the protective layer comprises a base non-metallic derivative, a second non-metallic derivative and a third non-metallic derivative of metals present in the metal alloy; and where the base non-metallic derivative, the second non-metallic derivative and the third non-metallic derivative are all chemically different from one another. 13. The method of claim 12 , where the protective layer comprises a plurality of layers; with an outermost layer comprising an oxide of calcium, strontium, or a combination thereof; while an inner layer comprises an oxide of scandium, yttrium, gadolium, cerium, neodymium, dysporium, or a combination thereof. 14. The method of claim 12 , wherein the second element is yttrium and the third element is scandium. 15. The method of claim 12 , wherein the second element is yttrium and the third element is selected from gadolium, cerium, neodymium, dysporium, or a combination thereof. 16. The method of claim 12 , wherein the second element is scandium and the third element is selected from gadolium, cerium, neodymium, dysporium, or a combination thereof. 17. The method of claim 1 , where the metal alloy comprises a base metal, a second element and a third element; where the base metal is magnesium, calcium, strontium, zinc, or a combination thereof where the second element is chemically different from the third element; and where the second element and the third element are gadolium, cerium, neodymium, dysporium, or a combination thereof; where the protective layer comprises a base non-metallic derivative, a second non-metallic derivative and a third non-metallic derivative of metals present in the metal alloy; and where the base non-metallic derivative, the second non-metallic derivative and the third non-metallic derivative are all chemically different from one another; and wherein the protective layer comprises a plurality of layers; with an outermost layer comprising an oxide of magnesium, calcium, strontium, or a combination thereof while an inner layer comprises an oxide of gadolium, cerium, neodymium, dysporium, or a combination thereof. 18. The method of claim 17 , wherein the outermost layer is an oxide of magnesium. 19. The method of claim 17 , wherein the outermost layer is an oxide of calcium. 20. The method of claim 17 , wherein the outermost layer is an oxide of strontium or an oxide of zinc.
Light metal alloys · CPC title
Alloys based on magnesium · CPC title
Modification of implant surfaces in order to improve biocompatibility, cell growth, fixation of biomolecules, e.g. plasma treatment · CPC title
Other specific inorganic materials not covered by A61L27/303 - A61L27/32 · CPC title
Other specific metals or alloys not covered by A61L27/042 - A61L27/045 or A61L27/06 · CPC title
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