Methods and Systems for Integrally Trapping a Glass Insert in a Metal Bezel
US-2015360283-A1 · Dec 17, 2015 · US
US9975173B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9975173-B2 |
| Application number | US-201414271764-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 7, 2014 |
| Priority date | Jun 3, 2013 |
| Publication date | May 22, 2018 |
| Grant date | May 22, 2018 |
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A method includes casting a metallic material ( 56 ) in a mold ( 20 ) containing a core, the core having a substrate ( 40, 44 ) coated with a coating ( 42 ). A removing of the metallic material from the mold and decoring leaves a casting having a layer formed by the coating. The coating has a ceramic having a porosity in a zone ( 50 ) near the substrate less than a porosity in a zone ( 52 ) away from the substrate.
Opening claim text (preview).
What is claimed is: 1. A method comprising: casting a metallic material ( 56 ) in a mold ( 20 ) containing a core, the core having a substrate ( 40 , 44 ) coated with a coating ( 42 ); and removing the metallic material from the mold and decoring to leave a cast article, wherein: the coating or at least one layer thereof reacts with the metallic material and/or survives the decoring to become a portion of the cast article; and the coating comprises a ceramic having a porosity in a zone ( 50 ) near the substrate less than a porosity in a zone ( 52 ) away from the substrate. 2. The method of claim 1 wherein: the substrate comprises a molded first ceramic and the coating ceramic comprises a second ceramic different from the first ceramic. 3. The method of claim 2 further comprising: applying the second ceramic to the first ceramic by PVD. 4. The method of claim 2 wherein: the first ceramic is silica-based; and the second ceramic is alumina-based. 5. The method of claim 1 wherein: the coating ceramic has a characteristic thickness of 1.0 to 10 mil (25 to 250 micrometers). 6. The method of claim 1 wherein: the coating comprises a first layer ( 50 ) applied by a first technique and a second layer ( 52 ) applied by a second technique, different from the first technique. 7. The method of claim 6 wherein: the first technique is a vapor deposition and the second technique is not a vapor deposition. 8. The method of claim 7 wherein: the second layer comprises a first sublayer ( 52 - 1 ) and a second sublayer ( 52 - 2 ) of differing porosities. 9. The method of claim 7 wherein: the second technique is a sol-gel process. 10. The method of claim 1 wherein: the coating further comprises a second metallic material ( 200 ) atop ( 202 ) and/or intermixed ( 204 ) with the ceramic. 11. The method of claim 10 wherein: at least a majority by weight of the second metallic material ( 200 ) diffuses into the metallic material ( 56 ). 12. The method of claim 1 wherein: the metallic material is a nickel-based superalloy. 13. The method of claim 1 wherein: the cast article has an airfoil. 14. The method of claim 1 further comprising: applying a coating to an exterior of the cast article, but not to the interior. 15. The method of claim 1 wherein: the cast article has one or more internal passageways; and said portion of the cast article forms a ceramic lining along the passageways, wherein: the ceramic lining has a porosity in a zone near the metallic material greater than a porosity in a zone away from the metallic material. 16. The method of claim 15 wherein: the metallic material at least partially fills the porosity of at least the zone near the metallic material. 17. The method of claim 15 wherein: the metallic material is a nickel-based superalloy. 18. The method of claim 15 wherein: the cast article forms a gas turbine engine component. 19. The method of claim 15 wherein: the cast article has a thermal barrier coating on an exterior surface of differing composition from said ceramic lining. 20. The method of claim 15 wherein: the cast article has an airfoil.
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