Presintered preform for repair of superalloy component
US-2015367456-A1 · Dec 24, 2015 · US
US10105798B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10105798-B2 |
| Application number | US-201514933154-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 5, 2015 |
| Priority date | Nov 5, 2015 |
| Publication date | Oct 23, 2018 |
| Grant date | Oct 23, 2018 |
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A method for improving the surface of an aluminum alloy article includes manufacturing the aluminum alloy article using an additive manufacturing technique, wherein the article as-manufactured includes one or more of cracks, roughness, or porosity at a surface of the article; coating the surface of the aluminum alloy article with a diffusion element, the diffusion element being capable of diffusing at least 0.2 mils into the article; heating the aluminum alloy article coated with the diffusion element to cause the diffusion element to diffuse the at least 0.2 mils into the article, thereby forming a diffusion layer of at least 0.2 mils in thickness comprising both aluminum alloy and diffusion element; and removing the diffusion layer from the aluminum alloy article, whereby upon the removing, a resulting improved surface of the article comprises fewer or smaller cracks, reduced roughness, or reduced porosity.
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What is claimed is: 1. A method for reducing roughness, porosity, and cracking of the surface of an aluminum alloy article comprising: manufacturing the aluminum alloy article using an additive manufacturing technique, wherein the article as-manufactured comprises one or more of cracks, roughness, or porosity at a surface of the article; coating the surface of the aluminum alloy article with an encapsulating element, which may or may not also be a diffusion element, to facilitate HIP response; coating the surface of the aluminum alloy article with a diffusion element wherein the diffusion element comprises zinc and wherein coating the surface comprises a zincate plating process, the diffusion element being capable of diffusing at least 0.2 mils (5 microns) into the article; heating the aluminum alloy article coated with the diffusion element at a temperature between 350° C. to 475° C. for a time period of 2 to 20 hours to cause the diffusion element to diffuse the at least 0.2 mils (5 microns) into the article, thereby forming a diffusion layer of at least 0.2 mils (5 microns) in thickness comprising both aluminum alloy and diffusion element; removing the diffusion layer from the aluminum alloy article using a chemical solvent of ferric chloride or nitric acid, whereby upon the removing, a resulting improved surface of the article comprises fewer or smaller cracks, reduced roughness, or reduced porosity, wherein coating with the encapsulating element occurs after the removing step. 2. The method of claim 1 , wherein the aluminum alloy composition comprises of a majority aluminum on a weight basis, and wherein the aluminum alloy article comprises an aluminum alloy selected from the group consisting of: cast alloys, wrought alloys, derivatives of said cast or wrought alloys, and non-conventional alloys. 3. The method of claim 1 , wherein the additive manufacturing technique is selected from the group consisting of: direct metal laser sintering, direct metal laser fusion, electron beam melting, and selective laser sintering. 4. The method of claim 1 , wherein the diffusion element diffuses at least 1 mil (25 microns) into the article. 5. The method of claim 1 , further comprising repeating the steps of coating, heating, and removing an additional one or more times. 6. The method of claim 1 , further comprising hot isostatic pressing the article. 7. The method of claim 1 , wherein hot isostatic pressing occurs after the removing step. 8. The method of claim 1 , wherein the aluminum alloy article is a component of a gas turbine engine.
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