Method for forming a directionally solidified replacement body for a component using additive manufacturing
US-2015321250-A1 · Nov 12, 2015 · US
US10570744B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10570744-B2 |
| Application number | US-201615228543-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 4, 2016 |
| Priority date | May 9, 2014 |
| Publication date | Feb 25, 2020 |
| Grant date | Feb 25, 2020 |
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A method of manufacturing a component includes additively manufacturing a crucible; directionally solidifying a metal material within the crucible; and removing the crucible to reveal the component. A component for a gas turbine engine includes a directionally solidified metal material component, the directionally solidified metal material component having been additively manufactured of a metal material concurrently with a core, the metal material having been remelted and directionally solidified.
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What is claimed is: 1. A method of manufacturing a component, comprising: additively manufacturing a crucible for casting of the component, wherein the crucible includes a core and a shell; adding metal material in powder form to the crucible, wherein the metal material is a superalloy; solidifying the metal material within the crucible to form a metal directionally solidified microstructure within the component; and removing the crucible to reveal the component; wherein the method further comprises: manufacturing the core and the shell of a material that is different from the metal material; additively manufacturing internal cooling passages of the component using a ceramic material; additively manufacturing locations for microcircuits of the component using a refractory metal material, wherein the microcircuits are smaller than and located outboard of the internal cooling passages; filling the internal cooling passages with a ceramic slurry to form the core; and curing the core. 2. The method as recited in claim 1 , further comprising: forming the shell over the component and the core by dipping the component into a ceramic powder and binder slurry to form a layer of ceramic material covering the component.
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