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US 10,570,744 B2Granted
Method for forming components using additive manufacturing and re-melt
AssigneeUnited Technologies Corporation
InventorJinQuan Xu
Life of this patent
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Abstract
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.
Claims2
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.
9 more elements
Dependencies are inferred from the claim text.