Method for forming components using additive manufacturing and re-melt

US10570744B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10570744-B2
Application numberUS-201615228543-A
CountryUS
Kind codeB2
Filing dateAug 4, 2016
Priority dateMay 9, 2014
Publication dateFeb 25, 2020
Grant dateFeb 25, 2020

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

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.

First claim

Opening claim text (preview).

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.

Assignees

Inventors

Classifications

  • Treating moulds or cores, e.g. drying, hardening · CPC title

  • Processes of additive manufacturing · CPC title

  • Products made by additive manufacturing · CPC title

  • Use of lost patterns · CPC title

  • of moulds · CPC title

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Frequently asked questions

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What does patent US10570744B2 cover?
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 meta…
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F01D5/18. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Feb 25 2020 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).