Process for producing an article

US2016258298A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016258298-A1
Application numberUS-201514639464-A
CountryUS
Kind codeA1
Filing dateMar 5, 2015
Priority dateMar 5, 2015
Publication dateSep 8, 2016
Grant date

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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 process of producing an article and an article made are provided. The process includes producing a near-net shape component. The process includes forming a consolidation shell by additive manufacturing. The consolidation shell defines an interior space having a geometry corresponding to a component. A metallic powder is provided to the interior space. Gas is removed from the interior space. The metallic powder is consolidated in the consolidation shell under sufficient heat and pressure to form the near-net shape component.

First claim

Opening claim text (preview).

What is claimed is: 1 . A process of producing a near-net shape component, the process comprising: forming a consolidation shell by additive manufacturing, the consolidation shell defining an interior space having a geometry corresponding to a component; providing a metallic powder to the interior space; removing gas from the interior space; and consolidating the metallic powder in the consolidation shell under sufficient heat and pressure to form the near-net shape component. 2 . The process of claim 1 , wherein the consolidating includes hot isostatic pressing. 3 . The process of claim 1 , wherein the metallic powder includes metals selected from the group consisting of nickel, cobalt, titanium, iron, alloys thereof and combinations thereof. 4 . The process of claim 1 , wherein the geometry corresponding to the component includes a geometry that forms the near-net shape component after consolidation. 5 . The process of claim 1 , further comprising removing the consolidation shell. 6 . The process of claim 5 , wherein removing the consolidation shell includes a removal process selected from the group consisting of machining, electrical removal or chemical removal. 7 . The process of claim 1 , wherein the consolidation shell includes a second, removable material to form channels in the component. 8 . The process of claim 1 , wherein the near-net shape component is a compressor blade. 9 . The process of claim 1 , wherein the providing a metallic powder to the interior space includes providing a first metallic powder and a second metallic powder. 10 . The process of claim 9 , wherein the first metallic powder and the second metallic powder have dissimilar compositions. 11 . The process of claim 9 , wherein the first metallic powder and the second metallic powder have dissimilar properties. 12 . The process of claim 1 , wherein the consolidation shell forms a coating material on the component. 13 . A consolidation shell comprising: an interior space having a geometry corresponding to a component; and a conduit extending from the interior space; wherein metallic powder is present in the interior space. 14 . The consolidation shell of claim 13 , wherein the component is a compressor blade. 15 . The consolidation shell of claim 13 , wherein the metallic powder is a metal selected from the group consisting of nickel, cobalt, titanium, iron, alloys thereof and combinations thereof. 16 . The consolidation shell of claim 13 , wherein the metallic powder includes a first metallic powder and a second metallic powder. 17 . A component comprising: a consolidation shell formed by additive manufacturing, the consolidation shell defining an interior space having a geometry corresponding to the component, the interior space being at least partially filled with a consolidated powder. 18 . The component of claim 17 , wherein the component is selected from the group consisting of a turbine bucket, a compressor blade, a compressor vane, an airfoil segment, a nozzle, a shroud, and a combustion component. 19 . The component of claim 17 , wherein the component is a compressor blade. 20 . The component of claim 17 , wherein the consolidation shell forms a coating on the component.

Assignees

Inventors

Classifications

  • B22F3/15Primary

    Hot isostatic pressing · CPC title

  • Thermal properties · CPC title

  • Container manufacturing · CPC title

  • Combustors or associated equipment · CPC title

  • turbine or like blades from one piece · CPC title

Patent family

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Frequently asked questions

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What does patent US2016258298A1 cover?
A process of producing an article and an article made are provided. The process includes producing a near-net shape component. The process includes forming a consolidation shell by additive manufacturing. The consolidation shell defines an interior space having a geometry corresponding to a component. A metallic powder is provided to the interior space. Gas is removed from the interior space. T…
Who is the assignee on this patent?
Gen Electric
What technology area does this patent fall under?
Primary CPC classification B22F3/15. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Sep 08 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).