Method of forming a cladding layer having an integral channel

US10150184B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10150184-B2
Application numberUS-201514918792-A
CountryUS
Kind codeB2
Filing dateOct 21, 2015
Priority dateOct 21, 2015
Publication dateDec 11, 2018
Grant dateDec 11, 2018

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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 including: submerging a ceramic preform ( 10 ) in a layer ( 12 ) of powdered superalloy material ( 14 ), wherein the preform defines a desired shape of a channel ( 60, 62, 64, 78 ) to be formed in a layer ( 42 ) of superalloy material; melting the powdered superalloy material around the preform without melting the preform; and cooling and re-solidifying the superalloy material around the preform to form the layer of superalloy material with the preform defining the shape of the channel therein.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method comprising: submerging a ceramic preform in a layer of powdered superalloy material, wherein the preform defines a desired shape of a void to be formed in a layer of superalloy material; melting the powdered superalloy material around the preform without melting the preform; cooling and re-solidifying the melted superalloy material around the preform to form the layer of superalloy material with the preform defining the shape of the void therein; forming a melt pool during the step of heating; and facilitating wetting of the preform by the melt pool through at least one of slowing a travel speed of a laser used to melt the powdered superalloy material proximate the preform, changing an angle of a process laser used to melt the powdered superalloy material proximate the preform, adjusting convective effects proximate the preform, adjusting surface tension effects proximate the preform, rotating the preform, and agitating the preform. 2. The method of claim 1 , wherein the ceramic preform comprises a hollow ceramic tube. 3. The method of claim 2 , further comprising removing the hollow ceramic tube via a mechanical or thermal shocking process. 4. The method of claim 1 , further comprising removing the ceramic preform to expose a surface that defines the void. 5. The method of claim 1 , further comprising coating an outer surface of the ceramic preform prior to the submerging and melting steps to facilitate wetting of the preform by the melted superalloy material. 6. The method of claim 5 , wherein the outer surface of the preform is coated with at least one of the group consisting of molybdenum-manganese, titanium, tungsten manganese, moly tungsten manganese, hafnium, chromium, zirconium, and niobium. 7. The method of claim 6 , further comprising plating the coating prior to the submerging and melting steps, wherein both the coating and the plating facilitate the wetting of the preform by the melted superalloy material. 8. The method of claim 7 , wherein the plating comprises nickel. 9. The method of claim 1 , wherein the preform comprises a raised or recessed surface feature on an exterior or interior surface, the method further comprising coating any raised or recessed surface feature on the exterior surface with a layer of material effective to facilitate wetting of the feature with the melted superalloy material during the melting step. 10. The method of claim 1 wherein the ceramic preform comprises at least one of the group consisting of alumina, zirconia, beryllium oxide, sapphire, silica, magnesium oxide, boron nitride, aluminum nitride, silicon nitride, silicon carbide, aluminum silicate and magnesium silicate. 11. The method of claim 1 , wherein the preform comprises a ceramic foam. 12. The method of claim 1 , further comprising coating a surface of the ceramic preform with a constituent component of the superalloy material prior to the submerging and melting steps. 13. The method of claim 1 , further comprising melting the powdered superalloy material via a selective laser heating process.

Assignees

Inventors

Classifications

  • Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties · CPC title

  • by mechanical means · CPC title

  • by thermal means (control of energy beam parameters for post heating B22F10/364) · CPC title

  • Treatment of workpieces or articles during build-up, e.g. treatments applied to fused layers during build-up · CPC title

  • of energy beam parameters · CPC title

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What does patent US10150184B2 cover?
A method including: submerging a ceramic preform ( 10 ) in a layer ( 12 ) of powdered superalloy material ( 14 ), wherein the preform defines a desired shape of a channel ( 60, 62, 64, 78 ) to be formed in a layer ( 42 ) of superalloy material; melting the powdered superalloy material around the preform without melting the preform; and cooling and re-solidifying the superalloy material around t…
Who is the assignee on this patent?
Siemens Energy Inc
What technology area does this patent fall under?
Primary CPC classification B23K26/342. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Dec 11 2018 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 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).