Methods for directionally recrystallizing additively-manufactured metallic articles by heat treatment with a gradient furnace

US2018056396A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2018056396-A1
Application numberUS-201615250057-A
CountryUS
Kind codeA1
Filing dateAug 29, 2016
Priority dateAug 29, 2016
Publication dateMar 1, 2018
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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Abstract

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A method for manufacturing a metallic article includes providing or obtaining a metallic material in powder form, using an additive manufacturing process, building the metallic article from the powder-form metallic material, layer-by-layer, in a build direction, wherein as a result of the additive manufacturing process, the metallic article comprises columnar grain structures oriented in the build direction, and conveying the metallic article through a gradient furnace in a direction of conveyance from a first area of the gradient furnace to a second area of the gradient furnace to increase a size of the columnar grain structures in the metallic article. The metallic article is conveyed through the gradient furnace in an orientation such that the columnar structures oriented in the build direction are substantially parallel to the direction of conveyance.

First claim

Opening claim text (preview).

What is claimed is: 1 . A method for manufacturing a metallic article comprising the steps of: providing or obtaining a metallic material in powder form; using an additive manufacturing process, building the metallic article from the powder-form metallic material, layer-by-layer, in a build direction, wherein as a result of the additive manufacturing process, the metallic article comprises columnar grain structures oriented in the build direction; building a sacrificial piece onto the metallic article using the additive manufacturing process, the sacrificial piece being metallurgically coupled to the metallic article and comprising the metallic material; and conveying the metallic article through a gradient furnace in a direction of conveyance from a first area of the gradient furnace to a second area of the gradient furnace to increase a size of the columnar grain structures in the metallic article, wherein the metallic article is conveyed through the gradient furnace in an orientation such that the columnar structures oriented in the build direction are substantially parallel to the direction of conveyance, wherein the first area of the gradient furnace heats the metallic article to a temperature that is below a solvus temperature of the metallic material and the second area of the gradient furnace heats the metallic article to a temperature that is above the solvus temperature of the metallic material, the temperature of the gradient furnace increasing in a gradated manner from the first area to the second area, and wherein the metallic article is oriented with respect to the gradient furnace such that the sacrificial piece enters the gradient furnace subsequent to the metallic article onto which the sacrificial piece is built. 2 . The method of claim 1 , wherein the additive manufacturing processes is either electron beam melting (EBM) or direct metal laser fusion (DMLF). 3 . The method of claim 1 , further comprising removing the sacrificial piece from the metallic article subsequent to the step of conveying the metallic article through the gradient furnace. 4 . The method of claim 1 , wherein the additive manufacturing process employs a heated build plate to maintain the metallic article at an elevated temperature as it is built, layer-by-layer, in the build direction. 5 . The method of claim 1 , wherein the additive manufacturing process employs a directionally-crystallized metallic seed layer and builds the metallic article, layer-by-layer, from the seed layer, thereby resulting in an improved columnar grain structure, oriented in the build direction, of the metallic article. 6 . The method of claim 1 , wherein the metallic material comprises a Ni-based superalloy. 7 . The method of claim 1 , wherein the metallic article comprises a gas turbine engine component, such as a turbine blade, vane, or nozzle. 8 . The method of claim 1 , further comprising, subsequent to conveying the metallic article through the gradient furnace, quenching the metallic article in a non-oil quenching medium. 9 . The method of claim 8 , further comprising, subsequent to quenching the metallic article, performing one or more of hot-isostatic pressing, ageing, and machining of the metallic article. 10 . The method of claim 1 , wherein the step of conveying the metallic article through the gradient furnace is performed at a conveyance rate of about 1 to about 2 inches per hour.

Assignees

Inventors

Classifications

  • by mechanical means · CPC title

  • Rollers · CPC title

  • Structures for supporting workpieces or articles during manufacture and removed afterwards · CPC title

  • of powder · CPC title

  • to achieve specific product aspects, e.g. surface smoothness, density, porosity or hollow structures · CPC title

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What does patent US2018056396A1 cover?
A method for manufacturing a metallic article includes providing or obtaining a metallic material in powder form, using an additive manufacturing process, building the metallic article from the powder-form metallic material, layer-by-layer, in a build direction, wherein as a result of the additive manufacturing process, the metallic article comprises columnar grain structures oriented in the bu…
Who is the assignee on this patent?
Honeywell Int Inc
What technology area does this patent fall under?
Primary CPC classification B22F3/24. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Mar 01 2018 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).