Control of solidification in laser powder bed fusion additive manufacturing using a diode laser fiber array

US11020955B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11020955-B2
Application numberUS-201916704831-A
CountryUS
Kind codeB2
Filing dateDec 5, 2019
Priority dateDec 16, 2013
Publication dateJun 1, 2021
Grant dateJun 1, 2021

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  1. Title

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  2. Abstract

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  5. First independent claim

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Abstract

Official abstract text for this publication.

A method of method of forming or repairing a superalloy article having a columnar or equiaxed or directionally solidified or amorphous or single crystal microstructure includes emitting a plurality of laser beams from selected fibers of a diode laser fiber array corresponding to a pattern of a layer of the article onto a powder bed of the superalloy to form a melt pool; and controlling a temperature gradient and a solidification velocity of the melt pool to form the columnar or single crystal microstructure.

First claim

Opening claim text (preview).

What is claimed is: 1. A superalloy article or repair formed by a method comprising the steps of: emitting a plurality of laser beams, from first selected fibers of a diode laser fiber array, corresponding to a pattern of a first layer of the article onto a powder bed of a superalloy to form a first melt pool; distributing additional powder across the first layer; emitting a plurality of laser beams, from second selected fibers of the diode laser fiber array, corresponding to a pattern of a second layer of the article onto the powder bed to form a second melt pool over the first layer; and controlling a temperature gradient and a solidification velocity of the first and second melt pools such that each of the first and second layers has a columnar or equiaxed or directionally solidified or amorphous or single crystal microstructure, the controlling comprising controlling a decay rate of a laser energy of each of the plurality of laser beams to control a cooling period of the melt pool. 2. A superalloy article or repair according to claim 1 , wherein the columnar microstructure is dendritic. 3. A superalloy article or repair according to claim 1 , wherein grains of the microstructure have a size of 10 μm-100 μm. 4. A superalloy article or repair according to claim 1 , wherein the superalloy is a CoCrMo material. 5. A superalloy article or repair according to claim 1 , wherein the superalloy is a Ni-based superalloy. 6. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and solidification velocity comprises decreasing the laser energy at 10 W/s to provide a 1 s cooling period. 7. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and solidification velocity comprises decreasing the laser energy at 1 W/s to provide a 10 s cooling period. 8. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and solidification velocity comprises decreasing the laser energy at 0.1 W/s to provide a 100 s cooling period. 9. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and solidification velocity comprises heating a substrate that supports the powder bed and/or heating a prior layer of the article formed by solidification of a prior melt pool. 10. A superalloy article or repair according to claim 9 , wherein heating the substrate comprises heating the substrate to a temperature below the melting temperature of the substrate. 11. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and the solidification velocity comprises controlling at least one of a duration of each laser beam, a pulse energy of each diode laser, a pulse width of each diode laser, an average output power of each diode laser, an energy distribution of each laser beam, power density of each laser beam, a rate of reduction of the power of each laser beam, and/or a distance of ends of the fibers from the powder bed. 12. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and a solidification velocity comprises emitting laser beams from fibers at least adjacent to the pattern of the layer and heating the powder adjacent to the powder of the layer to control a cooling rate of the melted powder. 13. A superalloy article or repair according to claim 12 , wherein heating the powder adjacent to the powder of the layer comprises heating the powder at least one of prior to and/or during and/or after simultaneous melting of the powder of the pattern of the layer. 14. A superalloy article or repair according to claim 12 , wherein a power density of the laser beams heating the powder adjacent the pattern is in a range of from about 100 W/cm 2 to about 100,000 W/cm 2 . 15. A superalloy article or repair according to claim 1 , further comprising: moving the selected fibers and the powder bed relative to each other; and controlling the laser beams of the selected fibers during relative movement. 16. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and the solidification velocity to form the columnar or single crystal microstructure comprises controlling a cooling rate of each layer in two dimensions. 17. A superalloy article or repair according to claim 16 , wherein controlling the cooling rate of each layer in two dimensions comprises controlling a cooling rate of a layer that forms a surface layer of the article or repair to have at least one of a predetermined surface roughness and density. 18. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and the solidification velocity comprises decreasing an output of each of the plurality of laser beams asymptotically towards a set value to control a cooling period of the melt pool. 19. A superalloy article or repair according to claim 1 , wherein the superalloy article is a turbine component. 20. A superalloy article or repair according to claim 19 , wherein the turbine component is an airfoil.

Assignees

Inventors

Classifications

  • Two or more · CPC title

  • characterised by the configuration of the radiation means · CPC title

  • characterised by the type, e.g. laser or electron beam · CPC title

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

  • Temperature or temperature gradient, e.g. temperature of the melt pool · CPC title

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What does patent US11020955B2 cover?
A method of method of forming or repairing a superalloy article having a columnar or equiaxed or directionally solidified or amorphous or single crystal microstructure includes emitting a plurality of laser beams from selected fibers of a diode laser fiber array corresponding to a pattern of a layer of the article onto a powder bed of the superalloy to form a melt pool; and controlling a temper…
Who is the assignee on this patent?
Gen Electric
What technology area does this patent fall under?
Primary CPC classification B23K26/0006. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jun 01 2021 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).