Additive manufacturing process distortion management
US-2016325503-A1 · Nov 10, 2016 · US
US10005239B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10005239-B2 |
| Application number | US-201514812762-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 29, 2015 |
| Priority date | Jul 29, 2015 |
| Publication date | Jun 26, 2018 |
| Grant date | Jun 26, 2018 |
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A support structure for an additive manufacturing system includes a support body with a support body material and an interface disposed on the support body with an interface material. The interface material has a ductile-to-brittle transition temperature that is higher than the ductile-to-brittle temperature of the support body material for selectively fracturing the interface material to separate an additively manufactured article from the support body.
Opening claim text (preview).
What is claimed is: 1. A support structure, comprising: a support body including a support body material; and an interface layer disposed over the support body and including an interface material, wherein the interface material has a ductile-brittle transition temperature that is higher than a ductile-brittle transition temperature of the support body material for separating three-dimensional articles formed on the interface material. 2. The support structure as recited in claim 1 , wherein the article includes a plurality of layers fused over top one another using a selective laser sintering process, an electron beam melting process, or an electron beam sintering process. 3. The support structure as recited in claim 1 , wherein the interface material has a resistance that is lower than a resistance of the support body material. 4. The support structure as recited in claim 3 , further including an article coupled to the interface layer with a resistance that is less than the resistance of the interface material. 5. The support structure as recited in claim 1 , further including source and drain leads connected to the interface layer. 6. The support structure as recited in claim 5 , wherein the source lead, the interface layer, and the drain lead form a resistive heating element. 7. The support structure as recited in claim 1 , further including an article coupled to the support structure by the interface layer, wherein the article has a ductile-to-brittle transition temperature lower than the ductile-to-brittle transition temperature of the interface material. 8. The support structure as recited in claim 1 , wherein the interface material includes carbon steel with an embrittlement constituent added to promote fracture of the interface layer. 9. The support structure as recited in claim 8 , wherein the embrittlement component at least one of oxygen, nitrogen, sulfur, and phosphorous. 10. The support structure as recited in claim 8 , wherein the embrittlement constituent includes a precipitate disposed at grain boundaries within a crystalline structure of the interface material. 11. The support structure as recited in claim 8 , wherein the embrittlement constituent includes at least one of an impurity, a non-metallic inclusion, and an intermetallic constituent. 12. The support structure as recited in claim 8 , wherein the embrittlement constituent includes an iron-nitride precipitate. 13. A method of separating an additively manufactured article from a support structure including a support body with a support body material, the method comprising: heating an interface layer coupling an article constructed by layer wise addition of layers on the interface layer, wherein the interface layer is disposed over the support body and includes an interface material, wherein the interface material has a ductile-brittle transition temperature that is higher than a ductile-brittle transition temperature of the support body material; and cooling the interface layer such that the interface layer fractures, wherein cooling the interface layer includes cooling the interface layer to a temperature that is below the ductile-to brittle transition temperature of a material forming the interface layer. 14. The method as recited in claim 13 , wherein cooling the interface layer includes cooling the interface layer to a temperature that is (a) above a ductile-to-brittle transition temperature of a material included in the support structure, and (b) above a ductile-to-brittle transition temperature of a material included in the article. 15. The method as recited in claim 13 , wherein heating the interface layer includes resistively heating the interface layer to a temperature that is above the blue brittleness temperature of a material forming the interface layer.
using layers of powder being selectively joined, e.g. by selective laser sintering or melting · CPC title
characterised by material · CPC title
Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title
Data acquisition or data processing for additive manufacturing · CPC title
for holding or positioning work · CPC title
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