IP Library Granted Patent US 10,710,306
Granted Patent B2
US 10,710,306 · App. 15/985,510 · Granted Jul 14, 2020

Support structures for additive manufacturing techniques

Inventors: Kiley James Versluys (Hartford, CT); Sergey Mironets (Charlotte, NC)
Assignee: Delavan Inc.
B29C64/386B23K37/04B29C64/153B29C64/40B33Y40/00Y10T29/49817
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Quick Facts
Patent No.
US 10,710,306
App. No.
15/985,510
Granted
Jul 14, 2020
Kind
B2
Abstract

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.

Claims (22)

1. A method of separating an additively manufactured article from a support structure, the method comprising:

heating an interface layer coupling an article constructed by layer wise addition of layers on the interface layer; 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 a ductile-to brittle transition temperature of a material forming the interface layer.

2. A method as recited in claim 1 , 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.

3. A method as recited in claim 1 , wherein heating the interface layer includes resistively heating the interface layer to a temperature that is above a blue brittleness temperature of a material forming the interface layer.

4. A method as recited in claim 1 , further comprising depositing the interface layer on the support structure.

5. A method as recited in claim 4 , wherein depositing the interface layer on the support structure includes depositing an inclusion with the interface layer.

6. A method as recited in claim 4 , wherein the depositing the interface layer on the support structure includes depositing an embrittlement component.

7. A method as recited in claim 6 , wherein the embrittlement component includes at least one of oxygen, nitrogen, sulfur, and phosphorous.

8. A method as recited in claim 6 , wherein the embrittlement component includes iron-nitride disposed at grain boundaries of a nitrogen-rich carbon steel material.

9. A method as recited in claim 1 , further comprising constructing the additively manufactured article layerwise on the interface layer.

10. A method as recited in claim 1 , wherein heating the interface layer comprises disposing a precipitate at grain boundaries within a crystalline structure of the interface layer.

11. A method as recited in claim 1 , wherein cooling the interface layer includes cooling the interface layer using an air quench or a nitrogen bath quench.

12. A method as recited in claim 1 , further comprising separating the additively manufactured article from the support structure.

13. A method of separating an additively manufactured article from a support structure, comprising:

depositing the interface layer on the support structure;

constructing the additively manufactured article layerwise on the interface layer;

heating an interface layer coupling an article constructed by layer wise addition of layers on the interface layer;

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 a ductile-to brittle transition temperature of a material forming the interface layer; and

separating the additively manufactured article from the support structure.

14. A 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. A method as recited in claim 13 , wherein heating the interface layer includes resistively heating the interface layer to a temperature that is above a blue brittleness temperature of a material forming the interface layer.

Assignments (2)
CHANGE OF NAME Recorded May 23, 2022
From: DELAVAN INC
To: COLLINS ENGINE NOZZLES, INC.
Reel/Frame 060158/0981 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 10, 2020
From: VERSLUYS, KILEY J.; MIRONETS, SERGEY
To: DELAVAN INC.
Reel/Frame 052893/0812 →
Continuity (2)
Division 14812762 · Jul 29, 2015
Related Publication 20180272609A1 · Sep 27, 2018