Thermal debinding techniques for additive manufacturing and related systems and methods

Patent metadata

Field	Value
Publication number	US-2021260654-A1
Application number	US-202117158673-A
Country	US
Kind code	A1
Filing date	Jan 26, 2021
Priority date	Feb 21, 2020
Publication date	Aug 26, 2021
Grant date	—

Abstract

Techniques for debinding additively fabricated parts are described that do not require solvent debinding or catalytic debinding, and that may be performed using only thermal debinding in a furnace. As a result, in at least some cases debinding and sintering may take place sequentially within a single furnace. In some embodiments, the techniques may utilize particular materials as binders that allow for a thermal debinding process that does not negatively affect the parts.

First claim

What is claimed is:

1 . A method of fabricating a part via additive fabrication according to a three-dimensional (3D) model, the method comprising:
identifying one or more geometrical regions of the 3D model; generating a second 3D model by modifying the one or more geometrical regions of the 3D model to increase porosity of the one or more geometrical regions; additively fabricating a part according to the second 3D model from a build material comprising at least one metal powder and a binder; and heating the part in a furnace to cause at least some of the binder to evaporate and/or sublimate into a gas, wherein portions of the part corresponding to the one or more geometrical regions of the second 3D model provide egress for said gas.

2 . The method of claim 1 , wherein modifying the one or more geometrical regions comprises generating one or more holes in an exterior surface of the one or more geometrical regions.

3 . The method of claim 2 , wherein the one or more holes have a diameter of less than 3 mm.

4 . The method of claim 1 , further comprising generating toolpaths for a plurality of layers of the second 3D model, wherein the part is additively fabricated according to the generated toolpaths.

5 . The method of claim 4 , wherein the toolpaths are configured to produce a gyroid infill pattern in at least some of the layers.

6 . The method of claim 4 , wherein the toolpaths for the plurality of layers of the second 3D model include one or more open spaces adjacent to at least some of the one or more geometrical regions of the second 3D model.

7 . The method of claim 6 , wherein the one or more open spaces include one or more channels coupled to the one or more geometrical regions of the second 3D model.

8 . The method of claim 7 , wherein the one or more channels include a network of channels coupled to one another with an open end of the network of channels arranged at one of the one or more geometrical regions of the second 3D model.

9 . The method of claim 1 , further comprising additively fabricating a raft structure and a support structure, wherein the support structure is fabricated on top of and attached to the raft structure, and wherein the part is fabricated on top of and attached to the support structure.

10 . The method of claim 1 , wherein identifying one or more geometrical regions of the 3D model comprises receiving input via a user interface identifying the one or more geometrical regions of the 3D model.

11 . A method of fabricating a part via additive fabrication according to a three-dimensional (3D) model, the method comprising:
generating a raft structure for the model; generating a porous support structure arranged between the raft structure and the model such that the model does not couple directly to the raft structure; additively fabricating a part, according to the 3D model, the raft structure and the porous support structure, from a build material comprising at least one metal powder and a binder; heating the part in a furnace to cause at least some of the binder to evaporate and/or sublimate into a gas, wherein the porous support structure provides egress for said gas.

12 . The method of claim 11 , wherein the porous support structure comprises a plurality of channels extending between a side of the porous support structure attached to the model and a side of the porous support structure attached to the raft.

13 . (canceled)

14 . The method of claim 11 , further comprising generating toolpaths for a plurality of layers of the second 3D model, wherein the part is additively fabricated according to the generated toolpaths.

15 . The method of claim 14 , wherein the toolpaths are configured to produce a gyroid infill pattern in at least some of the layers.

16 . The method of claim 14 , wherein the toolpaths for the plurality of layers of the second 3D model include one or more open spaces adjacent to the support structure.

17 . The method of claim 16 , wherein the one or more open spaces include one or more channels coupled to the one or more geometrical regions of the second 3D model.

18 . The method of claim 17 , wherein the one or more channels include a network of channels coupled to one another with an open end of the network of channels arranged next to at least one pore within the porous support structure.

19 . (canceled)

20 . A method of fabricating a part via additive fabrication according to a three-dimensional (3D) model, the method comprising:
identifying one or more geometrical regions of the 3D model; generating instructions for an additive fabrication device to form a part according to the 3D model wherein the part is configured to be formed from a solid exterior shell surrounding infill material, and wherein the solid exterior shell is arranged to have a first thickness within the identified one or more geometrical regions of the 3D model and to have a second thickness, greater than the first thickness, outside the identified one or more geometrical regions of the 3D model; additively fabricating the part using the additive fabrication device according to the generated instructions from a build material comprising at least one metal powder and a binder; and heating the part in a furnace to cause at least some of the binder to evaporate and/or sublimate into a gas, wherein portions of the part corresponding to the one or more geometrical regions of the second 3D model provide egress for said gas.

21 . The method of claim 20 , wherein the part is configured to include an empty space between the infill material and the regions of the solid exterior shell having the first thickness.

22 . The method of claim 21 , wherein the second thickness is equal to a thickness of the empty space combined with the first thickness.

23 - 31 . (canceled)

Assignees

• Desktop Metal Inc

Inventors

• Reidy John
• Tuncer Nihan
• Bose Animesh
• Craven Christopher
• Barbati Alexander C
• Fulop Ricardo
• Schofalvi Karl-Heinz

Classifications

• Y02P10/25

  Process efficiency · CPC title

• B22F10/14

  by jetting of binder onto a bed of metal powder · CPC title

• B22F3/1021 Primary

  Removal of binder or filler (removal of binder from ceramics C04B35/638) · CPC title

• B33Y70/10

  Composites of different types of material, e.g. mixtures of ceramics and polymers or mixtures of metals and biomaterials · CPC title

• B22F2999/00

  Aspects linked to processes or compositions used in powder metallurgy · CPC title