IP Library › Granted Patent US 10,046,524
Granted Patent B2
US 10,046,524 · App. 14/386,742 · Granted Aug 14, 2018

Substrate for additive manufacturing

Inventor: Jonathan Meyer (Calne, GB)
Assignee: AIRBUSGROUP LIMITED
B29C67/0092B29C64/00B29C64/153B29C64/20B29C64/40B33Y30/00B22F2003/1056B29K2995/0082B29L2031/757Y02P10/295
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Quick Facts
Patent No.
US 10,046,524
App. No.
14/386,742
Granted
Aug 14, 2018
Kind
B2
Abstract

A substrate for an additive manufacturing process, the substrate having a build surface for fusing to a part being formed on the substrate by the additive manufacturing process, wherein the substrate is configured to provide relatively high stiffness in a direction substantially perpendicular to the build surface, while having a low longitudinal stiffness in the plane of the build surface. Also, a method of forming the substrate, a system including the substrate, and use of the system for creating a part by an additive manufacturing process.

Claims (47)

1. A system for creating a part by an additive manufacturing process, the system including a substrate having a build surface for fusing to a part being formed on the substrate by the additive manufacturing process, wherein the substrate is re-useable for building successive parts by the additive manufacturing process, wherein the substrate has an upper portion nearest the build surface and a lower portion, wherein the upper portion includes an array of protrusions with their longitudinal axis aligned substantially perpendicular to the build surface, and wherein the protrusions include a different material to that of the lower portion, and the protrusions are not incorporated in the part created on the substrate.

2. A system according to claim 1 , wherein tops of the protrusions provide at least a portion of the build surface.

3. A system according to claim 1 , wherein bases of the protrusions are integrally formed with the lower portion of the substrate.

4. A system according to claim 1 , wherein the protrusions are slender and take the form of pillars having a generally planar top.

5. A system according to claim 1 , wherein the protrusions each have straight sides substantially perpendicular to the build surface.

6. A system according to claim 1 , wherein the substrate is a monolith.

7. A system according to claim 1 , wherein a gap between adjacent protrusions is filled by a material dissimilar to that of the protrusions.

8. A system according to claim 1 , wherein the array of projections are defined by an array of slits.

9. A system according to claim 8 , wherein the slits have a width of 0.1 mm or below.

10. A system according to claim 8 , wherein the slits form a grid.

11. A system according to claim 8 , wherein the slits have a substantially uniform width.

12. A system according to claim 8 , wherein the base of each slit has a radius corner.

13. A system according to claim 1 configured to create the part layer by layer.

14. A system according to claim 13 , configured to create the part by selectively sintering successive powder layers.

15. A system for creating a part by an additive manufacturing process, the system including a substrate having a build surface for fusing to a part being formed on the substrate by the additive manufacturing process, wherein the substrate is re-useable for building successive parts by the additive manufacturing process, wherein the substrate has an upper portion nearest the build surface and a lower portion, wherein the upper portion includes an array of protrusions with their longitudinal axis aligned substantially perpendicular to the build surface, and wherein the protrusions are slender, having an aspect ratio of at least 3, and take the form of pillars having a generally planar top.

16. A system according to claim 15 , wherein tops of the protrusions provide at least a portion of the build surface.

17. A system according to claim 15 , wherein bases of the protrusions are integrally formed with the lower portion of the substrate.

18. A system according to claim 15 , wherein the protrusions each have straight sides substantially perpendicular to the build surface.

19. A system according to claim 15 , wherein the substrate is a monolith.

20. A system according to claim 15 , wherein a gap between adjacent protrusions is filled by a material dissimilar to that of the protrusions.

21. A system according to claim 15 , wherein the array of projections are defined by an array of slits.

22. A system according to claim 21 , wherein the slits have a width of 0.1 mm or below.

23. A system according to claim 21 , wherein the slits form a grid.

24. A system according to claim 21 , wherein the slits have a substantially uniform width.

25. A system according to claim 21 , wherein the base of each slit has a radius corner.

26. A system according to claim 15 , configured to create the part layer by layer.

27. A system according to claim 26 , configured to create the part by selectively sintering successive powder layers.

28. A system for creating a part by an additive manufacturing process, the system including a substrate having a build surface for fusing to a part being formed on the substrate by the additive manufacturing process, wherein the substrate is re-useable for building successive parts by the additive manufacturing process, wherein the substrate has an upper portion nearest the build surface and a lower portion, wherein the upper portion includes an array of protrusions with their longitudinal axis aligned substantially perpendicular to the build surface, wherein the protrusions each have a taper of increasing cross section towards the build surface and wherein the array of projections are defined by an array of slits, wherein the slits have a width of 0.1 mm or below.

29. A system according to claim 28 , wherein tops of the protrusions provide at least a portion of the build surface.

30. A system according to claim 28 , wherein bases of the protrusions are integrally formed with the lower portion of the substrate.

31. A system according to claim 28 , wherein the protrusions are slender and take the form of pillars having a generally planar top.

32. A system according to claim 28 , wherein the substrate is a monolith.

33. A system according to claim 28 , wherein a gap between adjacent protrusions is filled by a material dissimilar to that of the protrusions.

34. A system according to claim 28 , wherein the slits are provided in an upper portion of the substrate, and a lower portion of the substrate is substantially solid.

35. A system according to claim 28 , wherein the slits form a grid.

36. A system according to claim 35 , wherein the slits have a substantially uniform width.

37. A system according to claim 35 , wherein the base of each slit has a radius corner.

38. A system according to claim 28 , configured to create the part layer by layer.

39. A system according to claim 38 , configured to create the part by selectively sintering successive powder layers.

40. A system for creating a part by an additive manufacturing process, the system including a substrate having a build surface for fusing to a part being formed on the substrate by the additive manufacturing process, and a plurality of slits extending from the build surface through part of the thickness of the substrate, wherein the substrate is re-useable for building successive parts by the additive manufacturing process, wherein the build surface is substantially rectangular, wherein the slits form a grid and are provided on only a portion of the build surface, and wherein the grid is aligned substantially with a diagonal of the build surface.

41. A system according to claim 40 , wherein the slits are provided in an upper portion of the substrate, and a lower portion of the substrate is substantially solid.

42. A system according to claim 40 , wherein the slits have a substantially uniform width.

43. A system according to claim 40 , wherein the substrate is a monolith.

44. A system according to claim 40 , wherein the base of each slit has a radius corner.

45. A system according to claim 40 , wherein the slits have a width of 0.1 mm or below.

46. A system according to claim 40 , configured to create the part layer by layer.

47. A system according to claim 46 , configured to create the part by selectively sintering successive powder layers.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 21, 2015
From: MEYER, JONATHAN
To: AIRBUSGROUP LIMITED
Reel/Frame 034772/0880 →
Priority Claims (1)
GB 1204922.7 · Mar 21, 2012 · national
Continuity (1)
Related Publication 20150054193A1 · Feb 26, 2015