Methods and apparatus for manufacturing optimized panels and other composite structures

Patent metadata

Field	Value
Publication number	US-11260582-B2
Application number	US-201816162301-A
Country	US
Kind code	B2
Filing date	Oct 16, 2018
Priority date	Oct 16, 2018
Publication date	Mar 1, 2022
Grant date	Mar 1, 2022

Abstract

The disclosure relates to additively manufactured (AM) composite structures such as panels for use in transport structures or other mechanized assemblies. An AM core may be optimized for an intended application of a panel. In various embodiments, one or more values such as strength, stiffness, density, energy absorption, ductility, etc. may be optimized in a single AM core to vary across the AM core in one or more directions for supporting expected load conditions. In an embodiment, the expected load conditions may include forces applied to the AM core or corresponding panel from different directions in up to three dimensions. Where the structure is a panel, face sheets may be affixed to respective sides of the core. The AM core may be a custom honeycomb structure. In other embodiments, the face sheets may have custom 3-D profiles formed traditionally or through additive manufacturing to enable structural panels with complex profiles. The AM core may include a protrusion to provide fixturing features to enable external connections. In other embodiments, inserts, fasteners, or internal channels may be co-printed with the core. In still other embodiments, the AM core may be used in a composite structure such as, for example a rotor blade or a vehicle component.

First claim

What is claimed is:

1. A panel for use in a transport structure, comprising;
at least one face sheet having a cutout region; and
an additively manufactured (AM) core affixed to the at least one face sheet and having a varying strength across at least a portion of the AM core for supporting expected load conditions determined across all three coordinate axes (x,y,z), the AM core having a protruding portion extending through the cutout region, and the protruding portion is coupled to a fixturing feature for engaging with an external structure.

2. The panel of claim 1 , wherein the at least one face sheet comprises a non-planar contour.

3. The panel of claim 1 , wherein the at least one face sheet comprises a variable thickness.

4. The panel of claim 1 , wherein the AM core comprises a homogenous material.

5. The panel of claim 1 , wherein the AM core has the varying strength along a plurality of directions.

6. The panel of claim 1 , wherein the expected load conditions comprise forces asserted in three dimensions.

7. The panel of claim 1 , wherein the expected load conditions comprise forces asserted from a plurality of directions.

8. The panel of claim 1 , wherein the expected load conditions comprise forces asserted on either or both of the panel or the AM core.

9. The panel of claim 1 , wherein the expected load conditions comprise forces asserted on a plurality of locations of the panel or the AM core.

10. The panel of claim 1 , wherein the AM core has one or more variable properties across one or more portions of the AM core for supporting the expected load conditions, wherein the one or more variable properties include one or more of a varying stiffness, a varying rigidity, a varying flexibility, a varying ductility, a varying density, a varying energy absorption, or a varying crush.

11. The panel of claim 10 , wherein one or more of the varying stiffness, the varying rigidity, the varying flexibility or the varying density vary in a plurality of directions in the AM core.

12. The panel of claim 1 , wherein the expected load conditions are derived from an intended application of the panel.

13. The panel of claim 1 , wherein the AM core comprises a modified honeycomb structure.

14. The panel of claim 1 , wherein the at least one face sheet is 3-D printed and has a contoured shape to form a non-flat panel when joined with the AM core.

15. The panel of claim 1 , wherein the at least one face sheet is formed and has a contoured shape to form a non-flat panel when joined with the AM core.

16. The panel of claim 1 , wherein the at least one face sheet comprises first and second face sheets,
the AM core is affixed between the first and second face sheets, and
the first and second face sheets are one of 3-D printed or formed and have contoured shapes to form a non-flat panel when joined with the AM core.

17. The panel of claim 16 , further comprising:
a first adhesive layer adhered to the first face sheet and a first side of the AM core; and
a second adhesive layer adhered to the second face sheet and a second side of the AM core.

18. The panel of claim 1 , wherein the AM core is quasi-isotropic.

19. The panel of claim 1 , wherein the AM core is one of anisotropic or orthotropic based on an intended panel application.

20. The panel of claim 1 , wherein the at least one face sheet comprises a carbon fiber reinforced composite material.

21. The panel of claim 1 , wherein the AM core comprises a metal, an alloy, or a plastic material.

22. The panel of claim 1 , wherein the AM core is additively manufactured to include one or more inserts.

23. The panel of claim 1 , wherein the AM core is additively manufactured to include, at or near a core boundary, a connecting feature for mating with a corresponding connecting feature or fastener coupled to another structure.

24. The panel of claim 1 , further comprising a connection feature or fastener co-printed with the AM core.

25. The panel of claim 1 , wherein the cutout region is disposed on an upper surface of the at least one face sheet and an upper surface of the fixturing feature is parallel with the upper surface of the at least one face sheet.

26. The panel of claim 1 , wherein the fixturing feature comprises at least one receptacle region for engaging with the external structure.

27. The panel of claim 1 , wherein the external structure comprises a part of the transport structure, and the fixturing feature is coupled to the external structure to secure the panel to the transport structure.

28. The panel of claim 1 , wherein the fixturing feature is adhered to the protruding portion via an adhesive.

29. The panel of claim 1 , wherein the AM core comprises a first custom interface feature for interlocking with an adjacent panel having a second custom interface feature, the first and second custom interface features each comprising one of a projection feature and a receiving feature to enable fixturing of the panels for attachment.

30. The panel of claim 1 , wherein the AM core comprises a custom interface feature having at least one connector for connecting the panel to one or more adjacent panels.

31. The panel of claim 30 , wherein the at least one connector comprises a protruding connector.

32. The panel of claim 30 , wherein the at least one connector comprises a receiving connector for engaging with a protruding connector.

33. The panel of claim 32 , wherein the protruding connector comprises a tab and the receiving connector comprises a slot.

34. The panel of claim 29 , wherein the receiving feature comprises a slide-in feature.

35. The panel of claim 29 , wherein at least one of the first and second custom interface features comprises a plate, the plate having apertures for receiving a fastener.

36. The panel of claim 1 , wherein the AM core comprises a powder removal feature.

37. The panel of claim 1 , wherein the AM core comprises at least one channel for enabling resin flow.

38. The panel of claim 37 , wherein the AM core further comprises at least one vacuum channel.

39. The panel of claim 1 , wherein the AM core and the at least one face sheet are co-printed.

40. The panel of claim 1 , wherein the AM core and the at least one face sheet are 3-D printed as a single integrated structure, and
the AM core is affixed to the at least one face sheet during the 3-D printing.

41. The panel of claim 40 , wherein the AM core and the at least one face sheet comprise an identical material.

Assignees

• Divergent Tech Inc

Inventors

• Tenhouten Broc William
• Bowden Jr Thomas Samuel
• Gunner Jon Paul

Classifications

• B33Y80/00 Primary

  Products made by additive manufacturing · CPC title

• B22F12/49

  Scanners · CPC title

• B22F10/85

  for controlling or regulating additive manufacturing processes · CPC title

• B22F10/47

  characterised by structural features · CPC title

• B22F10/25

  Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS] · CPC title