Methods for additively manufacturing composite parts

Patent metadata

Field	Value
Publication number	US-10112380-B2
Application number	US-201514841500-A
Country	US
Kind code	B2
Filing date	Aug 31, 2015
Priority date	Jul 31, 2015
Publication date	Oct 30, 2018
Grant date	Oct 30, 2018

Abstract

A method of additively manufacturing a composite part comprises pushing a continuous flexible line through a delivery guide. The continuous flexible line comprises a non-resin component and a photopolymer-resin component that is partially cured. The method also comprises depositing, via the delivery guide, a segment of the continuous flexible line along a print path. Additionally, the method comprises delivering curing energy at least to a portion of the segment of the continuous flexible line deposited along the print path.

First claim

What is claimed is:

1. A method of additively manufacturing a composite part, the method comprising:
pushing a continuous flexible line through a delivery guide using a feed mechanism, wherein the continuous flexible line comprises a non-resin component and a photopolymer-resin component that is partially cured, and wherein the feed mechanism comprises opposing rollers and a scraper in contact with at least one of the opposing rollers;
depositing, via the delivery guide, a segment of the continuous flexible line along a print path;
delivering curing energy at least to a portion of the segment of the continuous flexible line deposited along the print path;
removing, using the scraper, residue of the photopolymer-resin component produced by the engagement between the opposing rollers and the continuous flexible line as the opposing rollers rotate to selectively translate the continuous flexible line to push the continuous flexible line through the delivery guide; and
collecting, into a collection reservoir, the residue of the photopolymer-resin component, removed by the scraper.

2. The method according to claim 1 , wherein:
the delivery guide comprises a line passage through which the continuous flexible line is delivered to the print path;
the line passage of the delivery guide has an inlet;
the feed mechanism pushes the continuous flexible line through the line passage;
the opposing rollers having respective rotational axes;
the delivery guide further comprises a first end portion, a second end portion, and a junction between the first end portion and the second end portion;
the first end portion is shaped to be complementary to one of the opposing rollers and the second end portion is shaped to be complementary to another of the opposing rollers; and
a shortest distance (D) between the junction and a plane containing the respective rotational axes of the opposing rollers is less than a radius of a smallest one of the opposing rollers.

3. The method according to claim 2 , wherein the curing energy is delivered at least to the portion of the segment of the continuous flexible line as the continuous flexible line is pushed through the delivery guide toward the print path and after the segment of the continuous flexible line is deposited along the print path.

4. The method according to claim 2 , wherein the junction comprises an edge.

5. The method according to claim 1 , wherein:
the continuous flexible line comprises a prepreg composite material; and
the non-resin component comprises one or more of a fiber, a carbon fiber, a glass fiber, a synthetic organic fiber, an aramid fiber, a natural fiber, a wood fiber, a boron fiber, a silicon-carbide fiber, an optical fiber, a fiber bundle, a fiber tow, a fiber weave, a wire, a metal wire, a conductive wire, and a wire bundle.

6. The method according to claim 1 , wherein depositing the segment of the continuous flexible line along the print path comprises layering the continuous flexible line against itself to additively manufacture the composite part.

7. The method according to claim 1 , wherein depositing the segment of the continuous flexible line along the print path comprises depositing the continuous flexible line in a predetermined pattern to selectively control one or more physical characteristics of the composite part.

8. The method according to claim 1 , wherein at least one of depositing the segment of the continuous flexible line along the print path or delivering the curing energy at least to the portion of the segment of the continuous flexible line provides different physical characteristics at different locations of the composite part.

9. The method according to claim 8 , wherein the physical characteristics include at least one of strength, stiffness, flexibility, or hardness.

10. The method according to claim 1 , further comprising restrictively curing at least a portion of the composite part.

11. The method according to claim 10 , wherein the portion of the composite part is restrictively cured to facilitate subsequent processing of the portion of the composite part.

12. The method according to claim 1 , further comprising, simultaneously with depositing the segment of the continuous flexible line along the print path, compacting at least a section of the segment of the continuous flexible line after the segment of the continuous flexible line is deposited along the print path.

13. The method according to claim 12 , wherein compacting at least the section of the segment of the continuous flexible line after the segment of the continuous flexible line is deposited along the print path comprises imparting a desired cross-sectional shape to the segment of the continuous flexible line.

14. The method according to claim 1 , further comprising, simultaneously with depositing the segment of the continuous flexible line along the print path, roughening at least a section of the segment of the continuous flexible line after the segment of the continuous flexible line is deposited along the print path.

15. The method according to claim 14 , further comprising, simultaneously with roughening at least the section of the segment of the continuous flexible line, dispersing debris resulting from roughening at least the section of the segment of the continuous flexible line.

16. The method according to claim 14 , further comprising, simultaneously with roughening at least the section of the segment of the continuous flexible line, collecting debris resulting from roughening at least the section of the segment of the continuous flexible line.

17. The method according to claim 1 , further comprising selectively cutting the continuous flexible line.

18. The method according to claim 17 , wherein the continuous flexible line is selectively cut simultaneously with depositing the segment of the continuous flexible line along the print path.

19. The method according to claim 1 , further comprising, simultaneously with delivering the curing energy at least to the portion of the segment of the continuous flexible line, at least partially protecting at least the portion of the segment of the continuous flexible line from oxidation after the segment exits the delivery guide.

20. The method according to claim 19 , wherein at least the portion of the segment of the continuous flexible line is at least partially protected from the oxidation with a shielding gas.

21. The method according to claim 1 , further comprising, simultaneously with depositing the segment of the continuous flexible line along the print path, detecting defects in the composite part.

22. The method according to claim 1 , wherein depositing the segment of the continuous flexible line along the print path comprises depositing at least a portion of the segment of the continuous flexible line over a sacrificial layer.

23. The method according to claim 1 , wherein the continuous flexible line is a first continuous flexible line and the segment of the continuous flexible line is a first segment of the first continuous flexible line, and the method further comprises depositing a second segment of a second continuous flexible line along the print path, wherein the second continuous flexible line includes at least one component that differs from at least one component of the first continuous flexible line.

24. The method according to claim 1 , wherein:
at least one of the opposing rollers comprises a circumferential channel that contacts

Assignees

• Boeing Co

Inventors

• Evans Nick S
• Torres Faraón
• Ziegler Ryan G
• Harrison Samuel F
• Grijalva Iii Ciro J
• Osborn Hayden S

Classifications

• B29C35/0805

  using electromagnetic radiation · CPC title

• B29C2035/0844

  using X-ray · CPC title

• B29C70/38

  Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns {(application heads for tyres B29D30/28)} · CPC title

• B33Y30/00

  Apparatus for additive manufacturing; Details thereof or accessories therefor · CPC title

• B29C64/321

  Feeding · CPC title