Method for additively manufacturing composite parts

Patent metadata

Field	Value
Publication number	US-10279580-B2
Application number	US-201514841504-A
Country	US
Kind code	B2
Filing date	Aug 31, 2015
Priority date	Jul 31, 2015
Publication date	May 7, 2019
Grant date	May 7, 2019

Abstract

A method of additively manufacturing a composite part comprises depositing a segment of a continuous flexible line along a print path. The continuous flexible line comprises a non-resin component and further comprises a photopolymer-resin component that is uncured. The method further comprises delivering a predetermined or actively determined amount of curing energy at least to a portion of the segment of the continuous flexible line at a controlled rate while advancing the continuous flexible line toward the print path and after the segment of the continuous flexible line is deposited along the print path to at least partially cure at least the portion of the segment of the continuous flexible line.

First claim

What is claimed is:

1. A method of additively manufacturing a composite part, the method comprising:
depositing, via a delivery assembly, a segment of a continuous flexible line along a print path, wherein the continuous flexible line comprises a non-resin component and further comprises a photopolymer-resin component that is uncured; and
delivering a ring of a predetermined or actively determined amount of curing energy at least to a portion of the segment of the continuous flexible line at a controlled rate while advancing the continuous flexible line toward the print path and after the segment of the continuous flexible line is deposited along the print path to at least partially cure at least the portion of the segment of the continuous flexible line, wherein the ring of the curing energy is delivered by at least one galvanometer mirror-positioning system.

2. The method according to claim 1 , further comprising applying a photopolymer resin to the non-resin component while pushing the continuous flexible line through a delivery assembly, wherein the photopolymer-resin component comprises at least some of the photopolymer resin applied to the non-resin component.

3. The method according to claim 2 , wherein applying the photopolymer resin to the non-resin component while pushing the continuous flexible line through the delivery assembly comprises injecting the photopolymer resin into the delivery assembly.

4. The method according to claim 2 , wherein applying the photopolymer resin to the non-resin component while pushing the continuous flexible line through the delivery assembly comprises metering a flow of the photopolymer resin.

5. The method according to claim 4 , wherein metering the flow of the photopolymer resin comprises detecting a level of the photopolymer resin within the delivery assembly.

6. The method according to claim 5 , wherein metering the flow of the photopolymer resin comprises selectively reducing or selectively increasing the flow of the photopolymer resin to the delivery assembly responsive to the level of the photopolymer resin within the delivery assembly.

7. The method according to claim 4 , wherein metering the flow of the photopolymer resin comprises detecting a saturation level of the non-resin component with the photopolymer resin.

8. The method according to claim 7 , wherein metering the flow of the photopolymer resin comprises selectively reducing or selectively increasing the flow of the photopolymer resin to the delivery assembly responsive to the saturation level of the non-resin component with the photopolymer resin.

9. The method according to claim 2 , further comprising collecting excess photopolymer resin resulting from applying the photopolymer resin to the non-resin component.

10. 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 ring of the predetermined or actively determined amount of the curing energy at least to the portion of the segment of the continuous flexible line at the controlled rate provides different physical characteristics at different locations of the composite part.

11. The method according to claim 1 , wherein delivering the ring of the predetermined or actively determined amount of the curing energy at least to the portion of the segment of the continuous flexible line at the controlled rate comprises partially curing a first layer of the segment of the continuous flexible line as the first layer is being deposited and further curing the first layer as a second layer is being deposited against the first layer.

12. The method according to claim 1 , wherein delivering the ring of the predetermined or actively determined amount of the curing energy at least to the portion of the segment of the continuous flexible line at the controlled rate comprises curing less than an entirety of the composite part.

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

14. The method according to claim 1 , wherein delivering the ring of the predetermined or actively determined amount of the curing energy at least to the portion of the segment of the continuous flexible line at the controlled rate comprises selectively varying at least one of a delivery rate or a delivery duration of the curing energy to impart varying physical characteristics to the composite part.

15. 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.

16. 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.

17. The method according to claim 1 , further comprising selectively cutting the continuous flexible line, wherein the continuous flexible line is selectively cut simultaneously with depositing the segment of the continuous flexible line along the print path.

18. The method according to claim 1 , further comprising, simultaneously with delivering the ring of the predetermined or actively determined amount of the curing energy at least to the portion of the segment of the continuous flexible line at the controlled rate, at least partially protecting at least the portion of the segment of the continuous flexible line from oxidation after the segment exits a delivery guide.

19. 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.

20. The method according to claim 1 , wherein depositing the segment of the continuous flexible line along the print path comprises pushing the continuous flexible line through a delivery guide.

21. The method according to claim 1 , wherein:
delivering the ring of the predetermined or actively determined amount of the curing energy at least to the portion of the segment of the continuous flexible line at the controlled rate comprises delivering an actively determined amount of the curing energy at least to the portion of the segment of the continuous flexible line at the controlled rate;
the actively determined amount of the curing energy is based on real-time data, sensed from the continuous flexible line as it is being deposited; and
the real-time data comprises hardness, color, temperature, or glow of the continuous flexible line.

22. The method according to claim 21 , wherein delivering the actively determined amount of the curing energy at least to the portion of the segment of the continuous flexible line at the controlled rate comprises partially curing a first layer of the segment of the continuous flexible line as the first layer is being deposited and further curing the first layer as a second layer is being deposited against the first layer.

23. The method according to claim 21 , wherein delivering the actively determined amount of the curing energy at least to the portion of the segment of the continuous flexible line at the controlled rate comprises curing less than an entirety of the composite part.

Assignees

• Boeing Co

Inventors

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

Classifications

• B29K2101/10

  Thermosetting resins · CPC title

• B29C48/02

  Small extruding apparatus, e.g. handheld, toy or laboratory extruders · CPC title

• B29C70/28

  Shaping operations therefor · CPC title

• B29C64/40

  Structures for supporting 3D objects during manufacture and intended to be sacrificed after completion thereof · CPC title

• B29C64/25

  Housings, e.g. machine housings · CPC title