Systems and methods for additively manufacturing composite parts
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B29C-067/00
B33Y-070/00
B29C-069/00
B29C-070/28
B05D-001/26
B05D-001/34
B05D-003/06
B05D-003/12
B29C-035/16
B29C-070/16
B29C-070/38
B29C-070/54
C09D-005/00
B29B-011/00
B29B-011/16
C09D-201/00
B29C-047/00
B29C-064/106
B29K-105/00
B33Y-010/00
B29L-031/30
B29L-031/00
B33Y-030/00
B33Y-040/00
B29K-063/00
B29K-105/08
B29K-105/10
B33Y-050/02
B29K-101/10
B29K-105/12
B29C-035/08
B29K-105/06
B29C-064/135
B29C-064/129
B29C-064/25
출원번호
US-0920767
(2015-10-22)
등록번호
US-10166753
(2019-01-01)
발명자
/ 주소
Evans, Nick S.
Torres, Faraón
Ziegler, Ryan G.
Harrison, Samuel F.
Grijalva, III, Ciro J.
Osborn, Hayden S.
출원인 / 주소
The Boeing Company
대리인 / 주소
Dascenzo Intellectual Property Law, P.C.
인용정보
피인용 횟수 :
0인용 특허 :
20
초록▼
A method of additively manufacturing 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 deliver
A method of additively manufacturing 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.
대표청구항▼
1. A method of additively manufacturing a composite part, the method comprising: depositing a segment of a continuous flexible line along a print path, and wherein the continuous flexible line comprises a non-resin component and a photopolymer-resin component that is uncured; andwhile advancing the
1. A method of additively manufacturing a composite part, the method comprising: depositing a segment of a continuous flexible line along a print path, and wherein the continuous flexible line comprises a non-resin component and a photopolymer-resin component that is uncured; andwhile advancing the continuous flexible line toward the print path, delivering a ring of curing energy that intersects at least a portion of the segment of the continuous flexible line to at least partially cure at least the portion of the segment of the continuous flexible line, and 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 liquid photopolymer resin to the non-resin component while pushing the continuous flexible line through a delivery guide, and wherein the photopolymer-resin component comprises at least some of the liquid photopolymer resin applied to the non-resin component. 3. The method according to claim 2, wherein applying the liquid photopolymer resin to the non-resin component while pushing the continuous flexible line through the delivery guide comprises pulling the non-resin component through a vessel, containing a volume of the liquid photopolymer resin. 4. The method according to claim 3, further comprising detecting a level of the liquid photopolymer resin within the vessel and selectively delivering the liquid photopolymer resin to the vessel when the volume of the liquid photopolymer resin is at or below a lower-threshold level. 5. The method according to claim 3, wherein pulling the non-resin component through the vessel comprises limiting an amount of the liquid photopolymer resin that exits the vessel. 6. The method according to claim 3, wherein pulling the non-resin component through the vessel comprises uniformly applying the liquid photopolymer resin to the non-resin component. 7. The method according to claim 3, wherein pulling the non-resin component through the vessel comprises configuring the non-resin component to have no bend less than 60 degrees between any two sequential segments of the non-resin component within the vessel. 8. 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 or against a previously deposited segment to additively manufacture the composite part. 9. 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. 10. The method according to claim 9, wherein the physical characteristics include at least one of strength, stiffness, flexibility, ductility, or hardness. 11. 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 curing energy provides different physical characteristics at different locations of the composite part. 12. The method according to claim 11, wherein the physical characteristics include at least one of strength, stiffness, flexibility, ductility, or hardness. 13. The method according to claim 1, wherein delivering the ring of the curing energy 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. 14. The method according to claim 1, wherein delivering the ring of the curing energy comprises curing less than an entirety of the composite part. 15. The method according to claim 1, further comprising restrictively curing at least a portion of the composite part. 16. The method according to claim 15, wherein the portion of the composite part is restrictively cured to facilitate subsequent processing of the portion. 17. The method according to claim 1, wherein delivering the ring of the curing energy 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. 18. The method according to claim 17, wherein the varying physical characteristics include at least one of strength, stiffness, flexibility, ductility, or hardness. 19. 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. 20. The method according to claim 19, 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. 21. 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. 22. The method according to claim 21, 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. 23. The method according to claim 21, 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. 24. The method according to claim 1, further comprising selectively cutting the continuous flexible line, and wherein the continuous flexible line is selectively cut simultaneously with depositing the segment of the continuous flexible line along the print path. 25. 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. 26. 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. 27. The method according to claim 1, further comprising curing the composite part in an autoclave or in an oven. 28. The method according to claim 1, wherein: delivering the ring of the curing energy comprises delivering an actively determined amount of curing energy at least to the portion of the segment of the continuous flexible line at a controlled rate, to at least partially cure at least the portion of the segment of the continuous flexible line to a desired level of cure;the actively determined amount of the curing energy is based on real-time data, sensed from the continuous flexible line as the continuous flexible line is being deposited; andthe real-time data comprises hardness, color, temperature, or glow of the continuous flexible line. 29. The method according to claim 28, 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. 30. The method according to claim 28, 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. 31. The method according to claim 28, 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 restrictively curing at least a portion of the composite part; and the portion of the composite part is restrictively cured to facilitate subsequent processing of the portion of the composite part. 32. The method according to claim 28, 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 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; and the varying physical characteristics comprise at least one of strength, stiffness, flexibility, or hardness. 33. The method according to claim 1, wherein 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, or a wire bundle. 34. The method according to claim 1, wherein the photopolymer-resin component comprises at least one of an ultraviolet-light photopolymer resin, a visible-light photopolymer resin, an infrared-light photopolymer resin, or an x-ray photopolymer resin. 35. The method according to claim 1, further comprising, simultaneously with delivering the ring of the curing energy, at least partially protecting at least the portion of the segment of the continuous flexible line from oxidation. 36. The method according to claim 35, 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. 37. 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; andthe method further comprises removing the sacrificial layer to form the composite part. 38. The method according to claim 1, wherein: the continuous flexible line is a first continuous flexible line;the segment of the continuous flexible line is a first segment of the first continuous flexible line;the method further comprises depositing a second segment of a second continuous flexible line along the print path; andthe second continuous flexible line comprises at least one component that differs from at least one component of the first continuous flexible line.
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