Method and apparatus for forming a composite fuselage structure

Patent metadata

Field	Value
Publication number	US-11498293-B2
Application number	US-201916718821-A
Country	US
Kind code	B2
Filing date	Dec 18, 2019
Priority date	Dec 18, 2019
Publication date	Nov 15, 2022
Grant date	Nov 15, 2022

Abstract

A method and apparatus for tacking and trimming a thermoplastic tow. A thermoplastic tow is received from a braiding system over a braided structure on a surface. The thermoplastic tow is tack welded to the braided structure. A portion of the thermoplastic tow is trimmed to thereby trim the thermoplastic tow received over the braided structure.

First claim

What is claimed is:

1. A method for tacking and trimming a thermoplastic tow, the method comprising:
laying up a thermoplastic tow received from a braiding system over a braided structure on a surface; and
tack welding the thermoplastic tow to the braided structure;
trimming a portion of the thermoplastic tow received over the braided structure by applying laser energy to trim the portion of the thermoplastic tow received over the braided structure; and
supporting the portion of the tow using a conductive component while applying the laser energy to the portion of the tow.

2. The method of claim 1 , wherein a cross-sectional shape of the conductive component is wedge-shaped.

3. The method of claim 1 , wherein tack welding the thermoplastic tow comprises:
tack welding the thermoplastic tow to the braided structure using a tack welder secured to a support ring.

4. The method of claim 1 , wherein tack welding the thermoplastic tow comprises:
tack welding the thermoplastic tow to the braided structure using a tack welder that is secured to a support ring that surrounds the surface, wherein the tack welder is resistively heated.

5. The method of claim 1 , wherein the conductive component travels with a braiding ring that provides the thermoplastic tow.

6. The method of claim 1 , wherein the braided structure comprises a plurality of thermoplastic plies of overbraided continuous thermoplastic composite fibers.

7. The method of claim 1 , wherein applying the laser energy comprises:
absorbing the laser energy using the conductive component to protect the braided structure as the thermoplastic tow is trimmed.

8. The method of claim 1 , wherein laying up the thermoplastic tow comprises:
laying up the thermoplastic tow over the surface, the surface being formed by at least one of a tooling surface, a caul, a bladder, a stringer bladder, a partially-formed braided layup, a preform, or an integrated composite structure.

9. The method of claim 1 , wherein laying up the thermoplastic tow comprises:
laying up the thermoplastic tow to add a localized feature to the braided structure.

10. The method of claim 1 , wherein the method is used in the assembly of a portion of an aircraft composite barrel section.

11. The method of claim 1 , wherein the laying-up, the tack welding, and the trimming are performed by a tow tacking and trimming apparatus comprising:
a tacking-trimming system for use in the tack welding and the trimming; and
a support system to which the tacking-trimming system is attached, the support system sized and shaped to operatively place the tacking-trimming system relative to a cylindrical thermoplastic stackup.

12. The method of claim 11 , wherein the support system comprises:
a support ring sized and shaped to fully surround a surface that is circumferential, wherein the tacking-trimming system is secured to the support ring.

13. The method of claim 11 , wherein the tacking-trimming system comprises:
a tack welder secured to a portion of the support system, wherein the tack welder is resistively heated.

14. The method of claim 11 , wherein the tacking-trimming system comprises:
a trimmer secured to a portion of the support system, wherein the trimmer uses laser energy to trim the thermoplastic tow.

15. The method of claim 14 further comprising:
the conductive component positioned between the braided structure and the thermoplastic tow.

16. The method of claim 15 , wherein a cross-sectional shape of the conductive component is wedge-shaped.

17. The method of claim 15 , wherein the conductive component is thermally conductive and used to absorb the laser energy emitted by the trimmer to protect the braided structure.

18. The method of claim 15 , wherein the thermoplastic tow is received from a braiding ring and is passed over the conductive component.

19. The method of claim 11 , wherein the support system travels with a braiding ring that provides the thermoplastic tow.

20. The method of claim 11 , wherein the tacking-trimming system is one of a plurality of tacking-trimming systems distributed along the support system.

21. The method of claim 11 , wherein the braided structure comprises a plurality of thermoplastic plies of overbraided continuous thermoplastic composite fibers.

22. A method for tacking and trimming a thermoplastic tow, the method comprising:
laying up the thermoplastic tow received from a braiding system over a braided structure on a surface; and
tack welding the thermoplastic tow received from the braiding system to the braided structure; and
trimming the thermoplastic tow by applying laser energy to a portion of the thermoplastic tow;

wherein trimming the thermoplastic tow comprises:
applying the laser energy to the portion of the thermoplastic tow supported by a conductive component.

23. The method of claim 22 , further comprising:
supporting the portion of the thermoplastic tow by the conductive component;
wherein applying the laser energy comprises absorbing the laser energy using the conductive component to protect the braided structure as the thermoplastic tow is trimmed.

24. The method of claim 22 , wherein the conductive component moves relative to the braided structure during the laying-up.

25. The method of claim 22 , wherein the method is used in the assembly of a portion of an aircraft composite barrel section.

26. The method of claim 22 , wherein the laying-up, the track welding, and the trimming are performed by a tacking-trimming setup comprising:
a support ring sized and shaped to fully surround a surface that is circumferential;
a tacking-trimming system secured to the support ring for use in tacking the thermoplastic tow to the braided structure, wherein the tacking-trimming system comprises:
a tack welder secured to a portion of the support ring, wherein the tack welder is resistively heated; and
a trimmer secured to a portion of the support ring, wherein the trimmer uses laser energy to trim the thermoplastic tow; and

the conductive component positioned between the braided structure and the thermoplastic tow.

27. The method of claim 26 , wherein a cross-sectional shape of the conductive component is wedge-shaped and thermally conductive to absorb the laser energy emitted by the trimmer to protect the braided structure during trimming of the thermoplastic tow.

28. The method of claim 27 , wherein the tacking-trimming system is one of a plurality of tacking-trimming systems distributed along the support ring.

29. The method of claim 26 , wherein the braided structure comprises a plurality of thermoplastic plies of overbraided continuous thermoplastic composite fibers.

30. The method of claim 26 , wherein the surface is formed by at least one of a tooling surface, a caul, a bladder, a stringer bladder, a partially-formed braided layup, a preform, or an integrated composite structure.

Assignees

• Boeing Co

Inventors

• Marcoe Jeffery Lee
• Matsen Marc R

Classifications

• B29K2105/10

  Cords, strands or rovings, e.g.} oriented {cords, strands or rovings · CPC title

• B29K2101/12

  Thermoplastic materials · CPC title

• Y02T50/40

  Weight reduction · CPC title

• B29C66/721

  Fibre-reinforced materials (B29C66/729 takes precedence) · CPC title

• B29C65/168

  placed at the interface · CPC title