Methods of forming a mandrel for forming composite structures, methods of forming composite structures, and related tools

Patent metadata

Field	Value
Publication number	US-12285903-B2
Application number	US-202418591747-A
Country	US
Kind code	B2
Filing date	Feb 29, 2024
Priority date	Apr 1, 2021
Publication date	Apr 29, 2025
Grant date	Apr 29, 2025

Abstract

A tool for forming a composite structure may include two or more segments formed from a polymer material. The tool may further include a crush insert disposed between the two or more segments. The tool may also include a support shaft coupled between the two or more segments. A method of forming a mandrel may include forming segments of the mandrel through an additive manufacturing process. The method may further include assembling the segments relative to one another. The method may also include positioning a crush insert between each of the segments. A method of fabricating a composite structure is also disclosed.

First claim

What is claimed is:

1. A method of forming a mandrel for forming a composite structure comprising:
forming segments of the mandrel through an additive manufacturing process, the segments including at least two wedge segments and at least one connecting segment having substantially parallel sides;
assembling the segments relative to one another by positioning the at least one connecting segment between the at least two wedge segments where the substantially parallel sides of the at least one connecting segment abut against the at least two wedge segments; and
positioning a crush insert between adjacent segments.

2. The method of claim 1 , further comprising forming the segments from a polymer material.

3. The method of claim 1 , wherein forming the segments of the mandrel through the additive manufacturing process comprises forming the segments of the mandrel through at least one of a fused filament fabrication process or a large-scale additive manufacturing process.

4. The method of claim 1 , wherein assembling the segments comprises securing the segments of the mandrel to a support shaft.

5. The method of claim 4 , wherein securing the segments of the mandrel to the support shaft further comprises securing the segments of the mandrel to the support shaft via complementary alignment features.

6. The method of claim 1 , further comprising forming the crush insert through an additive manufacturing process.

7. The method of claim 1 , further comprising forming the crush insert of a material at least one of configured or formulated to deform under a load exerted by thermal expansion of the segments of the mandrel during a composite curing process.

8. The method of claim 1 , further comprising configuring the segments of the mandrel to comprise at least two wedge segments and at least one connecting segment.

9. The method of claim 8 , wherein assembling the segments relative to one another comprises securing the at least two wedge segments to a support shaft and positioning the at least one connecting segment between the at least two wedge segments.

10. The method of claim 9 , wherein the at least two wedge segments are configured to substantially prevent the at least one connecting segment from moving radially away from an axis of the mandrel and the support shaft is configured to substantially prevent the at least one connecting segment from moving radially toward the axis of the mandrel.

11. A method of fabricating a composite structure, the method comprising:
assembling a mandrel comprising:
forming segments of the mandrel; and
assembling the segments relative to one another;

removably coupling the segments to a support shaft through complementary alignment structures;
coupling the support shaft to a winding machine;
winding composite fibers around the mandrel to form the composite structure;
heating the composite structure; and
separating the mandrel from the composite structure.

12. The method of claim 11 , wherein separating the mandrel from the composite structure comprises:
de-coupling the segments from the support shaft; and
after de-coupling the segments from the support shaft, removing the segments from the composite structure.

13. The method of claim 11 , wherein removably coupling the segments to a support shaft through the complementary alignment structures comprises securing the segments rotationally and radially to the support shaft through the complementary alignment structures.

14. The method of claim 11 , wherein removably coupling the segments to a support shaft through the complementary alignment structures comprises removably coupling the segments to the support shaft through one or more of a key way, a channel, a ridge, or a combination thereof.

15. A method of fabricating a composite structure, the method comprising:
assembling a mandrel comprising:
forming segments of the mandrel through an additive manufacturing process, the segments including at least two wedge segments and at least one connecting segment;
assembling the segments relative to one another by positioning the at least one connecting segment between the at least two wedge segments;
positioning a crush insert between each of the segments; and
coupling the segments to a support shaft;

coupling the support shaft to a winding machine;
winding composite fibers around the mandrel to form the composite structure;
heating the composite structure; and
separating the mandrel from the composite structure by removing the at least one connecting segment from between the at least two wedge segments before removing the at least two wedge segments.

16. The method of claim 15 , wherein separating the mandrel from the composite structure comprises disassembling the segments of the mandrel.

17. The method of claim 16 , further comprising using a crush insert configured to deform to absorb thermal expansion of the segments of the mandrel when heating the composite structure.

18. The method of claim 15 , wherein separating the mandrel from the composite structure comprises:
de-coupling the segments from the support shaft;
after de-coupling the segments from the support shaft, removing the at least one connecting segment from between the at least two wedge segments; and
after removing the at least one connecting segment, removing the at least two wedge segments.

19. The method of claim 15 , wherein removing the at least one connecting segment from between the at least two wedge segments comprises moving the at least one connecting segment radially inward relative to the at least two wedge segments.

Assignees

• Northrop Grumman Systems Corp

Inventors

• Garcia Benjamin W
• Ketcham Jacob M
• Noorda Jared S
• Madsen Carl B
• Machac David R

Classifications

• B29L2031/757

  Moulds, cores, dies · CPC title

• B29K2879/085

  Thermoplastic polyimides, e.g. polyesterimides, PEI, i.e. polyetherimides, or polyamideimides; Derivatives thereof · CPC title

• B29K2705/02

  Aluminium · CPC title

• B29C70/86

  Incorporated in coherent impregnated reinforcing layers, {e.g. by winding} · CPC title

• B29C53/602

  for tubular articles having closed or nearly closed ends, e.g. vessels, tanks, containers · CPC title