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

Patent metadata

Field	Value
Publication number	US-11919223-B2
Application number	US-202217710255-A
Country	US
Kind code	B2
Filing date	Mar 31, 2022
Priority date	Apr 1, 2021
Publication date	Mar 5, 2024
Grant date	Mar 5, 2024

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 two or more segments of the mandrel from a polymer material through an additive manufacturing process;
assembling the two or more segments of the mandrel relative to one another;
removably securing the two or more segments of the mandrel to a support shaft through complementary alignment structures; and
positioning a crush insert between adjacent segments.

2. The method of claim 1 , wherein the additive manufacturing process comprises at least one of a fused filament fabrication process or a large scale additive manufacturing process.

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

4. 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 two or more segments of the mandrel during a composite curing process.

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

6. The method of claim 5 , wherein assembling the two or more 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.

7. The method of claim 6 , 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.

8. A tool for forming a composite structure, the tool comprising:
two or more segments formed from a polymer material;
a crush insert disposed between the two or more segments; and
a support shaft removably coupled between the two or more segments through complementary alignment structures.

9. The tool of claim 8 , wherein the crush insert is configured to deform under a load exerted by thermal expansion of a composite structure during a curing process.

10. The tool of claim 8 , wherein the crush insert comprises aluminum honeycomb.

11. The tool of claim 8 , wherein the two or more segments comprises a wedge segment, a straight segment, or a combination thereof.

12. The tool of claim 8 , wherein the two or more segments are formed from a polyetherimide material.

13. A method of fabricating a composite structure, the method comprising:
assembling a mandrel comprising:
forming two or more segments of the mandrel from a polymer material through an additive manufacturing process;
assembling the segments relative to one another;
positioning a crush insert between each of the segments; and
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.

14. The method of claim 13 , wherein separating the mandrel from the composite structure comprises disassembling the two or more segments of the mandrel.

15. The method of claim 14 , further comprising using a crush insert configured to deform to absorb thermal expansion of the two or more segments of the mandrel when heating the composite structure.

16. The method of claim 13 , wherein the two or more segments of the mandrel comprise at least two wedge segments and at least one connecting segment and assembling the two or more segments relative to one another comprises positioning the at least one connecting segment between the at least two wedge segments.

17. The method of claim 16 , wherein separating the mandrel from the composite structure comprises removing the at least one connecting segment from between the at least two wedge segments before removing the at least two wedge segments.

18. The tool of claim 8 , wherein the two or more segments are configured to be individually removed by moving radially inward after the support shaft is removed.

Assignees

• Northrop Grumman Systems Corp

Inventors

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

Classifications

• B29C53/824 Primary

  collapsible, e.g. elastic or inflatable; with removable parts, e.g. for regular shaped, straight tubular articles (B29C53/825 takes precedence) · CPC title

• B29C53/602

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

• B29C64/118

  using filamentary material being melted, e.g. fused deposition modelling [FDM] · CPC title

• B29C70/86

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

• B33Y10/00

  Processes of additive manufacturing · CPC title