System for minimizing wrinkles in composites

Patent metadata

Field	Value
Publication number	US-10131100-B2
Application number	US-201715644807-A
Country	US
Kind code	B2
Filing date	Jul 9, 2017
Priority date	Nov 2, 2012
Publication date	Nov 20, 2018
Grant date	Nov 20, 2018

Abstract

A wrinkle mitigation system includes at least one tooling rod disposed against a tool surface at a location on the tool where a composite ply is configured to overlap the tooling rod. The tooling rod may has an elongated shape and is generally oriented along a direction of wrinkle formation in the composite ply. The tooling rod has a rod width that results in the composite ply assuming a corrugated shape when compaction pressure is applied to the composite ply.

First claim

What is claimed is:

1. A system for controlling wrinkle formation in a composite ply, comprising:
a first tooling rod assembly including a plurality of tooling rods;
a second tooling rod assembly including a plurality of tooling rods;
the first tooling rod assembly being disposed against a tool surface at a location on a tool where a composite ply is configured to overlap the first tooling rod assembly such that an entirety of the first tooling rod assembly is located immediately adjacent the tool surface on a side of the composite ply facing the tool surface;
the second tooling rod assembly being positioned over the first tooling rod assembly with the composite ply sandwiched between the first tooling rod assembly and the second tooling rod assembly;
the plurality of tooling rods of the first tooling rod assembly and the plurality of tooling rods of the second tooling rod assembly having an elongated shape and being generally oriented along a direction of wrinkle formation in the composite ply; and
the plurality of tooling rods of the first tooling rod assembly and the plurality of tooling rods of the second tooling rod assembly having a rod width that results in the composite ply assuming a corrugated shape when compaction pressure is applied to the second tooling rod assembly, the composite ply, and the first tooling rod assembly against the tool surface, the first tooling rod assembly and the second tooling rod assembly being stationary relative to the tool surface during formation of the composite ply into the corrugated shape.

2. The system of claim 1 , wherein:
at least some of the plurality of tooling rods of at least one of the first tooling rod assembly and the second tooling rod assembly have end portions that extend outwardly beyond a ply edge of the composite ply.

3. The system of claim 1 , wherein:
the plurality of tooling rods of at least one of the first tooling rod assembly and the second tooling rod assembly are formed of at least one of metallic material, composite material, polymeric material, ceramic material, and wood.

4. The system of claim 1 , further comprising:
a protective film at least partially covering at least one of the first tooling rod assembly and the second tooling rod assembly such that the protective film is positioned between the composite ply and the first tooling rod assembly or the second tooling rod assembly.

5. The system of claim 1 , further comprising:
an attachment device mounting the first tooling rod assembly to the tool surface.

6. The system of claim 5 , wherein:
the attachment device is pressure-sensitive adhesive tape.

7. The system of claim 1 , wherein:
the first tooling rod assembly is positioned on the tool surface at a location where excess ply material gathers.

8. The system of claim 1 , wherein:
the first tooling rod assembly is positioned adjacent to a complex curvature in the tool surface.

9. The system of claim 8 , wherein:
the plurality of tooling rods of the first tooling rod assembly have a rod end, the rod end of the plurality of tooling rods being located within approximately 1 inch of a tangent of a corner radius the tool surface.

10. The system of claim 1 , wherein:
the plurality of tooling rods of the first tooling rod assembly are integrally-formed with the tool.

11. The system of claim 1 , wherein:
the plurality of tooling rods of at least one of the first tooling rod assembly and the second tooling rod assembly are configured in at least one of a cylindrical shape and a tapered shape.

12. The system of claim 1 , wherein:
the plurality of tooling rods of at least one of the first tooling rod assembly and the second tooling rod assembly have a tapered rod end.

13. The system of claim 1 , wherein:
the plurality of tooling rods of at least one of the first tooling rod assembly and the second tooling rod assembly have a rod width in a range of from approximately 0.050 to 0.25 inch.

14. The system of claim 1 , wherein:
the plurality of tooling rods of at least one of the first tooling rod assembly and the second tooling rod assembly have a rod length to rod width aspect ratio of at least 10.

15. The system of claim 1 , wherein:
the plurality of tooling rods of the first tooling rod assembly and the plurality of tooling rods of the second tooling rod assembly are oriented generally parallel to one another.

16. The system of claim 15 , wherein:
the plurality of tooling rods of the first tooling rod assembly and the plurality of tooling rods of the second tooling rod assembly are spaced apart at a rod spacing of between approximately 0.50 and 3.0 inch.

17. The system of claim 15 , wherein:
the plurality of the tooling rods of the first tooling rod assembly and the plurality of tooling rods of the second tooling rod assembly are positioned over each other such that the corrugated shape comprises a sine wave formation in the composite ply.

18. The system of claim 15 , further comprising:
a protective film encapsulating at least one of the first tooling rod assembly and the second tooling rod assembly.

19. A system for controlling wrinkle formation in a composite laminate, comprising:
a first tooling rod assembly including a plurality of tooling rods disposed against a tool surface at a location on a tool where the composite laminate is configured to overlap the first tooling rod assembly;
a second tooling rod assembly including a plurality of tooling rods and positioned over the first tooling rod assembly with the composite laminate sandwiched between the first tooling rod assembly and the second tooling rod assembly;
the plurality of tooling rods of the first tooling rod assembly and the plurality of tooling rods of the second tooling rod assembly oriented generally parallel to one another and each having an elongated shape and oriented along a general direction of wrinkle formation in the composite laminate; and
the plurality of tooling rods of the first tooling rod assembly and the plurality of tooling rods of the second tooling rod assembly have a rod width that results in the composite laminate assuming a corrugated shape when compaction pressure is applied to the composite laminate against the plurality of tooling rods;
the plurality of tooling rods of the first tooling rod assembly and the plurality of tooling rods of the second tooling rod assembly are spaced apart from one another at a rod spacing resulting in the composite laminate being in contact with the tool surface between at least one of adjacent pairs of the plurality of tooling rods of the first tooling rod assembly; and
the first tooling rod assembly and the second tooling rod assembly being stationary relative to the tool surface during formation of the composite laminate into the corrugated shape.

20. The system of claim 19 , further comprising:
at least some of the plurality of tooling rods of at least one of the first tooling rod assembly and the second tooling rod assembly have end portions that extend outwardly beyond a ply edge of the composite laminate.

Assignees

• Boeing Co

Inventors

• Kline William T

Classifications

• Y10T428/24628

  Nonplanar uniform thickness material · CPC title

• Y10T156/1002

  with permanent bending or reshaping or surface deformation of self sustaining lamina · CPC title

• B29C70/683 Primary

  Pretreatment of the preformed part, e.g. insert · CPC title

• B29C70/56

  Tensioning reinforcements before or during shaping · CPC title

• B29C70/543 Primary

  Fixing the position or configuration of fibrous reinforcements before or during moulding (for non-woven fabrics D04H3/08) · CPC title