System and method for minimizing wrinkles in composites

• US 9,731,457 B2
• Filed: 11/02/2012
• Issued: 08/15/2017
• Est. Priority Date: 11/02/2012
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Kline, William T.
• Primary Examiner(s): Sultana, Nahida
• Application Number:
  US13/668,210
• Publication Number:
  US 20140127473A1
• Time in Patent Office: 1,747 Days
• Field of Search: 264285, 264286, 264287, 156196
• CPC Class Codes: B29C 33/42 characterised by the shape of the moulding surface, e.g. ribs or grooves
• CPC Class Codes: B29C 70/543 Fixing the position or configuration of fibrous reinforcements before or during moulding for non-woven fabrics D04H3/08
• CPC Class Codes: B29C 70/56 Tensioning reinforcements before or during shaping
• CPC Class Codes: B29C 70/683 Pretreatment of the preformed part, e.g. insert
• CPC Class Codes: Y10T 156/1002 with permanent bending or reshaping or surface deformation of self sustaining lamina
• CPC Class Codes: Y10T 428/24628 Nonplanar uniform thickness material

Abstract

A wrinkle mitigation system may include 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 have an elongated shape and may be generally oriented along a direction of wrinkle formation in the composite ply. The tooling rod may have a rod width that results in the composite ply assuming a corrugated shape when compaction pressure is applied to the composite ply.

Claims

1. A method of controlling wrinkle formation in a composite laminate, comprising the steps of:

providing a tooling rod assembly including a plurality of tooling rods protruding above a tool surface on a tool side of a tool at a location adjacent to a juncture of the side with a contoured surface of the tool, the plurality of tooling rods having a lengthwise direction oriented locally parallel to the tool surface, the tooling rod assembly being one of;

mounted to the tool surface;

integral with the tool surface;

applying two or more composite plies over the tooling rod assembly and the tool surface such that an entirety of the tooling rod assembly is located immediately adjacent the tool surface on a side of the two or more composite plies facing the tool surface and such that at least one of the composite plies is in direct physical contact with the plurality of tooling rods;

applying a compaction pressure to the two or more composite plies against the plurality of tooling rods and against the tool surface; and

forming the two or more composite plies into a corrugated shape over the plurality of tooling rods with no tooling rods located between the two or more composite plies, the tooling rod assembly controlling wrinkle formation in the two or more composite plies, the tooling rod assembly being stationary relative to the tool surface during formation of the two or more composite plies into the corrugated shape having a plurality of corrugations.

2. The method of claim 1, further including:

removing the tooling rod assembly from the tool surface after forming the two or more composite plies into the corrugated shape; and

curing the two or more composite plies.

3. The method of claim 1, wherein the step of providing the tooling rod assembly includes:

removably attaching the tooling rod assembly to the tool surface using at least one attachment device.

4. The method of claim 1, further comprising the step of:

sizing one or more of the plurality of tooling rods of the tooling rod assembly in a rod width that substantially eliminates uncontrolled wrinkle formation in the two or more composite plies when the compaction pressure is applied to the two or more composite plies.

5. The method of claim 1, further comprising the step of:

applying a protective film over the tooling rod assembly prior to applying the two or more composite plies over the tooling rod assembly.

6. The method of claim 1, wherein the step of providing the tooling rod assembly with the tool surface comprises:

applying the tooling rod assembly adjacent to a complex curvature in the tool surface.

7. The method of claim 1, further comprising the step of:

spacing the-plurality of tooling rods of the tooling rod assembly at a rod spacing of between approximately 0.50 and 3.0 inch.

8. The method of claim 3, wherein:

the attachment device is pressure-sensitive adhesive tape.

9. The method of claim 1, wherein the step of providing the tooling rod assembly with the tool surface comprises at least one of the following:

machining the tooling rod assembly into the tool surface;

molding the tooling rod assembly into the tool surface.

10. The method of claim 1, further comprising:

positioning the tooling rod assembly on the tool surface such that a portion of at least one of the plurality of tooling rods of the tooling rod assembly extends outwardly beyond a ply edge of the two or more composite plies.

11. The method of claim 1, further comprising:

positioning the tooling rod assembly on the tool surface at a location where excess ply material gathers.

12. The method of claim 11, further comprising:

uniformly distributing the excess ply material within the corrugated shape.

13. The method of claim 1, further comprising:

providing at least one of the plurality of tooling rods of the tooling rod assembly in at least one of the following shapes;

a tapered shape, a cylindrical shape having a tapered rod end.

14. The method of claim 13, further comprising:

providing at least one of the plurality of tooling rods of the tooling rod assembly in a rod width in a range of from approximately 0.050 to 0.25 inch.

15. The method of claim 1, further comprising:

providing at least one of the plurality of tooling rods of the tooling rod assembly in a rod width resulting in a peak-to-peak amplitude of less than approximately 0.10 inch in the two or more composite plies.

16. The method of claim 1, further comprising:

providing at least one of the plurality of tooling rods of the tooling rod assembly in a rod length to rod width aspect ratio of at least 10.

17. The method of claim 1, further comprising:

orienting the plurality of tooling rods of the tooling rod assembly parallel to one another.

18. The method of claim 17, further comprising:

positioning at least one of the plurality of tooling rod of the tooling rod assembly such that a rod end is located within approximately 1 inch of a tangent of a corner radius in the tool surface.

19. The method of claim 1, wherein the tooling rod assembly immediately adjacent to the tool surface comprises a tool-mounted tooling rod assembly, the method further including:

applying a composite-mounted tooling rod assembly over the two or more composite plies to sandwich the two or more composite plies between the composite-mounted tooling rod assembly and the tool-mounted tooling rod assembly.

22. The method of claim 1, wherein the step of mounting the tooling rod assembly to the tool surface comprises:

mounting the tooling rod assembly against a planar tool surface.

23. The method of claim 1, wherein the step of mounting the tooling rod assembly to the tool surface comprises:

mounting two tooling rod assemblies in spaced-apart side-by-side relationship to one another on the tool surface.

24. The method of claim 1, wherein:

the corrugated shape comprises a sine wave formation in the two or more composite plies.

25. The method of claim 1, wherein the step of applying two or more composite plies over the tooling rod assembly and the tool surface includes:

laying up the two or more composite plies by hand.

26. The method of claim 1, wherein the step of applying two or more composite plies over the tooling rod assembly and the tool surface includes:

laying up the two or more composite plies using automated tape laying machinery.

27. The method of claim 1, further comprising:

applying a vacuum bag over the tooling rod assembly and the two or more composite plies;

sealing the vacuum bag to the tool; and

drawing a vacuum on the vacuum bag to cause the compaction pressure to be applied to the two or more composite plies.

20. A method of controlling wrinkle formation in a composite laminate, comprising the steps of:

mounting a tooling rod assembly including a plurality of tooling rods to a tool surface in a manner such that the plurality of tooling rods protrude above the tool surface on a tool side of a tool at a location adjacent to a juncture of the tool side with a contoured surface of the tool, the plurality of tooling rods having a lengthwise direction oriented locally parallel to the tool surface;

laying up a plurality of composite plies over the tooling rod assembly and the tool surface such that an entirety of the tooling rod assembly is located immediately adjacent the tool surface on a side of the plurality of composite plies facing the tool surface and such that at least one of the composite plies is in direct physical contact with the plurality of tooling rods;

applying a compaction pressure to the plurality of composite plies against the plurality of tooling rods and against the tool surface; and

forming the plurality of composite plies into a corrugated shape over the plurality of tooling rods with none of the plurality of tooling rods being located between the plurality of composite plies, the tooling rod assembly controlling wrinkle formation in the plurality of composite plies, the tooling rod assembly being stationary relative to the tool surface during formation of the plurality of composite plies into the corrugated shape having a plurality of corrugations.

21. The method of claim 20, wherein the step of mounting the tooling rod assembly to the tool surface comprises:

removably attaching the tooling rod assembly to the tool surface using pressure-sensitive adhesive tape.