Wrinkle diffuser system for composites

• US 9,649,809 B2
• Filed: 03/22/2014
• Issued: 05/16/2017
• Est. Priority Date: 11/02/2012
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Kline, William T., Lee, Tristan E., Hopkins, Andrew M.
• Primary Examiner(s): Sultana, Nahida
• Application Number:
  US14/222,617
• Publication Number:
  US 20150044430A1
• Time in Patent Office: 1,151 Days
• Field of Search: 264257, 264285, 264286, 156196, 38 44, 38 70, 38 99, 38100, 38102
• CPC Class Codes: B29C 33/42 characterised by the shape of the moulding surface, e.g. ribs or grooves
• CPC Class Codes: B29C 53/18 of plates or sheets
• 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: B32B 38/18 Handling of layers or the laminate
• CPC Class Codes: B32B 43/00 Operations specially adapted for layered products and not otherwise provided for, e.g. repairing; Apparatus therefor
• CPC Class Codes: Y10T 156/1002 with permanent bending or reshaping or surface deformation of self sustaining lamina
• CPC Class Codes: Y10T 156/1043 Subsequent to assembly
• CPC Class Codes: Y10T 428/24628 Nonplanar uniform thickness material
• CPC Class Codes: Y10T 428/24694 Parallel corrugations

Abstract

A system for diffusing wrinkles in a composite laminate may include at least one wrinkle diffuser. The wrinkle diffuser may include a diffuser body may be mounted to a tool in a manner such that a composite ply at least partially overlaps the wrinkle diffuser. A plurality of diffuser elements may be formed in the diffuser body to define a corrugated surface. The corrugated surface may cause a portion of the composite ply to assume a corrugated shape when a compaction pressure is applied to force the composite ply against the corrugated surface. The wrinkle diffuser may include an indexing feature to index the wrinkle diffuser to a ply edge of the composite ply.

Claims

1. A system for diffusing wrinkles in a composite laminate, comprising:

at least one wrinkle diffuser including a diffuser body and configured to be mounted to a tool in a manner such that a composite ply at least partially overlaps the at least one wrinkle diffuser, the diffuser body including;

a plurality of diffuser elements formed in the diffuser body and defining a corrugated surface, the corrugated surface causing a portion of the composite ply to assume a corrugated shape when a compaction pressure is applied to force the composite ply against the corrugated surface, the plurality of diffuser elements being arranged in a manner that the corrugated surface has a cross-sectional shape having a series of parallel ridges; and

a base flange formed along a lengthwise perimeter edge of the diffuser body, the base flange having a base edge oriented non-parallel to corrugations in the corrugated surface of the diffuser body and configured to be placed in direct contact with a ply edge of the composite ply for indexing the at least one wrinkle diffuser to the ply edge.

2. The system of claim 1, wherein:

the series of parallel ridges forms a sine wave cross-sectional shape of the corrugated surface.

3. The system of claim 1, wherein the plurality of diffuser elements have at least one of a following:

a triangular cross-sectional shape; and

a rounded cross-sectional shape.

4. The system of claim 1, wherein:

the at least one wrinkle diffuser includes an inner wrinkle diffuser and an outer wrinkle diffuser configured to be removably coupled to one another with the composite ply sandwiched therebetween; and

the outer wrinkle diffuser having a corrugated surface configured complementary to the corrugated surface of the inner wrinkle diffuser such that peaks of the corrugated surface of the outer wrinkle diffuser are aligned with troughs of the corrugated surface of the inner wrinkle diffuser.

5. The system of claim 4, wherein:

at least one of the inner wrinkle diffuser and the outer wrinkle diffuser includes a coupling feature configured to removably couple the outer wrinkle diffuser to the inner wrinkle diffuser.

7. The system of claim 1, wherein:

the plurality of diffuser elements are sized and configured such that when the composite ply is sandwiched between a mated pair of wrinkle diffusers of the at least one wrinkle diffuser, a gap between the corrugated surfaces is substantially equivalent to a thickness of the composite ply.

6. A system for diffusing wrinkles in a composite laminate, comprising:

an inner wrinkle diffuser and an outer wrinkle diffuser configured to be removably coupled to one another with at least one composite ply sandwiched therebetween;

each one of the inner wrinkle diffuser and the outer wrinkle diffuser including a diffuser body having a plurality of diffuser elements defining a corrugated surface;

the inner wrinkle diffuser configured to be mounted to a tool in a manner such that the at least one composite ply at least partially overlaps the inner wrinkle diffuser;

the corrugated surface of the outer wrinkle diffuser configured complementary to the corrugated surface of the inner wrinkle diffuser such that peaks of the corrugated surface of the outer wrinkle diffuser are aligned with troughs of the corrugated surface of the inner wrinkle diffuser;

the corrugated surface of the inner wrinkle diffuser and the outer wrinkle diffuser causing a portion of the at least one composite ply to assume a corrugated shape when a compaction pressure is applied to the outer wrinkle diffuser;

at least one of the inner wrinkle diffuser and the outer wrinkle diffuser having an indexing feature configured to index the at least one of the inner wrinkle diffuser and the outer wrinkle diffuser to a ply edge of the composite ply; and

at least one magnet mounted to the diffuser body of at least one of the inner wrinkle diffuser and the outer wrinkle diffuser and configured to be magnetically coupled to a remaining one of the at least one of the inner wrinkle diffuser and the outer wrinkle diffuser.

21. The system of claim 6, wherein:

the corrugated surface of the inner wrinkle diffuser and the outer wrinkle diffuser has a sine wave cross-sectional shape.

8. A wrinkle mitigation system for diffusing wrinkles in a composite ply, comprising:

an inner wrinkle diffuser configured to be mounted on a tool surface and including a corrugated surface defined by a plurality of diffuser elements;

an outer wrinkle diffuser having a corrugated surface formed complementary to the corrugated surface of the inner wrinkle diffuser;

the corrugated surface of the inner and outer wrinkle diffuser defining a gap sized to receive a composite laminate for forming a corrugated shape into the composite laminate when a compaction pressure is applied thereto;

a coupling feature configured to removably couple the outer wrinkle diffuser to the inner wrinkle diffuser in alignment with one another such that peaks of the corrugated surface of the outer wrinkle diffuser are substantially aligned with troughs of the corrugated surface of the inner wrinkle diffuser; and

the inner and outer wrinkle diffuser each having a diffuser body having a base flange formed along a lengthwise perimeter edge of the diffuser body, the base flange of the inner and outer wrinkle diffuser each having a base edge configured to be butted up against an edge of the composite laminate for respectively indexing the inner and outer wrinkle diffuser to the edge of the composite laminate.

22. The wrinkle mitigation system of claim 8, wherein:

the corrugated surface of the inner wrinkle diffuser and the outer wrinkle diffuser has a sine wave cross-sectional shape.

9. A method of controlling wrinkle formation in a composite ply, comprising the steps of:

mounting a wrinkle diffuser relative to a tool surface in a manner such that a composite ply at least partially overlaps the wrinkle diffuser, the wrinkle diffuser having a diffuser body including a plurality of diffuser elements forming a corrugated surface, the plurality of diffuser elements being arranged in a manner that the corrugated surface has a cross-sectional shape having a series of parallel ridges, the diffuser body including a base flange formed along a lengthwise perimeter edge of the diffuser body, the base flange having a base edge oriented non-parallel to corrugations in the corrugated surface;

placing the base edge directly against a ply edge of the composite ply to index the wrinkle diffuser to the ply edge;

applying a compaction pressure to the composite ply in a manner forcing the composite ply against the corrugated surface; and

forming a corrugated shape in a portion of the composite ply in response to forcing the composite ply against the corrugated surface.

10. The method of claim 9, wherein the step of mounting the wrinkle diffuser and applying compaction pressure includes:

coupling an outer wrinkle diffuser to an inner wrinkle diffuser such that the composite ply is sandwiched therebetween; and

applying the compaction pressure to the outer wrinkle diffuser and the composite ply to form the corrugated shape into the composite ply using the inner and outer wrinkle diffuser.

11. The method of claim 10, wherein the step of coupling the outer wrinkle diffuser to the inner wrinkle diffuser includes:

aligning peaks of the corrugated surface of the outer wrinkle diffuser with troughs of the corrugated surface of the inner wrinkle diffuser.

12. The method of claim 10, wherein the step of coupling the outer wrinkle diffuser to the inner wrinkle diffuser includes:

removably coupling the outer wrinkle diffuser to the inner wrinkle diffuser using a coupling feature included with at least one of the inner and outer wrinkle diffuser.

13. The method of claim 12, wherein the step of removably coupling the outer wrinkle diffuser to the inner wrinkle diffuser includes:

magnetically coupling the outer wrinkle diffuser to the inner wrinkle diffuser.

14. The method of claim 10, wherein the step of positioning the inner wrinkle diffuser includes:

positioning the inner wrinkle diffuser at a location of a corner radius on the tool.

15. The method of claim 10, wherein the step of positioning the inner wrinkle diffuser includes:

positioning the inner wrinkle diffuser on the tool such that a perimeter edge of the diffuser body is no further than approximately one inch from a tangent of the tool surface.

16. The method of claim 9, further comprising:

removing the wrinkle diffuser from the tool and the composite ply; and

applying compaction pressure to the composite ply to flatten the corrugated shape in the composite ply; and

curing the composite ply.

17. The method of claim 9, further comprising:

applying a caul plate over the composite ply to at least cover a portion of the corrugated shape; and

reducing a trough-to-peak height of the corrugated shape using the caul plate.

18. The method of claim 9, wherein the step of mounting the wrinkle diffuser relative to the tool surface comprises:

positioning the wrinkle diffuser at a location of a convex curvature on the tool.

19. The method of claim 9, wherein the step of mounting the wrinkle diffuser relative to the tool surface comprises:

mounting the wrinkle diffuser to the tool surface using pressure-sensitive adhesive tape.

20. The method of claim 9, wherein:

the diffuser elements are each tapered at a location adjacent to a perimeter edge of the diffuser body.