Method for producing contoured composite structures and structures produced thereby

• US 8,932,423 B2
• Filed: 03/02/2009
• Issued: 01/13/2015
• Est. Priority Date: 04/17/2008
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: McCarville, Douglas A., Sweetin, Joseph L., Guzman, Juan C.
• Primary Examiner(s): SCHATZ, CHRISTOPHER T
• Application Number:
  US12/396,418
• Publication Number:
  US 20090263618A1
• Time in Patent Office: 2,143 Days
• Field of Search: 156/121, 156/196, 156/214, 156/285, 156/212, 156/211, 156/267
• US Class Current: 156/211
• CPC Class Codes: B29C 70/304 In-plane lamination by juxtaposing or interleaving of plies, e.g. scarf joining
• CPC Class Codes: B29C 70/38 Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns application heads for tyres B29D30/28
• CPC Class Codes: B29D 99/0007 having a variable cross-section
• CPC Class Codes: B29L 2031/3082 Fuselages
• CPC Class Codes: Y10T 156/1002 with permanent bending or reshaping or surface deformation of self sustaining lamina
• CPC Class Codes: Y10T 156/1026 with slitting or removal of material at reshaping area prior to reshaping
• CPC Class Codes: Y10T 156/1028 by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith
• CPC Class Codes: Y10T 156/1031 with preshaping of lamina
• CPC Class Codes: Y10T 156/1052 with cutting, punching, tearing or severing
• CPC Class Codes: Y10T 156/108 Flash, trim or excess removal
• CPC Class Codes: Y10T 428/24124 Fibers

Abstract

A contoured composite structure is fabricated by laying up a composite charge that includes at least one ply formed by uni-directional fiber pre-preg ply segments having substantially constant widths. The ply segments are placed in side-by-side, overlapping relationship with their longitudinal centerlines aligned in a polar orientation related to the contour of the structure. The charge is formed into the shape of the structure and cured.

Claims

1. A method of fabricating a contoured composite structure, comprising:

laying up a composite charge, including laying up at least one ply of uni-directional fiber pre-preg ply segments, including placing the ply segments in side-by-side, overlapping relationship and aligning longitudinal centerlines of the ply segments in a polar orientation related to the contour of the structure, adjacent ply segments overlapping and forming pie shaped laps in an area adjacent an inner chord comprising said contour and forming pie shaped gaps in an area adjacent an outer chord comprising said contour, the ply segments positioned in overlapping relationship in a substantially flat configuration;

cutting a first end and a second end of the ply segments so as to form an angle in each ply segment that substantially matches the inner chord and the outer chord related to the contour of the structure;

forming the composite charge substantially into the shape of the structure so as to alter at least a portion of the composite charge from the flat configuration; and

curing the composite charge.

2. The method of claim 1, wherein placing the ply segments in side-by-side relationship includes maintaining a substantially constant amount of said overlap between the ply segments as the ply segments are being placed.

3. The method of claim 1, wherein laying up the ply includes cutting the ply segments from a length of composite tape.

4. The method of claim 1, wherein said gaps are created between adjacent ones of the ply segments due to the polar orientation of the ply segments, and laying up the ply further includes substantially minimizing the gaps.

5. The method of claim 1, wherein placing the ply segments and aligning the centerlines is performed by an automatically controlled tape application head.

6. The method of claim 1, wherein laying up the ply includes producing the ply segments by cutting segments from a length of composite fiber tape.

17. The method of claim 1, wherein the ply segments are positioned in the overlapping relationship in a substantially flat configuration such that the amount of overlapping is substantially constant among the ply segments.

7. A method of fabricating a contoured composite structure, comprising:

producing a composite charge using an automatically controlled tape placement head, including using the head to place each of a plurality of substantially constant width prepreg tape segments in side-by-side, overlapping relationship on a substrate and to align longitudinal centerlines of the tape segments in a polar orientation related to the contour of the structure, adjacent tape segments overlapping in an area adjacent an inner chord comprising said contour so as to form pie shaped laps and forming pie shaped gaps in an area adjacent an outer chord comprising said contour, the ply segments positioned in a substantially flat configuration;

cutting a first end of the plurality of segments proximate the inner chord and a second end of the plurality of segments proximate the outer chord so as to form an angle in each segment that substantially matches the inner chord and the outer chord related to the contour of the structure;

forming the composite charge substantially into the shape of the structure so as to alter at least a portion of the composite charge from the flat configuration; and

curing the composite charge.

8. The method of claim 7, wherein using the head to place the tape segments include moving the head across a substrate and cutting a length of composite tape into segments.

9. The method of claim 7, wherein using the head to align the tape segments includes aligning the longitudinal centerlines of the tape segments along radial coordinates in a polar coordinate system.

10. The method of claim 7, wherein using the head to place the tape segments includes using the head to maintain a substantially constant amount of said overlap between the tape segments as the tape segments are being placed.

11. The method of claim 7, wherein said gaps are created between adjacent ones of the tape segments due to the polar orientation of the tape segments, and using the head to place the tape segments includes substantially minimizing the gaps.

18. The method of claim 7, wherein the ply segments are positioned in the overlapping relationship such that the amount of overlapping is substantially constant among the ply segments.

12. A method of fabricating a contoured composite structure, comprising:

forming a substantially flat stack of fiber reinforced, pre-preg plies, including individually placing composite fiber tape segments in side-by-side, overlapping relationship and in a polar orientation related to the contour of the structure, the amount of overlapping being substantially constant among the ply segments;

cutting a first end of the plurality of segments proximate an inner chord of the contour and a second end of the plurality of segments proximate an outer chord of the contour so as to form an angle in each segment that substantially matches the inner chord and the outer chord related to the contour of the structure;

forming the flat stack of fiber reinforced, pre-preg plies substantially into the shape of the structure so as to alter at least a portion of the plies from the flat stack configuration; and

curing the fiber reinforced, pre-preg plies.

13. The method of claim 12, wherein placing the tape segments in side-by-side relationship includes maintaining a substantially constant amount of said overlap between the tape segments as the tape segments are being placed.

14. The method of claim 12, further comprising cutting the tape segments from a length of composite tape.

15. The method of claim 12, wherein gaps are created between adjacent tape segments due to the polar orientation of the tape segments.

16. The method of claim 12, wherein placing the tape segments is performed by an automatically controlled tape application head.