Mapping tow splices in composite structures

• US 8,753,458 B2
• Filed: 07/26/2009
• Issued: 06/17/2014
• Est. Priority Date: 07/26/2009
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Engelbart, Roger W., Hannebaum, Reed, Rector, Eric
• Primary Examiner(s): KOCH, GEORGE R
• Application Number:
  US12/509,471
• Publication Number:
  US 20110017380A1
• Time in Patent Office: 1,787 Days
• Field of Search: 156/64, 156/351, 156/361, 156/367, 156/378, 156/379, 356/237.1, 356/237.3, 356/237.4, 356/238.3
• US Class Current: 156/64
• CPC Class Codes: B29C 70/384 Fiber placement heads, e.g. component parts, details or accessories

Abstract

The three dimensional (3-D) locations of splices in pre-preg tows placed by an automatic fiber placement machine to form a laminated composite structure are mapped to allow visualization of alignment patterns in the splices.

Claims

1. A method of mapping a location of splices in a plurality of tows used to layup a laminated composite structure, comprising:

placing tows on a tool by using an automatic fiber placement machine comprising a compaction roller, such that placing tows comprises simultaneously placing the plurality of the tows on the tool as a band;

sensing, using a sensing device, a location of each splice as the plurality of tows are being simultaneously placed as the band during the layup;

generating, using a software program in a computer, a data file from a geometric database of the composite structure;

using the computer with a program code for;

receiving the data file from the geometric database, determining the location of the splices within the composite structure, the location being a three dimensional (3-D) location, receiving an inspection parameter, and generating a pass/fail status for the plurality of tows based upon the inspection parameter; and

,

using the data file to generate a 3-D display showing the 3-D location of the splices in the composite structure.

2. The method of claim 1, wherein sensing the location of each splice includes optically sensing a presence of a feature on the tows representing the location of a splice.

3. The method of claim 2, wherein:

sensing the location of each splice further includes illuminating the tows as the tows are being placed, and optically sensing the presence of the feature is performed using a camera.

4. The method of claim 3, wherein:

the feature includes visual indicia at each of the splices, and optically sensing the presence of the feature includes using the camera to record an image of the indicia.

5. The method of claim 1, wherein generating the data file includes recording the location of each splice in each of a plurality of plies of the structure.

6. A method of laying up a composite structure, comprising:

placing tows on a tool using an automatic placement machine comprising a compaction roller, said placing comprising simultaneously placing a plurality of the tows on the tool as a band;

generating, using a software program in a computer, a data file from a geometric database of the composite structure;

sensing, using a sensing device, splices in each of the tows as the tows of the band are placed on the tool;

recording, using the computer, a location of each splice as the splice is sensed;

using the computer with a program code for;

receiving the data file from the geometric database, determining a location of the splices within the composite structure, receiving an inspection parameter, and generating a pass/fail status for the plurality of tows based upon the inspection parameter; and

generating, for a user interface, an image of the structure showing the locations of the splices in the composite structure based on the recorded locations of the splices.

7. The method of claim 6, further comprising:

illuminating the band as the band is being placed on the tool, and sensing a passage of indicia through a strip across the band.

8. The method of claim 6, wherein recording the location includes recording the two dimensional position of each of the splices in each of a plurality of plies laid up on the tool by the machine.

9. The method of claim 8, further comprising:

using the recorded positions of the splices to generate the data file representing a 3-D image of the locations of each splice in the composite structure.

10. The method of claim 6, wherein sensing splices is performed using sensors mounted on the automatic placement machine.

11. A method of laying up a composite aircraft structure, comprising:

simultaneously placing bands of composite pre-preg tows on a tool using an automatic placement machine, comprising a compaction roller;

using a computer coupled with a sensor for sensing features on each of the tows in the band indicating a presence of a splice on the tow immediately after the tow has been placed on the tool by the placement machine;

using the computer for recording the location of each detected feature within each ply of a lay-up;

using the computer for retrieving geometric information from a geometric database of the composite structure;

using a recorded locations of each splice and the geometric information to generate a data file representing a 3-D location of splices within the composite structure;

and using the data file to generate a 3-D image of the structure showing a location of the splices within the structure.