Systems and methods for forming radius fillers for composite structures

Patent metadata

Field	Value
Publication number	US-9643395-B2
Application number	US-201414464467-A
Country	US
Kind code	B2
Filing date	Aug 20, 2014
Priority date	Aug 20, 2014
Publication date	May 9, 2017
Grant date	May 9, 2017

Abstract

Systems and methods for forming radius fillers for composite structures are disclosed herein. The systems include a sheet-locating structure that has a first support surface and a support surface edge. The systems further include a second support surface, a separation device, a conveyance structure, and a layup surface. The methods include locating a sheet of composite material on a first support surface and translating the sheet of composite material such that a first portion of the sheet is supported by the first support surface and a second portion of the sheet extends past the support surface edge. The methods also include supporting the second portion of the sheet with a second support surface and separating the second portion of the sheet from the first portion of the sheet to form a strip of composite material. The methods further include conveying the strip of composite material onto a layup surface.

First claim

The invention claimed is:

1. A system for forming a radius filler for a composite structure, the system comprising:
a sheet-locating structure having a first support surface configured to support a first portion of a sheet of composite material, wherein the first support surface has a support surface edge, and further wherein the sheet-locating structure is configured to selectively extend a second portion of the sheet of composite material past the support surface edge;
a second support surface that is adjacent the support surface edge of the first support surface, wherein the first support surface and the second support surface define a gap therebetween, and further wherein the second support surface is configured to support the second portion of the sheet of composite material;
a separation device configured to separate the second portion of the sheet of composite material from the first portion of the sheet of composite material to form a strip of composite material;
a conveyance structure configured to operatively translate the second support surface and the separation device along the support surface edge of the first support surface to form the strip of composite material; and
a layup surface configured to receive the strip of composite material from the second support surface subsequent to the strip of composite material being separated from the sheet of composite material.

2. The system of claim 1 , wherein the sheet-locating structure comprises:
a support table having a table surface and a table edge;
a charge-advance belt, wherein the charge-advance belt extends across the table surface and the table edge and defines the first support surface and the support surface edge; and
a charge-advance drive configured to selectively translate the charge-advance belt relative to the support table to selectively extend the second portion of the sheet of composite material past the support surface edge.

3. The system of claim 1 , wherein the system further includes a transition surface that extends from the second support surface to the layup surface, wherein the transition surface extends at a skew angle relative to the second support surface.

4. The system of claim 1 , wherein the separation device is configured to extend entirely through the sheet of composite material when separating the strip of composite material from the sheet of composite material.

5. The system of claim 1 , wherein the separation device extends both above and below the second support surface.

6. The system of claim 1 , wherein the second support surface and the separation device are operatively coupled to one another and configured to translate together via the conveyance structure.

7. The system of claim 1 , wherein the system further includes a controller programmed to automatically control the operation of at least a portion of the system.

8. The system of claim 7 , wherein the controller is programmed to control the operation of the sheet-locating structure to regulate a width of the second portion of the sheet of composite material that extends past the support surface edge to a preselected width.

9. The system of claim 7 , wherein the controller is programmed to control the conveyance structure to selectively translate the second support surface and the separation device along the support surface edge.

10. The system of claim 7 , wherein the system further includes a strip-detection structure configured to detect a location of the strip of composite material on the layup surface concurrently with separation of the strip of composite material from the sheet of composite material.

11. The system of claim 10 , wherein the controller is configured to receive a location indication signal from the strip-detection structure, and further wherein the system further includes a strip location-adjusting structure that is configured to adjust the location of the strip of composite material on the layup surface based, at least in part, on the location indication signal.

12. The system of claim 7 , wherein the system further includes a strip width-adjusting structure configured to adjust a width of the strip of composite material concurrently with separation of the strip of composite material from the sheet of composite material.

13. The system of claim 12 , wherein the strip width-adjusting structure is configured to translate the separation device and the second support surface relative to the first support surface to adjust the width of the strip of composite material, and further wherein the controller is configured to control the operation of the strip width-adjusting structure.

14. The system of claim 1 , wherein the system further includes a compaction roller configured to compact the strip of composite material on the layup surface concurrently with separation of the strip of composite material from the sheet of composite material.

15. The system of claim 1 , wherein the system is configured to sequentially locate a plurality of strips of composite material on the layup surface to form a stack of strips of composite material that defines the radius filler.

16. A method of utilizing the system of claim 1 for forming the radius filler for the composite structure, the method comprising:
locating the sheet of composite material on the first support surface that terminates at the support surface edge;
translating the sheet of composite material such that the first portion of the sheet of composite material is supported by the first support surface and the second portion of the sheet of composite material extends past the support surface edge;
supporting the second portion of the sheet of composite material with the second support surface that is adjacent to the first support surface;
separating the second portion of the sheet of composite material from the first portion of the sheet of composite material with the separation device to form the strip of composite material;
conveying the strip of composite material onto the layup surface, wherein the conveying is concurrent with the separating; and
repeating the translating, the supporting, the separating, and the conveying to sequentially locate a plurality of strips of composite material on the layup surface to form a stack of strips of composite material that defines the radius filler.

17. The method of claim 16 , wherein the separating includes conveying the second support surface and the separation device along the support surface edge and extending the separation device completely through the sheet of composite material.

18. The method of claim 16 , wherein the method further includes detecting a location of the strip of composite material on the layup surface, and further wherein the conveying includes regulating the location of the strip of composite material on the layup surface, wherein the regulating the location includes moving the layup surface relative to the first support surface such that the strip of composite material is placed at a predetermined location on the layup surface as a result of the conveying.

19. The method of claim 16 , wherein the method further includes compacting the strip of composite material on the layup surface with a compaction structure, wherein the compacting is concurrent with the separating and the conveying.

20. The method of claim 16 , wherein the method further includes detecting a width of the strip of composite material during the separating and regulating the width of the strip of composite material such that the strip of composite material has at

Assignees

• Boeing Co

Inventors

• Kline William Thomas
• Wilson Thomas Dean
• Zbinden Bruno
• Bergan Dalton C
• Warren Jr Joseph Fount
• Boroughs Nicholas A
• Krajca Scott Edward

Classifications

• B32B3/18

  characterised by an internal layer formed of separate pieces of material {which are juxtaposed side-by-side (B32B5/02 takes precedence)} · CPC title

• B32B2605/18

  Aircraft · CPC title

• B32B2260/046

  Synthetic resin · CPC title

• B32B2262/101

  Glass fibres · CPC title

• B32B5/26

  another layer {next to it} also being fibrous or filamentary {(relative arrangement of fibres or filaments of different layers B32B5/12)} · CPC title