Methods for forming radius fillers for composite structures

Patent metadata

Field	Value
Publication number	US-2017217110-A1
Application number	US-201715486149-A
Country	US
Kind code	A1
Filing date	Apr 12, 2017
Priority date	Aug 20, 2014
Publication date	Aug 3, 2017
Grant date	—

Abstract

Methods for forming radius fillers for composite structures are disclosed herein. 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

1 . A method of forming a radius filler for a composite structure, the method comprising:
locating a sheet of composite material on a first support surface that terminates at a support surface edge; translating the sheet of composite material such that a first portion of the sheet of composite material is supported by the first support surface and a 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 a 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 a separation device to form a strip of composite material; conveying the strip of composite material onto a 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.

2 . The method of claim 1 , wherein the separating includes conveying the second support surface and the separation device along the support surface edge.

3 . The method of claim 1 , wherein the separating includes extending the separation device completely through the sheet of composite material.

4 . The method of claim 1 , 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.

5 . The method of claim 4 , 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.

6 . The method of claim 1 , wherein the method further includes compacting the strip of composite material on the layup surface with a compaction structure.

7 . The method of claim 6 , wherein the compacting is concurrent with the separating and the conveying.

8 . The method of claim 1 , 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 based, at least in part, on a detected width of the strip of composite material.

9 . The method of claim 8 , wherein the regulating the width of the strip of composite material includes regulating such that the strip of composite material has at least one of:
(i) a predetermined width along a length of the strip of composite material; and (ii) a predetermined width profile along the length of the strip of composite material.

10 . The method of claim 8 , wherein the regulating the width of the strip of composite material includes regulating such that the stack of strips of composite material has at least one of:
(i) a predetermined cross-sectional area along a length of the stack of strips of composite material; and (ii) a predetermined cross-sectional area variation along the length of the stack of strips of composite material.

11 . The method of claim 8 , wherein the regulating the width of the strip of composite material is concurrent with at least one of:
(i) the separating; and (ii) the conveying.

12 . The method of claim 1 , wherein the locating includes at least one of:
(i) forming the sheet of composite material on the first support surface; and (ii) locating a previously formed sheet of composite material on the first support surface.

13 . The method of claim 1 , wherein the first support surface is defined by a charge-advance belt, and further wherein the translating includes moving the charge-advance belt.

14 . The method of claim 1 , wherein the translating includes cantilevering the second portion of the sheet of composite material over the support surface edge.

15 . The method of claim 1 , wherein the conveying includes translating the strip of composite material across the second support surface and onto the layup surface.

16 . The method of claim 1 , 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.

17 . The method of claim 1 , wherein the repeating includes forming a plurality of scraps of composite material and forming the plurality of strips of composite material, wherein the plurality of scraps of composite material is not conveyed onto the layup surface.

18 . The method of claim 17 , wherein each scrap of composite material of the plurality of scraps of composite material is formed intermediate to two strips of composite material of the plurality of strips of composite material, and further wherein the forming the plurality of scraps of composite material includes defining a desired edge profile on each strip of composite material of the plurality of strips of composite material.

19 . The method of claim 1 , wherein the second support surface and the separation device are operatively coupled to one another and configured to translate together, and further wherein the repeating includes repeatedly conveying the second support surface and the separation device along the support surface edge to form the plurality of strips of composite material.

20 . The method of claim 19 , wherein the translating the sheet of composite material and the conveying the strip of composite material are interleaved with the repeatedly conveying the second support surface and the separation device.

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

• B29K2105/0872

  Prepregs · CPC title

• B29C70/386 Primary

  Automated tape laying [ATL] · CPC title

• B29C70/545

  Perforating, cutting or machining during or after moulding · CPC title

• B29C70/34

  and shaping or impregnating by compression {, i.e. combined with compressing after the lay-up operation} · CPC title

• B32B2307/50

  having particular mechanical properties · CPC title