Composite filler

Patent metadata

Field	Value
Publication number	US-9566739-B2
Application number	US-201414182474-A
Country	US
Kind code	B2
Filing date	Feb 18, 2014
Priority date	Feb 18, 2014
Publication date	Feb 14, 2017
Grant date	Feb 14, 2017

Abstract

A method and apparatus is presented. Layers of composite material are laid down on a forming tool. A respective bend is formed in each of the layers to form the composite filler comprising bent layers on the forming tool. The composite filler comprising the bent layers is placed into a gap formed by at least one composite structure.

First claim

What is claimed is:

1. A method comprising:
laying down a first layer of composite material on a forming tool;
forming a bend in the first layer by pressing the first layer against the forming tool using a first die punch;
repeating said laying down and forming steps for additional successive layers of the composite material using successively smaller die punches to form a composite filler comprising bent composite layers on the forming tool, a respective bend in each of the successive layers being formed by pressing with a respective one of the smaller punches; and
transferring the composite filler from the forming tool into a gap formed by at least one composite structure.

2. The method of claim 1 , wherein each of the successive punches has a different cross-section and a different angle forming the respective bend in a respective one of the successive layers.

3. The method of claim 1 , wherein at least one of the successive layers comprises multiple plies of the composite material.

4. The method of claim 1 further comprising: adding an extruded composite material into an open space formed by the bend of the final successive layer prior to placing the composite filler into the gap.

5. The method of claim 1 , wherein a cross-section of the composite filler is substantially triangular.

6. The method of claim 1 , wherein each successive layer of composite material has a shorter width than a width of a previous layer of the composite material.

7. The method of claim 1 , wherein the bend in each of the first and successive layers forms angled first and second layer sides parallel to first and second sides of the composite filler, respectively.

8. The method of claim 1 , wherein the composite filler comprises at least the first layer having a first bent shape, a first successive layer having a second bent shape, and a second successive layer having a third bent shape.

9. The method of claim 1 , wherein each of the successive die punches has a progressively smaller height than a previous of the first and successive die punches.

Assignees

• Boeing Co

Inventors

• Chapman Michael R
• Pham Khanh Mai
• Vetter Derek Paul

Classifications

• G06F3/013

  Eye tracking input arrangements (G06F3/015 takes precedence) · CPC title

• B29L2031/3082

  Fuselages · CPC title

• B32B2250/44

  Number of layers variable across the laminate · CPC title

• B29C66/73941

  characterised by the materials of both parts being thermosets · CPC title

• B29C53/04 Primary

  of plates or sheets {(B29C63/04 takes precedence; bending or folding paper B31F1/0003; folding films B65H45/00)} · CPC title