Methods for forming a composite blade stiffener and facilitating application of barely visible impact damage treatments

Patent metadata

Field	Value
Publication number	US-10814568-B2
Application number	US-201916511384-A
Country	US
Kind code	B2
Filing date	Jul 15, 2019
Priority date	Nov 1, 2016
Publication date	Oct 27, 2020
Grant date	Oct 27, 2020

Abstract

An example method for forming a flat composite charge into a composite blade stiffener includes cutting a flat composite charge along a cut line into a first piece and a second piece having an angle, positioning the first piece and the second piece of the flat composite charge on a forming mandrel about a tooling plunger, activating the tooling plunger to drive the first piece and the second piece into a cavity of the forming mandrel resulting in the first piece and the second piece folding at the cut line, withdrawing the tooling plunger from the cavity of the forming mandrel, compressing the forming mandrel to apply a lateral pressure to the first piece and the second piece folded into the cavity, and applying a vertical pressure to a first flange and a second flange of the first piece and the second piece, respectively, to form the composite blade stiffener.

First claim

What is claimed is:

1. A method for forming a flat composite charge into a composite blade stiffener, comprising:
cutting a flat composite charge along a cut line into a first piece and a second piece separated by edges having an angle;
applying a reinforcement ply over the first piece and the second piece to hold the first piece and the second piece together;
positioning the first piece and the second piece of the flat composite charge on a forming mandrel about a tooling plunger such that the tooling plunger is aligned with the cut line; and
activating the tooling plunger to contact the reinforcement ply and drive the first piece and the second piece of the flat composite charge into a cavity of the forming mandrel resulting in the first piece and the second piece folding at the cut line.

2. The method of claim 1 , wherein cutting the flat composite charge along the cut line comprises cutting the flat composite charge along a centerline.

3. The method of claim 1 , wherein cutting the flat composite charge along the cut line into the first piece and the second piece separated by the edges having the angle comprises cutting the edges to have about a 45 degree angle.

4. The method of claim 1 , wherein cutting the flat composite charge along the cut line into the first piece and the second piece separated by the edges having the angle comprises cutting the edges to have opposing 45 degree edges angled outward from the cut line.

5. The method of claim 1 , wherein applying the reinforcement ply over the first piece and the second piece to hold the first piece and the second piece together comprises applying a composite fabric ply.

6. The method of claim 1 , further comprising:
applying a ply of contact material to the forming mandrel prior to positioning the first piece and the second piece of the flat composite charge on the forming mandrel; and
positioning the first piece and the second piece of the flat composite charge on the ply of contact material applied to the forming mandrel.

7. The method of claim 1 , further comprising:
withdrawing the tooling plunger from the cavity of the forming mandrel;
compressing the forming mandrel to apply a lateral pressure to the first piece and the second piece folded into the cavity; and
applying a vertical pressure to a first flange and a second flange of the first piece and the second piece, respectively, to form the composite blade stiffener.

8. The method of claim 7 , further comprising:
loading a plate over the first flange and the second flange subsequent to withdrawing the tooling plunger from the cavity of the forming mandrel; and
applying the vertical pressure to the first flange and the second flange using the plate.

9. The method of claim 1 , further comprising:
applying a barely visible impact damage (BVID) treatment to the composite blade stiffener; and
curing both the composite blade stiffener and the BVID treatment during a single curing process.

10. The method of claim 1 , further comprising:
heating the flat composite charge prior to activating the tooling plunger.

11. A method comprising:
forming a cut line on a flat composite charge having opposing 45 degree beveled edges angled outward from the cut line;
positioning the flat composite charge centered about a tooling plunger such that the tooling plunger is aligned with the cut line; and
activating the tooling plunger to move downward and fold the flat composite charge at the cut line into a cavity of a forming mandrel, wherein after moving the tooling plunger downward and folding the flat composite charge, the opposing 45 degree beveled edges form a substantially flat surface perpendicular to the cut line.

12. The method of claim 11 , further comprising:
separating the forming mandrel as the tooling plunger moves downward.

13. The method of claim 11 , further comprising:
applying a reinforcement ply over the flat composite charge.

14. The method of claim 11 , wherein after moving the tooling plunger downward and folding the flat composite charge, the opposing 45 degree beveled edges form the substantially flat surface perpendicular to the cut line and form a first flange and a second flange connected to the flat surface, and the method further comprising:
loading a plate over the first flange and the second flange following withdrawal of the tooling plunger from the cavity of the forming mandrel; and
applying a vertical pressure to the first flange and the second flange using the plate.

15. The method of claim 11 , wherein after moving the tooling plunger downward and folding the flat composite charge, the opposing 45 degree beveled edges form the substantially flat surface perpendicular to the cut line and form a first flange and a second flange connected to the substantially flat surface, wherein the substantially flat surface and the first flange and the second flange connected to the flat surface form a portion of a composite blade stiffener, and the method further comprises:
applying a barely visible impact damage (BVID) treatment to the composite blade stiffener; and
curing both the composite blade stiffener and the BVID treatment during a single curing process.

16. The method of claim 11 , further comprising:
heating the flat composite charge prior to activating the tooling plunger.

17. A method for forming a flat composite charge into a composite blade stiffener, comprising:
cutting the flat composite charge along a cut line into two pieces separated by edges that are angled outward from the cut line;
positioning the flat composite charge on a forming mandrel about a tooling plunger such that the tooling plunger is aligned with the cut line; and
activating the tooling plunger to drive the two pieces of the flat composite charge into a cavity of the forming mandrel resulting in the edges forming a substantially flat surface perpendicular to the cut line and a first flange and a second flange connected to the substantially flat surface.

18. The method of claim 17 , further comprising:
applying a reinforcement ply over the two pieces to hold the two pieces together.

19. The method of claim 17 , further comprising:
applying a ply of contact material to the forming mandrel; and
positioning the flat composite charge on the ply of contact material applied to the forming mandrel.

20. The method of claim 17 , further comprising:
loading a plate over the first flange and the second flange following withdrawal of the tooling plunger from the cavity of the forming mandrel; and
applying a vertical pressure to the first flange and the second flange using the plate.

Assignees

• Boeing Co

Inventors

• Carlson Lisa C
• Pham Kanna M
• Sweetin Joseph L
• Hanson Garrett C
• Reeves Jake A
• Chan Chilip
• Nguyen Kiet

Classifications

• B29D99/0003

  Producing profiled members, e.g. beams · CPC title

• B29C70/46 Primary

  using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs · CPC title

• B29C70/34 Primary

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

• B64C1/064

  Stringers; Longerons · CPC title

• B64C3/18

  Spars; Ribs; Stringers · CPC title