Wrinkle mitigation in contoured composite stiffeners

Patent metadata

Field	Value
Publication number	US-11806954-B2
Application number	US-202117644285-A
Country	US
Kind code	B2
Filing date	Dec 14, 2021
Priority date	Dec 14, 2021
Publication date	Nov 7, 2023
Grant date	Nov 7, 2023

Abstract

A composite charge is formed between two compression dies into a composite laminate stiffener. The stiffener is contoured along its length by contouring the dies. Wrinkle diffusers attached to, or embedded or incorporated into the tool surfaces of the dies, diffuse wrinkles formed on the inside radius of the stiffener during the contouring.

First claim

What is claimed is:

1 . Apparatus for forming a contoured composite laminate stiffener, comprising:
a first die and a second die between which a multi-ply composite charge may be formed into a stiffener, the first die and the second die being configured to form a contour in the stiffener; and at least a first diffuser positioned between the first die and the second die, and configured to diffuse wrinkles in the stiffener along the contour; wherein the first diffuser includes depressions therein into which the plies of the multi-ply charge may strain in response to compressive stress in the stiffener caused by forming the stiffener to the contour, and wherein the depressions form a plurality of peaks and troughs forming a serpentine pattern or a sine wave pattern.

2 . The apparatus of claim 1 , wherein the depressions include a plurality of slots spaced apart from each other.

3 . The apparatus of claim 1 , wherein:
the first diffuser is located at an inside radius of the contour of the stiffener in which compressive stresses are generated in the stiffener when the stiffener is formed to the contour, and the depressions configured to allow portions of the multi-ply charge at the inside radius to strain into the depressions and form wrinkles having a predetermined length-to-depth ratio.

4 . The apparatus of claim 1 , wherein:
the first diffuser is a plate having the depressions therein into which portions of the plies of the multi-ply charge in the contour may strain when the stiffener is formed to the contour, and the plate is removably attached to one of the first die and the second dies.

5 . The apparatus of claim 1 , further comprising:
at least a second diffuser positioned between the first die and the second die and opposing the first diffuser, the second diffuser including depressions therein configured to diffuse wrinkling of the plies of the multi-ply charge within the contour in the stiffener.

6 . Apparatus for making a contoured composite laminate stringer having a flange and a web, comprising:
a first die and a second die between which a multi-ply composite charge may be formed into a flange and a web having a contour; a first wrinkle diffuser on the first die; and a second wrinkle diffuser on the second die and opposing the first wrinkle diffuser; wherein the first and second wrinkle diffusers are configured to diffuse wrinkles in the contour of the flange and the web as the multi-ply composite charge is being formed; wherein each of the first wrinkle diffuser and the second wrinkle diffuser includes a plurality of depressions therein into which the multi-ply composite charge may strain within the contour as the multi-ply composite charge is being formed to the contour, and wherein the depressions in the first wrinkle diffuser are aligned with and oppose the depressions in the second wrinkle diffuser.

7 . The apparatus of claim 6 , wherein the depressions form a plurality of peaks and troughs forming a sine wave pattern.

8 . The apparatus of claim 6 , wherein the depressions include a plurality of slots spaced apart from each other.

9 . The apparatus of claim 8 , wherein:
the slots include a set of first slots each having a length, and a set of second slots each having a length less than the length of the first slots, and the first slots and the second slots are arranged in alternating relationship to each other.

10 . The apparatus of claim 6 , wherein:
each of the first wrinkle diffuser and the second wrinkle diffuser includes a plate attached to a corresponding one of the first die and the second die, and the depressions are formed in each plate.

11 . The apparatus of claim 6 , wherein:
each of the first wrinkle diffuser and the second wrinkle diffuser includes a plurality of plates, the depressions are located in the plates, and the plates are releasably connected with each other.

12 . A method of making a contoured composite laminate stiffener, comprising:
placing a multi-ply composite charge between first and second dies; placing at least one wrinkle diffuser between the first and second dies; forming the multi-ply composite charge into a stiffener having a desired cross sectional shape by compressing the multi-ply composite charge between the first and second dies; contouring the stiffener to a desired contour having an inside radius; and controlling wrinkling of the stiffener along the inside radius during the contouring using the wrinkle diffuser; wherein the wrinkle diffuser includes depressions therein into which the plies of the multi-ply charge may strain in response to compressive stress in the stiffener caused by forming the stiffener to the desired contour, and wherein the depressions form a plurality of peaks and troughs forming a serpentine pattern or a sine wave pattern.

13 . The method of claim 12 , wherein:
the contouring includes contouring the first and second dies, and placing the wrinkle diffuser includes installing the wrinkle diffuser on one of the first and second dies in an area along the inside radius.

14 . The method of claim 12 , wherein controlling the wrinkling includes forming wrinkles in the multi-ply composite charge having preselected length-to-depth ratios.

15 . The method of claim 12 , wherein placing the wrinkle diffuser includes:
interconnecting a plurality of diffuser plates together, and removably attaching the plurality of diffuser plates to at least one of the first and second dies.

16 . The method of claim 12 , wherein controlling wrinkling includes forcing the multi-ply composite charge into the depressions in the wrinkle diffuser.

17 . Apparatus for making a contoured composite laminate stringer having a flange and a web, comprising:
a first die and a second die between which a multi-ply composite charge may be formed into a flange and a web having a contour; a first wrinkle diffuser on the first die; and a second wrinkle diffuser on the second die and opposing the first wrinkle diffuser; wherein the first and second wrinkle diffusers are configured to diffuse wrinkles in the contour of the flange and the web as the multi-ply composite charge is being formed; wherein each of the first wrinkle diffuser and the second wrinkle diffuser includes a plurality of depressions therein into which the multi-ply composite charge may strain within the contour as the multi-ply composite charge is being formed to the contour; and wherein each of the first wrinkle diffuser and the second wrinkle diffuser includes a plurality of plates, the depressions are located in the plates, and the plates are releasably connected with each other.

18 . The apparatus of claim 17 , wherein the depressions form a plurality of peaks and troughs forming a serpentine pattern.

19 . The apparatus of claim 17 , wherein the depressions form a plurality of peaks and troughs forming a sine wave pattern.

20 . The apparatus of claim 17 , wherein the depressions include a plurality of slots spaced apart from each other.

Assignees

• Boeing Co

Inventors

• Saini Gagandeep
• Schroeder Ian Edward
• Willden Kurtis Shuldberg
• Carlson Lisa Christina

Classifications

• B29C70/549 Primary

  Details of caul plates, e.g. materials or shape · CPC title

• B29C70/462

  Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames · CPC title

• B29D99/0003 Primary

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

• B29L2009/00

  Layered products · CPC title

• B29L2031/001

  Profiled members, e.g. beams, sections · CPC title