Self-stiffened composite panel and method of producing same

Patent metadata

Field	Value
Publication number	US-10105938-B2
Application number	US-201414557074-A
Country	US
Kind code	B2
Filing date	Dec 1, 2014
Priority date	May 29, 2012
Publication date	Oct 23, 2018
Grant date	Oct 23, 2018

Abstract

The disclosure proposes a method for producing a panel having an outer skin and stiffeners that have a connecting portion, and at least one projecting portion, the method comprising a step of draping layers of fibers over at least one insert such that each layer of fibers has a connecting portion and a portion that projects downwardly from the connecting portion, a step of draping a layer of fibers that forms the outer skin, and a step of bonding the layers of fibers together. The disclosure also provides a device for implementing the method.

First claim

The invention claimed is:

1. A method for producing a self-stiffened composite panel having an outer skin and stiffeners, each stiffener having a portion for connecting the stiffener to the outer skin, and at least one portion that projects from the connecting portion, the method comprising:
draping layers of fibers, that are intended to form the stiffeners, over at least one insert having a complementary shape to a final shape of the stiffeners, such that each layer of fibers that is intended to form a stiffener has a connecting portion and a free lower end portion that projects vertically downwardly from the connecting portion;
draping a layer of fibers that is intended to form the outer skin over the connecting portion of the layers of fibers that are intended to form the stiffeners; and
simultaneously bonding all the layers of fibers together by a matrix using the at least one insert as a mold element;
wherein, during draping, the layers of fibers are not impregnated with matrix and bonding together comprises a phase of injecting the matrix and then a phase of hardening the matrix, and wherein injecting the matrix comprises injecting the matrix from a bottom upwards from the free lower end portion.

2. The method according to claim 1 , wherein draping layers of fibers over the at least one insert is followed by positioning each insert covered by the layer of fibers on a molding support.

3. The method according to claim 2 , comprising a positioning step comprising positioning the inserts covered by the layers of fibers in a manner adjacent to one another.

4. The method according to claim 1 , wherein the bonding together comprises positioning at least one of a demolding fabric, an air draining felt, a smoothing metal sheet and a vacuum bag on the layer of fibers that is intended to form the outer skin prior to the phase of injecting the matrix.

5. The method according to claim 1 , wherein the panel comprises metal accessories fixed to the stiffeners and/or to the outer skin, and wherein the method comprises fitting the accessories at a same time as draping the layers of fibers that are intended to form the stiffeners.

Assignees

• Airbus Operations Sas

Inventors

• Guittard Dominique
• Lannuzel Mathieu
• Blot Philippe
• Bezard Gilles

Classifications

• B32B37/1284 Primary

  Application of adhesive · CPC title

• B64C1/064

  Stringers; Longerons · CPC title

• B29C33/485

  cores or mandrels (collapsible mandrels for shaping tube ends B29C57/02; collapsible mandrels for winding and joining B29C53/824) · CPC title

• B32B2260/00

  Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material · CPC title

• B29K2705/00

  Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts · CPC title