Multi-layer braided article

Patent metadata

Field	Value
Publication number	US-11090880-B2
Application number	US-201815919369-A
Country	US
Kind code	B2
Filing date	Mar 13, 2018
Priority date	May 5, 2017
Publication date	Aug 17, 2021
Grant date	Aug 17, 2021

Abstract

A multi-layer braided article comprises a braid folded over itself to form a first layer and a second layer, and one or more blind stitches in the first layer. The one or more stitches define an edge of the first layer about which the braid folds from the first layer into the second layer.

First claim

The invention claimed is:

1. A multi-layer braided article comprising:
a braid folded over itself to form a first layer and a second layer;
a set of one or more blind stitches in the first layer, the one or more stitches defining an edge of the first layer about which the braid is folded; and
a core and an initial layer attached thereto;
wherein the one or more blind stitches penetrate through the first layer and into the initial layer attached to the core;
wherein the blind stitches attach the first layer of the braid to the initial layer; and
wherein the initial layer is a second braid.

2. The multi-layer braided article according to claim 1 , wherein the initial layer is attached to the core by an adhesive and/or by blind stitches in the initial layer that provide hoop tension around the core.

3. The multi-layer braided article according to claim 1 , wherein
the braid is formed from high strength fibres suitable for aeronautical applications.

4. The multi-layer braided article according to claim 3 , wherein the fibres are one or more of: carbon fibre, glass fibre, an aramid, or a mixture thereof.

5. The multi-layer braided article according to claim 1 , wherein
the braid is a bi-axial braid or a tri-axial braid.

6. The multi-layer braided article according to claim 1 , further comprising
a second set of one or more blind stitches extending at least through the second layer; and
a third layer formed on top of the second layer;
wherein the second set of one or more blind stitches in the second layer is configured to maintain tension in the second layer and define a second edge about which the second layer folds over itself into the third layer.

7. The multi-layer braided article according to claim 6 , wherein
the second set of blind stitches penetrates through the second layer and the first layer, and optionally, into the initial layer if present.

8. The multi-layer braided article according to claim 6 , wherein, for a given value of n>0:
an (n+2) th edge of a layer (n+2) is directly on top of an n th edge of another layer n, such that the edges are coincident; or
an (n+2) th edge of a layer (n+2) is not on top of the n th edge of another layer n, such that there is a stepped profile between the two layers.

9. The multi-layer braided article according to claim 1 , further comprising
reinforcement stitching comprising one or more blind stitches penetrating at least two layers of the multi-layer braided article at a location other than an edge about which the braid folds over itself;
wherein the reinforcement stitching is configured to provide delamination resistance for the multi-layer braided article.

10. An aircraft component comprising the multi-layer braided article of claim 1 ;
wherein the aircraft component is a blade, the blade further comprising a metal blade root configured to engage a rotor disc or hub.

Assignees

• Ratier Figeac Sas

Inventors

• Amat Pascal

Classifications

• D04C1/06 Primary

  Braid or lace serving particular purposes · CPC title

• F01D5/282

  Selecting composite materials, e.g. blades with reinforcing filaments · CPC title

• B32B2262/106

  Carbon fibres, e.g. graphite fibres · CPC title

• D10B2403/023

  Fabric with at least two, predominantly unlinked, knitted or woven plies interlaced with each other at spaced locations or linked to a common internal co-extensive yarn system · CPC title

• D10B2505/02

  Reinforcing materials; Prepregs · CPC title