Fibrous structure having variable numbering yarns

Patent metadata

Field	Value
Publication number	US-9597841-B2
Application number	US-201214364996-A
Country	US
Kind code	B2
Filing date	Dec 10, 2012
Priority date	Dec 14, 2011
Publication date	Mar 21, 2017
Grant date	Mar 21, 2017

Abstract

A fiber structure for reinforcing a composite material part, the structure being woven as a single piece by multilayer weaving between a first plurality of layers of yarns extending in a first direction and a second plurality of layers of yarns extending in a second direction. The second plurality of layers of yarns includes at least one layer of variable-weight yarns, each variable-weight yarn including a separable assembly of individual yarns, each having a determined weight. The fiber structure includes at least one portion of reduced thickness in which the variable-weight yarn presents a weight that is less than the weight that it presents prior to the reduced thickness portion.

First claim

The invention claimed is:

1. A fiber structure for reinforcing a composite material part, the structure being woven as a single piece by multilayer weaving between a first plurality of layers of yarns extending in a first direction and a second plurality of layers of yarns extending in a second direction,
wherein at least one of the first and second pluralities of layers of yarns includes at least one layer of yarns of variable weight, each variable-weight yarn including a separable assembly of individual yarns each having a determined weight; and
wherein the fiber structure includes at least one portion of reduced thickness in which the variable-weight yarns present weight that is less than the weight presented by the variable-weight yarns prior to the portion of reduced thickness.

2. A structure according to claim 1 , wherein the weight of each individual yarn of a variable-weight yarn is a divisor of the weight of the variable-weight yarn.

3. A structure according to claim 1 , wherein the variable-weight yarns are assembled yarns.

4. A structure according to claim 1 , wherein each variable-weight yarn has an initial weight of 48K and includes one of the following separable assemblies of individual yarns:
two individual yarns, each weighing 24K;
three individual yarns including one weighing 24K and two others, each weighing 12K; and
four yarns, each weighing 12K.

5. A structure according to claim 1 , wherein, in the portion of reduced thickness, the fiber structure has three layers of the first plurality of layers of yarns and two layers of the second plurality of layers of yarns.

6. A structure according to claim 1 , wherein the portion of reduced thickness includes at least one zone starting from which a layer of the first or second plurality of layers of yarns is interrupted, the interrupted layer of yarns being replaced thereafter in the portion of reduced thickness by individual yarns of a layer of variable-weight yarns adjacent to the interrupted layer.

7. A composite material part comprising fiber reinforcement densified by a resin matrix in which the fiber reinforcement is formed by a fiber structure according to claim 1 and densified by a matrix.

8. A part according to claim 7 , constituting an aeroengine blade.

9. A part according to claim 8 , wherein the reduced thickness portion of the fiber structure corresponds to a portion of the fiber reinforcement that forms a trailing edge of the blade.

10. A turboprop comprising a plurality of blades according to claim 9 .

11. An aircraft comprising at least one turboprop according to claim 10 .

12. A method of fabricating a fiber structure for reinforcing a composite material part, the method comprising:
weaving a fiber structure as a single piece by multilayer weaving between a first plurality of layers of yarns extending in a first direction and a second plurality of layers of yarns extending in a second direction,
wherein at least one of the first and second pluralities of layers of yarns includes at least one layer of yarns of variable weight, each variable-weight yarn including a separable assembly of individual yarns each having a determined weight; and
wherein the method further comprising reducing weight of variable-weight yarn during weaving of at least one portion of reduced thickness in the fiber structure.

13. A method according to claim 12 , wherein, during weaving of the reduced thickness in the fiber structure, a layer of the first or second plurality of layers of yarns is interrupted, the interrupted layer of yarns being replaced thereafter in the portion of reduced thickness by individual yarns of a layer of variable weight yarns adjacent to the interrupted layer.

Assignees

• Snecma

Inventors

• Dambrine Bruno Jacques Gerard
• Coupe Dominique
• Goering Jonathan
• Gilbertson Brock
• Mahieu Jean-Noel

Classifications

• D03D25/00 Primary

  Woven fabrics not otherwise provided for · CPC title

• D03D25/005

  Three-dimensional woven fabrics · CPC title

• B29C70/24

  oriented in at least three directions forming a three-dimensional [3D] structure · CPC title

• Y10T428/24603

  Fiber containing component · CPC title

• B29L2031/08

  Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers · CPC title