Fabricating composite core with woven composite fibers

Patent metadata

Field	Value
Publication number	US-10550499-B2
Application number	US-201715410416-A
Country	US
Kind code	B2
Filing date	Jan 19, 2017
Priority date	Jan 19, 2017
Publication date	Feb 4, 2020
Grant date	Feb 4, 2020

Abstract

In the present disclosure, a method may include forming a three-dimensional composite fiber pre-form by three-dimensionally weaving a plurality of composite fibers. The composite fiber pre-form includes a plurality of open cells formed adjacent to and interlocked with each other, and a composite fiber forms at least a portion of a first side of a first open cell and at least a portion of a second side of a second open cell. The first open cell and the second open cell are adjacent to and interlocked with each other.

First claim

What is claimed is:

1. A method comprising:
forming a three-dimensional composite fiber pre-form by three-dimensionally weaving a plurality of composite fibers, the composite fiber pre-form comprising a plurality of open cells formed adjacent to and interlocked with each other, wherein a composite fiber forms at least a portion of a first side of a first open cell and at least a portion of a second side of a second open cell, the first open cell and the second open cell adjacent to and interlocked with each other, wherein the open cells of every adjacent pair of open cells of the plurality of open cells are interlocked with each other, wherein the interlocked cells are formed from a continuous fiber, wherein the plurality of composite fibers comprises a first set of fibers oriented in an XZ plane and a second set of fibers oriented in an XY plane, wherein forming the composite fiber pre-form comprises three-dimensionally weaving the second set of fibers through the first set of fibers to form the plurality of open cells in the XZ plane.

2. The method of claim 1 wherein the first set of fibers and the second set of fibers are oriented at an angle to each other.

3. The method of claim 2 , wherein the angle is substantially 90 degrees or substantially 45 degrees.

4. The method of claim 1 , wherein forming the three-dimensional composite fiber pre-form by three-dimensionally weaving the plurality of composite fibers comprises at an intersection of two sides of the first open cell:
weaving a first subset of the second set of fibers to form a second side of the first open cell; and
weaving a second subset of the second set of fibers to form the second side of the second open cell.

5. The method of claim 2 , further comprising controlling a size of each open cell by controlling lengths of fibers in at least one of the first subset of the second set of fibers or the second subset of the second set of fibers.

6. The method of claim 1 , wherein each cell of the plurality of open cells has a nested geometry cross-section.

7. The method of claim 6 , wherein the nested geometry cross-section comprises at least one of a hexagon, a square, a triangle or a combination of at least two of the hexagon, the square or the triangle.

8. The method of claim 1 , further comprising:
inserting a plurality of mandrels through corresponding plurality of open cells; and
curing the composite fiber pre-form over the plurality of mandrels.

9. The method of claim 8 , wherein curing the composite fiber pre-form to the plurality of mandrels comprises introducing the composite fiber pre-form with resin.

10. A method comprising:
orienting a first set of composite fibers in a first direction;
orienting a second set of composite fibers in a second direction; and
three-dimensionally weaving the first set of composite fibers into the second set of composite fibers to form a three-dimensional composite fiber pre-form comprising a plurality of open cells formed adjacent to and interlocked with each other, wherein a composite fiber of the first set of composite fiber forms at least a portion of a side of each of a first open cell and a second open cell adjacent to and interlocked with the first open cell, wherein the open cells of every adjacent pair of open cells of the plurality of open cells are interlocked with each other, wherein the interlocked cells are formed from a continuous fiber, wherein the plurality of composite fibers comprises a first set of fibers oriented in an XZ plane and a second set of fibers oriented in an XY plane, wherein forming the composite fiber pre-form comprises three-dimensionally weaving the second set of fibers through the first set of fibers to form the plurality of open cells in the XZ plane.

11. The method of claim 10 , wherein the first set of composite fibers is oriented at an angle to the second set of composite fibers.

12. The method of claim 11 , wherein the angle is substantially 90 degrees or substantially 45 degrees.

13. The method of claim 10 , wherein three-dimensionally weaving the first set of composite fibers into the second set of composite fibers to form the three-dimensional composite fiber pre-form comprises, at an intersection of two sides of the first open cell:
weaving a first subset of the first set of fibers to form another side of the first open cell; and
weaving a second subset of the first set of fibers to form another side of the second open cell.

14. The method of claim 13 , further comprising controlling a size of each open cell by controlling lengths of fibers in at least one of the first subset or the second subset of the first set of fibers.

15. The method of claim 10 , wherein each cell of the plurality of open cells has a nested geometry cross-section comprising at least one of a hexagon, a square, a triangle or a combination of at least two of the hexagon, the square or the triangle.

16. The method of claim 10 , further comprising:
inserting a plurality of mandrels through corresponding plurality of open cells; and
curing the composite fiber pre-form to the plurality of mandrels.

17. A system comprising:
a three-dimensional composite fiber weaving machine;
a computer-readable medium storing instructions executable by one or more processors connected to the three-dimensional composite fiber weaving machine, the one or more processors configured to execute the instructions to cause the three-dimensional composite fiber weaving machine to perform operations comprising:
forming a three-dimensional composite fiber pre-form by three-dimensionally weaving a plurality of composite fibers, the composite fiber pre-form comprising a plurality of open cells formed adjacent to and interlocked with each other, wherein a composite fiber forms at least a portion of a first side of a first open cell and at least a portion of a second side of a second open cell, the first open cell and the second open cell adjacent to and interlocked with each other, wherein the open cells of every adjacent pair of open cells of the plurality of open cells are interlocked with each other, wherein the interlocked cells are formed from a continuous fiber, wherein the plurality of composite fibers comprises a first set of fibers oriented in an XZ plane and a second set of fibers oriented in an XY plane, wherein forming the composite fiber pre-form comprises three-dimensionally weaving the second set of fibers through the first set of fibers to form the plurality of open cells in the XZ plane.

18. The system of claim 17 , wherein the first set of fibers and the second set of fibers are oriented at an angle to each other, wherein the angle is substantially 90 degrees or substantially 45 degrees.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Kendrick Phillip
• Oldham Kathleen
• Armstrong Levi
• Oberle Elizabeth

Classifications

• B29D99/0089

  Producing honeycomb structures (consisting of porous ceramic ware C04B38/0006) · CPC title

• B29C70/48

  and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM] {, e.g. by vacuum} · CPC title

• D03D25/005 Primary

  Three-dimensional woven fabrics · CPC title

• B29C70/24

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

• B29D24/001

  formed of hollow ridges or ribs, e.g. separate ridges; continuous corrugated structure (B29D24/008 takes precedence) · CPC title