Method of through-thickness reinforcing a laminated material

Patent metadata

Field	Value
Publication number	US-9944023-B2
Application number	US-201414230402-A
Country	US
Kind code	B2
Filing date	Mar 31, 2014
Priority date	Apr 10, 2013
Publication date	Apr 17, 2018
Grant date	Apr 17, 2018

Abstract

A method of providing through-thickness reinforcement of a laminated material which includes a matrix material including a step of creating a locally heated zone in the laminated material so as to locally soften the matrix material by focussing a set of at least two energy beams at a location where through-thickness reinforcement is required and a step of inserting a reinforcement element through the thickness of the laminated material at the location of the locally heated zone to through-thickness reinforce the laminated material.

First claim

I claim:

1. A method of providing through-thickness reinforcement of a laminated material including a matrix material, comprising the steps of:
providing a laminated material;
before insertion of any articles into the laminated material, creating a locally heated zone in the laminated material so as to locally soften the matrix material by focusing a set of at least two energy beams on a focal zone which corresponds to a location where through-thickness reinforcement is required;
forming a hole at the locally heated zone in the laminated material;
inserting a reinforcement element into the hole; and
assisting insertion of the inserted reinforcement element through the thickness of the laminated material by applying a force to a first end of the inserted reinforcement element to through-thickness reinforce the laminated material.

2. The method according to claim 1 , wherein the step of creating the locally heated zone in the laminated material is by focusing a set of more than two energy beams on the focal zone.

3. The method according to claim 1 , wherein
the step of creating the locally heated zone includes creating an array of locally heated zones by focusing a corresponding array of sets of energy beams on a corresponding array of focal zones at locations where through-thickness reinforcing is required; and
the step of inserting a reinforcement element includes inserting a plurality of reinforcing elements through the thickness of the laminated material at the locations corresponding to the array of locally heated zones.

4. The method according to claim 3 , wherein the array of sets of energy beams and the corresponding array of focal zones are arranged linearly in a row.

5. The method according to claim 3 , further comprising a step, which follows the step of inserting of the plurality of reinforcing elements, of translating the laminated material relative to the array of sets of energy beams and the corresponding array of focal zones to another set of locations where through-thickness reinforcing is required.

6. The method according to claim 1 , wherein the step of creating the locally heated zone in the laminated material comprises forming a full-thickness heated zone that penetrates through the entire thickness of the laminated material.

7. The method according to claim 1 , wherein the steps of creating the locally heated zone in the laminated material and inserting the reinforcing element through the thickness of the laminated material are performed at substantially the same time.

8. The method according to claim 7 , wherein the reinforcing element has a tip and the step of creating the locally heated zone in the laminated material includes the focal zone tracking the tip of the reinforcing element as it is inserted such that the locally heated zone remains ahead of the tip as the reinforcing element is inserted through the thickness of the laminated material.

9. The method according to claim 1 , wherein the energy beams are microwaves.

10. The method according to claim 1 , wherein the step of creating the locally heated zone comprises restricting the locally heated zone from reaching a temperature corresponding to the gel point of the matrix material.

11. The method according to claim 1 , wherein the matrix material comprises a polymeric matrix material.

12. The method according to claim 1 , further including a step of curing the through-thickness reinforced laminated material to form a composite material.

13. A method of providing through-thickness reinforcement of a laminated material including a matrix material, comprising the steps of:
providing a laminated material;
creating a locally heated zone in the laminated material so as to locally soften the matrix material by focusing a set of at least two energy beams on a focal zone which corresponds to a location where through-thickness reinforcement is required;
forming a hole at the locally heated zone in the laminated material with a hole-forming tool;
after the hole is formed, inserting an insertion member through the thickness of the laminated material at the location of the locally heated zone,
wherein the focal zone is advanced ahead of the hole-forming tool as the hole-forming tool is inserted through the laminated material.

14. The method according to claim 13 , wherein the insertion member comprises a reinforcement member inserted through the laminated material to through-thickness reinforce the laminated material.

15. The method of claim 13 , further comprising assisting insertion of the inserted insertion member by hammering the insertion member.

16. A method of providing through-thickness reinforcement of a laminated material including a matrix material, comprising the steps of:
providing a laminated material;
before insertion of any articles into the laminated material, creating a locally heated zone in the laminated material so as to locally soften the matrix material by focusing a set of at least two energy beams on a focal zone which corresponds to a location where through-thickness reinforcement is required; and
inserting a reinforcement element through the thickness of the laminated material at the location of the locally heated zone to through-thickness reinforce the laminated material,
wherein the reinforcement element includes a first end and a second opposite end, and
wherein the step of inserting the reinforcement element comprises applying a force to the first end of the reinforcement element such that the second end penetrates the laminated material.

Assignees

• Rolls Royce Plc

Inventors

• Jevons Matthew Paul

Classifications

• Y10T156/1056

  Perforating lamina · CPC title

• B29L2031/08

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

• F01D5/282

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

• B29C65/1425

  Microwave radiation · CPC title

• B29C70/24 Primary

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