Composite laminate and a method of manufacturing a composite laminate

Patent metadata

Field	Value
Publication number	US-12208598-B2
Application number	US-202218049331-A
Country	US
Kind code	B2
Filing date	Oct 25, 2022
Priority date	Nov 10, 2021
Publication date	Jan 28, 2025
Grant date	Jan 28, 2025

Abstract

A method of manufacturing a composite laminate. The method comprises providing a base layer, providing a discontinuous reinforcing patch on the base layer, and providing a top layer over the base layer and discontinuous reinforcing patch. Also, a composite laminate having a discontinuous reinforcing patch interposed between a base layer and a top layer. The discontinuous reinforcing patch comprises a patterned nanomaterial layer with nanomaterial-filled zones and vacant zones.

First claim

We claim:

1. A method of manufacturing a composite laminate, the method comprising the steps of:
providing a base layer formed from polymeric material;
providing a continuous reinforcing patch on the base layer;
processing the continuous reinforcing patch to form a discontinuous reinforcing patch on the base layer, the discontinuous reinforcing patch comprising a patterned nanomaterial layer having at least one nanomaterial-filled zone and at least one vacant zone, wherein the nanomaterial layer in the at least one nanomaterial-filled zone comprises a plurality of aligned carbon nanotubes, and wherein processing the continuous reinforcing patch comprises:
providing a masking film on the base layer, the masking film including a discontinuous cut-out;
pressing the continuous reinforcing patch on the masking film, wherein nanomaterials in the continuous reinforcing patch transfer through the discontinuous cut-out and onto the base layer; and
removing the masking film to leave the discontinuous reinforcing patch on the base layer; and

providing a top layer formed of polymeric material over the base layer and discontinuous reinforcing patch such that the discontinuous reinforcing patch is interposed between the base layer and the top layer.

2. The method of claim 1 , wherein the masking film is formed from fluorinated ethylene propylene release film.

3. The method of claim 1 , wherein the plurality of carbon nanotubes in the at least one nanomaterial-filled zone have an average length between and including 5 μm to 60 μm.

4. The method of claim 1 , wherein the at least one nanomaterial-filled zone has an irregular shape.

5. The method of claim 1 , wherein the at least one nanomaterial-filled zone and the at least one vacant zone are arranged in an irregular pattern.

6. A method of manufacturing a composite laminate, the method comprising the steps of:
processing a continuous reinforcing patch to form a discontinuous reinforcing patch, wherein the discontinuous reinforcing patch is disposed on a base layer that is formed from polymeric material, wherein the discontinuous reinforcing patch comprises a patterned nanomaterial layer having at least one nanomaterial-filled zone and at least one vacant zone, the at least one nanomaterial-filled zone comprising a plurality of aligned carbon nanotubes; and
providing a top layer formed of polymeric material over the base layer and discontinuous reinforcing patch such that the discontinuous reinforcing patch is interposed between the base layer and the top layer.

7. The method of claim 6 , wherein the plurality of aligned carbon nanotubes have an average length between and including 5 μm to 60 μm.

8. The method of claim 6 , wherein the continuous reinforcing patch is processed to form the discontinuous reinforcing patch prior to being disposed on the base layer.

9. The method of claim 6 , wherein the continuous reinforcing patch is processed to form the discontinuous reinforcing patch in situ on the base layer.

10. The method of claim 6 , wherein a central axis of the plurality of aligned carbon nanotubes is approximately perpendicular to the base layer and the top layer.

11. The method of claim 6 , wherein the processing of the continuous reinforcing patch comprises etching or ablation to form the vacant zones.

12. The method of claim 6 , wherein the at least one nanomaterial-filled zone has an irregular shape.

13. The method of claim 6 , wherein the at least one nanomaterial-filled zone and the at least one vacant zone are arranged in an irregular pattern.

14. A method of manufacturing a composite laminate, the method comprising the steps of:
providing a base layer formed from polymeric material;
providing a continuous reinforcing patch on the base layer;
processing the continuous reinforcing patch to form a discontinuous reinforcing patch on the base layer, the discontinuous reinforcing patch comprising a patterned nanomaterial layer having at least one nanomaterial-filled zone and at least one vacant zone, wherein the processing of the continuous reinforcing patch comprises etching or ablation to form the vacant zones; and
providing a top layer formed of polymeric material over the base layer and discontinuous reinforcing patch such that the discontinuous reinforcing patch is interposed between the base layer and the top layer.

15. The method of claim 14 , wherein the nanomaterial layer in the at least one nanomaterial-filled zone comprises a plurality of aligned carbon nanotubes.

16. The method of claim 15 , wherein the plurality of carbon nanotubes in the at least one nanomaterial-filled zone have an average length between and including 5 μm to 60 μm.

17. The method of claim 14 , wherein the continuous reinforcing patch is provided on a substrate, wherein etching or ablation comprises etching or ablating portions of the continuous reinforcing patch off of the substrate.

18. The method of claim 14 , wherein the at least one nanomaterial-filled zone or the at least one vacant zone has an irregular shape.

19. The method of claim 14 , wherein the at least one nanomaterial-filled zone and the at least one vacant zone are arranged in an irregular pattern.

Assignees

• Rolls Royce Plc

Inventors

• Backhouse Robert C
• Worboys Robert C

Classifications

• B32B2603/00

  Vanes, blades, propellers, rotors with blades · CPC title

• B32B2313/04

  Carbon · CPC title

• B32B2307/732

  Dimensional properties · CPC title

• B32B2305/22

  Fibres of short length · CPC title

• B32B2305/08

  Reinforcements · CPC title