Method of making a large area graphene composite material

Patent metadata

Field	Value
Publication number	US-9574063-B2
Application number	US-201314028862-A
Country	US
Kind code	B2
Filing date	Sep 17, 2013
Priority date	Sep 17, 2013
Publication date	Feb 21, 2017
Grant date	Feb 21, 2017

Abstract

Large area graphene (LAG) sheets can be embedded in a polymer-based material as a mechanical reinforcement or to otherwise enhance the properties of the polymer-based material. The LAG sheets can be nanoperforated and/or functionalized to enhance interaction between the graphene and the polymer. Reactive functional groups can facilitate formation of covalent bonds between the graphene and the polymer so that the LAG sheets become an integral part of the cross-linked structure in curable polymer-based materials. Nanoperforations in the LAG sheets provide useful sites for the functional groups and can allow cross-links to form through the nanoperforations.

First claim

What is claimed is:

1. A method of making a composite panel, comprising the steps of:
embedding a large area graphene (LAG) sheet in a layer of material comprising a polymeric matrix material;
functionalizing the LAG sheet with reactive functional groups before the step of embedding; and
reacting the polymer matrix material with at least some of the reactive functional groups to form covalent bonds between the LAG sheet and the polymer matrix material.

2. The method of claim 1 , wherein the reactive functional groups include anhydrides, epoxides, silsesquixoanes, carboxyl groups, or any combination thereof.

3. The method of claim 1 , further comprising the step of forming nanoperforations through the LAG sheet before the step of embedding.

4. The method of claim 3 , wherein the functional groups are attached to carbon atoms of the LAG sheet located along edges of the nanoperforations.

5. The method of claim 1 , further comprising the step of embedding long or continuous fiber reinforcements in the polymeric matrix material.

6. The method of claim 1 , wherein the polymer matrix material is a curable material and the method further comprises the steps of curing the polymer matrix material and simultaneously forming the covalent bonds between the LAG sheet and the polymer matrix material.

7. The method of claim 1 , wherein the polymer matrix material is a thermoplastic material and the method further comprises the steps of heating and consolidating the polymer matrix material and simultaneously forming the covalent bonds between the LAG sheet and the polymer matrix.

8. The method of claim 1 , wherein the step of embedding comprises the steps of infiltrating the LAG sheet with a monomer and polymerizing the monomer to form the polymer matrix material, wherein the covalent bonds are formed between the LAG sheet and the polymer matrix material during polymerization.

9. A method of making a composite panel, comprising the step of embedding a large area graphene (LAG) sheet in a layer of material comprising a polymeric matrix material such that the polymer matrix material is present at both opposite faces of the LAG sheet.

10. The method of claim 9 , wherein the LAG sheet includes nanoperforations.

11. The method of claim 10 , wherein the LAG sheet has functional groups attached to carbon atoms of the LAG sheet located along edges of the nanoperforations.

12. The method of claim 9 , wherein covalent bonds are formed between the LAG sheet and the polymer matrix material.

13. The method of claim 12 , wherein the LAG sheet includes nanoperforations.

14. The method of claim 13 , wherein at least some of the covalent bonds between the LAG sheet and the polymer matrix material are located along edges of the nanoperforations.

15. The method of claim 12 , wherein the polymer matrix material is a curable material and the method further comprises the steps of curing the polymer matrix material and simultaneously forming the covalent bonds between the LAG sheet and the polymer matrix material.

16. The method of claim 12 , wherein the polymer matrix material is a thermoplastic material and the method further comprises the steps of heating and consolidating the polymer matrix material and simultaneously forming the covalent bonds between the LAG sheet and the polymer matrix.

17. The method of claim 12 , wherein the step of embedding comprises the steps of infiltrating the LAG sheet with a monomer and polymerizing the monomer to form the polymer matrix material, wherein the covalent bonds are formed between the LAG sheet and the polymer matrix material during polymerization.

18. The method of claim 12 , wherein the LAG sheet is functionalized with reactive functional groups before the step of embedding so that the polymer matrix material reacts with at least some of the reactive functional groups to form the covalent bonds between the LAG sheet and the polymer matrix material.

19. The method of claim 18 , wherein the reactive functional groups include anhydrides, epoxides, silsesquixoanes, carboxyl groups, or any combination thereof.

20. The method of claim 9 , further comprising the step of embedding long or continuous fiber reinforcements in the polymeric matrix material.

Assignees

• Lockheed Corp

Inventors

• Bullock Steven Edward
• Newell Clinton M

Classifications

• B32B37/0076

  characterised in that the layers are not bonded on the totality of their surfaces · CPC title

• B32B37/146

  whereby one or more of the layers is a honeycomb structure · CPC title

• C08K3/04 Primary

  Carbon · CPC title

• B32B3/20 Primary

  of hollow pieces, e.g. tubes; of pieces with channels or cavities · CPC title

• B32B2305/77

  Uncured, e.g. green · CPC title