Graphene-augmented composite materials
Composite materials are augmented with functionalized graphene having added amine groups, benzoxazine groups, imide groups, or a combination of amine groups and imide groups on a surface of the graphene, epoxide groups formed on at least one edge of the graphene and/or holes formed through the graphene. The functionalized graphene is integrated into a composite material as a supplement to or as a replacement for either the carbon reinforcement material or the resin matrix material to increase strength of the composite materials, and may be in the form of a functionalized graphene nanoplatelet, a flat graphene sheet or film, or a rolled or twisted graphene sheet or film.
1. A composite material comprising carbon reinforcement fibers and a matrix material, the matrix material comprising 0.1% to 100% by weight functionalized graphene nanoplatelets having imide groups formed on a surface of the graphene nanoplatelets.
2. The composite material of claim 1 , wherein the graphene nanoplatelets further comprise amine groups formed on the surface of the graphene nanoplatelets.
3. The composite material of claim 1 , wherein the graphene nanoplatelets further comprise holes formed through the graphene nanoplatelets.
4. The composite material of claim 3 , wherein the holes are substantially circular and have a diameter of 1-2 nanometers.
5. The composite material of claim 3 , wherein about 12-80 carbon atoms are removed from the graphene nanoplatelets to form each of the holes.
6. The composite material of claim 2 , wherein the imide groups and the amine groups on the surface of the graphene nanoplatelets have a surface density of about 4.0E10 to about 2.0E12 groups per square millimeter.
7. The composite material of claim 2 , wherein about 0.1% to about 5.0% of carbon atoms in the graphene nanoplatelets have imide groups or amine groups bonded thereto.
8. The composite material of claim 2 , wherein the matrix material comprises an aerospace-grade bismaleimide resin having 0.1% to 5.0% by weight functionalized graphene nanoplatelets.
9. The composite material of claim 8 , wherein the graphene nanoplatelets are present throughout bismaleimide resin and the bismaleimide resin is a macromolecular complex.
10. The composite material of claim 8 , wherein the graphene nanoplatelets form an interlayer between two layers of the bismaleimide resin, and the interlayer is a macromolecular complex of the bismaleimide resin.
11. The composite material of claim 2 , wherein the matrix material comprises 100% by weight functionalized graphene nanoplatelets, and the matrix material is a macromolecular complex of the graphene nanoplatelets.
12. An aircraft comprising composite structures made from the composite material of claim 1 .
13. A method of increasing strength of a composite material comprising carbon reinforcement fibers and a resin matrix material, the method comprising:
mixing functionalized graphene nanoplatelets into the resin matrix material to form a graphene-resin mixture, the functionalized graphene nanoplatelets having imide groups formed on a surface of the graphene nanoplatelets and epoxide groups formed on at least one edge of the graphene nanoplatelets;
combining the graphene-resin mixture with a plurality of the carbon reinforcement fibers to form a prepreg material; and
curing the prepreg material to form the composite material.
14. The method of claim 13 , wherein the graphene nanoplatelets further comprise amine groups formed on the surface of the graphene nanoplatelets.
15. The method of claim 14 , wherein graphene nanoplatelets have holes formed through the graphene nanoplatelets.
16. The method of claim 15 , wherein the holes are substantially circular and have a diameter of 1-2 nanometers.
17. The method of claim 15 , wherein about 12-80 carbon atoms are removed from the graphene nanoplatelets to form each of the holes.
18. The method of claim 14 , wherein the imide groups and the amine groups on the surface of the graphene nanoplatelets have a surface density of about 4.0E10 to about 2.0E12 groups per square millimeter.
19. The method of claim 14 , wherein about 0.1% to about 5.0% of carbon atoms in the graphene nanoplatelets have imide groups or amine groups bonded thereto.
20. The method of claim 14 , wherein the functionalized graphene nanoplatelets are mixed into the resin matrix material in an amount of 0.1% to 5.0% by weight of the graphene-resin mixture.
21. A method of increasing strength of a composite material comprising carbon reinforcement fibers and a resin matrix material, the method comprising:
combining the resin mixture with a plurality of the carbon reinforcement fibers to form a prepreg material;
depositing functionalized graphene nanoplatelets onto a top surface of the prepreg material to form a graphene interlayer, the functionalized graphene nanoplatelets having imide groups formed on a surface of the graphene nanoplatelets and epoxide groups formed on at least one edge of the graphene nanoplatelets;
laying a second prepreg material on top of the graphene interlayer; and
curing the prepreg material, the graphene interlayer and the second prepreg material to form the composite material.
22. The method of claim 21 , wherein the graphene nanoplatelets further comprise amine groups formed on the surface of the graphene nanoplatelets.
23. The method of claim 22 , wherein the graphene nanoplatelets further comprise holes formed through the graphene nanoplatelets.
24. The method of claim 23 , wherein the holes are substantially circular and have a diameter of 1-2 nanometers.
25. The method of claim 23 , wherein about 12-80 carbon atoms are removed from the graphene nanoplatelets to form each of the holes.
26. The method of claim 22 , wherein the imide groups and the amine groups on the surface of the graphene nanoplatelets have a surface density of about 4.0E10 to about 2.0E12 groups per square millimeter.
27. The method of claim 22 , wherein about 0.1% to about 5.0% of carbon atoms in the graphene nanoplatelets have imide groups or amine groups bonded thereto.
28. The method of claim 22 , wherein the prepreg material is cured to a cure state of 0.1.
29. A method of increasing strength of a composite material comprising carbon reinforcement fibers and a resin matrix material, the method comprising:
forming a bed of the carbon reinforcement fibers;
depositing functionalized graphene nanoplatelets through a top surface of the bed of the carbon reinforcement fibers to penetrate the entire bed of fibers and form a carbon fiber/graphene prepreg material, the functionalized graphene nanoplatelets having imide groups formed on a surface of the graphene nanoplatelets and epoxide groups formed on at least one edge of the graphene nanoplatelets; and
curing the carbon fiber/graphene prepreg material to form the composite material.
30. The method of claim 29 , wherein the graphene nanoplatelets further comprise amine groups formed on the surface of the graphene nanoplatelets.
31. The method of claim 30 , wherein the graphene nanoplatelets further comprise holes formed through the graphene nanoplatelets.
32. The method of claim 31 , wherein the holes are substantially circular and have a diameter of 1-2 nanometers.
33. The method of claim 31 , wherein about 12-80 carbon atoms are removed from the graphene nanoplatelets to form each of the holes.
34. The method of claim 32 , wherein the imide groups and amine groups on the surface of the graphene nanoplatelets have a surface density of about 4.0E10 to about 2.0E12 groups per square millimeter.
35. The method of claim 32 , wherein about 0.1% to about 5.0% of carbon atoms in the graphene nanoplatelets have imide groups or amine groups bonded thereto.
36. The method of claim 32 , wherein the prepreg material is cured to a cure state of 0.1.
37. The method of claim 32 , wherein the graphene nanoplatelets are rectangular in shape with sides having a length of 10 nanometers to 100 nanometers.
38. The composite material of claim 1 , wherein the graphene nanoplatelets are rectangular in shape with sides having a length of 10 nanometers to 100 nanometers.