Hybrid multifunctional composite material and method of making the same
US-2018111338-A1 · Apr 26, 2018 · US
US11365705B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11365705-B2 |
| Application number | US-201816170966-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 25, 2018 |
| Priority date | Oct 25, 2018 |
| Publication date | Jun 21, 2022 |
| Grant date | Jun 21, 2022 |
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Disclosed are laminates comprising a carbon fiber reinforced polymer sheet and a layer of polysilazane and methods for producing such laminates.
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What is claimed is: 1. A laminate comprising a sheet of carbon fiber reinforced polymer (CFRP), the sheet having a first side and a second side opposite the first side and at least one of the first side and the second side of the sheet is in electrical communication with a metal cellular core or a metal alloy cellular core; and a layer of polysilazane covering one or both of the first side and the second side of the sheet of CFRP, wherein the sheet of CFRP contains multiple perforations and at least one of the perforations extends entirely through the sheet, wherein the perforations include sidewalls and the sidewalls of the perforations are coated with polysilazane. 2. A laminate according to claim 1 , wherein the perforations have a diameter of from about 0.75 (0.03 in) to about 1.5 mm (0.06 in). 3. A laminate according to claim 2 , wherein the layer of polysilazane has a thickness of from about 1-10 μm. 4. A laminate according to claim 3 , wherein the perforations cover from about 5-20% of the first side of the sheet. 5. A laminate according to claim 4 , wherein the polysilazane is an inorganic polysilazane, an organic polysilazane, or a mixture thereof. 6. A laminate according to claim 5 , wherein the sheet of CFRP comprises exposed carbon fibers. 7. A laminate according to claim 6 , wherein the metal cellular core comprises aluminum. 8. A laminate according to claim 1 , wherein the sheet of CFRP comprises exposed carbon fibers. 9. A aircraft engine thrust reverser comprising a laminate according to claim 1 . 10. An aircraft engine thrust reverser according to claim 9 , wherein the metal cellular core comprises aluminum. 11. An aircraft engine thrust reverser according to claim 9 , wherein the perforations have a diameter of from about 0.75 (0.03 in) to about 1.5 mm (0.06 in). 12. An aircraft engine thrust reverser according to claim 11 , wherein the layer of polysilazane has a thickness of from about 1-10 μm. 13. A structure comprising a sheet of carbon fiber reinforced polymer (CFRP) coated with a discrete layer of a polysilazane, the sheet having a first side and a second side opposite the first side; a metal cellular core or a metal alloy cellular core in electrical communication with at least one of the first side and the second side of the sheet; and wherein the layer of polysilazane covers one or both of the first side and the second side of the sheet of CFRP, wherein the sheet of CFRP contains multiple perforations and at least one of the perforations extends entirely through the sheet, wherein the perforations include sidewalls and the sidewalls of the perforations are coated with polysilazane. 14. A structure according to claim 13 , wherein the perforations have a diameter of from about 0.75 (0.03 in) to about 1.5 mm (0.06 in). 15. A structure according to claim 14 , wherein the layer of polysilazane has a thickness of from about 1-10 μm. 16. A structure according to claim 15 , wherein the perforations cover from about 5-20% of the first side of the sheet. 17. A structure according to claim 16 , wherein the sheet of CFRP comprises exposed carbon fibers. 18. A structure according to claim 17 , wherein the metal cellular core or metal alloy cellular core comprises aluminum. 19. A structure according to claim 13 , wherein the perforations have a diameter of from about 1 mm (0.04 in) to about 1.25 mm (0.05 in). 20. A structure according to claim 14 , wherein the layer of polysilazane has a thickness of from about 2-3 μm.
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