Epoxy resin formulations and processes for producing aerospace-grade composites via low temperature, isothermal infusion
US-2024376278-A1 · Nov 14, 2024 · US
US9783648B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9783648-B2 |
| Application number | US-201514881899-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 13, 2015 |
| Priority date | Feb 24, 2012 |
| Publication date | Oct 10, 2017 |
| Grant date | Oct 10, 2017 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A composite comprising a combination of a self-healing polymer matrix and a carbon fiber reinforcement is described. In one embodiment, the matrix is a polybutadiene graft copolymer matrix, such as polybutadiene graft copolymer comprising poly(butadiene)-graft-poly(methyl acrylate-co-acrylonitrile). A method of fabricating the composite is also described, comprising the steps of manufacturing a pre-impregnated unidirectional carbon fiber preform by wetting a plurality of carbon fibers with a solution, the solution comprising a self-healing polymer and a solvent, and curing the preform. A method of repairing a structure made from the composite of the invention is described. A novel prepreg material used to manufacture the composite of the invention is described.
Opening claim text (preview).
What is claimed is: 1. A method of fabricating a composite comprising the steps of: dissolving a self-healing polymer with a solvent to form a solution; manufacturing a pre-impregnated unidirectional carbon fiber preform by wetting a plurality of carbon fibers with the solution; and curing the preform with heat and pressure to form the composite. 2. The method of claim 1 , wherein the self-healing polymer comprises a polybutadiene graft copolymer. 3. The method of claim 2 , wherein the self-healing polymer comprises poly(butadiene)-graft-poly(methyl acrylate-co-acrylonitrile). 4. The method of claim 2 , wherein the solvent comprises N-methylpyrrolidone. 5. The method of claim 1 , wherein the curing step comprises processing the wetted fibers in a vacuum press. 6. The method of claim 5 , wherein the curing step comprises the steps of: increasing the temperature in the vacuum press from about 25° C. to about 150° C. at about 2° C. per minute under full vacuum and holding at about 150° C. for about 60 minutes under full vacuum; increasing the temperature in the vacuum press to about 225° C. at about 2 CC per minute under full vacuum and holding at about 225° C. for about 60 minutes under full vacuum and about 1.7 MPa compaction pressure; and cooling the vacuum press to about 25° C. at about 2° C. per minute under full vacuum. 7. The method of claim 6 , wherein the sell-healing polymer is a polybutadiene graft copolymer. 8. The method of claim 7 , wherein the self-healing polymer is poly(butadiene)-graft-poly(methyl acrylate-co-acrylonitrile). 9. The method of claim 6 , wherein the solvent is N-methylpyrrolidone.
Elements · CPC title
grafted on to rubbers · CPC title
with carbon fibres · CPC title
grafted on to homopolymers or copolymers of aliphatic hydrocarbons containing only one carbon-to-carbon double bond · CPC title
impregnated with or embedded in a plastic substance {(not used)} · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.