Epoxy resin formulations and processes for producing aerospace-grade composites via low temperature, isothermal infusion
US-2024376278-A1 · Nov 14, 2024 · US
US10450432B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10450432-B2 |
| Application number | US-201715729189-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 10, 2017 |
| Priority date | Feb 24, 2012 |
| Publication date | Oct 22, 2019 |
| Grant date | Oct 22, 2019 |
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 polybutadiene graft copolymer with a solvent to form a solution; wetting a plurality of tows of a carbon fiber or a fabric of the carbon fiber with the solution; fabricating prepregs from the wetted tows or fabric in a prepreg machine; and laying up fabricated prepregs and process in a vacuum press to produce the composite, wherein the composite exhibits an average fiber volume fraction (FVF) of greater than 60%. 2. The method of claim 1 , wherein the fabricating step comprises: 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 60minutes under full vacuum; increasing the temperature in the vacuum press to about 225° C. at about 2 ° C. per minute under full vacuum and holding at about 225° C. for about 60 minutes under full vacuum and about 1.7MPa compaction pressure; and cooling the vacuum press to about 25° C. at about 2 ° C. per minute under full vacuum. 3. The method of claim 1 , wherein the polybutadiene graft copolymer comprises poly(butadiene)-graft-poly(methyl acrylate-co-acrylonitrile). 4. The method of claim 1 , wherein the composite exhibits an average void volume fraction (VVF) of less than 2%.
grafted on to rubbers · CPC title
Elements · 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
Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.