发明名称 |
Puncture-healing thermoplastic resin carbon-fiber-reinforced composites |
摘要 |
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. |
申请公布号 |
US9156957(B2) |
申请公布日期 |
2015.10.13 |
申请号 |
US201313774422 |
申请日期 |
2013.02.22 |
申请人 |
The United States of America as represented by the Administrator of the National Aeronautics and Space Administration |
发明人 |
Gordon Keith L.;Siochi Emilie J.;Grimsley Brian W.;Cano Roberto J.;Czabaj Michael W. |
分类号 |
C08K3/04;C08L51/00;C08J5/04;B32B5/28;C08K7/06 |
主分类号 |
C08K3/04 |
代理机构 |
|
代理人 |
Riley Jennifer L. |
主权项 |
1. A composite comprising a combination of a self-healing polymer matrix and a carbon-fiber reinforcement, wherein the composite is fabricated from an intermediate prepreg material, wherein the composite does not comprise microcapsules containing a healing agent, nor hollow glass fibers containing a healing agent, and wherein the composite exhibits an average fiber volume fraction (FVF) of greater than 60%. |
地址 |
Washington DC US |