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