Composite material suitable for aircraft interiors

B - Operations – Transporting – 32 – B

Patent

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Details

B32B 9/00 (2006.01) C08J 5/04 (2006.01) C08J 5/06 (2006.01) C08J 5/24 (2006.01)

Patent

CA 2288186

A fiber reinforced prepreg is provided comprising a carbon paper substrate and a thermoset resin with flame retardant components, the prepreg being particularly useful in the fabrication of aircraft interiors. The substrate may contain PAN carbon fibers and an alcohol binder. The resin may comprise between about 50 % to 80 % of the prepreg.

La présente invention concerne un pré-imprégné renforcé de fibres et comprenant un substrat de papier carbone et une résine thermodurciçable à composants ignifuges, le pré-imprégné étant particulièrememt utilisé dans la fabrication d'intérieurs d'aéronefs. Le substrat peut contenir des fibres de carbone de polyacrylonitrile et un liant alcool. La résine peut comprendre entre 50 % et 80 % environ de pré-imprégné.

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