PREPREG

The invention aims to provide a prepreg having high storage stability and serving suitably for producing components, such as structural members and interior members of aircraft and structural members of aircraft engines, that require high heat resistance under high temperature, high humidity conditi...

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Hauptverfasser: SUGIMOTO, Atsuki, ARAI, Atsuhito, WATARI, Ryohei
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Sprache:eng ; fre ; ger
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creator SUGIMOTO, Atsuki
ARAI, Atsuhito
WATARI, Ryohei
description The invention aims to provide a prepreg having high storage stability and serving suitably for producing components, such as structural members and interior members of aircraft and structural members of aircraft engines, that require high heat resistance under high temperature, high humidity conditions, good physical properties, and good combustion properties. The prepreg is produced by impregnating the component [A] specified below with an epoxy resin composition containing the components [B] to [D] specified below, wherein the component [A] in the prepreg accounts for 50 mass% or more: [A] carbon fiber, [B] epoxy resin, [C] fluorene type curing agent having a maximum particle size of 100 µm or less, and [D] thermoplastic resin.
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language eng ; fre ; ger
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subjects AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F,C08G
CHEMISTRY
COMPOSITIONS BASED THEREON
COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
GENERAL PROCESSES OF COMPOUNDING
METALLURGY
ORGANIC MACROMOLECULAR COMPOUNDS
THEIR PREPARATION OR CHEMICAL WORKING-UP
USE OF INORGANIC OR NON-MACROMOLECULAR ORGANIC SUBSTANCES ASCOMPOUNDING INGREDIENTS
WORKING-UP
title PREPREG
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