申请人:Toray Industries, Inc.
公开号:EP3842481A1
公开(公告)日:2021-06-30
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.
本发明的目的是提供一种具有高储存稳定性的预浸料,该预浸料适用于生产要求在高温、高湿条件下具有高耐热性、良好物理性能和良好燃烧性能的部件,如飞机的结构件和内部构件以及飞机发动机的结构件。该预浸料是通过将下述组分[A]与含有下述组分[B]至[D]的环氧树脂组合物浸渍而制成的,其中预浸料中的组分[A]占 50% 或以上:[A]碳纤维,[B]环氧树脂,[C]最大粒径不超过 100 微米的芴类固化剂,以及[D]热塑性树脂。