首页> 外国专利> Rocket booster casings made with semipreg having a thermoplastic toughened novolac-based epoxy resin matrix

Rocket booster casings made with semipreg having a thermoplastic toughened novolac-based epoxy resin matrix

机译:用半预浸料制成的火箭增力器壳体,具有热塑性增韧的酚醛清漆基环氧树脂基体

摘要

A semipreg that can be cured/molded to form aerospace composite parts including rocket booster casings. The semipreg includes a fibrous layer and a resin layer located on one side of the fibrous layer. The resin layer includes an epoxy component that is a combination of a hydrocarbon epoxy novolac resin and a trifunctional epoxy resin and optionally a tetrafunctional epoxy resin. The resin matrix includes polyethersulfone as a toughening agent and a thermoplastic particle component.
机译:一种半固化片,可以固化/成型以形成包括火箭助推器壳体在内的航空航天复合材料零件。该半固化片包括纤维层和位于纤维层的一侧上的树脂层。树脂层包括环氧组分,该环氧组分是烃环氧线型酚醛清漆树脂和三官能环氧树脂和任选的四官能环氧树脂的组合。树脂基体包括作为增韧剂的聚醚砜和热塑性颗粒组分。

著录项

  • 公开/公告号US10787997B1

    专利类型

  • 公开/公告日2020-09-29

    原文格式PDF

  • 申请/专利权人 HEXCEL CORPORATION;

    申请/专利号US201916592589

  • 申请日2019-10-03

  • 分类号F02K9/34;B29C70/50;B29B15/12;C08L63/04;C08L77/06;C08L79/08;

  • 国家 US

  • 入库时间 2022-08-21 11:29:41

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