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Method of forming composite prepreg articles utilizing heat- shrinkable braided sleeves

机译:利用热缩编织套管形成复合预浸料制品的方法

摘要

A method of forming composite prepreg articles. Prepreg plies (12) are laid up over a breakable mandrel (10), the mandrel having a configuration substantially matching the desired configuration of the composite prepreg article and being pre-coated to prevent the prepreg from sticking to it. A release film (14) is applied over the prepreg. A heat-shrinkable braided sleeve (16) is placed over the prepreg and release film and secured to the mandrel, thereby creating an assembly (28) . The prepreg is first compacted by encapsulating the assembly and applying a vacuum, and is then substantially cured by exposing the assembly to heat. After curing, the braided sleeve and release film are removed. The cured prepreg, which serves as the desired composite prepreg article, is separated from the mandrel by breaking the mandrel.
机译:一种形成复合预浸料制品的方法。预浸料帘布层(12)被放置在易碎的心轴(10)上,该心轴具有与复合预浸料制品的所需结构基本匹配的结构并且被预涂覆以防止预浸料粘结到其上。在预浸料上施加离型膜(14)。将可热收缩的编织套筒(16)放置在预浸料和释放膜上并固定至心轴,从而形成组件(28)。预浸料坯首先通过封装组件并施加真空进行压实,然后通过将组件暴露于热中而基本上固化。固化后,将编织套管和离型膜除去。通过破坏心轴将用作期望的复合预浸料制品的固化的预浸料与心轴分离。

著录项

  • 公开/公告号US5076871A

    专利类型

  • 公开/公告日1991-12-31

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US19900463435

  • 发明设计人 BRADLEY A. FRYE;MARCIA R. RILEY;

    申请日1990-01-11

  • 分类号B32B31/00;

  • 国家 US

  • 入库时间 2022-08-22 05:23:33

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