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Method for in-place fabrication of graphite epoxy bushings in graphite epoxy structures

机译:在石墨环氧结构中就地制造石墨环氧套管的方法

摘要

A method of forming a bushing in a graphite/epoxy structure in order to repair holes that are either too large or out-of-round. A mandrel having a diameter that is smaller than the desired hole diameter is wrapped with a strip of epoxy-impregnated graphite mat until the mandrel and mat tightly fit into the hole in the graphite/epoxy structure. The mandrel is then heated causing the mandrel to both expand and cure the epoxy resin in the mat. Expansion of the mandrel forces the mat against the edge of the hole to promote bonding between the mat and the graphite/epoxy structure. After the mat has cured, the mandrel is cooled thereby causing it to contract away from the mat so that it can be easily removed. Finally, the mat is trimmed to the thickness of the graphite/epoxy structure and a hole having the desired diameter is then machined in the mat.
机译:一种在石墨/环氧树脂结构中形成衬套的方法,以修复太大或不圆的孔。将直径小于所需孔直径的心轴用环氧树脂浸渍的石墨毡条包裹,直到心轴和毡紧密配合到石墨/环氧结构的孔中。然后加热心轴,使心轴膨胀并固化垫中的环氧树脂。心轴的膨胀迫使垫子抵靠孔的边缘,以促进垫子与石墨/环氧树脂结构之间的结合。在垫子固化之后,将心轴冷却,从而使其收缩而远离垫子,从而可以轻松地将其移除。最后,将垫子修整至石墨/环氧结构的厚度,然后在垫子中加工出具有所需直径的孔。

著录项

  • 公开/公告号US4867822A

    专利类型

  • 公开/公告日1989-09-19

    原文格式PDF

  • 申请/专利权人 THE BOEING CORPORATION;

    申请/专利号US19870081669

  • 发明设计人 ENGBERT T. BANNINK JR.;

    申请日1987-08-04

  • 分类号B32B31/16;

  • 国家 US

  • 入库时间 2022-08-22 06:27:25

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