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Process method to repair bismaleimide (BMI) composite structures

机译:修复双马来酰亚胺复合结构的方法

摘要

A method for repairing a damaged area, referred to as the repair area, of a composite structure comprises steps of: making alignment markings on the repair area; fabricating a pair of alignment templates; preparing the repair area for a hot bonded, vacuum bagged repair; assembling a repair patch; consolidating the repair patch; heating the repair patch; transferring and aligning the repair patch to the repair area; vacuum bagging, heating, and cooling the repair patch for a partial cure at the repair area; heating and cooling the repair patch in an oven; and bonding the repair patch to the repair area.
机译:一种修复复合结构损坏区域的方法,该方法包括以下步骤:在修复区域上做对准标记;制作一对对准模板;为热粘合真空包装的维修准备维修区域;组装维修补丁;巩固修复补丁;加热修补片;将修复补丁转移并对准修复区域;真空袋装,加热和冷却修补片,以在修补区域部分固化;在烤箱中加热和冷却维修贴片;并将修补程序粘贴到修补区域。

著录项

  • 公开/公告号US6761783B2

    专利类型

  • 公开/公告日2004-07-13

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US20020119562

  • 发明设计人 WESLEY S. OWEN;RUSSELL L. KELLER;

    申请日2002-04-09

  • 分类号B32B350/00;

  • 国家 US

  • 入库时间 2022-08-21 23:19:00

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