首页> 外国专利> Verifiable quick patch repair for composite structures

Verifiable quick patch repair for composite structures

机译:可验证的快速修补复合结构

摘要

A method for patching a hole in a composite parent structure. The method comprises: inserting an insert in the hole; placing a composite patch having a multiplicity of curved flexible members on one side of the composite parent structure in a position where a central portion of the composite patch overlies the insert and the flexible members confront opposing portions of the composite parent structure providing adhesive between the composite patch, the insert, and the composite parent structure; pressing the composite patch against the composite parent structure with sufficient pressure to force the flexible members to conform to the shape of the composite parent structure; and while the flexible members are in a stressed state, curing the adhesive in a manner that causes the flexible members to bond to the parent structure.
机译:一种修补复合父结构中的孔的方法。该方法包括:将插入物插入孔中;以及将插入物插入孔中。将具有多个弯曲挠性构件的复合补片放置在复合母体结构的一侧上的位置,在该位置,复合补片的中央部分覆盖插入物,并且挠性构件面对复合母体结构的相对部分,从而在复合体之间提供粘合剂补丁,插入和复合父结构;用足够的压力将复合贴片压在复合母体结构上,以迫使柔性构件与复合母体结构的形状相符。当柔性构件处于受压状态时,以使柔性构件粘结到母体结构的方式固化粘合剂。

著录项

  • 公开/公告号US10307977B2

    专利类型

  • 公开/公告日2019-06-04

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201615059321

  • 发明设计人 GARY E. GEORGESON;KENNETH H. GRIESS;

    申请日2016-03-03

  • 分类号B29C65;B29C65/02;B32B37;B32B38;B32B7/08;B29C73;B32B43;B29D7;B32B38/18;B32B3/26;B23P6;B29C73/14;B32B7/12;B32B37/10;B32B37/12;B32B27/08;B29K105/08;B29K105;B29L31/30;

  • 国家 US

  • 入库时间 2022-08-21 12:12:59

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号