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The adhesive patch having a tapered structural joint design 发明申请

2023-07-24 3190 249K 0

专利信息

申请日期 2025-06-29 申请号 JP2016564577
公开(公告)号 JP2017515703A 公开(公告)日 2017-06-15
公开国别 JP 申请人省市代码 全国
申请人 The Boeing Company
简介 A method and apparatus for reworking a composite structure. A composite rework patch system comprises a composite rework patch and a plurality of adhesive layers. The composite rework patch includes a first side having a contour conforming to an inconsistent area on the composite structure. The composite re patch comprises a plurality of regions having different structural properties. The plurality of adhesive layers is on the first side of the composite rework patch. The plurality of adhesive layers change in thickness within at least one region of the composite rework patch to form tapered adhesive sections.


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