发明名称 |
Repair apparatus and method for composite panels having a conductive layer |
摘要 |
A repair apparatus for an electrically conductive layer of a composite structure includes a dielectric layer, having a perimeter, secured to the structure, and a conductive layer, secured over the dielectric layer and to the structure around an entirety of the perimeter of the dielectric layer, the conductive layer being treated along a perimeter region thereof to improve a conductive path between the conductive layer and the structure. |
申请公布号 |
US9481157(B2) |
申请公布日期 |
2016.11.01 |
申请号 |
US201414199615 |
申请日期 |
2014.03.06 |
申请人 |
THE BOEING COMPANY |
发明人 |
Ackerman Patrice K;Anderson Weston K;Heeter Russell J |
分类号 |
B32B37/12;B32B37/18;B32B37/00;B32B38/00;B29C73/10;B64D45/02;B64F5/00;B29L31/30 |
主分类号 |
B32B37/12 |
代理机构 |
Parsons Behle & Latimer |
代理人 |
Parsons Behle & Latimer |
主权项 |
1. A method for temporarily repairing a conductive composite panel having a damaged area near a metal fastener, comprising:
preparing a surface of the panel in the region of the damaged area and the fastener; affixing a dielectric material to the panel with an adhesive, the dielectric material covering the damaged area and the fastener; providing an adhesive on a conductive patch; scoring the adhesive along a perimeter region of the adhesive on the conductive patch; affixing the conductive patch to the dielectric material and the panel with the adhesive, the conductive patch entirely covering the dielectric material and defining a perimeter region in contact with the panel; and wherein scoring the adhesive increases an electrical conductivity between the panel and the conductive patch. |
地址 |
Chicago IL US |