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