发明名称 Hybrid structure and methods for forming the same
摘要 A method for forming a hybrid structure is provided. The method includes applying a sealant to a first component fabricated from a first material, coupling an isolation sheet to the sealant, and coupling a second component to the isolation sheet. The isolation sheet and the second component are fabricated from a second material that is different than the first material to facilitate preventing formation of a galvanic cell within the hybrid structure.
申请公布号 US9393761(B2) 申请公布日期 2016.07.19
申请号 US201313832181 申请日期 2013.03.15
申请人 The Boeing Company 发明人 Erickson Marcus Alexander
分类号 B29C65/00;B29C65/02;B32B37/00;B32B38/00;B32B7/08;B32B38/04;C09J7/00;B32B3/06;B32B3/10;B32B15/00;B32B17/06;B32B17/10;B32B37/16;B29C65/48;B29C65/56;B29C65/72;C23F13/10;B29L31/30;F16B33/00 主分类号 B29C65/00
代理机构 Armstrong Teasdale LLP 代理人 Armstrong Teasdale LLP
主权项 1. A method for forming a hybrid structure, said method comprising: applying a sealant to a first component fabricated from a first material; coupling an isolation sheet to the sealant, wherein the sealant has a thickness and covers a surface area of the first component such that the isolation sheet is separated from the first component; forming at least one bore hole through at least one of the isolation sheet, the sealant, and the first component; and coupling a second component to the isolation sheet with a fastener at the at least one bore hole, wherein the second component and the isolation sheet are both fabricated from a second material that is different than the first material to facilitate preventing formation of a galvanic cell within the hybrid structure.
地址 Chicago IL US