公开(公告)号：US11220064B2

公开(公告)日：2022-01-11

申请号：US16132311

申请日：2018-09-14

申请人： The Boeing Company

发明人： Marc R. Matsen ,  Bret Alan McGinness Voss ,  Vincent C. Ku ,  Christopher J. Hottes

IPC分类号： B29C65/36 ,  B29C65/00 ,  B64C1/12 ,  B64C25/16 ,  B32B37/14 ,  B64C1/00 ,  B29L31/30

摘要： A composite sandwich panel includes a first composite part and a second composite part. A plurality of stiffeners extend between the first and second composite parts. A fiberglass composite perimeter edge closeout is positioned along one or more edges of the first and second composite parts. The fiberglass composite perimeter edge closeout controls a magnetic flux to bond the first and second composite parts to the plurality of stiffeners.

公开(公告)号：US20200086582A1

公开(公告)日：2020-03-19

申请号：US16132311

申请日：2018-09-14

申请人： The Boeing Company

发明人： Marc R. Matsen ,  Bret Alan McGinness Voss ,  Vincent C. Ku ,  Christopher J. Hottes

IPC分类号： B29C65/36 ,  B29C65/00 ,  B64C1/12 ,  B64C25/16

摘要： A composite sandwich panel includes a first composite part and a second composite part. A plurality of stiffeners extend between the first and second composite parts. A fiberglass composite perimeter edge closeout is positioned along one or more edges of the first and second composite parts. The fiberglass composite perimeter edge closeout controls a magnetic flux to bond the first and second composite parts to the plurality of stiffeners.