| 发明名称 |
Panel-Insert Assembly and Method |
| 摘要 |
A panel-insert assembly including a panel having a core and a skin layer positioned over the core, wherein the skin layer defines an opening therein, and an insert positioned below the skin layer, wherein the insert is aligned with the opening. |
| 申请公布号 |
US2016368242(A1) |
申请公布日期 |
2016.12.22 |
| 申请号 |
US201615251195 |
申请日期 |
2016.08.30 |
| 申请人 |
THE BOEING COMPANY |
发明人 |
LEWIS MICHAEL S.;SAKURAI JESSICA;REEVES BRAD J. |
| 分类号 |
B32B7/08;B32B3/12;F16B5/01;B64C1/06;F16B21/02;F16B37/12;B64F5/00;B32B3/26;F16B5/02 |
主分类号 |
B32B7/08 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method for connecting an insert to a panel, said panel comprising a core and a skin layer, said method comprising:
forming an opening in said skin layer; inserting said insert through said opening such that said insert is positioned below said skin layer; and rotating said threaded insert relative to said opening. |
| 地址 |
CHICAGO IL US |
