| 发明名称 |
METHOD OF FORMING A COMPOSITE STRUCTURE |
| 摘要 |
A method of forming a sandwich composite structure by placing a core under a compressive force or a tensile force and applying a first layer to a first surface of the core. The core and first layer are then heated. The compressive or tensile force is then released, allowing the composite structure to take shape. |
| 申请公布号 |
US2016375668(A1) |
申请公布日期 |
2016.12.29 |
| 申请号 |
US201514704164 |
申请日期 |
2015.05.05 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
Bremmer Jonathan;Lacko Robert A.;Sauer Jeffrey G.;Toni Darryl Mark |
| 分类号 |
B32B37/06;B32B38/00 |
主分类号 |
B32B37/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of forming a sandwich composite structure, comprising:
placing a core under a compressive force or a tensile force; applying a first layer to a first surface of the core; heating the core and the first layer; and releasing the compressive force or the tensile force. |
| 地址 |
Stratford CT US |
