发明名称 |
COMPOSITE BEAM CHORD BETWEEN REINFORCEMENT PLATES AND RELATED METHOD OF MANUFACTURING |
摘要 |
<p>A composite beam chord (7) is between first and second reinforcement plates (8, 9). The beam chord (7) includes a first ply of reinforcing fibers with a fiber orientation of +a (degrees with respect to a longitudinal axis of the beam chord (7) and a second ply of reinforcing fibers with a fiber orientation of - a degrees with respect to the longitudinal axis. The angle a is between 2 and 12 degrees for suppression or delay of ply splitting.</p> |
申请公布号 |
WO2011142920(A1) |
申请公布日期 |
2011.11.17 |
申请号 |
WO2011US31985 |
申请日期 |
2011.04.11 |
申请人 |
THE BOEING COMPANY;KISMARTON, MAX, U. |
发明人 |
KISMARTON, MAX, U. |
分类号 |
B29C70/20;B29C65/00;B29C65/08;B29C65/56;B29C65/72;B29C70/54;B32B5/12 |
主分类号 |
B29C70/20 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|