发明名称 |
COMPOSITE BEAM CHORD BETWEEN REINFORCEMENT PLATES AND RELATED METHOD OF MANUFACTURING |
摘要 |
<p>A composite beam chord is between first and second reinforcement plates. The beam chord includes a first ply of reinforcing fibers with a fiber orientation of +α degrees with respect to a longitudinal axis of the beam chord and a second ply of reinforcing fibers with a fiber orientation of −α degrees with respect to the longitudinal axis. The angle α is between 2 and 12 degrees for suppression or delay of ply splitting.</p> |
申请公布号 |
EP2569144(A1) |
申请公布日期 |
2013.03.20 |
申请号 |
EP20110716714 |
申请日期 |
2011.04.11 |
申请人 |
THE BOEING COMPANY |
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 |
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代理人 |
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主权项 |
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地址 |
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