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