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 +&alpha; degrees with respect to a longitudinal axis of the beam chord and a second ply of reinforcing fibers with a fiber orientation of &minus;&alpha; degrees with respect to the longitudinal axis. The angle &alpha; 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
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