发明名称 Composite beam chord between reinforcement plates
摘要 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.
申请公布号 US8201371(B2) 申请公布日期 2012.06.19
申请号 US20100777250 申请日期 2010.05.10
申请人 THE BOEING COMPANY 发明人 KISMARTON MAX U.
分类号 E04C1/00 主分类号 E04C1/00
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