发明名称 OPTIMIZED CROSS-PLY ORIENTATION IN COMPOSITE LAMINATES
摘要 A composite laminate has a primary axis of loading and comprises a plurality resin plies each reinforced with unidirectional fibers. The laminate includes cross-plies with fiber orientations optimized to resist bending and torsional loads along the primary axis of loading.
申请公布号 CA2814894(A1) 申请公布日期 2013.12.08
申请号 CA20132814894 申请日期 2013.05.02
申请人 THE BOEING COMPANY 发明人 KISMARTON, MAX U.
分类号 B32B5/12;B32B27/04;B32B37/00 主分类号 B32B5/12
代理机构 代理人
主权项
地址