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 US2013330503(A1) 申请公布日期 2013.12.12
申请号 US201213491784 申请日期 2012.06.08
申请人 KISMARTON MAX U.;THE BOEING COMPANY 发明人 KISMARTON MAX U.
分类号 B32B5/12;B32B37/00 主分类号 B32B5/12
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