发明名称 複合材積層板の屈曲繊維経路の設計
摘要 A computational optimization process uses the variable stiffness performance of composite laminates attributed to steered fiber to guide the design of stream functions describing the fibers to build it. This design process combines a finite element-based analysis tool, failure criteria and geometry optimization to determine steered angles associated with stream functions by an optimization program to meet target performance requirements, e.g., load condition(s), and failure criteria for quasi-static or dynamic events. The fiber angle distribution and thickness buildup are computed based on the stream function. The simulated structure is analyzed using finite element analysis. The disclosed process allows the designer to impose manufacturing constraints such as fiber steering radius.
申请公布号 JP5972062(B2) 申请公布日期 2016.08.17
申请号 JP20120137776 申请日期 2012.06.19
申请人 ザ・ボーイング・カンパニーThe Boeing Company 发明人 ラサイアン, モスタファ;グリムショウ, マシュー トッド;グランディーン, トーマス エー.;パターソン, マシュー スティーブン
分类号 G06F17/50 主分类号 G06F17/50
代理机构 代理人
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