发明名称 COMPOSITE JOINT OPTIMIZATION
摘要 A method including receiving a joint parameter for a joint between at least two composite structural components, a ply stackup for each of the at least two composite structural components and an electromagnetic effect parameter in a controller, iteratively processing with the controller, the joint parameter and the ply stackup and outputting an optimized joint parameter based on at least a convergence of an electromagnetic effect resistance of the joint and the at least two composite structural components, and changing, with the controller, a value of one or more of the joint parameters and the ply stackup during the iterative processing to reach the convergence of the electromagnetic effect resistance.
申请公布号 EP3124386(A1) 申请公布日期 2017.02.01
申请号 EP20160180526 申请日期 2016.07.21
申请人 The Boeing Company 发明人 KHOSRAVANI, Shahriar;NAKHJAVANI, Omid B;BELL, Vincent;TENNYSON, Laine;DABIRI, Farhad
分类号 B64D45/02;B29C65/00;B29C65/56;B29C65/82;B64F5/00;G06F17/11;G06F17/50 主分类号 B64D45/02
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