发明名称 スパイラル積層構造の円錐及び製造方法
摘要 A cone-shaped composite article may include an inner sublaminate containing at least four unidirectional plies having an inner stacking sequence with fiber angles of 0, 90, -45, and +45 degrees such that the inner laminate has a quasi-isotropic layup pattern at any location on the inner laminate. The cone-shaped composite article may also include an outer sublaminate containing at least four unidirectional plies having an outer stacking sequence that is a mirror image of the inner stacking sequence. Each one of the unidirectional plies may be continuous along a ply arclength wrapping 360 degrees around the cone-shaped composite article and may have opposing ply ends terminating at a ply seam.
申请公布号 JP6038057(B2) 申请公布日期 2016.12.07
申请号 JP20140023024 申请日期 2014.02.10
申请人 ザ・ボーイング・カンパニーThe Boeing Company 发明人 アストン, リチャード ダブリュ.;コープ, ブレット ティー.;ストリート, アンドリュー アール.
分类号 B32B1/00;B29C70/06;B29C70/10;B29C70/30;B32B5/26;B32B5/28;B64G1/00 主分类号 B32B1/00
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