发明名称 Spiral laminated structural cone and manufacturing method
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 EP2767391(B1) 申请公布日期 2016.04.20
申请号 EP20140154613 申请日期 2014.02.11
申请人 THE BOEING COMPANY 发明人 ASTON, RICHARD W.;COPE, BRETT T.;STREETT, ANDREW R.
分类号 B32B5/02;B32B7/00;B64G1/10 主分类号 B32B5/02
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