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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|