| 发明名称 |
Optimized Cross-Ply Orientation in Composite Laminates |
| 摘要 |
A composite laminate has a primary axis of loading and comprises a plurality resin plies each reinforced with unidirectional fibers. The laminate includes cross-plies with fiber orientations optimized to resist bending and torsional loads along the primary axis of loading. |
| 申请公布号 |
US2016200054(A1) |
申请公布日期 |
2016.07.14 |
| 申请号 |
US201615076405 |
申请日期 |
2016.03.21 |
| 申请人 |
The Boeing Company |
发明人 |
Kismarton Max U. |
| 分类号 |
B29C70/20;B29C70/30 |
主分类号 |
B29C70/20 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of laying up a composite aircraft skin having a primary axis of loading, comprising:
laying up cross-plies of resin reinforced with unidirectional fibers, including orienting the cross-plies at angles that vary along the primary axis of loading. |
| 地址 |
Chicago IL US |
