| 发明名称 |
Stiffened composite panels |
| 摘要 |
A stiffened panel comprises a composite panel, and a stiffener including a base flange on the composite panel. The base flange is tapered towards the panel. The stiffened panel further comprises a composite overwrap layer on only the composite panel and a tapered surface of the base flange. |
| 申请公布号 |
US2016176500(A1) |
申请公布日期 |
2016.06.23 |
| 申请号 |
US201314902850 |
申请日期 |
2013.08.09 |
| 申请人 |
THE BOEING COMPANY |
发明人 |
Ross Joshua Amory;Cuda Shane Frank;McLaughlin Mark Ronald;Rush Michael Robert;Farr Colin Lee;Smith David Bruce;Desai Nihar Ashokkumar;Kennedy Thomas Joseph;Deobald Lyle Ray |
| 分类号 |
B64C3/26;B64C3/18;B29D99/00 |
主分类号 |
B64C3/26 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A stiffened panel comprising:
a composite panel; a stiffener including a base flange on the composite panel, the base flange tapered towards the panel; and a composite overwrap layer on only the composite panel and a tapered surface of the base flange. |
| 地址 |
Chicago IL US |
