| 发明名称 |
Method for Forming Bends In Composite Panels and Composite Panels Made Thereby |
| 摘要 |
A composite panel with a bend therein is formed by first and second adjacent panel sections having a common facesheet forming an outer radius of the bend, and a substantially void-free joint between the adjacent panel sections.
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| 申请公布号 |
US2009110879(A1) |
申请公布日期 |
2009.04.30 |
| 申请号 |
US20080253957 |
申请日期 |
2008.10.18 |
| 申请人 |
THE BOEING COMPANY |
发明人 |
LEWIS MICHAEL S.;ROETS GUY W. |
| 分类号 |
B32B3/10;B26D1/00;B27N3/00;B32B1/04;B32B3/04 |
主分类号 |
B32B3/10 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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