| 发明名称 |
Method of sealing core material |
| 摘要 |
A molded composite structure and a method of manufacturing a molded composite structure are disclosed. In one embodiment, an aircraft wing panel and a method for manufacturing an aircraft wing panel are disclosed. In another embodiment, the method of manufacturing a molded composite structure uses a resin transfer molding process.
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| 申请公布号 |
US2007207323(A1) |
申请公布日期 |
2007.09.06 |
| 申请号 |
US20070790997 |
申请日期 |
2007.04.30 |
| 申请人 |
TOYOTA MOTOR SALES, U.S.A., INC. |
发明人 |
MAXWELL MICHAEL K.;GARDINER RICHARD J. |
| 分类号 |
B32B9/04;A45C5/02;A45C5/06;A45C5/14;A45C13/02;A45C13/36;A63B55/00;B29C65/00 |
主分类号 |
B32B9/04 |
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