发明名称 |
Method for molding structures |
摘要 |
A method for molding composite structures whereby a material stack including a core having first and second opposing sides is prepared. The preparing of the material stack includes applying a fibrous support layer on at least one of the first side and the second side of the core section, applying an adhesive layer on the support layer, and applying a thermoplastic barrier layer on the adhesive layer. The method also includes preparing a resin and a mold; placing the material stack in the mold; sealing the core; infusing the mold and material stack with resin; curing the structure; and removing the structure from the mold. In one embodiment, the method creates a composite aircraft wing panel.
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申请公布号 |
US7226559(B2) |
申请公布日期 |
2007.06.05 |
申请号 |
US20010000148 |
申请日期 |
2001.12.04 |
申请人 |
TOYOTA MOTOR SALES, U.S.A., INC. |
发明人 |
MAXWELL MICHAEL K.;GARDINER RICHARD J. |
分类号 |
B29C70/48;B29C70/08;B29C70/44;B32B3/12 |
主分类号 |
B29C70/48 |
代理机构 |
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代理人 |
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地址 |
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