发明名称 |
METHOD OF MANUFACTURING A HOLLOW SECTION, GRID STIFFENED PANEL |
摘要 |
<p>A method of manufacturing a hollow section grid-stiffened panel comprises providing a tool ( 10 ) having a surface ( 12 ). The stiffened skin composite panel is preassembled comprising laminating a composite outer skin ( 14 ) on the surface, placing a separator outer layer ( 16 ) on the composite outer skin ( 14 ), and laminating a composite stiffener ( 20 ) on the mandrel ( 18 ), the mandrel being positioned on the separator layer ( 16 ), wherein the separator layer ( 16 ) separates the stiffener ( 20 ) and the mandrel ( 18 ) from the outer composite skin ( 14 ). The preassembled outer skin composite panel is cured on the tool. The separator layer ( 16 ) and mandrel ( 18 ) are removed from the preassembled stiffened skin composite panel. The stiffened skin composite panel is reassembled, comprising applying an adhesive between the composite outer skin ( 14 ) and the composite stiffener ( 20 ). The reassembled stiffener skin composite panel is cured on the tool to bond the stiffener skin to the outer skin.</p> |
申请公布号 |
EP1401658(A4) |
申请公布日期 |
2008.01.23 |
申请号 |
EP20020731292 |
申请日期 |
2002.04.04 |
申请人 |
GENERAL DYNAMICS ARMAMENT AND TECHNICAL PRODUCTS,INC. |
发明人 |
PURIEFOY, MILTON;HALSEY, DAVID |
分类号 |
B29C33/76;B29C37/00;B29C65/48;B29C70/22;B29C70/34;B29C70/54;B29D24/00;(IPC1-7):B32B31/00 |
主分类号 |
B29C33/76 |
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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