发明名称 |
Method for producing a monolithic, thermostructural and double-walled composite body and composite body obtained by this method |
摘要 |
<p>Thermo-structural component (20) is made from two layers (21, 22) of a composition material, e.g. based on carbon fibres, joined together by spacers (23) formed by stitches of a filament passed through the outer skins and an intermediate core of a supple material through which a needle can pass. The resulting sandwich structure is then impregnated with a viscous resin and after the resin has set, the core is eliminated by pyrolysis to leave the two skins with spacers in the gap between them</p> |
申请公布号 |
EP1342552(B1) |
申请公布日期 |
2006.01.25 |
申请号 |
EP20030290447 |
申请日期 |
2003.02.26 |
申请人 |
EADS SPACE TRANSPORTATION SAS;MBDA FRANCE |
发明人 |
SALMON, THIERRY;CAHUZAC, GEORGES;BOUCHEZ, MARC;FALEMPIN, FRANCOIS |
分类号 |
B29C70/24;B32B3/22;B29C70/54;B32B5/26;B32B5/28;B32B7/08 |
主分类号 |
B29C70/24 |
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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