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
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