发明名称 Verfahren zur Herstellung eines monolithischen, doppelwandigen und hitzebeständigen Verbundwerkstoffteiles und danach hergestelltes Verbundwerkstoffteil
摘要 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
申请公布号 DE60303348(T2) 申请公布日期 2006.08.17
申请号 DE2003603348T 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, FRANUPSILONOIS
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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