发明名称 Method for Repairing a Composite Structural Outer Skin
摘要 A composite structure including two external skins and an internal core between them, wherein a portion of one of the external skins has to be replaced, with pressure from a counter-form and suction. The repair is accomplished by piercing a vent hole in the opposite external skin to discharge the air in the cells of the core, which improves adhesive bonding of the new portion on the core.
申请公布号 US2008283172(A1) 申请公布日期 2008.11.20
申请号 US20060066677 申请日期 2006.09.27
申请人 AIRBUS FRANCE 发明人 BERNUS CHRISTOPHE;MARTY JEAN-CLAUDE
分类号 B29C73/10 主分类号 B29C73/10
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