发明名称 PANNEAU COMPOSITE POUR MOBILIER AVION
摘要 <p>The composite panel (4) has a central core formed of a honeycomb type panel (1) provided with a preimpregnated resin fabric layer (2). A face of the honeycomb type panel is covered with a thin log veneer (301). An assembly is assembled and integrated under pressure. An aluminum film (303) is interposed between the thin log veneer and the resin fabric layer. The aluminum film is integrated on one of faces of the thin log veneer by an adhesive layer (302) i.e. phenolic resin layer. An independent claim is also included for a method for realizing a composite panel.</p>
申请公布号 FR2962362(B1) 申请公布日期 2012.08.17
申请号 FR20100055672 申请日期 2010.07.12
申请人 CATHERINEAU ALAIN 发明人 CATHERINEAU ALAIN
分类号 B32B3/12;B29D24/00;B64D11/00 主分类号 B32B3/12
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