发明名称 Composite sandwich structure producing method for aircraft construction, involves providing core structure with cell structure having fold valleys that forms open channels with open ends and channel sides at edges of structure
摘要 <p>The method involves providing a core structure with a folded cell structure having fold valleys that forms continuous open channels (4) with open ends and open channel sides at edges of the structure. Two cover layers are applied on respective sides of the structure. The ends and the sides are closed and sealed by forming an edge seal having a limited spatial volume in an edge region on one of the edges of the structure.</p>
申请公布号 DE102004013145(A1) 申请公布日期 2005.10.13
申请号 DE20041013145 申请日期 2004.03.17
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 ENDRES, GREGOR CHRISTIAN;WEBER, HANS-JUERGEN
分类号 B32B3/02;B32B3/08;B32B3/12;B32B3/28;E04B1/00;(IPC1-7):B32B3/12 主分类号 B32B3/02
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