发明名称 Leichtbauverbundplatte und Anwendung eines Kernes zur Herstellung einer Leichtbauverbundplatte
摘要 A process for mfg. a lightweight composite plate with upper (1) and lower (9) facing layers and a core (2), all consisting of fibre-reinforced plastic involves: (a) cutting the upper (1) and lower (9) facing layers to size; (b) cutting a preimpregnated fabric core (2) from a pre-prepared material of suitable thickness; (c) placing the lower layer (9) in a tool cavity with the integral side flaps against the cavity walls; (d) locating the core (2) in the cavity; (e) folding over the upper areas of each flap onto the upper face of the core (2); (f) laminating the upper layer (1) onto the core (2) face; (g) curing the assembly (1, 2, 9) under pressure and heat. A tool for moulding the plate comprises a base plate with a rectangular cavity formed by a frame and an upper compression plate.
申请公布号 DE19512304(C2) 申请公布日期 1999.01.28
申请号 DE1995112304 申请日期 1995.04.01
申请人 DAIMLER-BENZ AEROSPACE AIRBUS GMBH, 21129 HAMBURG, DE 发明人 RODE, KLAUS, DIPL.-ING., 82041 DEISENHOFEN, DE;BORNSCHLEGEL, HEINZ, 86911 DIESEN, DE;RUSSO, ROLAND, DIPL.-ING., 80809 MUENCHEN, DE
分类号 B29C70/00;B29C70/24;B32B3/02;B32B27/04;B32B27/12;B64C1/40;B64D11/00;C08J3/24;C08J5/24;C09K21/00;(IPC1-7):B29C70/00;B32B35/00 主分类号 B29C70/00
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