发明名称 Method for manufacturing a laminated body
摘要 <p>The laminated composite component comprises a substrate(8) based on at least one fibre layer(9) and an outer facing layer(13) incorporating particles(16), metal fibres and/or other fibres(17), both substrate and facing layer being impregnated with a binder(11) to bond them into a single component(1). In a process for manufacturing a laminated component(1) particles are deposited in the facing layer near the fibres(17) before impregnation of both substrate(8) and facing layer(13) with the binder(11).</p>
申请公布号 EP0836931(B1) 申请公布日期 2006.04.05
申请号 EP19970117118 申请日期 1997.10.02
申请人 MTU AERO ENGINES GMBH 发明人 SIKORSKI, SIEGFRIED;SCHOBER, MICHAEL;SCHOENACHER, REINHOLD
分类号 B32B5/28;B32B15/02;B29C70/02;B29C70/64;B32B5/22;B32B15/08;B64C11/20;F01D5/28;F04D29/02 主分类号 B32B5/28
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