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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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