发明名称 Production method of workpiece made of fiber-composite material used in load bearing structure for aircraft, involves removing support and secondary material formed on upper surface of workpiece blank to form workpiece
摘要 <p>The method involves fitting a main material (6) made of pre-impregnated fiber semi-finished product e.g. carbon fiber and a secondary material (7) made of glass fiber to a support (3) for forming blank-mold areas (1,10) comprising main material and secondary material. The pressure is applied to the blank-mold areas to form a workpiece blank (14) such that the support is formed on the upper surface of the workpiece blank. The support and the secondary material are removed from the workpiece blank to form a workpiece. Independent claims are included for the following: (1) workpiece production apparatus; (2) method for producing plastic fiber-composite component; and (3) semi-finished product.</p>
申请公布号 DE102006038666(A1) 申请公布日期 2008.02.28
申请号 DE20061038666 申请日期 2006.08.17
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 SANDER, PETER;MARQUARDT, HANS;LENGSFELD, HAUKE
分类号 D04H3/04;B32B5/26;B32B27/12;B32B37/10 主分类号 D04H3/04
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