发明名称 METHOD FOR FINISHED-RIB COMPACTING A THERMOPLASTIC COMPOSITE PART WITH CONTINUOUS FIBRES
摘要 The invention relates to a method for producing a structural part including at least two flanges extending in intersecting planes, consisting of a composite thermoplastic material with a fibre reinforcement including at least two plies of continuous fibres, said fibres extending from one flange to the other, wherein said method includes: a cutting step consisting of cutting the at least two plies in a fabric and/or a web of fibres preimpregnated with a thermoplastic resin; a drape-forming step for assembling the plies in order to create a blank; and a consolidation step for compacting said blank into the defined shape of the part by subjecting the same to a predetermined temperature and pressure cycle. The invention also relates to equipment for implementing the above method. Such equipment includes a rigid punch and a rigid die so that the closing of the equipment forms a sealed chamber with the shape of the part being formed between the punch and the die.
申请公布号 WO2010097547(A2) 申请公布日期 2010.09.02
申请号 WO2010FR50317 申请日期 2010.02.24
申请人 AIRBUS OPERATIONS (S.A.S);KURTZ, DIDIER;CHOTARD, FLORIAN 发明人 KURTZ, DIDIER;CHOTARD, FLORIAN
分类号 B29C70/46;B29C70/54 主分类号 B29C70/46
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