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 |
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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