发明名称 |
METHOD FOR FINISHED-RIB COMPACTING A THERMOPLASTIC COMPOSITE PART WITH CONTINUOUS FIBRES |
摘要 |
A method for manufacturing a structural part including at least two wings extending in intersecting planes made of thermoplastic fiber-reinforced composite material including at least two plies of continuous fibers. The fibers extend from one wing to another. The method includes cutting the at least two plies in a fabric and/or a tape of fibers pre-impregnated with a thermoplastic resin; assembling the plies to create a preform; and compacting the preform to a final shape of the part by subjecting the preform to a defined cycle of temperature and pressure. A toolset can implement the method described above. Such a toolset includes a rigid punch and die such that closing the tool creates a sealed chamber in a shape of the part between the punch and the die.
|
申请公布号 |
US2012067509(A1) |
申请公布日期 |
2012.03.22 |
申请号 |
US201013203350 |
申请日期 |
2010.02.24 |
申请人 |
KURTZ DIDIER;CHOTARD FLORIAN;AIRBUS OPERARATIONS (INC AS A SOCIETE PAR ACT SIMPL) |
发明人 |
KURTZ DIDIER;CHOTARD FLORIAN |
分类号 |
B32B37/10 |
主分类号 |
B32B37/10 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|