Method for manufacturing a composite part reinforced with nanotubes
AssigneeSafran Aircraft Engines
InventorDidier Fromonteil
Life of this patent
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Abstract
A method for manufacturing a composite part reinforced with nanotubes, includes stacking a plurality of composite plies of prepreg and at least one composite ply integrating nanotubes, the at least one composite ply integrating nanotubes being positioned in an inter-ply space between two composite plies of prepreg, wherein the at least one composite ply integrating nanotubes is a ply having a thermoplastic component, the nanotubes being integrated in the thermoplastic component.
Claims12
A method for manufacturing a composite part reinforced with nanotubes, said method comprising a stacking step that includes stacking a plurality of composite plies of prepreg and at least one composite ply integrating nanotubes, said at least one composite ply integrating nanotubes being positioned in an inter-ply space between two composite plies of prepreg, wherein said at least one composite ply integrating nanotubes is a ply having a thermoplastic component, said nanotubes being integrated in said thermoplastic component, the method including a step of manufacturing said composite ply integrating nanotubes that comprises:
- a sub-step of extruding a mixture resulting from a mixing sub-step through a die dimensioned to obtain filaments of thermoplastic polymer filled with nanotubes;
- a sub-step of melting and blow forming said filaments of thermoplastic polymer filled with nanotubes and without using a chemical binder,
- said at least one composite ply integrating nanotubes integrates multiwalled carbon nanotubes and is a web of thermoplastic fibres, said nanotubes being integrated in said thermoplastic fibres and the web of thermoplastic fibres has a weight per unit area comprised between 15 g/m2 and 100 g/m2.
Dependencies are inferred from the claim text.