This invention discloses a method for enhancing the interlayer strength of continuous
fiber 3D printed parts, belonging to the field of
composite material manufacturing technology. The method includes the following steps: Step 1, carbon
fiber pretreatment; Step 2, prepreg filament preparation; Step 3, additive manufacturing of
interlocking structures: using the prepreg filament obtained in Step 2 for 3D printing, during the printing process,
laser preheating and regular tapping are used to form protruding structures in each layer. In subsequent
layers,
laser preheating and tapping are used to form hook-like protruding structures, achieving interlayer
interlocking; Step 4,
carbon nanotube pretreatment; Step 5, placing the printed part obtained in Step 3 in a
solvent, adding an activating agent, and then adding the aminated carbon nanotubes obtained in Step 4, allowing the carbon nanotubes to be grafted onto the carbon
fiber surface through an amidation reaction, forming a root structure. This invention can effectively enhance the interlayer peel strength in the layer height direction, meeting the high strength requirements of aircraft structural components.