The invention discloses a
laser repairing method for a thermosetting carbon
fiber reinforced resin-based
composite material, relates to the technical field of
carbon fiber composite material repairing, and is suitable for in-situ efficient repairing of military and civilian components in the
aviation field. Aiming at the problems of secondary damage, low efficiency and poor
interface bonding in the prior art, the method comprises the following steps: 1) removing a damaged area by
picosecond or
femtosecond laser, and
processing a step structure of a repair area; 2)
etching a microgroove which is consistent with the surface carbon
fiber in direction, the depth D of the microgroove meets the condition that D is equal to 5 + 0.656 * [(TlaserTmelt) * MFR] 0.4, and the width W of the microgroove meets the condition that W / D is larger than or equal to 0.5 and smaller than or equal to 5; (3) a
thermoplastic film is laid in the repairing area, and fusion anchoring is achieved through
laser irradiation in combination with rolling or fixed compaction; 4, the
thermoplastic prepreg tape is laid through large-spot laser, filling is completed in a multi-layer and multi-channel mode, according to another preferred embodiment, the
thermoplastic film is pre-compounded on the surface of the prepreg tape, and the independent film laying step is omitted. According to the method, the repairing period of the
carbon fiber composite material can be greatly shortened, the method is suitable for various damage types, and efficient and high-quality in-situ repairing is achieved.