The invention discloses an aero-engine
silicon carbide ceramic matrix composite part crack damage repairing method which comprises the following steps: removing an environmental barrier
coating on the surface of a part, cleaning and
drying; powdery active
metal brazing filler metal and a connecting agent are selected to be mixed and then coated on cracks and nearby areas on the surface of the part; vacuum
brazing, weld joint
polishing, cleaning and
drying are conducted; preparing a bonding layer and a middle layer of the environmental barrier
coating by using atmospheric
plasma spraying equipment, and preparing a
surface layer of the environmental barrier
coating by using a
plasma-
physical vapor deposition method; and the environmental barrier coating is polished, annealing treatment is conducted, and crack damage repairing of the
silicon carbide ceramic matrix composite part of the aero-engine is completed. According to the vacuum
brazing process, the strength of the base material can be effectively recovered by 50%-60%, the
usable time of the base material is prolonged, parts can continue to serve, and the parts are prevented from being scrapped in advance; in addition, according to the EBC coating preparation technology, the
porosity of the coating can be reduced, and therefore the
service time of the repaired part is further prolonged.