The invention discloses a method for repairing a guide groove of a
piston rod of an aircraft refueling probe, which belongs to the field of guide groove repairing methods and comprises the following steps: step 1, designing and manufacturing an inner hole cladding head with the outer
diameter of not more than 40mm, the
laser focal length of 15-20mm and the
powder coke of 15-20mm; 2, an inner groove of the oil receiving probe to be repaired is pretreated, namely a
dry lubricant on the surface is removed through
abrasive paper, and
alcohol or
acetone is used for cleaning after ultrasonic cleaning; 3, the high-strength stainless steel
powder is subjected to
vacuum drying at a certain temperature, the
powder is taken out after being cooled, the powder is loaded into a powder bin of
external powder feeding equipment, heating is started, and the temperature is set to be 50-80 DEG C; and 4, the oil receiving exploring tube is fixed to an external positioner. According to the method, the
laser inner hole cladding repairing technology is adopted, the special inner hole cladding gun is assembled, the
reachability of repairing the guide groove is good, the method has the advantages of low heat input, high repairing precision, small
surface roughness and the like, the post-
processing difficulty is greatly reduced, and the repairing success rate is high.