A method for removing a ceramic core of a hollow blade of a turbine of an aircraft engine comprises the four steps of primary core removing, secondary core removing, third core removing and ultrasonic cleaning. The concentration of KOH alkali liquor used in primary core removing is 40%, the concentration of KOH alkali liquor used in secondary core removing is 30%, and the concentration of KOH alkali liquor used in third core removing is 40%. Every time core removing is conducted, the temperature of the alkali liquor ranges from 160 DEG C to 200 DEG C, the pressure of the alkali liquor fluctuates between 0.4 MPa and 0.5 MPa, water is added every six hours, and soaking time is 48 hours. According to the method, the concentration of the alkali liquor is reduced, the water is added every six hours, and it is guaranteed that salt generated due to reactions is sufficiently dissolved; the alkali liquor is replaced every 48 hours, the concentration of the alkali liquor changes in a stepped mode, and it can be guaranteed that the chemical reactions are conducted effectively; the pressure of the alkali liquor fluctuates in a pulse mode, core cracking can be facilitated, the reaction interface between the alkali liquor and the core is enlarged, and the reacting dose is increased. Through the method, the ceramic core removing period can be shortened to six days from over twenty days, and the first pass yield of core removing can be higher than 90%.