The invention discloses an assembling method for a three-fulcrum bearing of an aircraft engine, belonging to the technical field of engine overhaul. The assembling method comprises the following steps that: a central
bevel gear is placed in a heating oven for heating, and a bearing outer ring is assembled in the central
bevel gear; a spring ring is mounted on the central bevel bear for fixing the bearing, and the bearing is mounted in a manner that a marking face of the bearing faces to the spring ring; the bearing is cooled to achieve the temperature of an ambient medium, the
maximum diameter and the minimum
diameter of a
runway of the bearing outer ring mounted in the central
bevel gear are measured, then diameters on four planes of the
runway of the bearing outer ring are measured, and then an average value is obtained; a bearing
retainer and a bearing rolling rod are mounted in an inner ring of the bearing outer ring, and the bearing
retainer is mounted in an manner that a marking face of the bearing
retainer faces to the spring ring; a bearing inner ring is mounted on a low-pressure
turbine shaft, and numbers in sets face to the front end face of the low-pressure
turbine shaft; the bearing inner ring is cooled, and the low-pressure
turbine shaft is cooled to obtain the temperature of ambient environment; and the
maximum diameter and the minimum
diameter are determined by measuring the diameters on six planes of a
runway of the bearing inner ring, and then the bearing assembling play is calculated.