The invention relates to a device for automatically detecting remainders in an aerospace engine, and belongs to the technical field of detecting the remainders in the aerospace engine. The device aims to solve the problem of low detecting efficiency in the traditional remainder detecting method during swinging or swaying in the aerospace engine. A detecting device which is arranged on a turn table comprises an industrial personal computer, a servo amplifier, a servo motor, a planetary reducer, a No. 1 synchronous pulley, a synchronous cog belt, a No. 2 synchronous pulley, an output rotating shaft, an electromagnetic shielding box, a conducting slip ring, a tote cart, a clamp, an acoustic sensor group, a sensor cable, a conditioning circuit, a six-channel synchronous data acquisition card and a fast chuck, wherein the aerospace engine is arranged on the tote cart; the industrial personal computer controls the servo motor to drive the output rotating shaft to rotate, the fast chuck for mounting and clamping the aerospace engine is mounted at one end of the output rotating shaft, and the electromagnetic shielding box and the rotor part of the conducting slip ring is mounted at the other end of the output rotating shaft; the detection signal of the acoustic sensor group is fed back to the industrial personal computer.