The invention discloses a high-torque motor for a multi-rotor unmanned aerial vehicle. The high-torque motor comprises a shell, a drive shaft, an electric brush and a commutator, wherein the commutator is in contact connection with the electric brush and is arranged on the drive shaft; a middle segment, located in the shell, of the drive shaft is fixedly sleeved with a rotor main body formed by superposing multiple silicon steel sheets; the rotor main body is provided with a winding group formed by multiple windings; and a corresponding permanent magnet group is arranged at the position, closeto the inner wall of the shell, on the outer circumference, employing the drive shaft as the circle center, of any layer of winding in the winding group. The magnetic field can be strengthened underthe condition of the same voltage supply through correspondingly adding the multiple windings and permanent magnets, thereby increasing the torque; and furthermore, multiple layers of windings are arranged along the direction of the drive shaft in a staggered manner, so that the problem of a dead angle in a gap between magnetic force and driving force can be solved and torque output is more linearand stable.