The utility model relates to the technical field of wheel-side speed reducers for high-altitude operation, in particular to a wheel-side speed
reducer convenient for an electric high-altitude operation platform, which comprises a speed
reducer body, a first-stage sun gear, a first-stage
planet group, a second-stage
planet group, a second-stage sun gear, a second-stage
planet group, a third-stage planet group, a fourth-stage planet group, a fourth-stage planet group and a fourth-stage planet group, the motor is input through the first-stage sun gear, first-stage
speed reduction is carried out through the first-stage planet set, second-stage
speed reduction is carried out through the splines, then second-stage
speed reduction is carried out
through transmission to the second-stage planet set, third-stage speed reduction is carried out
through transmission to the third-stage planet set, third-stage speed reduction is carried out
through transmission, and finally output is carried out through the shell. By the adoption of the three-planet-set speed reduction structure, the gear, the planet carrier and the gear ring needed by first-stage speed reduction are all placed in the planet carrier needed by third-stage speed reduction, compact three-stage speed reduction is achieved, the structure is compact, space is saved when the whole
aerial work platform is arranged, and therefore the working efficiency of the
system is improved.