The invention relates to the technical field of reducers, in particular to a large-torque
bevel gear-double-cycloidal
speed reduction device of a
rocket launching movable platform. The
speed reduction device is characterized in that a secondary
speed reduction device is composed of a
bevel gear pair and a double-cycloidal transmission, wherein (A) the double-cycloidal transmission consists of a frame, an output shaft, supporting bearings, three cycloidal gears with a
phase angle of 120 degrees, an eccentric bearing, a
hypocycloid gear ring, a front frame, an input shaft and a W output mechanism, the input shaft is supported in the inner hole of the front frame through the bearing, the shaft extension end of the input shaft is linked with the eccentric bearing, and the input end of the input shaft is linked with a large
bevel gear; the front frame is sequentially linked with the
hypocycloid gear ring and the frame into a whole; and the output shaft is supported in the inner hole of the frame through the bearing; and (B) two symmetrical devices of small bevel gear shafts, which are meshed with the large bevel gear are supported in box wall holes of the front frame through the bearings, one small bevel gear shaft is linked with a motor, and the other small bevel gear shaft is linked with a manual
handle. The large-torque bevel gear-double-cycloidal speed reduction device has the following beneficial effects: (a) the double reduction is realized, the axial size is short, the weight is light, and high degree of lightweight is realized; (b) the cycloidal gears have no
broken teeth, and the three cycloidal gears have the transmission
bearing capacity greater than that of a
planet with only four planetary gears; and (c) the cost is reduced by 40-55%.