The invention discloses a split torque transmission deceleration device for helicopters. The split torque transmission deceleration device for the helicopters is characterized by comprising an outputstage system, four two-stage split torque systems, four one-stage split torque systems and two input stage systems; the output stage system comprises a herringbone gear and an output shaft; each two-stage split torque system comprises a first shafting and a second shafting; each first shafting comprises a spur gear I, an intermediate shaft I, a helical gear I and a helical gear II; each second shafting comprises a spur gear II, an intermediate shaft II, a helical gear III and a helical gear IV; each first-stage split torque system comprises a bevel gear shaft, a supporting frame, a differential gear train, a spur gear III, an intermediate shaft III and a spur gear IV; and each input stage system comprises an input shaft, two intermediate shafts IV and two bevel gears. According to the split torque transmission deceleration device for the helicopters, a symmetrical arrangement structures and a differential shafting are adopted, so that all stages of split torque transmission are realized, the load-uniformizing requirement is met, and the service performance of a split torque transmission system is improved.