The invention discloses a main speed
reducer of a fan of a novel GTF aircraft engine. The main speed
reducer of the fan of the novel GTF aircraft engine is characterized in that sun gears and star gears use integrated double
helical teeth, an inner tooth ring A and an inner tooth ring B are
helical internal gears connected with a gear
coupling through
helical external splines, the gear
coupling is connected with an output shaft through a straight-tooth internal spline, the speed
reducer does not have an independent planetary rack, all the star gears are fixed on a left box body cover through star gear shafts, each star gear only revolves on its axis, the space position of each star gear is not changed in running, a bush of each star gear shaft uses a special structure that the
diameter of the central hole is gradually changed to automatically compensate the flexible deformation of a
cantilever end, and each of the input shaft and star gear shafts comprises a
cantilever and a hollow structure to increase the elastic deformation ability and play a role of storing lubricating oil. The main speed reducer of the fan of the novel GTF aircraft engine has beneficial effects of simple structure, simple technique, good uniform loading and floating effect, small speed reducer volume, strong
bearing capacity, large transmission power and small vibration
noise and is capable of realizing the fixed-point spray
lubrication for the star gears and bearing.