The invention discloses a cast
copper outer rotor acting on an
aviation exhaust heat dissipation
system. Comprising an upper end ring, guide bars, a rotor core and a lower end ring, upper guide grooves and lower guide grooves are uniformly distributed in the inner ring surfaces of the upper end ring and the lower end ring respectively, mounting grooves are uniformly distributed in the inner ring surfaces of rotor
punching sheets, the cross section of each guide bar is of an
isosceles trapezoid structure, the inner side width of each guide bar is smaller than the outer side width, and the structures of the mounting grooves, the upper guide grooves and the lower guide grooves are matched with the structures of the guide bars. The guide bars are in one-to-one correspondence with the mounting grooves, the upper guide grooves and the lower guide grooves, the middle parts of the guide bars are embedded in the corresponding mounting grooves, the two ends of the guide bars are respectively
cut and mounted in the corresponding upper guide grooves and lower guide grooves, and the inner side surfaces of the guide bars are flush with the inner ring surfaces of the rotor iron core, the upper end ring and the lower end ring; cooling holes are formed in the rotor
punching sheet, the cooling holes are distributed in an
annular array by taking the axis of the rotor core as the center, and an included angle is formed between the axis of each cooling hole and the axis of the rotor core; unclosed flow guide holes are formed in the
peripheral surfaces of the upper end ring and the lower end ring; and the flow guide holes correspond to the cooling holes one by one. According to the invention, triple effects of low loss,
high heat dissipation and high reliability are realized.