The present application relates to aircraft, and specifically provides a
turbofan, aiming at solving the problem that the existing
turbofan is too large in size and too heavy in weight, and is not suitable for the demand of low-altitude aircraft. To this end, the second center ring of the
turbofan of the present application is sleeved outside the first center ring, the first and second support rings are correspondingly connected at both ends of the first and second center rings, the first and second
spoke rings are correspondingly connected at both ends of the second center ring, the first and second
spoke rings are further curved towards the height center line of the second center ring and finally form
abutment, and the plurality of first blades of the first
spoke ring and the plurality of second blades of the second spoke ring are mirror images. The turbofan is a mechanical full
balance design, the turbofan is manufactured by using a 3D printing process, the turbofan removes the reaction force
support system of the
propeller, and can meet the demand of low-altitude aircraft on the light weight, high efficiency and low
failure rate of the
propeller.