The invention relates to completely-new wing auxiliary equipment or a novel wing. According to the present invention, the front part of a wing tip is provided with a circle or a plurality of circles of impellers, a fairing is arranged on the front and the rear of a shaft disc of the 
impeller and extends to the whole wing tip, variable 
pitch blades are arranged in front of the wing tip through a wheel hub, a gear and a rotation shaft, and drive an 
electricity generation device arranged on the wing 
tip position or other transmission devices, the 
impeller is driven to rotate through facing 
airflow, the blade can rotate in a direction against an upward turning eddy flow of the wing tip under pushing of the incoming flow with an installation angle ( as shown in Figure 1) of the blade, such that right wing tip counterclockwise rotation wing tip eddy flow generated in the normal wing profile is previously decreased, rotation airflows generated by the impellers on both edges upward 
impact the wings from the bottom of the wings so as to further increase lifting force, and substantial lifting increase and resistance reduction are achieved with the benign effects. The multifunction wing tip 
turbine engine even can replace an electromotor driven by the aircraft motor part or generate auxiliary power, such that safety 
threat on the back flying aircraft by the wing tip wake of the front flying aircraft can be decreased, and 
aviation industry safety can be improved.