Simulation of air jets for controlling stall in a centrifugal fan

摘要

The main goal of the present work is to analyze the three-dimensional unsteady flow field of a centrifugal fan by solving Navier-Stokes equations, coupled with the throttle condition. The results show that rotating stall occurs in the original fan when the flow rate is 4.30m(3)/s, and the stall inception first appears at three impeller passages near the volute tongue and front disc. An active control method is proposed to inhibit the stall inception, which involves blowing air at the inlets of the three impeller passages. This blowing control method cannot inhibit the stall inception when the blowing speed is lower than 50m/s. The stability margin of the centrifugal fan is extended when the blowing speed is increased from 50 to 110m/s, while no further effect is obvious with a further increase in the blowing speed. At a blowing speed of 110m/s, rotating stall occurs again when the fan flow reaches 3.46m(3)/s. After the application of the nozzle blowing, the safety margin of the centrifugal fan is extended by 13%, and an obvious stability enhancement effect is achieved. From an engineering standpoint, this new active control method for rotating stall offers a valuable means to ensure the safe operation of a centrifugal fan.