Abstract
This study aims to improve the performance of centrifugal fans employed in totally enclosed fan-cooled (TEFC) motors by introducing leading-edge serrations, mimicking the leading-edge comb on owl wings, and suction-side ridges, imitating the soft down coat on the owl wing surface. A numerical wind tunnel is established according to the experimental standards of the Air Movement and Control Association (AMCA) 210. The reliability and accuracy of the simulation are first verified through an observed agreement between the simulation results and experimental measurements of the original fan. The influences and optimal values of four geometric dimensions related to the bionic structures, namely, the serration height, serration width, ridge height, and ridge spacing, are studied next in use of the Taguchi method and analysis of variance (ANOVA) at low, medium, and high flow rates. The investigation shows that the optimal bionic fan can effectively reduce the overall turbulent kinetic energy and produces a stronger, more uniform flow field behind the fan, thereby enhancing the fan's aerodynamic performance.