Noise Reduction Analysis of Electronic Device Cooling Fan With Duct and Its Application Under Variable Working Conditions

Author:

Sun Zonghan1,Tian Jie2,Liśkiewicz Grzegorz3,Du Zhaohui1,Ouyang Hua2

Affiliation:

1. School of Mechanical Engineering, Shanghai Jiao Tong University, Dongchuan Road, Shanghai 200240, China

2. School of Mechanical Engineering, Shanghai Jiao Tong University, Dongchuan Road, Shanghai 200240, China; Engineering Research Center of Gas Turbine and Civil Aero Engine, Ministry of Education, Cenglin Road, Shanghai 201306, China

3. Institute of Turbomachinery, Łódź University of Technology, Wólczanska 219/223, Łódź 90-924, Poland

Abstract

Abstract A noise reduction method for axial flow fans using a short inlet duct is proposed. The pattern of noise reduction imposed by the short inlet duct on the axial flow cooling fan under variable working conditions was experimentally and numerically examined. A 2-cm inlet duct was found to reduce tonal noise. As the tip Mach number of the fan increased from 0.049 to 0.156, the reduction in the total average sound pressure level at 1 m from the fan increased from 0.8 dB(A) to 4.3 dB(A), and further achieved 4.8 dB(A) when a 1-cm inlet duct was used. The steady computational fluid dynamics (CFD) showed that the inlet duct has little effect on the aerodynamic performance of the fan. The results of the full passage unsteady calculation at the maximum flow rate showed that the duct has a significant influence on the suction vortexes caused by the inlet flow nonuniformity. The suction vortexes move upstream to weaken the interaction with the rotor blades, which significantly reduces the pulsating pressure on the blades. The sound pressure level (SPL) at the blade passing frequency (BPF) contributed by the thrust force was calculated to reduce by 36 dB at a 135 deg observer angle, reflecting the rectification effect of the duct on the nonuniform inlet flow and the improvement in characteristics of the noise source. The proper orthogonal decomposition (POD) of the static pressure field on the blades verified that the main spatial mode is more uniformly distributed due to the duct, and energy owing to the rotor-inlet interaction decreases. A speed regulation strategy for the cooling fan with a short inlet duct is proposed, which guides the application of this noise reduction method.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

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