Effect of extending tip chord on the performance and noise of an axial flow fan

In this paper, the leakage flow in the blade tip clearance of an axial flow fan is studied, and an improved strategy for increasing the chord length of the blade tip toward the inflow direction is proposed. It has been proved that extending the tip chord can move the flow leakage backward. This results in an attenuation of the leakage vortex intensity and a mitigation of flow losses. Through comparative unsteady simulations, it is observed that a reduction in the amplitude of pressure pulsations surrounding the tip clearance and trailing edge leads to a corresponding decrease in the intensity of the noise source. The experiment results show that, under the target operating condition, the static pressure efficiency is increased by 1.02%. The amplitudes of both discrete and broadband noise are reduced, resulting in a decrease in the total sound power level at the outlet by 1.7 dB(A).

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Publication Details

Journal
International Journal of Aeroacoustics
Published
2025-03-24
DOI
https://doi.org/10.1177/1475472x251326965
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
Field-Weighted Citation Impact
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article

Effect of extending tip chord on the performance and noise of an axial flow fan

Haijiang He, Liu Jinglong, Jiaming Wang, Kunfeng Liang et al.
International Journal of Aeroacoustics
Aerodynamics and Acoustics in Jet Flows
article

Effect of extending tip chord on the performance and noise of an axial flow fan

Haijiang He, Liu Jinglong, Jiaming Wang, Kunfeng Liang, Anyu Zhou
article en

Abstract

In this paper, the leakage flow in the blade tip clearance of an axial flow fan is studied, and an improved strategy for increasing the chord length of the blade tip toward the inflow direction is proposed. It has been proved that extending the tip chord can move the flow leakage backward. This results in an attenuation of the leakage vortex intensity and a mitigation of flow losses. Through comparative unsteady simulations, it is observed that a reduction in the amplitude of pressure pulsations surrounding the tip clearance and trailing edge leads to a corresponding decrease in the intensity of the noise source. The experiment results show that, under the target operating condition, the static pressure efficiency is increased by 1.02%. The amplitudes of both discrete and broadband noise are reduced, resulting in a decrease in the total sound power level at the outlet by 1.7 dB(A).

International Journal of AeroacousticsVol. 24(3-4)
Henan University of Science and Technology (CN)
Openalex Percentile: Top 93%
Aerodynamics and Acoustics in Jet Flows
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