Abstract

Axial fan is an important piece of equipment in the thermal power plant that provides enough air for combustion of coal. This paper focuses on the aerodynamic noise characteristics of an axial fan in the development from stall inception to stall cells. The aerodynamic noise characteristic of monitoring region in time and frequency domains was simulated employing the large-eddy simulation (LES), with the addition of throttle setting and the Ffowcs Williams-Hawkings (FW-H) noise model. The numerical results show that, under the design condition, the acoustic pressure presents regular periodicity along with the time. The noise energy is concentrated with high energy of the fundamental frequency and high order harmonics. During the stall inception stage, the acoustic pressure amplitude starts fluctuating and discrete frequencies are increased significantly in the low frequency; among them, there are three obvious discrete frequencies: 27.66 Hz, 46.10 Hz and 64.55 Hz. On the rotating stall condition, the fluctuation of the acoustic pressure level and amplitude are more serious than that mentioned above. During the whole evolution process, the acoustic pressure peak is difficult to keep stable all the time, and a sudden increase of the peak value at the 34.5th revolution corresponds to the relative velocity’s first sudden increase at the time when the valve coefficient is 0.780.

Highlights

  • Axial fan is an important piece equipment in the thermal power plant that provides enough air for combustion of coal

  • The unsteady phenomenon of rotation stall in an axial fan is numerically studied through large eddy simulation with throttle valve model and Ffowcs Williams-Hawkings (FW-H) noise model

  • Flow fields are analyzed in detail in the evolution process of rotating stall

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Summary

Introduction

Axial fan is an important piece equipment in the thermal power plant that provides enough air for combustion of coal. Yamada et al [10] conducted a numerical analysis of the rotating stall inception on a multi-stage axial flow compressor for an actual gas turbine by large eddy simulation. Toge and Pradeep [12] attempted to study the stall inception mechanism of the low speed, contra rotating axial fan stage by wavelet transforming the unsteady pressure date from the casing wall sensor. Mao et al [20] studied the effect of the end- plate on the static and noise characteristics of the small axial fan by numerical simulation and experiment He showed that the mechanism of noise reduction is due to the decrease of the vorticity of the blade surface caused by the end plate. When the unsteady phenomenon of rotating stall occurs, the flow field in axial fan will be significantly different with no stall conditions. Pressure level and amplitude at the rotor blade domain are investigated under the four conditions mentioned above

Subsection with Geometry
Governing Equations
Boundary Conditions
Simulation Process of Rotating Stall
The Time Domain Characteristic of Acoustic Pressure
The Time Domain Analysis of the Acoustic Pressure Peak
Spectrum Analysis of the Noise
Conclusions
Full Text
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