Abstract

The reduction of fan noise in ducts is a challenging task for acoustic engineers. Usually, the confined space where an absorber can be integrated is small. In addition, one has to consider the influence of the absorber on the flow field and the attenuation of noise should be as great as possible. In this contribution, we investigate the application of a micro-perforated absorber (MPA) in the direct vicinity of a low-pressure axial fan operating at low Mach number conditions. The micro-perforated plates (MPP) are modeled using the Johnson–Champoux–Allard–Lafarge (JCAL) model for porous materials. The entire geometrical setup of duct, fan and MPA is then simulated with the Finite Element (FE) method; the pre-processing effort is reduced by using non-conforming grids to discretize the different regions. The influence of the cavity length and the positioning of the fan are analyzed. The results are then applied to the construction of a full-sized MPA duct component that takes the limited space into consideration. Simulation results and overall functionality are compared to experimental results obtained in an axial-fan test rig. The Finite Element framework proved to be robust in predicting overall sound pressure level reduction in the higher volume flow rates. It is also shown that the MPP increases sound reduction in the low-frequency regime and at two resonant frequencies of the MPA setup. However, its main benefit lies in maintaining the efficiency of the fan. The location of the fan downstream or within the MPA has a significant effect on both the simulated and measured sound reduction.

Highlights

  • The sound emission spectrum created by an axial fan operating at low Mach number conditions is influenced by various mechanisms

  • The same micro-perforated plates (MPP) arrangement was tested on an axial fan in [16], where they showed the effectiveness of such a design on the reduction of emitted fan noise

  • We have presented the simulation framework for the design of a micro-perforated absorber in the direct vicinity of a low-pressure axial fan

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Summary

Introduction

The sound emission spectrum created by an axial fan operating at low Mach number conditions is influenced by various mechanisms. Adding passive sound absorbing structures is beneficial to overall in-situ performance as well as costefficient through further reduction of sound emission They should be compact due to the limitation of space and have a minimal influence on the flow field [7, 10, 11]. In a smaller geometry scale study, Lee [12] showed the effect of various cylindrical micro-perforated duct elongations in a limited frequency range, mainly the blade passage frequency regime His main focus was the investigation of flow resistance variations of customized micro-perforated material. The central questions investigated in this contribution deal with the accuracy of the Finite Element (FE) based simulated sound emission spectra compared to experimental data obtained in a -designed large-scale test rig. Fan efficiency, pressure rise and accumulated sound emission curves with and without MPA are compared

Prerequisites to design and simulation
Material
Modeling and parameter fitting
Zm sinðkmhmÞ jZm sinðkmhmÞ cosðkmhmÞ ð5Þ
Acoustic sources
Finite element framework
Inlet test chamber and MPA design
Radiated sound and directivity
Sound mission spectra
Characteristic curve results
Conclusion
27. DIN EN ISO 10534
35. VDI 2081 Blatt 1
38. DIN EN ISO 5801
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