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Axial Fan Blade Tone Cancellation Using Optimally Tuned Quarter Wavelength Resonators

机译:使用最佳调谐的四分之一波长谐振器消除轴流风扇叶片音调

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摘要

Fan noise challenges noise control engineers in developing products ranging in scale from small ventilation systems to large turbomachines. The dominant noise source in many axial fans is the tonal noise due to rotor/stator interactions at the fundamental blade passing frequency. Flow-excited resonators have been used in the past for minimizing blade tone sound pressure levels (SPLs) generated by centrifugal fans through means of secondary source cancellation. The focus of this research is to extend that cancellation method to axial fans by attaching flow-driven quarter wavelength resonators fitted with optimal mouth perforations around the perimeter of the fan's shroud. A ducted-fan test facility was developed to measure upstream and downstream noise radiated from a test fan. Resonators were mounted at specific locations around the fan's shroud to obtain reductions in blade tone SPLs in both flow directions. They were driven into resonance via the unsteady pressure from the passing blades. An analytical model using transmission line theory was developed and validated experimentally to characterize the resonator's behavior under various flow conditions and mouth geometries. This model was used to predict the resonator's potential for reducing in-duct blade tones for specific flows and mouth perforation patterns. In a series of experiments to obtain the optimal resonator mouth perforations, it was observed that upstream and downstream SPL attenuations require different placement of the resonator mouth relative to the blade of the fan. With a single tuned resonator it was demonstrated that the fundamental blade tone SPLs can be reduced by as much as 20 dB in either the upstream or the downstream duct but not in both directions simultaneously. This behavior results when combining the resonator's monopolelike sound field with the dipolelike sound field of the fan's blades. Further studies are underway to extend the above method to higher pressure fans operating at speeds that generate higher order duct modes.
机译:风扇噪声在开发从小型通风系统到大型涡轮机的各种规模产品时,对噪声控制工程师提出了挑战。在许多轴流风扇中,主要的噪声源是在基本叶片通过频率下由于转子/定子相互作用而产生的音调噪声。过去已经使用了流激励谐振器,以最小化离心风扇通过次级声源消除而产生的叶片音声压级(SPL)。这项研究的重点是通过将气流驱动的四分之一波长谐振器连接到风扇罩周围的最佳开口中,从而将这种消除方法扩展到轴流风扇。开发了管道风扇测试设备,以测量从测试风扇辐射的上游和下游噪声。将谐振器安装在风扇罩周围的特定位置,以减小两个流向的叶片音调SPL。它们通过传递的叶片产生的不稳定压力而引起共振。开发了一种使用传输线理论的分析模型,并通过实验进行了验证,以表征谐振器在各种流动条件和喷嘴几何形状下的行为。该模型用于预测谐振器降低特定流量和嘴部穿孔方式的感应叶片音调的潜力。在获得最佳谐振器口孔的一系列实验中,观察到上游和下游SPL衰减要求谐振器口相对于风扇叶片的位置不同。通过单调谐谐振器,已证明基本叶片音调SPL可以在上游或下游管道中降低多达20 dB,但不能同时在两个方向上降低。当将谐振器的单极声场与风扇叶片的偶极声场结合时,就会出现这种现象。正在进行进一步的研究以将上述方法扩展到以产生更高阶风道模式的速度运行的高压风机。

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  • 来源
    《Journal of Vibration and Acoustics》 |2009年第2期|9-21|共13页
  • 作者

    Lee Gorny; Gary H. Koopmann;

  • 作者单位

    Department of Mechanical and Nuclear Engineering, The Pennsylvania State University, 157 Hammond Building, State College, PA 16802;

    Center of Acoustics and Vibrations, The Pennsylvania State University, 157 Hammond Building, State College, PA 16802rn;

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