亚声速轴流风扇静子宽频辐射噪声预报与参数影响研究

武星宇,魏应三,靳栓宝,王东,祝昊,胡鹏飞,孙方旭

振动与冲击 ›› 2021, Vol. 40 ›› Issue (8) : 28-34.

PDF(1177 KB)
PDF(1177 KB)
振动与冲击 ›› 2021, Vol. 40 ›› Issue (8) : 28-34.
论文

亚声速轴流风扇静子宽频辐射噪声预报与参数影响研究

  • 武星宇,魏应三,靳栓宝,王东,祝昊,胡鹏飞,孙方旭
作者信息 +

Prediction and parameter study of rear-stator’s broadband radiated noise in subsonic axial fans

  • WU Xingyu,WEI Yingsan,JIN Shuanbao,WANG Dong,ZHU Hao,HU Pengfei,SUN Fangxu
Author information +
文章历史 +

摘要

为预报亚声速轴流风扇静子的宽频辐射噪声,介绍并推导了叶栅宽频辐射声功率计算表达式,考虑到工作在转子尾流中静子的情况,采用Park-Gauss尾流模型模拟转子尾流,建立转子尾流三维湍流波数频率谱模型,推导得到考虑转子尾流作用的静子宽频辐射声功率级计算公式。通过与Boeing和NASA风扇模型试验结果对比,结果显示上述公式较Hanson计算公式能够更准确的预报静子的宽频辐射声功率级,其预报结果与试验结果相差在5 dB以内。在NASA风扇模型的基础上改变静子叶片设计参数,显示减少静子叶片数可在高频段降低风扇的宽带噪声。

Abstract

To predict the broadband radiated noise of rear-stator’s in subsonic axial fans, a calculation formula of cascade broadband acoustic power was introduced and derived. On this base, considering the actual fan stator working in the rotor wake, the rotor wake turbulence wave spectrum model was established with the Park-Gauss wake model and the broadband acoustic power calculation formula of the interaction between the stator and the rotor was derived. The difference between the prediction result by above formula and the Boeing and NASA rear-stator test result is within 5 dB, and the prediction result is more accurate than the rear-stator broadband sound power predicted by the Hanson’s formula. For the NASA test model, reducing the blade number can suppression fan broadband noise at high frequencies.

关键词

静子 / 亚声速 / 转子尾流 / 叶片数 / 宽频辐射声功率

Key words

rear-stator / subsonic / rotor wake / blade number / broadband radiated acoustic power

引用本文

导出引用
武星宇,魏应三,靳栓宝,王东,祝昊,胡鹏飞,孙方旭. 亚声速轴流风扇静子宽频辐射噪声预报与参数影响研究[J]. 振动与冲击, 2021, 40(8): 28-34
WU Xingyu,WEI Yingsan,JIN Shuanbao,WANG Dong,ZHU Hao,HU Pengfei,SUN Fangxu. Prediction and parameter study of rear-stator’s broadband radiated noise in subsonic axial fans[J]. Journal of Vibration and Shock, 2021, 40(8): 28-34

参考文献

[1]王良锋, 乔渭阳, 纪良,等.风扇进口噪声预测模型的改进[J].推进技术,2015,36(2): 226-231.
WANG Liangfeng, QIAO Weiyang, JI Liang, et al. An improved prediction model for fan inlet noise[J]. Journal of Propulsion Technology, 2015,36(2): 226-231.
[2]WOODWARD R, HUGHES C, JERACKI R, et al. Fan noise source diagnostic test: far-field acoustic results[C]//8th AIAA/CEAS Aeroacoustics Conference & Exhibit. Breckenridge: AIAA, 2002.
[3]NALLASAMY M, ENVIA E. Computation of rotor wake turbulence noise[J]. Journal of Sound & Vibration, 2005,282(3): 649-678.
[4]MORIN B L. Broadband fan noise prediction system for turbofan engines. Volume 3: BFANS validation and test cases: CR-2010-216898[R]. Washington, D.C.: NASA, 2010.
[5]POSSON H, MOREAU S, ROGER M. Broadband noise prediction of fan outlet guide vane using a cascade response function[J]. Journal of Sound & Vibration, 2011,330(25): 6153-6183.
[6]FFOWCS WILLIAMS J E, HAWKINGS D L. Sound generation by turbulence and surfaces in arbitrary motion[J]. Philosophical Transcations of the Royal Society A, 1969,264(1151): 321-342.
[7]张建华, 楚武利, 刘炜.单级轴流风扇单音噪声源及噪声辐射特性的数值研究[J]. 动力工程学报, 2015,35(7): 574-580.
ZHANG Jianhua, CHU Wuli, LIU Wei. Numerical study on tone noise source and noise radiation characteristics of single stage axial flow fan[J]. Journal of Chinese Society of Power Engineering, 2015,35(7): 574-580.
[8]SEARS W R. Some aspects of non-stationary airfoil theory and its practical application[J]. Journal of Aeronautical Sciences, 1941,8(3): 104-108.
[9]WHITEHEAD D, MECH E M I. Vibration and sound generation in a cascade of flat plates in subsonic flow: CUED/A-Turbo/TR15[R]. Cambridge: Cambridge University Engineering Laboratory, 1972.
[10]SMITH S N. Discrete frequency sound generation in axial flow turbomachines[R]. [S.l.]: Aeronautical Research Council Reports and Memoranda, 1973.
[11]NAMBA M. Three-dimensional analysis of blade force and sound generation for an annular cascade in distorted flows[J]. Journal of Sound & Vibration, 1977,50(4): 479-508.
[12]乔渭阳. 桨扇近场噪声的FFT算法[J]. 航空学报, 1993,14(6): 254-262.
QIAO Weiyang. A numerical prediction method for the near-field harmonic noise of prop-fan[J]. Acta Aeronautica et Astronautica Sinica, 1993,14(6): 254-262.
[13]ZHANG W, WANG X, SUN X. A broadband noise model for turbulence/annular-cascade interaction[C]//AIAA/CEAS Aeroacoustics Conference. Berlin: AIAA,2013.
[14]ZHANG W G, WANG X Y, SUN X F. Predictions of fan broadband noise using lifting surface method[J]. AIAA Journal, 2015,53(10): 1-11
[15]左曙光, 何慧娟, 吴旭东, 等.叶片旋转噪声激励下漩涡风机壳体声辐射计算理论及分析[J]. 振动与冲击, 2015,34(24): 59-65.
ZUO Shuguang, HE Huijuan, WU Xudong, et al. Study of the regenerative blower’s shell sound radiation under the rotational noise excitation [J]. Journal of Vibration and Shock, 2015,34(24): 59-65.
[16]李晓东,段传波,于潮. 三维FW-H方程与CAA数值模拟匹配技术研究[J].工程热物理学报, 2005,26(1): 51-54.
LI Xiaodong, DUAN Chuanbo, YU Chao. On the matching technology between the 3D FW-H equation and CAA numerical simulations[J]. Journal of Engineering Thermophysics, 2005,26(1): 51-54.
[17]MANI R, HORVAY G. Sound transmission through blade[J]. Journal of Sound & Vibration, 1970,12(1): 59-83.
[18]KOCH W. On the transmission of sound waves through a blade row[J]. Journal of Sound & Vibration, 1971,18(1): 111-128.
[19]PEAKE N. The interaction between a high-frequency gust and a blade row[J]. Journal of Fluid Mechanics, 1992,241(1): 261-289.
[20]PEAKE N. The scattering of vorticity waves by an infinite cascade of flat plates in subsonic flow[J]. Wave Motion, 1993,18(3): 255-271.
[21]GLEGG S A L. The response of a swept blade row to a three-dimensional gust[J]. Journal of Sound & Vibration, 1999,227(1): 29-64.
[22]POSSON H, ROGER M, MOREAU S. On a uniformly valid analytical rectilinear cascade response function[J]. Journal of Fluid Mechanics, 2010,663: 22-52.
[23]POSSON H, ROGER M. Experimental validation of a cascade response function for fan broadband noise predictions[J]. AIAA Journal, 2012,49(9): 1907-1918.
[24]HANSON D B.Theory of broadband noise for rotor and stator cascade with inhomogeneous inflow turbulence including effects of lean and sweep: CR-210762[R]. Washington, D.C.: NASA, 2001.
[25]HANSON D B. Predicting broadband noise from a stator vane of a gas turbine engine: US 6353789 B1[P]. 2002-03-05.
[26]GANZ U, JOPPA P, PATTEN T, et al. Boeing 18-inch fan rig broadband noise test: CR-1998-208704[R]. Washington, D.C.: NASA, 1998.
[27]STEWART A L. Broadband fan noise generated by small scale turbulence: CR-207752[R]. Washington, D.C.: NASA, 1998.
 
 

PDF(1177 KB)

Accesses

Citation

Detail

段落导航
相关文章

/