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高速列车受电弓气动噪声分析与空腔降噪研究
引用本文:袁贤浦,苗晓丹,杨俭,袁天辰,袁丁. 高速列车受电弓气动噪声分析与空腔降噪研究[J]. 电子科技, 2022, 35(1): 45-52. DOI: 10.16180/j.cnki.issn1007-7820.2022.01.008
作者姓名:袁贤浦  苗晓丹  杨俭  袁天辰  袁丁
作者单位:1.上海工程技术大学 城市轨道交通学院,上海 2016202.上海工程技术大学 机械与汽车工程学院,上海 201620
基金项目:国家自然科学基金(U1834201)
摘    要:随着高速列车运行速度的不断提高,受电弓气动噪声也愈加严重。针对这一问题,文中采用LES大涡模拟、边界层噪声源模型和FW-H声类比法,通过建立某型号受电弓局部1:1气动噪声分析模型进行数值模拟。文中研究了受电弓各部位的气动噪声贡献量,还探究了针对较大噪声位置空腔采用射流降噪方法的降噪效果。结果表明,当网格总数为4 323万个时,数值模拟精确度满足要求。受电弓空腔上游和空腔中部绝缘子是气动噪声的主要来源。在射流降噪前后,空腔内部气动噪声均为宽频带噪声,主要能量集中在0~4 500 Hz。对250 km·h-1行驶速度下的空腔进行主动射流降噪,距列车25 m远处的垂向监测点声压级最小值为81.65 dB,比降噪前降低了2.64 dB。

关 键 词:高速列车  受电弓  气动噪声  大涡模拟  FW-H声学模型  数值模拟  宽频带噪声  射流降噪  
收稿时间:2020-10-03

Aerodynamic Noise Analysis for High-Speed Train' s Pantograph and Study on Noise Reduction of the Cavity of Pantograph
YUAN Xianpu,MIAO Xiaodan,YANG Jian,YUAN Tianchen,YUAN Ding. Aerodynamic Noise Analysis for High-Speed Train' s Pantograph and Study on Noise Reduction of the Cavity of Pantograph[J]. Electronic Science and Technology, 2022, 35(1): 45-52. DOI: 10.16180/j.cnki.issn1007-7820.2022.01.008
Authors:YUAN Xianpu  MIAO Xiaodan  YANG Jian  YUAN Tianchen  YUAN Ding
Affiliation:1. School of Urban Railway Transportation,Shanghai University of Engineering Science,Shanghai 201620,China2. School of Mechanical and Automotive Engineering,Shanghai University of Engineering Science, Shanghai 201620,China
Abstract:In view of the increasing speed of high-speed trains and the increasing aerodynamic noise of the pantograph, LES large eddy simulation, boundary layer noise source model and FW-H acoustic analogy method are used to carry out numerical simulation by establishing a local 1:1 aerodynamic noise analysis model of a certain type of pantograph. The contribution of aerodynamic noise of each part of the pantograph is studied, and the noise reduction effect of the jet noise reduction method for the cavity of the larger noise position is explored. The results show that the numerical simulation accuracy is accurate when the number of grids is 43.23 million. The insulator upstream of the pantograph cavity and the middle of the cavity are the main sources of aerodynamic noise. Before and after the jet noise reduction, the internal aerodynamic noise is broadband noise, the main energy is concentrated in 0~4 500 Hz. The inclined jet noise reduction is performed on the cavity at a traveling speed of 250 km·h-1, and the minimum sound pressure level of the vertical monitoring point 25 m away from the train is 81.65 dB, which is 2.64 dB lower than that before noise reduction.
Keywords:high-speed train  pantograph  aerodynamic noise  large eddy simulation  FW-H acoustic model  numerical simulation  broadband noise  jet noise reduction  
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