单圆弧等厚叶片前后缘多元耦合仿生设计及降噪机理研究

刘小民; 赵嘉; 李典

doi:10.7652/xjtuxb201503001

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单圆弧等厚叶片前后缘多元耦合仿生设计及降噪机理研究

更新时间：2025-07-09

- 单圆弧等厚叶片前后缘多元耦合仿生设计及降噪机理研究
- Noise Reduction Mechanism of Single-Arc Bionic Blade with Wave Shape Leading Edge Coupled with Serrated Trailing Edge
- 西安交通大学学报 2015年49卷第3期页码：1-10
- 作者机构：
  
  西安交通大学能源与动力工程学院,西安,710049
- 作者简介：
- 基金信息：
  
  : 2014-07-20。作者简介: 刘小民(1971—),男,教授。基金项目: 高等学校博士学科点专项科研基金资助项目(20120201110064);陕西省科学技术研究发展计划资助项目(2014K06-24)
- DOI：10.7652/xjtuxb201503001
  中图分类号： TB535;TH432
- 网络首发：2015-03-10，
  
  纸质出版：2015
- 稿件说明：
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刘小民, 赵嘉, 李典. 单圆弧等厚叶片前后缘多元耦合仿生设计及降噪机理研究[J]. 西安交通大学学报, 2015,49(3):1-10.

Noise Reduction Mechanism of Single-Arc Bionic Blade with Wave Shape Leading Edge Coupled with Serrated Trailing Edge[J]. 2015, 49(3): 1-10.
刘小民, 赵嘉, 李典. 单圆弧等厚叶片前后缘多元耦合仿生设计及降噪机理研究[J]. 西安交通大学学报, 2015,49(3):1-10. DOI： 10.7652/xjtuxb201503001.

Noise Reduction Mechanism of Single-Arc Bionic Blade with Wave Shape Leading Edge Coupled with Serrated Trailing Edge[J]. 2015, 49(3): 1-10. DOI： 10.7652/xjtuxb201503001.

摘要

采用计算流体力学(CFD)方法和实验测量方法分别研究了多元耦合仿生叶片的降噪机理及其对多翼离心风机气动性能和噪声特性的影响。基于逆向工程设计方法

通过提取苍鹰翼翅前后缘典型结构特征

设计了一种前缘波形结构耦合尾缘齿形结构的仿生叶片

同时对仿生叶片和多翼离心风机用单圆弧等厚度叶片的气动性能及流动和噪声特性进行了数值分析

通过比较揭示了多元耦合仿生叶片的降噪机理

得到仿生叶片尾缘的齿形结构可改变叶片尾缘脱落涡结构和频率、前缘的非光滑波形结构可减小叶片表面脉动以及气流对叶片前缘的冲击等结果。相对于原型叶片

仿生叶片的基频和倍频均有所下降

仿生叶片的A计权声压级降低了2.1 dB。6种仿生叶片应用于多翼离心风机的实验研究表明:仿生叶片前后缘结构设计参数会影响多翼离心风机的风量、风压和噪声; 采用多元耦合仿生叶片

风机噪声最大下降1.5 dB

而风机的风量和风压基本不变。

Abstract

Noise-reduction mechanism for multi-factor coupling bionic design and the influence on aerodynamic performance and noise of multi-blade centrifugal fan are numerically and experimentally investigated. The noise-reduction characteristics of the leading edge and trailing edge structures of the goshawk wing are extracted

and multi-factor coupling bionic blade with the serrated trailing edge and non-smooth leading edge is designed by reverse reconstruction. The large eddy simulation coupled with the wall-adapting local eddy-viscosity model and the Ffowcs Williams-Hawkings equation are solved to simulate the flow field and the sound field of the bionic blade. By analyzing the flow characteristics

noise reduction mechanism of bionic blade is revealed. The serrated trailing edge structure alters the vortex shedding structure of the bionic blade to reduce the continuity and the shedding frequency

while the non-smooth leading structure effectively suppresses pressure fluctuation on blade surfaces and weakens airflow impact to leading edge of the bionic blade. Compared with the original blade

both the fundamental frequency and frequency multiplication of the bionic blade are reduced. A-weighted sound pressure level decreases by 2.1 dB. Six kinds of blade are applied to a multi-blade centrifugal fan

the effects of the blades with different structure parameters on the performance and noise are experimentally studied. It is found that the maximum noise of the multi-blade centrifugal fan decreases by 1.5 dB but the flow rate and pressure remain unchanged.

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Keywords

references

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