非对称锯齿结构对叶片气动声学性能的影响

李一枭, 陈坤, 高瑞彪, 冯文慧, 许宁

太阳能学报 ›› 2022, Vol. 43 ›› Issue (12) : 336-343.

PDF(3745 KB)
欢迎访问《太阳能学报》官方网站,今天是
PDF(3745 KB)
太阳能学报 ›› 2022, Vol. 43 ›› Issue (12) : 336-343. DOI: 10.19912/j.0254-0096.tynxb.2021-0656

非对称锯齿结构对叶片气动声学性能的影响

  • 李一枭1, 陈坤1, 高瑞彪1, 冯文慧1, 许宁2
作者信息 +

INFLUENCE OF ASYMMETRIC SAWTOOTH STRUCTURE ON AEROACOUSTIC PERFORMANCE OF BLADE OF WIND TURBINE

  • Li Yixiao1, Chen Kun1, Gao Ruibiao1, Feng Wenhui1, Xu Ning2
Author information +
文章历史 +

摘要

为降低水平轴风力机叶片的气动噪声,受鸮类静音飞行能力的启发,提取鸮类翅膀羽毛的非对称锯齿结构,并重构于风力机叶片尾缘处。采用大涡模拟(LES)和FW-H方程对改型叶片和原型叶片的流场及声场特性分别进行研究。同时通过改变非对称锯齿尾缘的结构参数,以探究不同锯齿夹角、锯齿宽度和锯齿间距对非对称锯齿尾缘的降噪效果的影响。结果显示:非对称锯齿尾缘具有较好的降噪效果,尤其是在低频和中频区域,总声压级最多可降低10 dB。当锯齿夹角分别为30°、40°和50°时,随着锯齿夹角的增加,噪声声压级在多数方位角下呈增加的趋势;锯齿宽度分别为10、12.5和15 mm时,随着锯齿宽度的增加,噪声声压级在多数方位角下明显降低;锯齿间距的改变,对0°方位角下的噪声声压级影响显著。而从涡分布图中可发现,非对称锯齿尾缘未改变叶片表面涡脱落的位置,但会减小涡结构和涡强度,增大涡间距,从而抑制噪声的产生。

Abstract

To reduce the aerodynamic noise of horizontal axis wind turbine blade, inspired by the quiet flight ability of owls, the asymmetric sawtooth structure of owl wing feather was been extracted and reconstructed for the trailing edge of wind turbine blade. Large eddy simulation (LES) and FW-H equation were used to analyze the flow field and sound field characteristics of the modified blade and the prototype blade. Meanwhile, the noise reduction efficiency of the blade with asymmetric sawtooth trailing edge under different structural parameters were explored. The changing structural parameters include sawtooth angle, sawtooth width and sawtooth space. The results show that the asymmetric sawtooth trailing edge has excellent effect on noise reduction, especially in the low and intermediate frequency regions. The overall sound pressure level can be reduced by 10 dB at most. When the sawtooth angle is 30°, 40° and 50°, with the increase of the sawtooth angle, the sound pressure level shows an increasing trend in most azimuth angles. When the sawtooth width is 10mm, 12.5 mm and 15 mm, with the increase of the saw tooth width, the sound pressure level decreases significantly in most azimuths. The change of saw tooth spacing has a significant impact on the noise sound pressure level at 0°azimuth angle. From the vortex distribution, it can be found that the asymmetric sawtooth trailing edge does not change the position of vortex shedding on the blade surface, but it will reduce the vortex structure and vortex intensity, increase the vortex spacing, so as to suppress the generation of noise.

关键词

气动声学 / 风力机 / 叶片 / 仿生学 / 非对称锯齿尾缘 / 计算流体力学

Key words

aeroacoustics / wind turbine / blades / bionics / asymmetric sawtooth trailing edge / computational fluid dynamics

引用本文

导出引用
李一枭, 陈坤, 高瑞彪, 冯文慧, 许宁. 非对称锯齿结构对叶片气动声学性能的影响[J]. 太阳能学报. 2022, 43(12): 336-343 https://doi.org/10.19912/j.0254-0096.tynxb.2021-0656
Li Yixiao, Chen Kun, Gao Ruibiao, Feng Wenhui, Xu Ning. INFLUENCE OF ASYMMETRIC SAWTOOTH STRUCTURE ON AEROACOUSTIC PERFORMANCE OF BLADE OF WIND TURBINE[J]. Acta Energiae Solaris Sinica. 2022, 43(12): 336-343 https://doi.org/10.19912/j.0254-0096.tynxb.2021-0656
中图分类号: TB535   

参考文献

[1] HOWE M S.Aerodynamic noise of a serrated trailing edge[J]. Journal of fluids and structures, 1991, 5(1): 33-45.
[2] LILLEY G.A study of the silent flight of the owl[C]//4th AIAA/CEAS Aeroacoustics Conference, Toulouse, France, 1998: 1-6.
[3] DASSEN T, PARCHEN R, BRUGGEMAN J, et al.Results of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edges[R]. Germany: NLR, NLR TP 96350, 1996.
[4] BRAU K A, VAN DER BORG N, DESSAN A G M, et al. Noise reduction by using serrated trailing edge[C]//European Wind Energy Conference, Dublin, Ireland, 1997: 472-475.
[5] OERLEMANS S, FISHER M, MAEDER T, et al.Reduction of wind turbine noise using optimized airfoils and trailing-edge serrations[J]. AIAA journal, 2009, 47(6): 1470-1481.
[6] GRUBER M, JOSEPH P, CHONG T P.Experimental investigation of airfoil self noise and turbulent wake reduction by the use of trailing edge serrations[C]//16th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, 2010: 7-9.
[7] CHONG T P, JOSEPH P E, GRUBER M.Airfoil self-noise reduction by non-flat plate type trailing edge serrations[J]. Applied acoustics, 2013, 74: 607-613.
[8] 刘小民, 汤虎, 王星, 等. 苍鹰翼尾缘结构的单元仿生叶片降噪机理研究[J]. 西安交通大学学报, 2012, 46(1): 35-41.
LIU X M, TANG H, WANG X, et al.Noise-reduction mechanism of bionic coupling blade based on the trailing edge of goshawk wing[J]. Journal of Xi’an Jiaotong University, 2012, 46(1): 35-41.
[9] 仝帆, 乔渭阳, 王良锋, 等. 仿生学翼型尾缘锯齿降噪机理[J]. 航空学报, 2015, 36(9): 2911-2922.
TONG F, QIAO W Y, WANG L F, et al.Noise reduction mechanism of bionic airfoil trailing edge serrations[J]. Acta aeronautica et astronautica sinica, 2015, 36(9): 2911-2922.
[10] CHEN E Y, MA Y, YANG A Y, et al.Experimental investigation on noise emissions of an airfoil with non-flat plate trailing edge serrations[J]. Journal of mechanical science and technology, 2019, 33(7): 3069-3074.
[11] 汪瑞欣, 赵振宙, 王同光, 等. 锯齿尾缘DU91-W2-250风力机翼型气动及噪声特性分析[J]. 太阳能学报, 2020, 41(12): 221-228.
WANG R X, ZHAO Z Z, WANG T G, et al.Research on aerodynamics and noise characteristics of DU91-W2-250 airfoil of wind blade with serrated trailing edge[J]. Acta energiae solaris sinica, 2020, 41(12): 221-228.
[12] 许影博, 李晓东, 何敬玉. 刷毛翼型尾缘噪声控制实验研究[J]. 南京航空航天大学学报, 2011, 43(5): 612-616.
XU Y B, LI X D, HE J Y.Experiment on noise control of trailing edge brushes[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2011, 43(5): 612-616.
[13] FINZE A, JACOB M, JONDEAU E, et al.Broadband noise reduction with trailing edge brushes[C]//16th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, AIAA, 2010.
[14] GEYER T, SARRADJ E, FRITZSCHE C.Porous Airfoils: noise reduction and boundary layer effects[J]. International journal of aeroacoustics, 2009, 9(6): 787-820.
[15] KOH S R, ZHOU B, MEINKE M, et al.Numerical analysis of the impact of variable porosity on trailing edge noise[J]. Computers and fluids, 2018, 167: 66-81.
[16] 久保大次郎. 小型风力发电机设计与制作[M]. 姚兴佳, 王益全, 译. 北京: 科学出版社, 2012.
[17] CHEN K, LIU Q P, LIAO G H, et al.The sound suppression characteristics of wing feather of owl(Bubo bubo)[J]. Journal of bionic engineering, 2012, 9: 192-199.

基金

国家自然科学基金(51765062); 新疆维吾尔自治区高校科研计划(XJEDU2017S013)

PDF(3745 KB)

Accesses

Citation

Detail

段落导航
相关文章

/