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小型風(fēng)力機(jī)翼羽仿生耦合槳葉結(jié)構(gòu)研究
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國家高技術(shù)研究發(fā)展計(jì)劃(863計(jì)劃)資助項(xiàng)目(2012AAxxx0902)和吉林省科技發(fā)展計(jì)劃資助項(xiàng)目(20120415)


Investigation of Bionic Coupling Blades Structure for Small Wind Turbine Wing Feathers
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    摘要:

    針對(duì)小型風(fēng)力發(fā)電機(jī)葉片徑向氣流利用率低的問題,采用仿生耦合技術(shù),對(duì)長耳鸮翼羽結(jié)構(gòu)加以研究。利用3D Scanner激光掃描儀系統(tǒng)逆向重構(gòu)了鸮的翼羽結(jié)構(gòu),建立了仿生耦合槳葉結(jié)構(gòu)模型,通過對(duì)NACA 0015基準(zhǔn)翼型和仿生翼型進(jìn)行對(duì)比計(jì)算,發(fā)現(xiàn)仿生翼型的升力隨著節(jié)距與弦長比值s/c的減小而增加,當(dāng)仿生耦合翼型節(jié)距與弦長比值s/c=0.33時(shí),失速攻角達(dá)到16°,最大升力系數(shù)約為1.26,比基準(zhǔn)翼型高 13.5%。

    Abstract:

    With the aim to solve the specific problem of low utilization rate of small wind turbine generator blade radial flow, in order to investigate the long eared owl wing structure, the bionic coupling technology was adopted. The wing structure of the reverse reconstruction for the long eared owl was built by 3D Scanner laser scanner system and the bionic coupling blades structure theory model was established based on the wing feathers of sequential arrangement way. Through the comparison of the baseline NACA 0015 airfoil and the bionic coupling blades structure airfoil, the lift coefficient for the bionic coupling blades structure airfoil increases with blade pitch and chord length ratio s/c decreases. When s/c=0.33, the CL value is the highest at α=16°, CL=1.26, which increases by 13.5% than baseline foil.

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高藝,徐成宇,曹國華.小型風(fēng)力機(jī)翼羽仿生耦合槳葉結(jié)構(gòu)研究[J].農(nóng)業(yè)機(jī)械學(xué)報(bào),2014,45(6):193-197. Gao Yi, Xu Chengyu, Cao Guohua. Investigation of Bionic Coupling Blades Structure for Small Wind Turbine Wing Feathers[J]. Transactions of the Chinese Society for Agricultural Machinery,2014,45(6):193-197.

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  • 收稿日期:2014-03-17
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  • 在線發(fā)布日期: 2014-06-10
  • 出版日期: 2014-06-10