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动态入流对叶片气动性能和叶面压力分布影响的数值分析
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  • 英文篇名:Numerical analysis of the influence of aerodynamic performance and pressure distribution on the blade surface under dynamic inflow
  • 作者:马剑龙 ; 李学彬 ; 吕文春 ; 吴雨晴 ; 汪建文
  • 英文作者:Ma Jianlong;Li Xuebin;Lv Wenchun;Wu Yuqing;Wang Jianwen;School of Energy and Power Engineering, Inner Mongolia University of Technology;Technology and Vocational Education Research Center, Inner Mongolia Technical College of Mechanics and Electrics;
  • 关键词:动态入流 ; 叶片 ; 气动性能 ; 压力分布 ; 数值分析
  • 英文关键词:dynamic inflow;;blade;;aerodynamic performance;;pressure distribution;;numerical simulation
  • 中文刊名:NCNY
  • 英文刊名:Renewable Energy Resources
  • 机构:内蒙古工业大学能源与动力工程学院;内蒙古机电职业技术学院科技与职教研究中心;
  • 出版日期:2019-05-10 14:18
  • 出版单位:可再生能源
  • 年:2019
  • 期:v.37;No.249
  • 基金:内蒙古自治区高等学校青年科技英才支持计划项目(NJYT-17-B24);; 内蒙古自治区高等学校科学技术研究项目(NJZY18271,19270);; 内蒙古机电职业技术学院自然科学研究项目(NJDZJZR1802,1805)
  • 语种:中文;
  • 页:NCNY201905016
  • 页数:8
  • CN:05
  • ISSN:21-1469/TK
  • 分类号:100-107
摘要
基于稳定风、渐变风、阵风等入流方式,建立了不同变风阶段叶片气动载荷非稳态计算模型,研究了不同风速变化速率对叶片气动性能以及叶面压力分布的影响规律。研究结果表明,在相同风速下,不同风速变化率会对风轮输出转矩产生影响,且风的加速度越大,其影响越显著。同风速下的压力面渐变风压力小于稳定入流压力,且两种入流方式的压力差随展向位置逐渐增大,而吸力面上的压力分布差异较小,但压力变化梯度随展向位置却有明显不同。阵风入流中,在相同风速的阵风加速与阵风减速时刻,压力面、吸力面的压力分布差异较大,但其压差随叶片展向位置波动较小;在叶根到叶片展向位置0.7R处,阵风加速出力大于阵风减速;在0.7R处到叶尖位置,阵风减速出力效果相对更好。
        Unsteady calculation model of blade aerodynamic loads at different stages of variable wind are established based on steady, gradual and gust inflow modes, and the effects of different wind speed variation rates on aerodynamic performance and aerodynamic load distribution of blades are studied. The results show that the output torque of the wind turbine will be affected by different wind speed variations at the same wind speed, and the greater the wind acceleration, the more significant the impact. At the same wind speed, the gradual wind pressure on the pressure surface is less than the steady inflow pressure, and the pressure difference between the two inflow modes increases gradually with the spanwise position, while the discrepancy of pressure distribution on suction surface is small, the pressure gradient is obviously different with the spanwise position. In gust inflow, when gust acceleration and gust deceleration occur at the same wind speed, the pressure distribution on pressure surface and suction surface is quite different,however, the pressure difference varies slightly with the blade orientation. The gust acceleration output is greater than the gust deceleration at 0.7 R from the blade root to the blade extension position, and the deceleration output of gust is better at 0.7 R to blade tip position.
引文
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