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旋翼几何参数对共轴双旋翼悬停性能的影响

王强 陈铭 王保兵 苏兵兵

王强, 陈铭, 王保兵, 苏兵兵. 旋翼几何参数对共轴双旋翼悬停性能的影响[J]. 航空动力学报, 2014, (6): 1434-1443. doi: 10.13224/j.cnki.jasp.2014.06.025
引用本文: 王强, 陈铭, 王保兵, 苏兵兵. 旋翼几何参数对共轴双旋翼悬停性能的影响[J]. 航空动力学报, 2014, (6): 1434-1443. doi: 10.13224/j.cnki.jasp.2014.06.025
WANG Qiang, CHEN Ming, WANG Bao-bing, SU Bing-bing. Effect of geometric parameters of rotor on hovering performance of coaxial rotor[J]. Journal of Aerospace Power, 2014, (6): 1434-1443. doi: 10.13224/j.cnki.jasp.2014.06.025
Citation: WANG Qiang, CHEN Ming, WANG Bao-bing, SU Bing-bing. Effect of geometric parameters of rotor on hovering performance of coaxial rotor[J]. Journal of Aerospace Power, 2014, (6): 1434-1443. doi: 10.13224/j.cnki.jasp.2014.06.025

旋翼几何参数对共轴双旋翼悬停性能的影响

doi: 10.13224/j.cnki.jasp.2014.06.025
详细信息
    作者简介:

    王强(1986- ),男,四川绵阳人,博士生,主要从事直升机空气动力学、直升机飞行力学方面的研究.

  • 中图分类号: V211.52

Effect of geometric parameters of rotor on hovering performance of coaxial rotor

  • 摘要: 为研究旋翼几何参数对共轴双旋翼悬停性能的影响,建立了基于自由尾迹法和2阶升力线法的共轴双旋翼气动模型,分别计算和分析了共轴双旋翼的旋翼翼型、上下旋翼半径之比、上下旋翼间距、桨叶扭转角以及桨叶尖削比等参数对共轴双旋翼悬停性能的影响,最后基于分析结果综合优化了悬停状态下各旋翼的几何参数.结果表明:旋翼翼型、上下旋翼间距、桨叶扭转角以及桨叶尖削比对共轴双旋翼悬停性能有一定的影响,上下旋翼间距对其影响较小,综合优化旋翼在拉力系数为0.01时与基准旋翼相比,扭矩系数降低10.5%,悬停效率提高9.5%.

     

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出版历程
  • 收稿日期:  2013-06-17
  • 刊出日期:  2014-06-28

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