期刊文献+

仿鸟扑翼的功率消耗研究

Study on Power Consumption of Bird-like Flexible Flapping Wing
下载PDF
导出
摘要 为了提高仿鸟扑翼飞机的能量利用率,找到其最佳能量消耗参数,在风洞中对不同来流速度下模型的扭矩与功率消耗两个重要物理量进行了测量,找出功率消耗随风速的变化关系。实验使用了一个曲柄连杆扑翼模型。模型的扑翼采用平面结构布局,并且具有一定柔性。实验分别测试模型在不同风速下扑翼扑动的需用扭矩和功率,结果显示在风速2~16 m/s之间,模型的扑动扭矩和功率随风速的增加都逐渐减小,其中需用扭矩最大减小量约为30%。这一发现可以降低扑翼机对发动机推重比的要求,也可以降低对扑翼材料的力学要求。这在一定程度上解释了鸟类迁徙节能的原因,也对扑翼飞机的发展具有一定促进作用。 To improve the energy utilization rate of the aircraft with bird-like flapping wings,and find its optimal energy consumption parameters,the two important physical indicators of torque and power consumption of the model were measured at different inflow velocities in the wind tunnel,finding the relation between the power consumption and the change of the wind speed. A crank-link flapping wing model was used in the experiment. The flapping wing of the model is planar and has a certain flexibility. The tests were carried out respectively to determine the torque and power required for flapping of the flapping wing at different wind speeds. The results showed that the torque and power required for flapping of the model decreased with the increase of the wind speed when the wind speed range is within 2 to 16 m/s,of which the maximum reduction in torque was about 30%. This discovery not only can reduce the requirement on the thrust-weight ratio of engine by an ornithopter,but also can reduce the mechanical requirement on the material of the flapping wing. This explains to some extent the reasons for the energy efficiency of the migration of birds,and has a certain role in promoting the development of aircraft with flapping wings.
出处 《机械科学与技术》 CSCD 北大核心 2017年第S1期44-48,共5页 Mechanical Science and Technology for Aerospace Engineering
关键词 流体力学 扑翼 柔性 扭转 功率 扭矩 效率 fluid mechanics flapping wing flexibility twisting power torque efficiency
  • 相关文献

参考文献3

二级参考文献19

  • 1ANG HaiSong,XIAO TianHang,DUAN WenBo.Flight mechanism and design of biomimetic micro air vehicles[J].Science China(Technological Sciences),2009,52(12):3722-3728. 被引量:8
  • 2李占科,宋笔锋,张亚锋.微型飞行器空气动力学研究[J].系统工程理论与实践,2005,25(9):137-141. 被引量:5
  • 3曾锐,昂海松,梅源,季健.扑翼柔性及其对气动特性的影响[J].计算力学学报,2005,22(6):750-754. 被引量:21
  • 4左德参,彭松林,张卫平,陈文元.扑翼微飞行器飞行时的数值模拟与分析(英文)[J].空气动力学学报,2007,25(1):125-131. 被引量:4
  • 5KATZ J,PLOTKIN A.Low Speed Aerodynamics:From Wing Theory to Panel Methods[M].McGraw-Hill Book Co.,New York,1991.
  • 6GIESING.Nonlinear two-dimension unsteady potential flow with lift[J].Journal of Aircraft,1968,5(2):135-143.
  • 7BASU.The unsteady motion of a two-dimension aerofoil in incompressible inviscid flow[J].Journal of Fluid Mechanics,1978,87(1):159-178.
  • 8HALL K C,PIGOTT S A.Power requirements for large-amplitude flapping flight[J].Journal of Aircraft,1998,35(3):352-361.
  • 9TOBALAKE D.Flight kinematics of black-billed magpies and pigeons over a wide range of speeds[J].Journal of Experimental Biology,1996,199(2):263-280.
  • 10DAVID Attenborouch.The Mastery of Flight[M].BBC VCD,ISRC CN-A01-01-0010-0/V.G3.

共引文献29

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部