首页> 外文OA文献 >Flapping mechanism design and aerodynamic analysis for the flapping wing micro air vehicle
【2h】

Flapping mechanism design and aerodynamic analysis for the flapping wing micro air vehicle

机译:襟翼微型飞行器的拍击机构设计和空气动力学分析

摘要

This paper introduces a biological flapping micro air vehicle (FMAV) with four wings, instead of two wings, where wing clap-and-fling of real insects has been mimicked. The total weight is 2.236g. A spatial linkage is implemented in the flapping wing system, which is symmetry. This can prevent the flapping wing MAV from tilting toward the left or the right in the course of flight. By using the computational fluid dynamics (CFD), it has been confirmed that the flapping wing system can utilize the clap-and-fling mechanism, which is essential to enhance the lift and thrust in the insect flight.
机译:本文介绍了一种生物扑翼微型飞行器(FMAV),该飞行器具有四个机翼,而不是两个机翼,其中模仿了真实昆虫的机翼拍打和飞行。总重量为2.236克。在襟翼系统中实现了空间连接,这是对称的。这可以防止襟翼MAV在飞行过程中向左或向右倾斜。通过使用计算流体动力学(CFD),已确认拍打翼系统可以利用拍打和甩开机制,这对于增强昆虫飞行中的升力和推力至关重要。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号