The effect of folding on motion flapping wing aero vehicle

Do Young Kim, D. Yun
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引用次数: 2

Abstract

An interesting about MAV and a research for flapping wing aero vehicle has been increased. It is required that take-off and landing abilities to lift up a vehicle by flapping motion to achieve a special purpose for flapping wing aero vehicle. An airfoil has to generate lift force more than a weight of the body to work take-off from the ground without additional force. MAV can generate enough lift force, abilities of MAV: load capacity, reliability, damage reduction. In this study, we propose a four-bar linkage structure to generate lift force. And an experiment will be set up to measure the lift force with a folding mechanism of flapping wing. After this, the result will be used for development of nature-inspired bird robot.
折叠对扑翼飞行器运动的影响
近年来,人们对微型飞行器和扑翼飞行器的研究越来越感兴趣。为了实现扑翼飞行器的特殊目的,对扑翼飞行器的起降能力提出了要求。机翼必须产生超过身体重量的升力才能在没有额外力的情况下从地面起飞。MAV能产生足够的升力,MAV的能力:承载能力、可靠性、减损性。在这项研究中,我们提出了一个四杆连杆结构来产生升力。并利用扑翼折叠机构进行升力测量实验。在此之后,研究结果将用于开发大自然启发的鸟类机器人。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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