带有扑翼的微型飞行器

Lung-Jieh Yang, Cheng-Kuei Hsu, Jen-Yang Ho, Hsin-Hsiung Wang, Gwo-Hwa Feng
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引用次数: 5

摘要

微型飞行器的研究是低雷诺数流研究的一个新领域,在先进航空领域受到广泛关注。许多天生的飞行者证明,扑翼是飞行小于6英寸物体的最合适方式。然而,扑翼的非定常气动特性研究仍有很大的空间。扑翼重量轻,强度高,最初由钛合金框架和聚二甲苯表皮组成。这样的集成制造需要MEMS加工的帮助。此外,机翼制造后的扑动试验和智能机翼蒙皮的相应信号分析为本项目画上了圆满的一笔,为不久的将来进行风洞验证/修正奠定了基础。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The micro aerial vehicle (MAV) with flapping wings
The research of micro aerial vehicles (MAVs) is a new field of low-Reynolds-number flow, which attracts much attention in the advanced aeronautical area. The flapping wing, proved by many natural flyers, is the most appropriate way of flying objects which sizes are less than 6 inches. However, there is still plenty of room for studying on the unsteady aerodynamic characteristics of flapping wings. The flapping wing, which is light weighted and high strengthened, is originally composed of the titanium-alloy frame and the parylene skin. Such an integration of fabrication needs the help of MEMS processing. Additionally, the flapping test after the wing fabrication and the corresponding signal analysis from the smart wing skin concluded this project and set the bases for the wind-tunnel verification/correction in the very near future.
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