扑翼蝴蝶机器人机翼气动力分析

2020 International Conference on Electronics, Information, and Communication (ICEIC) Pub Date : 2020-01-01 DOI:10.1109/ICEIC49074.2020.9051389

K. Sukvichai, Kan Yajai

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引用次数: 4

摘要

可飞行机器人的行为总是让人类惊叹不已。扑翼机器人的设计非常复杂，需要考虑机翼的空气动力学和气动弹性。在本研究中，对机翼截面气动力进行了解释。为了得到作用在蝴蝶各翼段上的升力和推力，推导和估计了几个气动方程。利用一个扑动周期的平均升力来设计原型蝴蝶机器人的机翼结构和运动。机翼结构是根据真实的蝴蝶翅膀尺寸设计的。为了达到机翼的刚性和薄翼型的性能，机翼是由增强的层流塑料片。考虑到分离伺服驱动扑动机构的灵活性和性能，本研究选择了分离伺服驱动扑动机构。最后，设计了原型蝶翼。

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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Aerodynamics Force Analysis for Designing a Flapping Butterfly Robot Wing

Flyable robots are always amazed human because its behavior. Designing a flapping wing robot is complex since wing aerodyanamics and aeroelastics have to be considered. In this research, wing section aerodynamics forces are explained. Several aerodynamic equations are derived and estimated in order to obtain lift and thrust forces that acted on each butterfly wing section. Average lift force over one flapping cycle is used to design the prototype butterfly robot wing structure and motion. Wing structure is designed based on the real butterfly wing dimension. Wing was made by a reinforced laminar plastic sheet in order to achieve wing's rigidity and properties of thin airfoil. Separated servo driven flapping mechanism is selected in this research due to its flexibility and performance. Finally, prototype butterfly wing is designed.

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来源期刊

2020 International Conference on Electronics, Information, and Communication (ICEIC)

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