扑翼飞行器具有弹性阻尼扑动机构的能耗对比分析与研究

doi:10.7527/S1000-6893.2018.21966

材料工程与机械制造

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扑翼飞行器具有弹性阻尼扑动机构的能耗对比分析与研究

张威^1,2, 刘光泽¹, 张博利³

1. 中国民航大学航空工程学院, 天津 300300;
2. 中国民航航空地面特种设备研究基地, 天津 300300;
3. 中国民航大学基础实验中心, 天津 300300

收稿日期:2017-12-22 修回日期:2018-01-28 出版日期:2018-09-15 发布日期:2018-05-28
通讯作者: 张威 E-mail:drwadecheung@gmail.com
基金资助:
国家自然科学基金委员会与中国民航局联合资助项目（U1533103）；中央高校基本科研业务费（3122017049）

Energy consumption comparative analysis and research of flapping wing vehicle with elastic damping flapping mechanism

ZHANG Wei^1,2, LIU Guangze¹, ZHANG Boli³

1. College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China;
2. Aviation Ground Special Equipment Research Base, Tianjin 300300, China;
3. Basic Experiment Center, Civil Aviation University of China, Tianjin 300300, China

Received:2017-12-22 Revised:2018-01-28 Online:2018-09-15 Published:2018-05-28
Supported by:
National Natural Science Foundation of China, Civil Aviation Administration of China (U1533103); the Fundamental Research Funds for the Central Universities (3122017049)

摘要/Abstract

摘要： 以"Sparrow"微小仿生扑翼飞行器（FWMAV）为基础，提出了3种带弹性元件的扑动机构构型。对原构型和3种弹性构型进行的理论研究及仿真试验发现，安装有弹性元件的仿生扑翼机构不仅可以在很大程度上减小电机输入的峰值转矩，而且能凭借减小峰值转矩的最优构型提高能量利用率。同时，原模型在翅翼下扑阶段所产生的冲击力大而上扑阶段所产生的冲击力小，电机因负载不均在快速运转时易受冲击。引入弹性元件后，可有效减小电机所受到的冲击力，降低机体材料的冲击及疲劳损伤，延长其使用寿命；对峰值力的优化还可以降低噪声，减小飞行时被发现的几率，提高其在战场环境中的生存率。这将为扑翼飞行器由理论向工程应用过渡提供基础。

关键词: 微小扑翼飞行器, 柔性系统, 峰值转矩, 能量利用率, 降噪

Abstract: Three flexible flapping mechanism configurations are herein proposed for the model of "Sparrow" Flapping Wing Micro Air Vehicle (FWMAV). Analytical research and simulation tests on the original model and the three proposed configurations unveil that an FWMAV with a flexible flapping mechanism can greatly reduce the peak torque of motor input, and then improve energy efficiency. In addition, when running rapidly without the flexible system, the motor of a FWMAV is found easy to get shocked by uneven loads due to a smaller impact force at the stage of down flapping and a bigger one at the stage of up flapping. When an elastic component is introduced into the vehicle, the impact force effected on the motor and the flapping mechanism reduces effectively. The service life of the vehicle can be consequently prolonged. It is also shown that the proposed flexible flapping mechanisms have lower noises, meaning that the survival rate of the vehicles in the battlefield environment will be raised up. This study lays a foundation for applications of the FWMAV model.

Key words: flapping wing micro air vehicle, flexible system, peak torque, energy efficiency, noise reduction

中图分类号:

V276

张威, 刘光泽, 张博利. 扑翼飞行器具有弹性阻尼扑动机构的能耗对比分析与研究[J]. 航空学报, 2018, 39(9): 421966-421979.

ZHANG Wei, LIU Guangze, ZHANG Boli. Energy consumption comparative analysis and research of flapping wing vehicle with elastic damping flapping mechanism[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(9): 421966-421979.

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

扑翼飞行器具有弹性阻尼扑动机构的能耗对比分析与研究

Energy consumption comparative analysis and research of flapping wing vehicle with elastic damping flapping mechanism

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