National Key Laboratory of Vehicular Transmission, Beijing Institute of Technology, Beijing 100081, People's Republic of China.
Beijing Institute of Technology, Institute of advanced Technology, Jinan, People's Republic of China.
Bioinspir Biomim. 2022 Aug 17;17(5). doi: 10.1088/1748-3190/ac7afd.
This paper presents the principle of motion, mechanical modeling and key characteristics of the propulsive force of a new flexible-fin traveling wave propulsion mechanism used in an amphibious robot. Firstly, the form of motion and the basic propulsion principle of traveling wave propulsion of flexible fins on the ground are described. During fluctuation of the flexible fins, the relative motion between the outermost contact line on the fin surface and the ground generates the propulsive force of forward motion and the lateral force along the fin surface. Based on the laws of flexible-fin fluctuation kinematics and the basic principles of friction mechanics, the propulsion mechanics model of flexible fins during traveling wave propulsion on the ground is established. By numerically solving the propulsive force equation, the relationship between the propulsive force of the flexible fin and the motion parameters of the fin surface can be obtained. Numerical calculations combined with the results of experimental tests reveal that the flexible-fin propulsive force shows periodic variations within one fluctuation period of the fin surface, and the variation period is related to the number of waves present on the fin surface. The wavenumber on the fin surface has a large impact on the fluctuation amplitude of the propulsive force. In the range of 1.6-1.9 waves on the fin surface, the average propulsive force is the most ideal, while in the range of fin-surface inclinations less than 50° and fluctuation amplitudes greater than 30°, the propulsive force of the flexible fin is the ideal parameter range. This research provides theoretical support for the design of a flexible-fin traveling wave propulsion mechanism.
本文介绍了一种新型柔性翼片波状游动推进机构在两栖机器人中的运动原理、力学建模和关键推进力特性。首先,描述了柔性翼片在地面上的运动形式和波状游动推进的基本推进原理。在柔性翼片波动过程中,翼片表面最外接触线与地面之间的相对运动产生了前进运动的推进力和沿翼片表面的侧向力。基于柔性翼片波动运动学规律和摩擦力学基本原理,建立了柔性翼片在地面波状游动推进的推进力学模型。通过数值求解推进力方程,可以得到柔性翼片推进力与翼面运动参数之间的关系。数值计算与实验测试结果相结合表明,柔性翼片的推进力在翼面波动周期内呈现周期性变化,且变化周期与翼面的波数有关。翼面波数对推进力的波动幅度有较大影响。在翼面波数为 1.6-1.9 个波的范围内,平均推进力最理想,而在翼面倾斜角度小于 50°且波动幅度大于 30°的范围内,柔性翼片的推进力是理想的参数范围。本研究为柔性翼片波状游动推进机构的设计提供了理论支持。