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Effect of Local Constraint on Driving Torque of Driving Mechanism for Half-rotating Wing

机译:局部约束对半旋翼驱动机构驱动力矩的影响

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Half-rotating wing (HRW) is a new kind of flapping wing system with rotating-type flapping instead of oscillating-type flapping. For the complex mechanical transmission and high weight which is not suitable for flight of traditional half-rotating mechanism (HRM).The simplified HRM with local constraint was proposed as the driving mechanism of HRW in this paper. The performing process and characteristics of local constraint was further given. According to contact state between moving components, the performing process of local constraint was divided into two stages. To analyze the influence of local constraint on the driving torque exerted in the crank of driving mechanism, the model of driving torque under different stages were respectively established. Based on the model, the change curve of driving torque was obtained through simulation by MATLAB, which showed that local constraint had little influence on driving torque. The results could provide guidance for the choice of motor of HRW and optimization of dynamics.
机译:半旋翼(HRW)是一种新型的襟翼系统,其具有旋转式襟翼而不是摆动式襟翼。由于机械传动复杂,重量大,不适合传统的半旋转机构的飞行。本文提出了一种具有局部约束的简化HRM作为HRW的驱动机构。进一步给出了局部约束的执行过程和特点。根据运动部件之间的接触状态,将局部约束的执行过程分为两个阶段。为了分析局部约束对施加在驱动机构曲柄上的驱动扭矩的影响,分别建立了不同阶段的驱动扭矩模型。在该模型的基础上,通过MATLAB仿真得到了驱动转矩的变化曲线,表明局部约束对驱动转矩的影响很小。研究结果可为HRW电机的选择和动力学优化提供指导。

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