超声马达驱动变弧度机翼的研究

Weidong Liu, Hua Zhu
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引用次数: 1

摘要

本文利用超声电机扭矩大、体积小、重量轻、自锁、响应快等优点,设计了一种由超声电机驱动的变弧度机翼。变形翼能够获得良好的气动效率,适用于低马赫数的小型无人机。设计了超声电机驱动的平行四边形连杆机构,并将其应用于变弧度机翼后缘驱动。该机构采用分布式布局,产生连续变形,可获得适合不同飞行状态的各种气动外形。马达独立布置在翼板内,分别驱动翼段变形。整个变形机构放置在机翼内部,并在机翼表面覆盖光滑的柔性蒙皮,以减小气动阻力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Research on variable camber wing driven by ultrasonic motors
Taking the Advantages of ultrasonic motors such as high torque, small size, light weight, self-lock and rapid response, a kind of variable camber wing driven by ultrasonic motors is designed in this paper. The morphing wing is suitable for small UAV of low Mach number because it is able to obtain a good aerodynamic efficiency. Parallelogram linkage driven by ultrasonic motor is designed and applied to the variable camber wing to drive the trailing edge. Distributed layout of the mechanism is adopted and continuous deformations can be produced, so various aerodynamic profiles suitable for different flying states can be obtained. The motors are arranged independently in the wing panel, and individually drive the wing sections to morph separately. The whole morphing mechanism is placed in the interior of the wing and the wing surface is covered with smooth flexible skin in order to decrease the aerodynamic drag.
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