Šišovas Laurynas, Čeponis Andrius, Mažeika Dalius, Borodinas Sergejus
Department of Aeronautical Engineering, Antanas Gustaitis' Aviation Institute, Vilnius Gediminas Technical University, LT-10223 Vilnius, Lithuania.
Institute of Mechanical Science, Faculty of Mechanics, Vilnius Gediminas Technical University, LT-10223 Vilnius, Lithuania.
Micromachines (Basel). 2024 Dec 14;15(12):1495. doi: 10.3390/mi15121495.
This paper presents the design, development, and investigation of a novel piezoelectric inertial motor whose target application is the low Earth orbit (LEO) temperature conditions. The motor utilizes the inertial stick-slip principle, driven by the first bending mode of three piezoelectric bimorph plates, and is compact and lightweight, with a total volume of 443 cm and a mass of 28.14 g. Numerical simulations and experimental investigations were conducted to assess the mechanical and electromechanical performance of the motor in a temperature range from -20 °C to 40 °C. The results show that the motor's resonant frequency decreases from 12,810 Hz at -20 °C to 12,640 Hz at 40 °C, with a total deviation of 170 Hz. The displacement amplitude increased from 12.61 μm to 13.31 μm across the same temperature range, indicating an improved mechanical response at higher temperatures. The motor achieved a maximum angular speed up to 1200 RPM and a stall torque of 13.1 N·mm at an excitation voltage amplitude of 180 V. The simple and scalable design, combined with its stability under varying temperature conditions, makes it well suited for small satellite applications, particularly in precision positioning tasks such as satellite orientation and free-space optical (FSO) communications.
本文介绍了一种新型压电惯性电机的设计、开发和研究,其目标应用是低地球轨道(LEO)温度条件。该电机利用惯性粘滑原理,由三个压电双晶片的第一弯曲模式驱动,结构紧凑、重量轻,总体积为443立方厘米,质量为28.14克。进行了数值模拟和实验研究,以评估该电机在-20°C至40°C温度范围内的机械和机电性能。结果表明,电机的共振频率从-20°C时的12810赫兹降至40°C时的12640赫兹,总偏差为170赫兹。在相同温度范围内,位移幅度从12.61微米增加到13.31微米,表明在较高温度下机械响应有所改善。在180伏的激励电压幅度下,该电机实现了高达1200转/分钟的最大角速度和13.1牛·毫米的堵转扭矩。这种简单且可扩展的设计,加上其在不同温度条件下的稳定性,使其非常适合小型卫星应用,特别是在卫星定向和自由空间光(FSO)通信等精密定位任务中。