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Electric Motor Noise from Small Quadcopters: Part Ⅱ - Source Characteristics

机译:小型四轴飞行器的电动机噪声:第二部分-源特性

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The increased interest in electric motors for aircraft propulsion systems has driven interest in quantifying the contribution of electric motor noise to the overall sound levels and possibly human annoyance of the propulsion system. This work presents acoustic measurements of electric motors used for small quadcopters to quantify the sound produced by a number of outrunner motors with different types of controllers. Results are presented for loaded and unloaded motors as well as installed and uninstalled configurations. Motor resonance frequencies were measured and computed. Current probe measurements showed significant harmonic content in the supply current from the controllers for both the conventional and sinewave controllers. Acoustic results showed motor noise is typically radiated at frequencies near that for azimuthal vibration mode number 2 of the rotor which occurs at roughly 5000 Hz. Electric motor noise was evident in the spectra produced by many of the motor-controller combinations for motors loaded with propellers with levels often greater than those for the motor alone due to increases in the stator magnetic flux density with increased current. An installed quadcopter configuration produced increases in acoustic radiation over that of the uninstalled motor in a frequency range near the 1200 Hz azimuthal vibration mode 1 of the rotor.
机译:对用于飞机推进系统的电动机的兴趣的增加已经引起了对量化电动机噪声对推进系统的总体声级和可能的人类烦恼的贡献的兴趣。这项工作介绍了用于小型四轴飞行器的电动机的声学测量,以量化由许多采用不同类型控制器的离群电动机所产生的声音。列出了已加载和已卸载电机以及已安装和已卸载配置的结果。测量并计算出电机共振频率。电流探头的测量结果表明,对于常规控制器和正弦波控制器,控制器的电源电流中均含有大量谐波。声学结果表明,电动机噪声通常以接近于转子的2号方位振动模式的频率辐射,该频率发生在大约5000 Hz处。在许多装有螺旋桨的电动机中,由于定子磁通密度随电流的增加而增加,因此,在许多电动机-控制器组合所产生的频谱中,电动机噪声明显高于单个电动机。在接近转子的1200 Hz方位振动模式1的频率范围内,已安装的四旋翼飞机配置产生的声辐射比未安装的电动机的声辐射增加。

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