Filtering Suppression for Large Peak Conducted EMI From High-Speed Axial Flow Fan

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-10-17 DOI:10.1109/TAES.2024.3483155
Jinsheng Yang;Yanhong Wei;Xuan Zhao;Zeyu Pan;Bao-Lin Nie;Pingan Du
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Abstract

An axial flow fan is widely used for heat dissipation in aviation and aerospace electronic devices. Due to its frequent speed regulation to adapt to the change in heat load, the fan will produce significant electromagnetic interference (EMI). This article presents a conducted EMI filtering suppression for a high-speed pulsewidth modulation axial flow fan. The conducted EMI of the fan is first measured to identify some large peak voltages much exceeding the specified limitation; then, a time-domain circuit simulation model of the fan driving system is created to predict the insertion loss of the designed filter. By analyzing the mechanism of conducted EMI and its propagation path, the dominant parameters are identified, and the topology structure and key parameters of the filter are optimized. The results show that the insertion loss of filter suppression for EMI is improved from the predicted 5.65 dB to the measured 50.1 dB without affecting the effective signal.
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对高速轴流风扇产生的大峰值传导 EMI 进行滤波抑制
轴流风机广泛用于航空航天电子设备的散热。风机由于频繁调速以适应热负荷的变化,会产生明显的电磁干扰(EMI)。本文介绍了一种用于高速脉宽调制轴流风机的传导EMI滤波抑制方法。首先测量风扇的传导电磁干扰,以确定一些远远超过规定限制的大峰值电压;然后,建立了风扇驱动系统的时域电路仿真模型来预测所设计滤波器的插入损耗。通过分析传导电磁干扰的产生机理及其传播路径,确定了主导参数,并对滤波器的拓扑结构和关键参数进行了优化。结果表明,在不影响有效信号的情况下,滤波器抑制EMI的插入损耗从预测的5.65 dB提高到实测的50.1 dB。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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