A New Two-Switch PFC DCM Boost Rectifier for Aviation Applications

T. Sadílek, Misha Kumar, Y. Jang, P. Barbosa
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引用次数: 1

Abstract

A new two-switch, single-phase, power-factor-correction (PFC), discontinuous-conduction-mode (DCM) boost rectifier that features zero-voltage switching (ZVS) and can achieve less than 5% input-current total harmonic distortion (THD) by injecting a simple feedforward signal obtained from input and output voltages to the output voltage feedback control is introduced. Since low THD is achieved without high bandwidth active current shaping control, the proposed topology is suitable for modern aviation applications that require line frequency up to 800 Hz. The evaluation was performed on a 320 W prototype designed to operate from 94-134 V line input and deliver 220 V dc output. The prototype achieves 2.3% THD at full load over the line frequency range from 360 Hz to 800 Hz and meets the required harmonic limits specified by the DO-160 standard that describes the environmental conditions and test procedures for airborne equipment.
一种新型航空用双开关PFC DCM升压整流器
介绍了一种新型的双开关、单相、功率因数校正(PFC)、不连续传导模式(DCM)升压整流器,该整流器具有零电压开关(ZVS)的特点,通过将输入输出电压获得的简单前馈信号注入到输出电压反馈控制中,可以实现小于5%的输入电流总谐波失真(THD)。由于低THD是在没有高带宽有源电流整形控制的情况下实现的,因此所提出的拓扑结构适用于需要线频率高达800 Hz的现代航空应用。评估是在一个320 W的原型上进行的,该原型设计用于从94-134 V线输入和提供220 V直流输出。在360 Hz至800 Hz的线路频率范围内,样机在满载时达到2.3%的THD,并满足描述机载设备环境条件和测试程序的DO-160标准规定的谐波限制。
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