航空变频电网功率因数校正技术研究
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摘要
变频电源系统是未来飞机电源系统的发展方向之一,随着现代航空电网性能要求的进一步提高,机载电子设备的广泛应用,谐波对航空电网的污染也越来越严重。不同于民用电网,变频航空电网因具有独立小容量、电源内阻抗大、电网频率较高等特征,使其在三相PWM整流器技术上具有特殊性,系统应具有快速的电流跟踪性能。
     本文首先分析了PWM变换器的工作原理,分别在三相静止坐标系、两相静止坐标系和两相旋转坐标系中建立了低频和高频数学模型,并在dq坐标系中给出了解耦控制的数学模型;为抑制输出直流电压波动,提高系统动态性能,给出了一种优化的负载电流前馈补偿控制策略,有效地改善了系统对输入电压突变和负载突变的响应特性;深入分析了影响输出电压动态响应的主要因素,研究给出了基于系统小信号平均模型前馈补偿控制器的设计原则和方法;采用电压空间矢量PWM(Space Vector PWM, SVPWM)调制方法,以获得网侧低电流谐波,提高直流侧电压利用率;为验证原理分析,设计了基于DSP2812的硬件实验系统,介绍了硬件系统的电感、电容的参数设计和软件实现过程,针对不同电网频率条件下,在实验样机上进行了实验,得到了一些实验数据和波形,验证了三相PWM整流器应用于航空变频电网的可行性和正确性。
Currently for the generation of constant frequency AC voltages will be replaced in future by less complex lighter variable speed generators in combination with power electronics. With the increasing requirements of performance for the modern aircraft, more and more electronic equipments are applied. The AC power utility in aircraft is affected seriously by harmonics. There are some characteristics in the AC power utility: independent lower capacity system, larger inner impedance, etc. The three-phase PWM rectifier techniques for aircraft AC power utility are unique, the good current track performance is required.
     First of all, the theory of PWM rectifier was introduced in details, constructing the high and low-frequency mathematical model are set up in ABC coordinate,α-βcoordinate and d-q coordinate respectively, decoupled its mathematical model in the dq reference frame. In order to restrain dc-bus voltage fluctuation and improve system dynamic characteristics, an optimum feedforward control strategy is proposed, and the system response performance to stepping input voltage and stepping load are improved greatly. The key issues which hurt the output voltage transient are analyzed in detail. The design rule for the feedforward compensation controller is developed based on the averaged small-signal model. The SVPWM is employed to achieve low harmonic distortion and raise the utilizable ratio at DC side. To verify the validity of the proposed method, the hardware system was designed on the basis of TMS320F2812 and parameters design of inductance and capacitance was presented. The experimental results are received under the different conditions. The feasibility and validity of the three-phase PWM for Aircraft Variety-Frequency Electrical Systems are proved.
引文
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