摘要
提出了一种适用于低压大电流输出的航空静止变流器方案。分析了方案的原理,特别是逆变器控制系统和滤波参数的设计以及各自对系统性能的影响。最后给出了仿真和试验结果,证明该方案具有高可靠性、高功率密度、输出波形好,实现简单等特点。
A aircraft static inverter( ASI) suit of low votage,high current input condition is presented in this paper. The operation principle of the ASI, especially the design of control system and filter parameters of the inverter is analysed in detail. At last the results of simulate and experiment are given and testify that the ASI ahs high reliability,hign pwer density, high output voltage quality and easy realization.
出处
《电力电子》
2004年第4期32-34,共3页
Power Electronics
