飞机起动/发电机起动控制系统逆变组件的研究  

Research on Converter Unit of Aircraft Starter/Generator Starting Control System

作　　者：杨娟 杨占刚 YANG Juan;YANG Zhan-gang(Engineering Technical Training Center,Civil Aviation University of China,Tianjin 300300,China;College of Electronic Information and Automation,Civil Aviation University of China,Tianjin 300300,China)

机构地区：[1]中国民航大学工程技术训练中心,天津300300 [2]中国民航大学电子信息与自动化学院,天津300300

出　　处：《控制工程》2021年第4期693-698,共6页Control Engineering of China

基　　金：国家自然科学基金民航联合基金重点支持项目(U2033204);中央高校基本科研业务费资助项目(3122020029);中国民用航空局民航专业安全能力建设项目(AADSA2019026-5)。

摘　　要：起动逆变组件的计算与分析是飞机起动/发电机起动控制研究的关键。分析研究直流/交流主逆变器的电流滞环跟踪型控制策略,计算研究电流可调/电压限制型励磁电流生成电路,搭建仿真模型;结合三级式同步无刷电机起动功能下系统模型,进行起动系统仿真实验。仿真结果表明,起动控制系统能够可靠稳定运行,直流/交流主逆变器能够准确产生三相脉冲宽度调制电流,励磁电流生成电路输出满足副励磁机定子绕组励磁要求。研究起动/发电双功能系统中起动逆变组件对后期研究多电飞机主发动机电起动技术具有借鉴意义。The calculation and analysis of starting converter unit is the key technology of starter/generator starting control. The current hysteresis tracking control strategy of direct current/alternating current(DC/AC) main converter is analyzed. The current regulated/voltage limited exciter current generation circuit is calculated. The simulation models are established. Combined with the system model of the three-level synchronous brushless machine under the starting condition, the simulation experiment of starting system is conducted. The results of the simulation show that the starting control system can operate reliably and stably, the DC/AC main converter produces three-phase pulse width modulation(PWM) current accurately, and the output of the excitation current generation circuit satisfies the stator winding excitation requirement of auxiliary exciter. The research of the starting converter unit in the starter/generator dual-function system has reference for the later research of electric starting technology of the main engine of more electric aircraft.

关 键 词：起动/发电机 起动逆变组件 电流跟踪型 电流可调/电压限制型 

分 类 号：V233.6[航空宇航科学与技术—航空宇航推进理论与工程]