The thesis studies mainly the drive and control technique of aeronautic linear DC step motor(LDCSM) used in emergency discharging oil valve on airplane.
本文针对“十五”航空基金项目—新型航空用直线直流电动机驱动控制系统，研究了飞机应急放油阀用航空直线步进电动机的驱动控制技术。
The hydraulic motor, hydraulic cylinder and oil cup are controlled digitally in the control module.
控制模块对转向器输入端正反转，液压缸的向前、向后加载，内泄油杯放油等数字量控制。
Motor control centre for DC drives shall be included, comprising also DC power supply for DC oil pump with accumulators.
应包括直流驱动电机控制中心，由带蓄能器的直流油泵用直流电源组成。
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