摘要
简要介绍了同步整流技术的原理,提出了以同步整流技术测量航空发动机磁感应式传感器信号的方法,实现了信号测量准零温度漂移的目的。
The principle of synchronous rectification technology is introduced briefly. The measure method of the aeroengine magnetic induction sensor signal with the synchronous rectification is presented, and the object of quasi zero temperature drift is achieved with signal measurement.
出处
《航空发动机》
2007年第4期40-42,共3页
Aeroengine
关键词
航空发动机
控制系统
同步整流
信号测量
滑油压力
aeroengine
control system
synchronous rectification
signal measurement
oil pressure
