电液伺服舵机加载系统设计与研究  

Design and Research of Electro-hydraulic Servo Actuator Loading System

作　　者：尤向荣[1] 秦现生[1] 张双权[1] 牛强[1] 

机构地区：[1]西北工业大学机电学院,西安710072

出　　处：《机电一体化》2010年第8期42-46,共5页Mechatronics

摘　　要：分析了电液伺服舵机加载系统中多余力控制、电液伺服阀的工作原理、控制系统设计等多项舵机加载系统中的关键技术,并在此基础上阐述了电液伺服舵机加载系统的组成部分和设计过程。Electro-hydraulic servo actuator loading system is designed for simulation of force on the rudder of the aircraft and testing the capability of the actuator. Much important technology is discussed, for example the control of surplus torque, the work elements of electro-hydraulic servo-valve, control system and so on. Based on the technology, the structure and process of design of electro-hydraulic servo actuator loading system are introduced.

关 键 词：多余力 电液伺服阀 舵机 加载系统 

分 类 号：V249[航空宇航科学与技术—飞行器设计]