旋翼试验台液压伺服控制系统设计  

Design on Hydraulic Servo-control System of Helicopter Rotor Test-bed

作　　者：刘湘一[1] 王秀霞[1] 胡国才[1] 刘书岩[1] 

机构地区：[1]海军航空工程学院飞行器工程系,山东烟台264001

出　　处：《机床与液压》2012年第10期77-79,共3页Machine Tool & Hydraulics

摘　　要：为了满足直升机旋翼试验台的操纵和激振的需求,设计了液压伺服控制系统。该系统由泵站、伺服控制器、伺服动作器等部分组成。系统的额定压力13.5 MPa,额定流量40 L/min,输出频率0～100 Hz。使用结果表明,该系统满足所有的设计要求。In order to achieve the function of steering and excitation, a hydraulic servo-control system was designed for helicopter rotor test-bed. The system contains three components ： pumping station, servo controller and servo actuator. The rated pressure of the system is 13.5 MPa, rated flow is 40 L/min, and output frequency is 0-100 Hz. The utilization indicates that the system can meet all requirements.

关 键 词：液压伺服控制系统 直升机 旋翼试验台 

分 类 号：TH137[机械工程—机械制造及自动化]