| 旋翼试验台液压伺服控制系统设计 |
| |
| 引用本文： | 刘湘一,王秀霞,胡国才,刘书岩.旋翼试验台液压伺服控制系统设计[J].机床与液压,2012,40(10):77-79. |
| |
| 作者姓名： | 刘湘一 王秀霞 胡国才 刘书岩 |
| |
| 作者单位： | 海军航空工程学院飞行器工程系,山东烟台,264001 |
| |
| 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。
|
| 关 键 词： | 液压伺服控制系统 直升机 旋翼试验台 |
Design on Hydraulic Servo-control System of Helicopter Rotor Test-bed |
| |
| LIU Xiangyi
,
WANG Xiuxia
,
HU Guocai
,
LIU Shuyan.Design on Hydraulic Servo-control System of Helicopter Rotor Test-bed[J].Machine Tool & Hydraulics,2012,40(10):77-79. |
| |
| Authors: | LIU Xiangyi WANG Xiuxia HU Guocai LIU Shuyan |
| |
| Affiliation: | (Department of Airborne Vehicle Engineering,Naval Aeronautical & Astronautical University,Yantai Shandong 264001,China) |
| |
| Abstract: | 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. |
| |
| Keywords: | Hydraulic servo-control system Helicopter Rotor test-bed |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
|
