期刊文献+

旋转式电静液作动器设计与仿真 被引量:1

Simulation and Design of Rotary Electro-hydrostatic Actuator
下载PDF
导出
摘要 以某型无人机武器舱门为负载对象,为满足无人机对质量、体积的限制要求,实现舱门的快速、大角度开闭运动,设计了闭式回路和开式回路两种旋转式电静液作动器方案。通过对两种方案的工作原理分析及元件参数计算,开式回路方案的旋转式电静液作动器在电机功率、泵的排量及系统发热功率上有较大优势。利用AMESim仿真平台,对所设计的旋转式电静液作动器进行了运动仿真。仿真模型较好地反应了实际系统的性能。仿真结果表明:开式回路方案系统响应速度快、调节时间短,满足设计要求。 Based on the weapon bay door of a certain type of UAVas a loading object,in order to meet requirements of the UAV restrictions on the weight and size,to achieve rapid and large angleof the door opening and closing movement,closed circuit and open circuitoftwo rotary electro-hydrostatic actuator of schemes were designed. Through analyzing the working principle and the element parameter calculation of two kinds of schemes,the open circuit system of rotary electro-hydrostatic actuator had a great superiority in the motor power,pump delivery and system heating power. By using AMESim simulation platform,the designed rotary electro-hydrostatic actuatorwas simulated in movement. The performance of actual system was well reflected by the simulation model. The simulation results show that thescheme of open circuit hydraulic system has advantages infast response speed and short adjusting time,which satisfied the requirements in design.
出处 《机床与液压》 北大核心 2016年第19期94-97,共4页 Machine Tool & Hydraulics
关键词 武器舱门 电静液作动器 AMESIM Weapons bay door Electro-hydrostatic actuator AMESim
  • 相关文献

参考文献4

二级参考文献21

  • 1李运华,王占林.电气液压复合调节容积式舵机的精确线性化控制[J].机械工程学报,2004,40(11):21-25. 被引量:9
  • 2马纪明,付永领,李军,高波.一体化电动静液作动器(EHA)的设计与仿真分析[J].航空学报,2005,26(1):79-83. 被引量:42
  • 3马纪明,付永领,高波.基于定量反馈理论的EHA控制器设计[J].北京航空航天大学学报,2006,32(5):553-557. 被引量:8
  • 4徐树森,焦裕松.飞行控制用的三种作动系统[J].航空科学技术,1997(2):15-17. 被引量:6
  • 5[3]Alden R E.Flight demonstration, evaluation and proposed applications for various all electric flight control actuation system concepts[A].AIAA/AHS/ASEE Aerospace Design Conference[C].Irvine, 1993
  • 6[4]Croke S, Herrenschmidt J.More electric initiative power-by-wire actuation alternatives[A].Proceedings of the IEEE 1994 National Aerospace & Electronics Conference[C].New York:IEEE, 1994.1338~1346
  • 7[5]Cloyd J S.Status of the united states air force's more electric aircraft initiative[J].Aerospace and Electronic Systems Magazine, IEEE, 1998,13(4):17 ~ 22
  • 8[6]Chang Jie.EHA system for 'more-electric' aircraft[A].Rockwell Power Seminar[C].Mequon, 2000
  • 9[7]Williams K, Brown D.Electrically powered actuator design (EPAD)[R].NASA/USAF/Navy,1997
  • 10[9]Navarro R.Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft[R].NASA/TM-97-206224,1997

共引文献54

同被引文献5

引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部