机载电静液作动系统的发展现状与关键技术研究  

Present Development Status and Key Technology Research of Airborne Electro-Hydrostatic Actuation System

作　　者：李军[1] 付永领[1] 王占林[1] 

机构地区：[1]北京航空航天大学自动化科学与电气工程学院

出　　处：《航空制造技术》2005年第11期73-77,共5页Aeronautical Manufacturing Technology

基　　金：高等学校博士学科专项科研基金项目(20020006006)

摘　　要：总结了新型机载作动系统的发展背景与研究意义,介绍了用于功率电传的电静液作动器和机电作动器的发展现状,综述了机载电静液作动系统设计、开发和取得的技术成果,论述了机载电静液作动系统发展中有待于进一步研究的问题,提出了开展该项研究的建议和措施。The background and benefits of development of new type airborne actuation system are summarized. The present development status of electrohydrostatic actuator and electro-mechanical actuator used for power-by-wire （PBW） are introduced. The design and development of airborne electro-hydrostatic actuator and the technical achievements obtained are summed up. Some problems to be solved in the development of the airborne electro-hydrostatic actuation system are expounded. Some suggestions and measures are pointed out.

关 键 词：机载作动系统 功率电传 电静液作动器 机电作动器 

分 类 号：V227[航空宇航科学与技术—飞行器设计]