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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,北京100083
出 处:《北京航空航天大学学报》2008年第2期131-134,共4页Journal of Beijing University of Aeronautics and Astronautics
基 金:国家自然科学基金资助项目(50675009)
摘 要:针对典型的EHA(Electro-Hydrostatic Actuator)系统存在的频响较低的问题,为了兼顾作动系统的效率和频响,将控制阀引入了EHA系统,提出了3种泵阀协调控制的EHA方案,分别是:采用EHSV(Electro-Hydraulic Servo Valve)的EHA系统,采用DDV(DirectDrive Valve)的EHA系统以及采用TPCV(Total Pressure Control Valve)的EHA系统.阐述了这3种方案的系统组成及工作原理,采用AMESim对这3种方案及典型的EHA进行了仿真对比分析.从仿真结果可以看出:泵阀协调控制的EHA系统可以大大提高系统的频响,同时还具有较高的效率.作为3种过渡方案,将对目前机载电动静液作动系统的研制具有实际指导意义.Aiming at the problem of low response which existed in the typical electro-hydrostatic actuator (EHA) systems, control valve was introduced into EHA systems to find a trade-off between efficiency and response. Three schemes of pump-valve coordinated control EHA were put forward. First was EHA with electrohydraulic servo valve, second was EHA with direct drive valve, and third was EHA with total pressure control valve. The system composition and operating principle of the three schemes were analyzed. Also each scheme was simulated and compared in AMESim. The simulation results show that pump-valve coordinated control EHA will greatly improve the system response and its efficiency is also higher. As three transitional schemes, they have practical guidance significance to the research and development of present airborne electro-hydrostat- ic actuation system.
关 键 词:功率电传 电动静液作动器 泵阀协调控制 电液伺服阀 直接驱动阀 总压力控制阀
分 类 号:V245.1[航空宇航科学与技术—飞行器设计] TH137[机械工程—机械制造及自动化]
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