Scheme analysis of pump-valve coordinated control electro-hydrostatic actuator
-
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(Direct Drive 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.Abstract: 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 electro-hydraulic 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-hydrostatic actuation system.
-
[1] Croke S, Herrenschmidt J. More electric initiative-power-by-wire actuation alternatives Proceedings of IEEE- 94 National Aerospace & Electronics Conference. Piscataway: IEEE Aerospace & Electronics Systems Sco, 1994:1338-1346 [2] Botten S L, Whitley C R, King A D. Flight control actuation technology for next generation all-electric aircraft [J]. Technology Review Journal——Millennium Issue, 2000: 55-68 [3] Frischemeier S. Electrohydrostatic actuators for aircraft primary flight control-types, modelling and evaluation The 5th Scandinavian International Conference on Fluid Power. Sweden: Linkping University, 1997:1-16 [4] Kazmeier B, Feldmann D G. A quantitative comparison of three concepts of an electro-hydraulic actuator of small power focused on dynamic behaviour and energy lossed The 5th Scandinavian International Conference on Fluid Power. Sweden:Linkping University, 1997:215-230 [5] Andersson J, Krus P, Nilsson K. Optimization as a support for selection and design of aircraft actuation system . AIAA-98-4887, 1998 [6] 王占林. 液压伺服控制[M]. 北京 : 北京航空学院出版社, 1987:113-118 Wang Zhanlin. Hydraulic servo control [M]. Beijing: Press of Beijing Aeronautic College, 1987: 113-118(in Chinese) [7] 祁晓野, 付永领, 王占林. 功率电传机载作动系统方案分析[J]. 北京航空航天大学学报, 1999, 25(4) :426-430 Qi Xiaoye, Fu Yongling, Wang Zhanlin. Scheme analysis of power-by-wire airborne actuator systems [J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(4):426-430 (in Chinese) [8] Hsu Y N, Lai C Y, Hsu M H, et al. Development of the direct drive valve (DDV) actuation system on the IDF aircraft The 29th International Pacific Air and Space Technology Conference and Aircraft Symposium. United States: Society of Automotive Engineers, Inc, 1991:871-881 [9] 郎燕, 李运华. 电液复合调节一体化舵机的复杂建模与AMESim 仿真 航空宇航科学与技术全国博士生论坛论文集(下). 北京: 北京航空航天大学, 2006: 86-91 Lang Yan, Li Yunhua. Complex modeling and AMESim simulation of electro-hydraulic compound regulating integrated actuator Paper Collection (II) of Aeronautics & Astronautics Science & Technology Doctoral Forum of China. Beijing: Beijing University of Aeronautics and Astronautics, 2006:86- 91 (in Chinese)
点击查看大图
计量
- 文章访问数: 4381
- HTML全文浏览量: 190
- PDF下载量: 1238
- 被引次数: 0