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泵阀协调控制电动静液作动器方案分析

齐海涛 付永领 王占林

齐海涛, 付永领, 王占林等 . 泵阀协调控制电动静液作动器方案分析[J]. 北京航空航天大学学报, 2008, 34(02): 131-134.
引用本文: 齐海涛, 付永领, 王占林等 . 泵阀协调控制电动静液作动器方案分析[J]. 北京航空航天大学学报, 2008, 34(02): 131-134.
Qi Haitao, Fu Yongling, Wang Zhanlinet al. Scheme analysis of pump-valve coordinated control electro-hydrostatic actuator[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(02): 131-134. (in Chinese)
Citation: Qi Haitao, Fu Yongling, Wang Zhanlinet al. Scheme analysis of pump-valve coordinated control electro-hydrostatic actuator[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(02): 131-134. (in Chinese)

泵阀协调控制电动静液作动器方案分析

基金项目: 国家自然科学基金资助项目(50675009)
详细信息
    作者简介:

    齐海涛(1981-),男,山东淄博人,博士生,haitao8642@163.com.

  • 中图分类号: V 245.1;TH 137

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.

     

  • [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: Linkping 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:Linkping  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)
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出版历程
  • 收稿日期:  2007-01-30
  • 网络出版日期:  2008-02-29

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