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功率电传机载一体化电作动系统的研究

沙南生 李军

沙南生, 李军. 功率电传机载一体化电作动系统的研究[J]. 北京航空航天大学学报, 2004, 30(09): 909-912.
引用本文: 沙南生, 李军. 功率电传机载一体化电作动系统的研究[J]. 北京航空航天大学学报, 2004, 30(09): 909-912.
Sha Nansheng, Li Jun. Research on airborne power-by-wire integrated electrical actuation and control systems[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(09): 909-912. (in Chinese)
Citation: Sha Nansheng, Li Jun. Research on airborne power-by-wire integrated electrical actuation and control systems[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(09): 909-912. (in Chinese)

功率电传机载一体化电作动系统的研究

基金项目: 高等学校博士点专项科研基金资助项目(20020006006)
详细信息
    作者简介:

    沙南生(1963-),男,江西宁都人,博士生,shalao5@sina.com.

  • 中图分类号: V 245.1; TH 137

Research on airborne power-by-wire integrated electrical actuation and control systems

  • 摘要: 概述了近10年国内外机载功率电传一体化电动作动系统的研究发展状况,已成功的机载电力作动系统主要包括电静液作动器和机电作动器,得出了电作动器可用于未来机载作动系统相关的一系列结论;归纳了采用电力作动系统的优点;阐述了发展该机载一体化电作动系统的关键技术,包括高性能永磁、无刷直流电机-泵及其集成设计、冗余管理、高响应高精度控制等;指出了机载一体化电作动系统的研制目标和技术难点,为发展机载功率电传一体化电作动系统进行了深入的探讨.

     

  • [1] 王占林,陈 斌. 未来飞机液压系统的特点[J].中国工程科学,1999,1(3):5~10 Wang Zhanlin, Chen Bin. Characters of future aircraft hydraulic system[J]. Engineering Science, 1999,1(3):5~10(in Chinese) [2] 于 敦.飞机电力作动系统发展方向 . 航空信息研究报告, HY95007, 北京:中国航空信息中心,1995 Yu Dun. Development orientation of airborne electrical actuation systems . Aero Information research report, HY95007, Beijing:China Aero Information Center, 1995(in Chinese) [3] Alden R E. Flight demonstration, evaluation and proposed applications for various all electric flight control actuation system concepts . AIAA/AHS/ASEE Aerospace Design Conference . Irvine, 1993 [4]Croke S, Herrenschmidt J. More electric initiative power-by-wire actuation alternatives . Proceedings of the IEEE 1994 National Aerospace & Electronics Conference . New York:IEEE, 1994.1338~1346 [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 [6]Chang Jie. EHA system for ‘more-electric’ aircraft . Rockwell Power Seminar . Mequon, 2000 [7]Williams K, Brown D. Electrically powered actuator design (EPAD) . NASA/USAF/Navy,1997 [8] 徐步力.一体化机载作动系统原理样机的性能研究 .北京:北京航空航天大学自动化科学与电气工程学院,2002 Xu Buli. Research on an EHA prototype of flight control system . Beijing:School of Automation Science and Electric Engineering, Beijing University of Aeronautics and Astronautics, 2002(in Chinese) [9] Navarro R. Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft . NASA/TM-97-206224,1997 [10] Jensen S C. Flight test experience with an electro mechanical actuator on the F-18 systems research aircraft . NASA/H-2425,2000 [11]Habbi S , Goldenberg A . Design of a new high performance electrohydraulic actuator . 1999 IEEE/ASME International Conference on Advanced Intelligent Mechatronics Proceedings . New York:IEEE, 1999, 227~232 [12] Churn P M, Maxwell C J,Schofield N, et al. Electro-hydraulic actuation of primary flight control surfaces . All Electric Aircraft, IEE Colloquium . London, 1998 [13] 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 actuation systems[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(4):426~430(in Chinese)
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出版历程
  • 收稿日期:  2003-09-29
  • 刊出日期:  2004-09-30

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