功率电传机载一体化电作动系统的研究

沙南生; 李军

功率电传机载一体化电作动系统的研究

沙南生,
李军

北京航空航天大学自动化科学与电气工程学院, 北京 100083

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
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- 被引次数: 0
出版历程
- 收稿日期: 2003-09-29
- 网络出版日期: 2004-09-30

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

School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

摘要

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.
- 飞机附件 /
- 操舵系统 /
- 功率电传 /
- 电作动系统 /
- 电动静液压作动器 /
- 机电作动器 /
- 集成设计制造
Abstract: The development of airborne integrated electrical actuation systems in the latest ten years and main results were summed up. It concluded the virtues of integrated electrically actuation system. The successful airborne electrical actuators consist of electro-hydrostatic actuator and electro-mechanic actuator. It summarized series results referring the electrical actuators which will apply to aircrafts in the future. It presented the key technologies of power-by-wire (PBW) electrically powered actuation systems including high performance hard magnetic material, brushless DC motor-pump, integrated designing and manufacturing, redundancy management, fast response and high precision control. It pointed out the R&D targets and the urgent need technique difficulties to develop the next generation airborne actuation system.
- aircraft accessories /
- steering control systems /
- power-by-wire /
- electrical actuation and control system /
- electro-hydrostatic actuator /
- electro-mechanical actuator /
- integrated design and manufacture

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参考文献(1)

[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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