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Volume 38 Issue 10
Oct.  2012
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Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  38(10): 1395-1399.
Luo Caijin, Shang Yaoxing, Jiao Zongxiaet al. Design and efficiency analysis for loading actuator used in aircraft structure test[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(10): 1395-1399. (in Chinese)
Citation: Luo Caijin, Shang Yaoxing, Jiao Zongxiaet al. Design and efficiency analysis for loading actuator used in aircraft structure test[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(10): 1395-1399. (in Chinese)
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Design and efficiency analysis for loading actuator used in aircraft structure test

  • Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 20 Jun 2012
  • Publish Date: 30 Oct 2012
    Abstract
  • Based on the characteristics of low speed and low system flow in plane structure test especially in the static loading test, a new type of valve-control electro-hydraulic actuator for aircraft structure loading test was designed. The system components and working principle was described, and the efficiency of valve-control system was analyzed. A scheme of reducing the oil source pressure setting was proposed in order to improve the system efficiency, while modeling and simulation work of the electro-hydraulic actuator system was completed through the AMESim platform, and the effectiveness of proposed scheme in improving the system efficiency was proved. The simulation results demonstrate that the designed electro-hydraulic actuator can totally meet the expected design requirements, and can be widely used in aircraft structural loading test system.

     

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    • References(8)
  • [1]
    吴森.结构试验基础[M].北京:航空工业出版社,1992:1-9 Wu Seng.The foundation of structural test[M].Beijing:Aviation Industry Press,1992:1-9(in Chinese)
    [2]
    马健.B777全尺寸静力和疲劳试验[J].民航经济与技术,1997(6):33-35 Ma Jian.B777-scale static and fatigue test[J].Civil Aviation Economics & Technology,1997(6):33-35 (in Chinese)
    [3]
    Vepa R.Aeroelastic analysis of wing structures using equivalent plate models[J].AIAA,2008,46(5):1216-1225
    [4]
    Feraboli P.Composite materials strength determination within the current certification methodology for aircraft structures[J].AIAA,2009,46(4):1365-1374
    [5]
    孙卫华,胡贵彦.新型机载作动系统研究[M].北京:中国物资出版社,2009:94-98 Sun Weihua,Hu Guiyan.New airborne actuator system research[M].Beijing:China Supplies Press,2009:94-98
    [6]
    王占林.近代电气液压伺服控制[M].北京:北京航空航天大学出版社,2005 Wang Zhanlin.Modern electric-hydraulic servo control[M].Beijing:Beijing University of Aeronautics and Astronautics Press,2005(in Chinese)
    [7]
    纪友哲.电机-泵-阀联合控制作动器的研究 .北京:北京航空航天大学自动化科学与电气工程学院,2008 Ji Youzhe.Research on motor-pump-valve combined control actuator .Beijing:School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astronautics,2008(in Chinese)
    [8]
    王春行.液压控制系统[M].北京:机械工业出版社,1996:19 Wang Chunxing.Hydraulic control system[M].Beijing:Mechanical Industry Press,1996:19(in Chinese)
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