留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

电脉冲除冰(EIDI)系统电动力学模型分析

李广超 何江 林贵平

李广超, 何江, 林贵平. 电脉冲除冰(EIDI)系统电动力学模型分析[J]. 航空动力学报, 2011, 26(1): 54-59.
引用本文: 李广超, 何江, 林贵平. 电脉冲除冰(EIDI)系统电动力学模型分析[J]. 航空动力学报, 2011, 26(1): 54-59.
LI Guang-chao, HE Jiang, LIN Gui-ping. Research of electrodynamics in electro-impulse de-icing (EIDI) system[J]. Journal of Aerospace Power, 2011, 26(1): 54-59.
Citation: LI Guang-chao, HE Jiang, LIN Gui-ping. Research of electrodynamics in electro-impulse de-icing (EIDI) system[J]. Journal of Aerospace Power, 2011, 26(1): 54-59.

电脉冲除冰(EIDI)系统电动力学模型分析

基金项目: “凡舟”青年基金(20100508)

Research of electrodynamics in electro-impulse de-icing (EIDI) system

  • 摘要: 总结了电脉冲除冰(EIDI)系统电动力学模型的研究现状,针对几种常见的计算模型进行了分析,以Bernhart-Schrag模型为例,重点阐述了电动力学模型的理论基础、等效模型的建立以及状态方程的求解,分析了模型的正确性.针对由环状平绕线圈及金属平板构成的EIDI简化系统,Bernhart-Schrag模型可以预测通电线圈中电流的变化规律以及蒙皮受到的脉冲作用.

     

  • [1] Lynch F T,Khodadoust A.Effects of ice accretions on aircraft aerodynamics[J].Progress in Aerospace Sciences,2001,37(8):669-767.
    [2] Khatkhate A A,Skavuzzo R J,Chu M L.A finite element study of the EIDI system .AIAA Paper 88-0022,1988.
    [3] George N L,Ioannis D D,Milan M S.Simulation of the electroimpulse de-icing process of aircraft wings[J].Journal of Aircraft,2006,43(6):1876.
    [4] Levin I A.USSR electric impulse de-icing design[J].Aircraft Engineering and Aerospace Technology,1993,44(7):7-10.
    [5] Kodet A C.Electro-impulse deicing //Proceedings of the 1988 IEEE.Binghamton,NY:IEEE,1988:193-200.
    [6] Zumwalt G W,Friedberg R A.Designing an electroimpulse de-icing system .AIAA Paper 86-0545,1986.
    [7] 刘根林,沈海军.飞机防冰与除冰技术综述[J].江苏航空,2003(4):18-20.
    [8] 陈明生.我国大型飞机防冰系统研制的设想 //大型飞机关键技术高层论坛暨中国航空学会2007年年会论文集.深圳:中国航空学会,2007:82.
    [9] 裘亦纲.NASA结冰研究和防冰技术发展[J].国际航空,1993(4):60-62. QIU Yigang.The development of ice accretion study and anti-icing technology by NASA[J].International Aeronautics,1993(4):60-62.(in Chinese)
    [10] Zumwalt G W.Electromagnetic emissions from an electro-impulse deicing system in a composite wing equipped with lightning protection .FAA Report DOT/FAA/CT-TN90/32,1991.
    [11] Macarthur C,Thomas S,Cassoni R.Aircraft anti-icing and deicing techniques and modeling[J].Journal of Aircraft,1996,33(5):841-854.
    [12] Bernhart W D,Schrag R L.Electro-impulse deicing:electrodynamic solution by discrete elements[J].Journal of Aircraft,1989,26(6):547-553.
    [13] Henderson R A,Schrag R L.Theoretical analysis of the electrical aspects of the basic electro-impulse problem in aircraft de-icing applications .NASA Contractor Report 180845,1987.
    [14] Bernhart W D,Gien P H.A structural dynamics investigation related to EIDI applications .AIAA Paper 86-0550,1986.
    [15] 姚远,林贵平.电脉冲除冰系统的建模与计算分析[J].飞机设计,2008,28(1):64-70. YAO Yuan,LIN Guiping.Modeling and analysis of electro-impulse de-icing system[J].Aircraft Design,2008,28(1):64-70.(in Chinese)
  • 加载中
计量
  • 文章访问数:  1657
  • HTML浏览量:  1
  • PDF量:  11
  • 被引次数: 0
出版历程
  • 收稿日期:  2010-04-20
  • 修回日期:  2010-10-25
  • 刊出日期:  2011-01-28

目录

    /

    返回文章
    返回