期刊文献+

电脉冲除冰(EIDI)系统电动力学模型分析 被引量:3

Research of electrodynamics in electro-impulse de-icing(EIDI) system
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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. The current status of the research on electrodynamics in electro-impulse de-icing(EIDI) system was summarized in this paper;several common calculation models were analyzed.By taking Bernhart-Schrag model,for example,the theoretical basis of electrodynamics model,the establishment of equivalent model and the solution of state equation were expatiated;the correctness of the model was also analyzed.For the simplified system of EIDI composed of circular flat coil and metal flat plate,Bernhart-Schrag model can help to predict the regular variation pattern of current in the coil and the pulse effect under the skin.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2011年第1期54-59,共6页 Journal of Aerospace Power
基金 "凡舟"青年基金(20100508)
关键词 电脉冲除冰 电动力学 计算模型 有限元方法 离散求解 脉冲力 electro-impulse de-icing electrodynamics calculation models finite element method discrete solution impulse force
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参考文献15

  • 1Lynch F T,Khodadoust A. Effects of ice accretions on air- craft aerodynamics[J]. Progress in Aerospace Sciences, 2001,37(8) :669 -767.
  • 2Khatkhate A A,Skavuzzo R J ,Chu M L. A finite element study of the EIDI system[R]. AIAA Paper 88-0022,1988.
  • 3George N L, Ioannis D D, Milan M S. Simulation of the electroimpulse de-icing process of aircraft wings[J]. Jour- nal of Aircraft,2006,48(6) :1876.
  • 4Levin I A. USSR electric impulse de-icing design[J]. Air- craft Engineering and Aerospace Technology, 1993, 44 (7) : 7-10.
  • 5Kodet A C. Electro impulse deicing[C]//Proceedings of the 1988 IEEE. Binghamton, NY : IEEE, 1988 : 193-200.
  • 6Zumwalt G W,Friedberg R A. Designing an electroimpulse de icing system[R]. 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. 被引量:16
  • 8陈明生.我国大型飞机防冰系统研制的设想[C]//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. 被引量:4
  • 10Zumwalt G W. Electromagnetic emissions from an electro- impulse deicing system in a composite wing equipped with lightning protection [R]. FAA Report DOT/FAA/CT- TN90/32,1991.

二级参考文献5

  • 1[1]Westphal P W,Wagnerl O.Flight accident prevention withhazard priprity based real time risk reduction[R].AIAA Non-Deterministic Approaches Forum / 42nd SDM Conference Seattle,WA,Sheraton Seattle Hotel & Towers,2001,16-19.
  • 2[2]Bernhart W,Zumwalt G.Electro-impulse deicing:structural dynamic studies,icing tunnel tests and applications[R].AIAA-84-0022,1984.
  • 3王苑.电子脉冲系统的飞行试验和风洞试验[J].国际航空,1995,5(12):519.
  • 4[4]Schrag R L,Zumwal G W.Electro-impulse deicing:concept and electrodynamic studies[R].Wichita State University,1984,1-2.
  • 5[5]Zumwalt G W,Schrag R L,Bernhart W D,et al.Electro-impulse de-icing testing analysis and design[R].Wichita State University,1988,82-89.

共引文献34

同被引文献44

  • 1钟长生,洪冠新.飞机翼面结冰对飞行特性影响的研究[J].航空科学技术,2004(3):32-34. 被引量:3
  • 2裘燮纲,郭宪民.电脉冲除冰系统参数的合理选择[J].南京航空学院学报,1993,25(2):211-218. 被引量:11
  • 3谢毅.飞机结冰事故的统计分析[J].国外试飞,1996(3):23-28. 被引量:4
  • 4裘燮纲 韩凤华.飞机防冰系统[M].北京:航空专业教材编审组,1985..
  • 5Federal Aviation Administration. Large aircraft ground de-icing[R]. Pilot Guide U S, Department of Transportation, AC 120-58, Sept 30, 1992.
  • 6Bergrun N. Warming trend for icing research[J]. Aerospace America, 1995: 22-27.
  • 7Heinrich A, Ross R, Zumwalt G, et al. Aircraft icing handbook[R]. ADA238 040, DOT/FAA/CT-88/8-2, 1991.
  • 8Paraschivoiu I, Saeed F. Aircraft icing[R]. John Wiley & Sons, Inc., xxvii-xxviii.
  • 9Westphal P W, Wagnerl O. Flight accident prevention with hazard priority based real time risk reduction [R]. AIAA Non-Deterministic App roaches Forum/42nd SDM Conference Seattle, WA, Sheraton Seattle Hotel & Towers, 2001.
  • 10Newton D. Severe weather flying[J]. Aviation Supplies& Academics, Inc, 2002.

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