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电脉冲除冰系统的建模与计算分析
引用本文: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):64-70,75.
作者姓名:姚远  林贵平
作者单位:北京航空航天大学,航空科学与工程学院,北京,100083
摘    要:电脉冲除冰系统是上世纪80年代以来新兴的飞机用电动-机械式除冰技术,国内关于该方面的研究起步较晚,文中在阐述了电脉冲除冰研究重要性和研究方法后,首先对电容充放电电路进行了分析与设计计算,接着给出电动力学模型,并计算了系统中感兴趣的关键参数,对计算结果进行处理后得到了能够指导设计的重要参数间的关系图,结合工程实例给予了分析与评价,提出了下一步研究解决的问题。

关 键 词:电脉冲除冰  电动力学模型  线圈电流  涡流  法向力
文章编号:1673-4599(2008)01-0064-07
收稿时间:2007-08-17
修稿时间:2007-12-05

Modeling and Analysis of Electro-Impulse De-icing System
YAO Yuan,LIN Gui-ping.Modeling and Analysis of Electro-Impulse De-icing System[J].Aircraft Design,2008,28(1):64-70,75.
Authors:YAO Yuan  LIN Gui-ping
Institution:YAO Yuan, LIN Gui-ping ( School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China)
Abstract:Electro-Impulse De-Icing is classified as a electric-mechanical method to expel ice on aircraft.This technology arose in the 80th age last century.Interiorly,as a result of commencing late it is lack of interrelated research and conclusion about electro-impulse de-icing.This paper addresses an essentiality and study methods about the system and gives out the results of calculation and design for the circuit at first,and then presents an electro-dynamical model to calculates key parameters and protracts their graphs.At last,valuable analysis and evaluation according to a design example is given to solve further problems.
Keywords:electro-impulse de-icing(EIDI)  electro-dynamical model  coil current  eddy current  normal force
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