| 飞机电脉冲除冰系统的建模与仿真 |
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| 引用本文： | 吴小华,杨堤,张晓斌,马亮,范冰洁.飞机电脉冲除冰系统的建模与仿真[J].系统仿真学报,2010,22(4). |
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| 作者姓名： | 吴小华 杨堤 张晓斌 马亮 范冰洁 |
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| 作者单位： | 西北工业大学自动化学院,西安,710072 |
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| 摘 要： | 介绍了飞机电脉冲除冰系统中利用电磁力除去飞机机翼前端和发动机进气口处的冰层的原理和过程,利用ANSYS有限元仿真软件对飞机电脉冲除冰系统装置进行了建模,对飞机表面上的铝盘的电磁力进行了仿真,并且观测气隙间距对系统的影响以及铝盘内涡流的分布情况,从而指导系统参数的选择,为实际应用提供了有效的分析和设计手段。
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| 关 键 词： | 电脉冲除冰 ANSYS 涡流 电磁力 气隙间距 |
Modeling and Simulation of Aircraft Electro-impulse De-icing System |
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| WU Xiao-hua,YANG Di,ZHANG Xiao-bin,MA Liang,FAN Bing-jie.Modeling and Simulation of Aircraft Electro-impulse De-icing System[J].Journal of System Simulation,2010,22(4). |
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| Authors: | WU Xiao-hua YANG Di ZHANG Xiao-bin MA Liang FAN Bing-jie |
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| Abstract: | The theory and process of electromagnetism at the front of aircraft wing and engine were proposed for the de-icing device based on ANSYS soft. Through modeling for aircraft electro-impulse de-icing system,the simulation result of the electromagnetism force was obtained for the aluminum pan on the surface of the aircraft. The electromagnetism force and eddy current was deeply related to the air gap. The analysis of the modeling and simulation offers an effective means for the design and the choice of the sys... |
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| Keywords: | electro-impulse de-icing ANSYS eddy current electromagnetism force air gap distance |
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