| 直升机旋翼防除冰设计与分析 |
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| 引用本文： | 邹小玲.直升机旋翼防除冰设计与分析[J].直升机技术,2009(3). |
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| 作者姓名： | 邹小玲 |
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| 作者单位： | 中航工业直升机设计研究所,景德镇,333001 |
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| 摘 要： | 旋翼防除冰是保证直升机在中等结冰条件下安全飞行的基本功能,目前,国内旋翼防除冰技术还未应用于工程设计。本文从旋翼防除冰设计出发,分析研究电热防除冰方法和防除冰控制律,电热防除冰设计涉及的旋翼防冰范围,热力计算以及防除冰加热方法。
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| 关 键 词： | 直升机 旋翼 防除冰 |
The Design and Analysis of Helicopter Rotor Anti-icing/Deicing System |
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| Authors: | ZOU Xiaoling |
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| Institution: | ZOU Xiaoling(AVIC Helicopter Research and Development Institute; Jingdezhen; 333001); |
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| Abstract: | Helicopter Rotor Anti/De-icing System is a primary requirement for safe flight in medium icing condition.There is no engineering application of Rotor Anti/De-icing Technology in our country currently.Electro-thermal Anti/De-icing method and control schema,Rotor Blade Anti/Deicing Area,heat computation and Anti/De-icing heating method is discussed here. |
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| Keywords: | helicopter rotor anti-icing/deicing |
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