| 民用客机机翼热气防冰系统问题初探 |
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| 引用本文： | 霍西恒,刘鹏,贾丽杰.民用客机机翼热气防冰系统问题初探[J].民用飞机设计与研究,2010(4):16-18,27. |
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| 作者姓名： | 霍西恒 刘鹏 贾丽杰 |
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| 作者单位： | 1. 上海飞机设计研究院环控氧气系统设计研究部,上海,200235
2. 上海飞机制造有限公司,上海,200436 |
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| 摘 要： | 简单介绍了热气防冰系统的特点及工作原理,同时对前缘缝翼笛形管的两种基本布置方式进行了描述,最后对波音737系列、空客320系列以及空客340等飞机的机翼热气防冰系统进行了介绍和对比分析。
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| 关 键 词： | 防冰系统 前缘缝翼 笛形管 |
Research of the Wing Hot Air Anti-icing System for the Civil Aircraft |
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| Huo Xiheng,Liu Peng,Jia Lijie.Research of the Wing Hot Air Anti-icing System for the Civil Aircraft[J].Civil Aircraft Design and Research,2010(4):16-18,27. |
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| Authors: | Huo Xiheng Liu Peng Jia Lijie |
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| Institution: | Huo Xiheng1 Liu Peng1 Jia Lijie2(1.Environment Control System Department,Shanghai Aircraft Design and Research Institute,Shanghai 200235,2.Shanghai Aircraft Manufacturing CO.,Ltd,Shanghai 200436) |
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| Abstract: | The characteristic and work principle of wing hot air anti-icing system was introduced briefly first,and then two main piccolo layout forms in the leadingedge was described in this paper. Lastly,the hot air anti-icing system of the B737,A320 and A340 etc. were introduced and analyzed. |
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| Keywords: | Anti-icing System Leadingedge Piccolo |
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