| 超薄翼型上液压系统布置的设计分析 |
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| 引用本文： | 肖翔,夏语冰,姜逸民,郑占君,戴攀.超薄翼型上液压系统布置的设计分析[J].民用飞机设计与研究,2010(4):6-8. |
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| 作者姓名： | 肖翔 夏语冰 姜逸民 郑占君 戴攀 |
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| 作者单位： | 上海飞机设计研究院液压系统设计研究部,上海,200436 |
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| 摘 要： | 超薄翼型飞机后梁空间狭小,无法为液压管路系统提供足够的空间。分别从液压系统泄漏、液压油介质的腐蚀性、穿燃油箱的密封性、对燃油箱温度的影响以及对液压能源系统本身的影响等设计问题进行分析,提出了将部分液压管路布置在燃油箱内的方案。试验证明此设计方案能满足系统要求和适航要求。
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| 关 键 词： | 超薄翼型 燃油箱 液压导管设计 导管安装 |
Hydraulic System Design Analysis in Wing |
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| Xiao Xiang,Xia Yubing,Jiang Yimin,Zheng Zhanjun,Dai Pan.Hydraulic System Design Analysis in Wing[J].Civil Aircraft Design and Research,2010(4):6-8. |
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| Authors: | Xiao Xiang Xia Yubing Jiang Yimin Zheng Zhanjun Dai Pan |
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| Institution: | Xiao Xiang Xia Yubing Jiang Yimin Zheng Zhanjun Dai Pan(Hydraulic Systems Department,Shanghai Aircraft Design and Research Institute,Shanghai 200436) |
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| Abstract: | The space of supercritical wing rear spar is narrowness and difficult to layout hydraulic tube system. The document analyzed the design base on leakage,corrosive,seal,temperature and so on. Design part of tubes in fuel tank. The tests show the design can meet the system and certification requirements. |
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| Keywords: | Supercritical wing Wing fuel tank Hydraulic tube design Tube installation |
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