| 飞机液压系统管路设计分析 |
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| 引用本文： | 张春山,王岳基.飞机液压系统管路设计分析[J].飞机工程,2007(1):44-46. |
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| 作者姓名： | 张春山 王岳基 |
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| 作者单位： | [1]中国人民解放军驻西飞公司军代表室,西安 [2]空军第三飞行学院航理教研室,辽宁锦州 |
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| 摘 要： | 飞机液压系统管路设计，应考虑导管材料、直径和壁厚的选择及系统工作压力、介质流量与工作环境相适应，既要保证导管有足够的强度，又要使系统重量最轻，寿命可靠性高。这里从导管管径设计、壁厚确定、爆破压力和管路安装等方面对飞机液压管路系统的设计作了分析，提供了导管设计的计算方法。
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| 关 键 词： | 液压系统 导管管径 导管壁厚 爆破压力 |
| 修稿时间： | 2006-12-25 |
Pipeline Design of Aircraft Hydraulic System |
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| Authors: | ZHANG Chunshan WANG Yueji |
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| Abstract: | The pipeline material, diameter and wall thickness should be adapted to hydraulic system operating pressure, flow and work environment when designing aircraft hydraulic system pipeline. This adaptability should ensure pipeline have enough strength, and also the least weight and high reliability. Based on the analysis of pipeline diameter design, wall thickness determine, bursting pressure and pipeline installation, the calculation method of aircraft hydraulic system pipeline design is presented. |
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| Keywords: | hydraulic system pipeline diameter pipeline wall thickness bursting pressure |
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