| 飞机液压系统温度仿真计算与分析 |
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| 引用本文： | 谢三保,焦宗夏.飞机液压系统温度仿真计算与分析[J].机床与液压,2005(5):67-68,5. |
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| 作者姓名： | 谢三保 焦宗夏 |
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| 作者单位： | 北京航空航天大学自动化科学与电气工程学院,北京,100083 |
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| 摘 要： | 利用动态油温计算法，建立了各种液压元件的温度模型，并对飞机液压系统在典型飞行状态下进行温度仿真计算。分析了影响液压系统温度的主要因素和降低油温的措施。
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| 关 键 词： | 飞机液压系统 温度模型 温度仿真计算 |
| 文章编号： | 1001-3881(2005)5-067-2 |
Temperature Simulating Calculation and Analysis of Aircraft Hydraulic System |
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| XIE San-bao,JIAO Zong-xia.Temperature Simulating Calculation and Analysis of Aircraft Hydraulic System[J].Machine Tool & Hydraulics,2005(5):67-68,5. |
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| Authors: | XIE San-bao JIAO Zong-xia |
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| Abstract: | The thermal model of each hydraulic component was built to use the dynamic fluid temperature method,the aircraft hydraulic system thermal simulating calculation was deduced in typical flight status,and the primary influence factors to the temperature of aircraft hydraulic system were analyzed,and how to take reasonable measure to limit the temperature under control was also considered. |
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| Keywords: | Aircraft hydraulic system Thermal model Thermal simulating calculation |
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